CRJ Series

Operational Evaluation Report

Revision: 5

Date: 2024-07-12

MHI RJ Aviation ULC
CRJ Series

Type Certificate Data Sheet (TCDS)* TCDS Identifier/Master Series Marketing Name Pilot Type Rating

A-276

CL-600-2B19

CRJ100
CRJ200
CRJ440

(CRJ100/200/440)

CL65

A-276

CL-600-2C10

CRJ700
CRJ701
CRJ702

(CRJ700/701/702)

CL65

A-276

CL-600-2C11

CRJ550

CL65

A-276

CL-600-2D15

CRJ705

CL65

A-276

CL-600-2D24

CRJ900

CL65

A-276

CL-600-2E25

CRJ1000

CL65

Approved by Philippe Ngassam,
Director, National Aircraft Certification Branch (AARD)
Transport Canada, Civil Aviation

Original signed by Philippe Ngassam

Management co-ordination sheet

Office of Primary Interest (OPI):

Steve Charest
Chairman CRJ Operational Evaluation Board
Civil Aviation Safety Inspector, Flight Technical and Operator Certification (FTOC)
Commercial Flight Standards (AARTFT)
Transport Canada Civil Aviation

Original signed by Steve Charest

Benoit Saulnier
Program Manager, Flight Technical and Operator Certification (FTOC)
Commercial Flight Standards (AARTFT)
Transport Canada Civil Aviation
330 Sparks Street, Ottawa, Ontario
K1A 0N8
Tel: 613-292-4238
e-mail: benoit.saulnier@tc.gc.ca

Original signed by Benoit Saulnier

Craig Leonard
A/Chief, Commercial Flight Standards (AARTF)
Transport Canada, Civil Aviation, Standards Branch

Original signed by Craig Leonard

Linda Melnyk
Director Standards (AART)
Transport Canada, Civil Aviation, Standards Branch

Original signed by Linda Melnyk

Table of contents

1. Record of revisions

Table 1 Record of revisions
Revision Number Section(s) / Page(s) from previous Revisions Date

Initial issue

All

2000-11-22

1

Page 20

2004-11-15

2

All

2005-04-30

3

Page 27

2006-11-09

4

Pages 27, 117, 118

2008-10-14

5

All

2024-07-12

2. Introduction

2.1 General

The Transport Canada Flight Technical and Operator Certification (FTOC) section of the Civil Aviation Standards Branch is responsible for the TCCA Operational Evaluation (OE) program. FTOC’s objectives during the operational evaluation of a new or modified aircraft are to determine:

  • a) The acceptability of a manufacturers training program for use by Canadian operators;
  • b) Pilot qualification and type rating requirements including training, checking, and currency requirements, and;
  • c) The operational suitability of an aircraft type.

This report lists those determinations for use by:

  • a) TCCA Inspectors who approve training programs;
  • b) TCCA inspectors; Approved Check Pilots (ACPs) who conduct Pilot Proficiency Checks (PPCs) and Advanced Qualification Program (AQP) Evaluators who conduct Line Operational Evaluations (LOEs); and
  • c) Air operators, private operators and training providers, to assist them in developing their flight-crew member training, checking and currency programs.

Determinations made in this report are based on the evaluations of specific variants of the CRJ aircraft series made in accordance with current regulations, standards and guidance. Modifications and upgrades made to the series described herein, or introduction of new related aircraft, may require amendment of the findings in this report.

Notes

  1. MHI RJ AVIATION ULC training programs evaluated during OEs are not granted TCCA approval. It is incumbent upon the air operators or private operators to ensure their CRJ aircraft series training program is approved or accepted by the Minister under their relevant TCCA regulatory framework (as applicable under subpart 705, 704 or 604 of the Canadian Aviation Regulations (CARs)) and with the material indicated in this report.
  2. The OE activity assesses a specific training program and its content which is relevant to a specific date. Determinations made in this report do not account for any subsequent changes to the training program which have not been evaluated by the OEB.

2.2 Regulatory requirements / language

This OE report uses mandatory terms such as “must”, “shall” and “is/are required” to convey the intent of the regulatory requirements and other guidance documents. The term “should” is understood to mean that the proposed method of compliance must be used, unless an alternate means of compliance has been determined and approved.

Note

The terms “Pilot” and “Flight Crew” may be used interchangeably within this report and should be used specifically when dictated by the context of their use.

3. Highlights of change

This Operational Evaluation Board (OEB) report revision 5 is in an entirely new TCCA OE report format, update content and more closely harmonizes with the FAA Flight Standardization Board Report (FSBR) original issue for the CRJ1000, dated November 8, 2011 and the Revision 7 for the other CRJ, dated December 11, 2019. This OE report revision incorporate & supersede the letter of acceptance (LOA) – CRJ550 dated August 6, 2019, and the National Aircraft Certification (NAC) letter title Bombardier CRJ1000 - operational evaluation board results dated January, 2011. This revision also reflects a change of ownership that resulted in the type certificate (TC) No. A-276 being transferred from Bombardier Inc. to MHI RJ Aviation ULC dated June 1, 2020. Change bars are not included in this document because the entire report is revised and updated.

The following are highlights of changes in the report:

  • Cover page – Table updated;
  • Table of contents – updated;
  • Section 1 – Record of revisions updated;
  • Section 2 – Editorial updated;
  • Section 3 – Highlights of change updated;
  • Section 4 – CRJ550 and CRJ1000 added and editorial updated;
  • Section 5 – Acronyms added and removed;
  • Section 6 – Editorial updated;
  • Section 7 – CRJ550 and CRJ1000 added, CRJ1000 note added and editorial updated;
  • Section 8 – CRJ550 and CRJ1000 added;
  • Section 9 – CRJ550 and CRJ1000 added and editorial updated;
  • Section 10 – CRJ550 and CRJ1000 added and editorial updated;
  • Section 11 – Subpart 705 of the CARs MFF currency requirements specific between all CRJ variants added;
  • Section 12 - CRJ550 and CRJ1000 added and editorial updates
  • Section 13 – CRJ550 and CRJ1000 added and editorial updated;
  • Section 14 – References updated;
  • Appendix 1 – Editorial updated;
  • Appendix 2 – Master differences requirements (MDR) table updated to include the CRJ550 and the CRJ1000 and currency requirement removed;
  • Appendix 3 – Difference tables updated, CRJ550 and CRJ1000 added, note regarding the CRJ1000 added and currency column removed;
  • Appendix 4 – New Appendix titled Transition Line Indoctrination (TLI) using content moved from the main body of the previous version of the report, CRJ550 and CRJ1000 added;

4. General

4.1 Scope of report

This OE report applies to all CRJ variants and is in accordance with current regulations, standards, and guidance. The contents of this report are harmonized where possible with the FAA and the EASA reports.

Notes

  1. This report refers to the CRJ aircraft series by their TCDS/ Master Series identifier (e.g., CL-600-2B19, CL-600-2C11), by their marketing names (CRJ100/200/440, CRJ700/701/702, CRJ550, CRJ705, CRJ900 or CRJ1000) or by his pilot type rating designator (CL65) as necessary for convenience and clarity.
  2. Through this report, the terms «All CRJ variants» or «all CRJ aircraft series» are sometime used to replace «CRJ100/200/440, CRJ700/701/702, CRJ550, CRJ705, CRJ900 and CRJ1000» when applicable.
  3. This revision also reflects a change of ownership that resulted in the Type Certificate (TC) No. A-276 being transferred from Bombardier Inc. to MHI RJ Aviation ULC dated June 1, 2020.
    1. The corporate name «Bombardier» has been removed from the marketing names of the CRJ aircraft series and is reflected as follows:
      Table 2 Former and current marketing names comparison table
      Former marketing names Current marketing names

      Bombardier CRJ100/200/440

      CRJ100/200/440

      Bombardier CRJ700/701/702

      CRJ700/701/702

      Bombardier CRJ550

      CRJ550

      Bombardier CRJ705

      CRJ705

      Bombardier CRJ900

      CRJ900

      Bombardier CRJ1000

      CRJ1000

4.2 Guidance material

TCCA OEs were conducted in accordance with the latest revisions of FAA Advisory Circular (AC) AC-120-53B Change 1, Guidance for Conducting and Use of Flight Standardization Board (FSB) Evaluations, and the JOEB OPS/FCL Common Procedures for conducting Operational Evaluation Boards (Common Procedures Document (CPD)).

Note

Test evaluation processes (T1/T2/T3/T5) referred through this report are processes used by the OEB to validate the training differences levels proposed by the Original Equipment Manufacturer (OEM). Guidance material listed above can provide more details on those processes.

4.3 OE report effectivity

Provisions of this report are effective until amended, superseded, or withdrawn by subsequent OE findings.

TCCA reserves the responsibility and authority to re-evaluate and modify sections of this report based on new or revised advisory material, amended Canadian Aviation Regulations (CARs), aircraft operating experience, or the evaluation of new or modified aircraft under the provisions of the CPD or FAA AC-120-53B Change 1 (latest revision).

4.4 Application of OE report

All relevant parts of this report are applicable on the effective date of this report.

4.5 Alternate means of compliance

The OEB Chairman, the Program Manager of Flight Technical and Operator Certification (FTOC) and/or the Chief of Commercial Flight Standards (CFS) should be consulted when alternate means of compliance, other than those specified in this report, are proposed. An applicant shall be required to submit a proposed alternate means that provides an equivalent level of safety to the provisions of the CARs and this OE report. Analysis, demonstrations, proof of concept testing, differences documentation, and/or other substantiation may be required.

In the event an alternate compliance is sought, training program credits, simulator approvals, and device approvals may be significantly limited and reporting requirements may be increased to ensure equivalent levels of training, checking, and currency are maintained. TCCA will generally not consider relief through alternate compliance means unless sufficient lead-time has been planned by an operator to allow for any necessary testing and evaluation.

4.6 AQP/OEB report relationship

Where an air operator has an approved AQP, differences between this report and an operator’s proposed training, checking, and currency requirements under an AQP should be substantiated and documented as part of the operator’s AQP approval process. Program approvals under AQP need to ensure the provisions and requirements of this report have been addressed, and where necessary, coordination with the OEB has been completed.

4.7 CRJ100/200/440

The CRJ100 entered service in 1992.

Notes

  1. The CRJ100/200/440 is comprised of three separate aircraft variants: the CRJ100, CRJ200 and the CRJ440 respectively.
  2. The CRJ200 is a marketing designator for the CRJ100 aircraft with the General Electric CF-34-3B1 engines installed.

4.8 Differences between the CRJ100/200/440 and the CRJ700/701/702

In September 2000, TCCA and the FAA jointly evaluated differences from the CRJ100/200/440 (base aircraft) and the CRJ700/701/702 (related aircraft). Master level C/C differences were established between the CRJ100/200/440 and the CRJ700/701/702.

Note

The CRJ700/701/702 is comprised of three separate aircraft variants: CRJ700, CRJ701 and the CRJ702 respectively.

4.9 Differences between the CRJ100/200/440, the CRJ700/701/702 and the CRJ900

  • 4.9.1 Differences between the CRJ700/701/702 and the CRJ900

    In August 2002, TCCA, the FAA and JAA jointly evaluated differences from the CRJ700/701/702 (base aircraft) and the CRJ900 (related aircraft) using a T1 evaluation process. Master level A/A differences were established between the CRJ700/701/702 and the CRJ900.

  • 4.9.2 Differences between the CRJ100/200/440 and the CRJ900

    In October 2002, TCCA, the FAA and JAA jointly evaluated differences from the CRJ100/200/440 (base aircraft) and the CRJ900 (related aircraft) using a T2/T3 evaluation process. Master level C/C differences were established between the CRJ100/200/440 and the CRJ900.

4.10 Differences between the CRJ900 and the CRJ705

In March 2005, TCCA, the FAA and EASA jointly evaluated differences from the CRJ900 (base aircraft) and the CRJ705 (related aircraft) through an analysis process. Master level A/A differences were established between the CRJ900 and the CRJ705.

4.11 Differences between the CRJ700/701/702 and the CRJ550

In July 2019, TCCA evaluated differences from the CRJ700/701/702 (base aircraft) and the CRJ550 (related aircraft) through an analysis process. Master level A/A differences were established between the CRJ700/701/702 and the CRJ550.

4.12 CRJ1000

In 2010, TCCA, the FAA and JAA jointly evaluated differences from the CRJ100/200/440 (base aircraft) and the CRJ700/701/702 (base aircraft) to the CRJ1000 (related aircraft) using a T2/T3 and T5 evaluation process. Master level D/D differences were established.

The evaluations of the reverse differences from the CRJ1000 to the CRJ100/200/440 and CRJ700/701/702 aircraft were not accomplished. The CRJ1000 was therefore assigned the CL65 pilot type rating on an interim basis. The CL65 pilot type rating for the CRJ1000 is subject to revision if a future OE takes place to establish reverse difference credits from the CRJ1000 to other CRJ variants.

Notes

  1. The CRJ1000 was type certified in Canada dated November 01, 2010, and is therefore included on the TCCA TCDS A-276; and
  2. Principal Operations Inspectors (POIs) and Technical Team Leads (TTLs) should contact the Program Manager of FTOC if an alternate means of compliance is proposed (See section 4.5 of this report).

5. Acronyms

AC
Advisory Circular
ACFT
Aircraft
ACP
Approved Check Pilot
ADG
Air Driven Generator
AFCS
Automatic Flight Control System
AFM
Airplane Flight Manual
AGL
Above Ground Level
APU
Auxiliary Power Unit
AQP
Advanced Qualification Program
AV
Audiovisual Presentation
BATC
Bombardier Aerospace Training Centre
CARs
Canadian Aviation Regulations
CASS
Commercial Air Service Standard
CAT
Category
CBT
Computer Based Training
CPD
Common Procedures Document
CPT
Cockpit Procedures Trainer
EASA
European Union Aviation Safety Agency
EFIS
Electronic Flight Instrument Systems
FAA
Federal Aviation Administration
FADEC
Full Authority Digital Engine Control
FCP
Flight Control Panel
FD
Flight Director
FFS
Full Flight Simulator
FLT CHAR
Flight Characteristics
FMA
Flight Mode Annunciator
FMS
Flight Management System
FSB
Flight Standardization Board (FAA)
FSBR
Flight Standardization Board Report
FSTD
Flight Simulation Training Device
FTD
Flight Training Device
FTOC
Flight Technical and Operator Certification (TCCA)
GLD
Ground Lift Dumpers
GPS
Global Positioning System
GSD
Galley Service Door
HGS
Head-Up Guidance System
HO
Handout
HUD
Head-Up Display
ICBI
Interactive Computer Base Instruction
ILS
Instrument Landing System
IOE
Initial Operating Experience
JAA
Joint Aviation Authorities
JOEB
Joint Operational Evaluation Board
LOA
Letter of Acceptance
LOC
Localizer
LOE
Line Operational Evaluation
MDR
Master Differences Requirements
MFF
Mixed Fleet Flying
MLW
Maximum Landing Weight
MTOW
Maximum Takeoff Weight
MZFW
Maximum Zero Fuel Weight
NAC
National Aircraft Certification
N1
Rotational Speed of the Low-Pressure Compressor in a Dual-Spool Gas Turbine Engine
OE
Operational Evaluation
OEB
Operational Evaluation Board
OEM
Original Equipment Manufacturer
PFD
Primary Flight Display
PIC
Pilot In Command
POI
Principal Operations Inspector
PPC
Pilot Proficiency Check
PROC CHNG
Procedural Changes
PTT
Part Task Trainers
QRH
Quick Reference Handbook
RNP
Required Navigation Performance
RNP AR
Required Navigation Performance Authorization Required
RVR
Runway Visual Range
SIC
Second In Command
SU
Stand-Up Instruction
TASE
Training Area of Special Emphasis
TCAS
Traffic Collision Avoidance System
TCBI
Tutorial Computer Based Instruction
TCCA
Transport Canada Civil Aviation
TCDS
Type Certificate Data Sheet
TLI
Transition Line Indoctrination
TTL
Technical Team Leader
V1
Takeoff Decision Speed
VFE
Maximum Flap Extension Speed
VREF
Reference Landing Speed

6. Definitions

These definitions are for the purposes of this report only.

  • 6.1 Base aircraft - An aircraft identified for use as a reference to compare differences with another aircraft.

  • 6.2 Current – A crewmember meets all requirements to operate the aircraft under the applicable CAR or CASS.

  • 6.3 Differences tables – Describe the differences between a pair of related aircraft, and the minimum levels operators must use to conduct differences training and checking of flight crew members. Difference levels range from A to E.

  • 6.4 Initial operating experience (IOE)/Initial line indoctrination –Supervised line flying experience acquired on a particular aircraft type. IOE terminology applies to an advanced qualification program (AQP).

  • 6.5 Master differences requirements (MDR) – Specifies the highest training and checking difference levels between a pair of related aircraft derived from the Differences Tables.

  • 6.6 Mixed fleet flying (MFF) program – A program permitting the operation of a base aeroplane and one or more variant(s) of the same, common or different type by one or more flight crew member, between training or checking events in accordance with an approved process based on the recommendations of an OE report that is acceptable to the Minister.

  • 6.7 Operational evaluation – A TCCA evaluation of the pilot qualifications requirements of an aircraft type (pilot type rating, minimum flight crew member training, checking and currency requirements, and unique or special pilot qualification requirements (e.g., specific flight characteristics, no-flap landing)), operational suitability of an aircraft type and the Original Equipment Manufacturer (OEM) training program.

  • 6.8 Operational suitability – A determination during an operational evaluation that an aircraft or system may be used in the Canadian airspace system and meets the applicable operational regulations (e.g., CAR subparts 604, 605, 701,702,703,704 and 705 as applicable).

  • 6.9 Qualified – A flight crewmember holds the appropriate licenses and ratings as required by the applicable operating regulations.

  • 6.10 Related aircraft – Any two or more aircraft of the same make with either the same or different type certificates that have been demonstrated and determined by TCCA to have commonality.

  • 6.11 Seat dependent tasks – Maneuvers or procedures using controls that are accessible or operable from only one flight crewmember seat.

  • 6.12 Specific flight characteristics – A maneuver or procedure with unique handling or performance characteristics that TCCA has determined must be checked.

  • 6.13 Training Areas of Special Emphasis (TASE) – A training requirement unique to the aircraft, based on a system, procedure, or maneuver, which requires additional highlighting during training. It may also require additional training time, specialized training devices or training equipment.

  • 6.14 Variant – Synonym for related aircraft. A variant is an aeroplane or a group of aeroplanes with the same characteristics that have pertinent differences from a base aeroplane. Pertinent differences are those that require different or additional flight crew member knowledge, skills and/or abilities that affect flight safety. (See Related aircraft)

7. Pilot type rating

The pilot type rating designator for all CRJ variants is CL65. The CL65 pilot type rating published in Appendix A Aircraft Type Designator Tables of Standard 421 - Flight Crew Permits, Licenses and Ratings – Canadian Aviation Regulations (CARs) has been assigned to the CRJ100/200/440, CRJ700/701/702, CRJ550, CRJ705, CRJ900 and CRJ1000.

Note

The CL65 pilot type rating has been assigned to the CRJ1000, on an interim basis. (See Section 4.12 of this report).

8. Related aircraft

8.1 Related aircraft on same TCDS

The CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24 and the CL-600-2E25 are related aircraft listed on TCCA TCDS A-276.

Note

Refer to table on the cover page of this OE report for the relationship between TCDS designators, marketing names and pilot type rating designator.

8.2 Related aircraft on different TCDS

Reserved.

9. Pilot training

Note

Only references from subpart 705 of the CARs are provided in the following sections 9, 10 and 11. If the aircraft is to be operated under a different subpart of the CARs:

  • a) Private operators training programs are to be developed in accordance with the requirements of subpart 604 of the CARs; and/or
  • b) Air Operators training programs are to be developed in accordance with the requirements of subpart 704 of the CARs.

9.1 Previous experience

The provisions of this section apply to CRJ training programs for pilots who have experience with air operator from subpart 705 of the CARs or equivalent operations (i.e., CAR 704, CAR 604) and multi-engine transport category turbojet or turboprop aeroplanes. Pilots receiving CL65 type training should have experience in high altitude operations, highly integrated avionics systems with EFIS and FMS. Pilots without this experience may require additional training.

9.2 CRJ initial type training course requirement

CRJ air operator’s initial type training course must meet the flight training requirements of CASS 725.124 (11) level C or CASS 725.124(12) level D training program. The initial type training course must satisfy the type rating requirements of CASS 421.40(3) (a) (iii), and the training requirements of CASS 725.106(1).

The OEM training courses evaluated can be used by POIs to assist them in approving or accepting training programs to operate CRJ aircraft series in respectively commercial air services (CARs 705 or CARs 704) or private operations (CARs 604).

Note

  1. TCCA does not retain any courseware since the OEs were initially conducted. The OEB Chairman, or the Program Manager of FTOC should be consulted for inquiries related to course content initially evaluated.
  2. The following training provider was contracted during OEs:
    1. Bombardier Aerospace Training Centre (BATC) was the training provider for all CL65 OEs.

9.3 CRJ initial training

Air operators must establish an initial training program that is compliant with CAR 705.124(2)(a). Initial training for flight crews must include appropriate training in accordance with CASS 725.124 or an approved advanced qualification program (AQP) program.

  • 9.3.1 Ground training

    CRJ air operator’s initial ground training program shall include the technical initial ground training requirements of CASS 725.124(6)(a).

  • 9.3.2 Flight training

    CRJ air operator’s initial flight training program must meet the flight training requirements of CASS 725.124 (11) level C or CASS 725.124 (12) level D training program.

    Notes

    1. The CRJ700/701/702, CRJ550, CRJ900 and CRJ705 are considered to be functionally equivalent and, as a result, can be all addressed within the same initial course provided respective differences training is tough by the operator as specified in the Appendix 2, 3 and 4;
    2. Under CARs subpart 704 only, the air operators training program are approved by TCCA and are required to meet the minimum time as per CASS 724.115. These minimum times indicated do not include any aircraft differences training, specialty training and training associated with special authorizations/specific approvals (SA);

9.4 Recurrent Training

Air operators must establish a recurrent training program that is compliant with CAR 705.124(2)(a)(iv). Recurrent training for flight crews must include appropriate training in accordance with CASS 725.124 or an approved AQP program.

In addition, air operators must include the applicable training areas of special emphasis (TASE) from section 9.5 of this report.

  • 9.4.1 Ground training

    A CRJ air operator’s recurrent ground training program must incorporate the technical annual ground training requirements of CASS 725.124(6)(b) of the CASS.

  • 9.4.2 Flight training

    A CRJ air operator’s recurrent flight training program must incorporate appropriate maneuvers and procedures in accordance with CASS 725.124 or an approved AQP program.

9.5 Training Areas of Special Emphasis (TASE)

Notes

  1. References to “pilots” in this section include both pilots in command (PIC) and second in command (SIC) unless otherwise specified.
  2. TASE must be included in initial, upgrade, transition, and recurrent training.

Pilots must receive special emphasis training in the following areas:

  • 9.5.1 TASE - Ground training

    • 9.5.1.1 TASE - Ground training – All CRJ aircraft series except the CRJ1000

      Pilots must receive special emphasis on the following areas during ground training:

      • a) Flight control panel (FCP);
      • b) Flight mode annunciator (FMA);
      • c) FADEC (if applicable);
      • d) FMS (an expanded training footprint should be considered for pilots without previous FMS experience); and
      • e) Engine (or thrust) mode annunciator.

        Note

        TASE ground training applicable to all series of CRJ except the CRJ1000.

    • 9.5.1.2 TASE – Ground Training – CRJ1000

      Pilots must receive special emphasis on the following areas during ground training:

      • a) Primary flight displays (PFDs) and multifunction displays (MFDs);
      • b) Flight control panel (FCP), including light bar/switch position functionality;
      • c) Flight mode annunciator (FMA);
      • d) FADEC (if applicable) and engine indication and crew alerting system (EICAS);
      • e) FMS (an expanded training footprint should be considered for pilots without previous FMS experience); and
      • f) Engine (or thrust) Mode Annunciator;
      • g) Coupled and non-coupled V-Nav.

        Note

        TASE ground training applicable to the CRJ1000 only.

  • 9.5.2 TASE - Flight training

    Pilots must receive special emphasis on the following areas during flight training:

    • a) Aileron PCU runaway;
    • b) Dual hydraulic system malfunctions (System 1 or 2 and 3);
    • c) Air driven generator (ADG) deployment;
    • d) Dutch roll (with and without both yaw dampers operative;
      • i. High altitude / slow speed;
      • ii. 10,000 feet / landing configuration;
    • e) ILS approach on standby instruments;
    • f) Landing with ground lift dumpers (GLD) not deployed;
    • g) Aircraft performance in low energy go-around situations;
    • h) Circling approach and maneuvering at night;
    • i) Effects of wing leading edge contamination;
    • j) Inadvertent thrust reverser deployment;
    • k) Windshear;
    • l) GPS (if applicable);
    • m) HGS (if applicable);
    • n) TCAS;
    • o) Flight control system (modes of operation, control-by-wire rudder system) (for the CRJ1000 only)

      Note

      TASE flight training applicable to all series of CRJ except where indicated.

9.6 Special training

  • 9.6.1 Special training applicable to the CRJ100/200/440

    Pilots must receive special training on the following areas:

    • a) Enhanced take-off procedures and winter operations training – Enhancement to take-off operational safety margins training (Refer to airworthiness directive CF-2008-15R1 and AFM CRJ100/200 Chapter 2 – Limitations – Operations Limitations).

    Note

    Applicable only to the CRJ100/200/440.

9.7 Specific flight characteristics

There are no specific flight characteristics.

9.8 Seat dependent tasks

Pilots must receive training in these seat dependent tasks during initial, upgrade, transition and recurrent training:

  • a) Tiller Usage (left seat).
  • b) HUD / HGS (left seat).

9.9 Flight Simulation Training Devices (FSTD)

An approved level C or D CL65 full flight simulator (FFS) equipped with day and night visual scenes that is representative of an operator’s specific CL65 configuration is required for flight training.

Training and checking under CARs Part IV, VI and VII must be conducted on a certified FTD and FFS in accordance with section 606.03 of the CARs.

FTD and FFS characteristics are designated in the Aeroplane and Rotorcraft Simulator Manual (TP 9685). The FSTD specific systems qualifications are found in the TCCA Qualification Certificate.

9.10 Training equipment

There are no specific systems or procedures that are unique to the CRJ aircraft series that require specific training equipment.

9.11 Differences training

  • 9.11.1 Differences training between related aircraft

    Pilots must receive differences training between all CRJ variants. Refer to appendices 2, 3 and 4 of this report.

    Note

    Subpart 705 of the CARs air operators who established a transition / mixed fleet flying (MFF) approved training program(s) should refer to section 9.13 of this report.

  • 9.11.2 Differences training – Optional equipment

    Reserved.

    Note

    Operator specific optional equipment items have not been evaluated under the scope of OEs. Operators should note that the CRJ aircraft series has a wide range of optional equipment which may require additional flight crew training. TCCA approved training programs for initial, recurrent, transition and upgrade training, as applicable, must include training on TCCA certified optional equipment.

9.12 Other training

Note

Specialty training activities have not been evaluated under the scope of OEs. Operators should note that the CRJ has a wide range of specialty training which require additional flight crew training. These activities covered by specialty training may require a special authorization/specific approval (SA) from TCCA. TCCA approved training programs for initial, recurrent, transition and upgrade training, as applicable, may include specific training on the operator’s specialty training.

  • 9.12.1 HUD / HGS

    When HUD is installed and an operator is authorized HUD operations, training must address appropriate flight training elements for both HUD and non-HUD operations. This item must be included in initial, upgrade, transition, differences, and recurrent training.

    Note

    A type certified heads up guidance system (HGS) is capable of providing guidance to permit manually flown approaches and landings in low visibility weather conditions.

9.13 Subpart 705 of the CARs transition / mixed fleet flying (MFF) approved training program(s)

A subpart 705 of the CARs air operator may develop an approved transition program to obtain credits for training, checking, consolidation period requirements, line checks, line indoctrination and validity periods in order to transition from a base aeroplane to one or more variants of the same type, common type or different type under an approved transition program as set out in the air operator’s company operations manual.

Additionally, a subpart 705 of the CARs air operator may develop an approved MFF program to operate a base aeroplane and one or more variants of the same type, common type or different type under an approved MFF program after complying with the requirements of a transition program, in order to provide relief for 90 days pilot qualification requirements on the applicable aeroplane type(s) intended to be operated between training and checking events.

Notes

  1. Pilots transitioning between any CRJ variants (e.g., CRJ100/200/440 to CRJ700/701/702 or CRJ550 or CRJ900 or CRJ705, CRJ100/200/440 or CRJ700/701/702 or CRJ550 or CRJ900 or CRJ705 to CRJ1000) or conducting MFF with different CRJ variants (e.g. CRJ100/200/440 and CRJ700/701/702, CRJ100/200/440 or CRJ700/701/702 and CRJ1000) require exemptions to specific provisions of CAR 705.106, CASS 725.106 and CAR 705.113. Appendices 2, 3 and 4 provide the training, checking and Transition credits between the CRJ aircraft series. TCCA Policy Letter AARX No. 173, Original issue, dated July 25, 2005 (RDIMS # 1040396) provide guidance on flight crew member qualification credits for transition programs and mixed fleet flying programs.
  2. Provisions found in this section are only applicable for subpart 705 of the CARs.
  • 9.13.1 Alternating recurrent training between CRJ variants

    Under an approved transition/MFF program(s), recurrent training may alternate between CRJ variants.

    The air operator shall provide recurrent technical ground training on one variant with differences technical ground training on the other variant(s) as detailed in the appendix 3.

    The air operator must include the applicable training areas of special emphasis (TASE) from section 9.5 of this report for all CRJ variants operated under an approved transition/MFF program(s).

    Note

    Air operators involved in a MFF operations with any variant(s) of the CRJ700/701/702, CRJ550, CRJ900 or CRJ705 paired with any other CRJ variant(s) should considered the CRJ700/701/702, CRJ550, CRJ900 and CRJ705 as the same variant for the purposes of alternating recurrent simulator training under an approved transition/MFF training program(s).

  • 9.13.2 Transition line indoctrination (TLI)

    Transition line indoctrination (TLI) related to CRJ aircraft series are provided in Appendix 4 of this report.

10. Pilot checking

10.1 Landing from a no flap or non standard flap approach

Reserved.

10.2 Specific flight characteristics

There are no specific flight characteristics.

10.3 Seat dependent tasks

During initial, transition, and upgrade checking, pilots must be checked in these seat dependent tasks:

  • a) Tiller usage (left seat).
  • b) HUD (left seat).

10.4 Other checking items

Note

Specialty training activities have not been evaluated under the scope of OEs. Operators should note that the CRJ has a wide range of specialty training which may require additional flight crew checking. The activities covered by specialty training may require a special authorization/specific approval (SA) from TCCA. TCCA approved training programs for initial, recurrent, transition and upgrade training, as applicable, may include specific checking on the operator’s specialty training.

  • 10.4.1 Special checking

    • 10.4.1.1 Special checking applicable to the CRJ100/200/440

      It is required that the special training at 9.6.1.1 will be follow by a successful checking event.

  • 10.4.2 Head up Guidance System (HGS)

    When HGS use is approved, checking must include a suitable demonstration of HGS use for modes and phases of flight authorized. Checking standards for HGS are equivalent to those for non-HGS operations. Periodic assessment of non-HGS skills should also be demonstrated. Therefore, an ACP/inspector may request that authorized maneuvers be performed without use of HGS (e.g., if manual CAT II F/D operations are authorized, the pilots being checked may be requested to perform the maneuver without HGS).

    Note

    A type certified heads up guidance system (HGS) is capable of providing guidance to permit manually flown approaches and landings in low visibility weather conditions.

10.5 FSTD

An approved level C or D CL65 FFS equipped with day and night visual scenes that is representative of an operator’s specific CRJ aircraft series configuration is required for flight checking.

10.6 Equipment

There are no specific systems or procedures that are unique to the CRJ aircraft series that require specific equipment.

10.7 Differences checking between related aircraft

Differences checking between certain CRJ variants may be required. The level of checking is specified in appendix 2 and 3.

Note

Subpart 705 of the CARs air operators who established a transition / MFF approved training program(s) should refer to section 10.8 of this report.

10.8 Subpart 705 of the CARs transition / mixed fleet flying (MFF) approved training program(s)

A subpart 705 of the CARs air operator may develop an approved transition program to obtain credits for training, checking, consolidation period requirements, line checks, line indoctrination and validity periods in order to transition from a base aeroplane to one or more variants of the same type, common type or different type under an approved transition program as set out in the air operator’s company operations manual.

Additionally, a subpart 705 of the CARs air operator may develop an approved MFF program to operate a base aeroplane and one or more variants of the same type, common type or different type under an approved MFF program after complying with the requirements of a transition program, in order to provide relief for 90 days pilot qualification requirements on the applicable aeroplane type(s) intended to be operated between training and checking events.

Notes

  1. Pilots transitioning between any CRJ variants (e.g., CRJ100/200/440 to CRJ700/701/702 or CRJ550 or CRJ900 or CRJ705, CRJ100/200/440 or CRJ700/701/702 or CRJ550 or CRJ900 or CRJ705 to CRJ1000) or conducting MFF with different CRJ variants (e.g. CRJ100/200/440 and CRJ700/701/702, CRJ100/200/440 or CRJ700/701/702 and CRJ1000) require exemptions to specific provisions of CAR 705.106, CASS 725.106 and CAR 705.113. Appendices 2, 3 and 4 provide the training, checking and transition credits between the CRJ aircraft series. TCCA Policy Letter AARX No. 173, Original issue, dated July 25, 2005 (RDIMS # 1040396) provide guidance on flight crew member qualification credits for transition programs and mixed fleet flying programs.
  2. Line checks conducted in one variant should satisfy the requirements for all CRJ variants. If the operator’s line operations (e.g., route structure, area of operation, ETOPS) of one variant is significantly different from another variant, then separate line checks should be conducted.
  3. The currency requirements detailed at sections 11 of this report shall be maintained.
  4. Provisions found in this section are only applicable for subpart 705 of the CARs.
  • 10.8.1 Alternating PPC between CRJ variants

    Under an approved transition/MFF program(s), recurrent checking events may alternate between CRJ variants.

    PPCs should alternate each six months for flight crew members.

    When such alternating checks are accomplished, the differences checking assessment of the other variant within the series grouped may be satisfied by ground training, written questionnaire, oral review, or other method approved by the Principal Operations Inspector (POI) or Technical Team Leader (TTL). However, such simplified programs may not be approved if they result in progressive loss of knowledge or skills related to particular differences over successive recurrent periods.

    Note

    Air operators involved in a MFF operations with any variant(s) of the CRJ700/701/702, CRJ550, CRJ900 or CRJ705 paired with any other CRJ variant(s) The CRJ700/701/702, CRJ550, CRJ900 and CRJ705 should be considered the CRJ700/701/702, CRJ550, CRJ900 and CRJ705 as the same variant for the purposes of alternating recurrent simulator checking under an approved transition/MFF training program(s).

11. Pilot currency

There are no additional currency requirements for the CRJ aircraft series other than those already specified in subparts 705, 704 and 604 of the CARs.

11.1 Differences currency between related aircraft

Not established for operators from subparts 604 and 704 of the CARs.

For currency credit established between related aircraft for subpart 705 of the CARs air operators, refer to section 11.2.1 of this report.

11.2 Subpart 705 of the CARs mixed fleet flying (MFF) approved training program

A subpart 705 of the CARs air operator may develop an approved transition program to obtain credits for training, checking, consolidation period requirements, line checks, line indoctrination and validity periods in order to transition from a base aeroplane to one or more variants of the same type, common type or different type under an approved transition program as set out in the air operator’s company operations manual.

Additionally, a subpart 705 of the CARs air operator may develop an approved MFF program to operate a base aeroplane and one or more variants of the same type, common type or different type under an approved MFF program after complying with the requirements of a Transition program, in order to provide relief for 90 days pilot qualification requirements on the applicable aeroplane type(s) intended to be operated between training and checking events.

Notes

  1. Pilots conducting MFF between any CRJ variants (e.g., CRJ100/200/440 and CRJ700/701/702, CRJ100/200/440 or CRJ700/701/702 and CRJ1000) require exemptions from subparagraphs 705.106(1)(b)(i) and (ii), of the CARs. TCCA Policy Letter AARX No. 173, Original issue, dated July 25, 2005 (RDIMS # 1040396) provide guidance on flight crew member qualification credits for transition programs and mixed fleet flying programs.
  2. Those provisions found in section 11.2 are only applicable for subpart 705 of the CARs.
  • 11.2.1 Subpart 705 of the CARs MFF currency requirements between CRJ variants

    Under an approved MFF program and with reference to section 11.1 of this report, there are no differences currency requirements between CRJ variants except:

    • a) Flight crews operating the CRJ100/200/440 and the CRJ1000, should complete at least three take-offs and landings within the previous 90 days, and a minimum of one sector in each variant within the previous 90 days. (No currency credit.)
    • b) Flight crews operating the CRJ700/701/702 or the CRJ550 and the CRJ1000, should perform at least one take-off and landing on the CRJ700/701/702 or the CRJ550 and at least one take-off and landing on the CRJ1000, when performing the required take-offs and landings within the previous 90 days. (Partial currency credit.)

11.3 Special currency applicable to the CRJ100/200/440

It is required that the special training at section 9.6.1.1 of this report will be successfully completed within the preceding 12 calendar months from take-off procedures, ground icing conditions and cold weather operations as detailed in the applicable AFM CRJ100/200 Chapter 2 – Limitations - Operations Limitations.

12. Operational suitability

All CRJ aircraft series are operationally suitable for operations under subparts 705, 704 and 604 of the CARs.

Note

The aircraft may be authorized by the Minister to be operated under subpart 704 of the CARs - Commuter Operations for passenger configurations of 19 or fewer passengers. Refer to section 12.1.1 below for more details.

12.1 Requirement for flight attendants

  • 12.1.1 Commercial air services

    The OEB found that all CRJ variants fall under the subpart 705 of the CARs, due to a MCTOW of more than 8 618 kg (19,000 pounds) and a Canadian type certificate authorizing the transport of 20 or more passengers. However, the aircraft may be authorized by the Minister to be operated under subpart 704 of the CARs - Commuter operations for passenger configurations of 19 or fewer passengers. This authority shall be accompanied by a requirement to have a flight attendant on all passenger carrying flights for the following reasons:

    • 12.1.1.1 Nature of the interior

      The interior of the representative aircraft presented by the manufacturer has the forward area immediately behind the cockpit occupied with passenger service area, main entrance, and forward lavatory between the main passenger cabin bulkhead and the cockpit bulkhead. This arrangement prevents the supervisory control over passengers during flight by visual and aural means by the flight crew.

    • 12.1.1.2 Length of the aircraft

      The length of the main cabin precludes visual supervision of passengers from a cockpit seat. This would be compounded in those configurations where an additional bulkhead forming passenger sleeping compartments and/or office areas is installed in an executive configuration.

  • 12.1.2 Private operations

    For subpart 604 of the CARs private operators, the requirement for a flight attendant starts at thirteen passengers in those aeroplanes that cannot provide for flight crew supervision of the passengers by visual and aural means. If the flight crew have the ability to supervise passengers a flight attendant is required at 20 passengers. Thus, for the foregoing reasons, all CRJ variants flights under subpart 604 of the CARs shall carry a flight attendant for thirteen passengers or more. If an operator feels that their particular aircraft interior configuration is such that a flight attendant should not be a requirement, Principal Operations Inspectors (POIs) and Technical Team Leads (TTLs) should contact the Program Manager of FTOC if an alternate means of compliance is proposed (See section 4.5 of this report).

    Notes

    1. CRJ100/200/440 aircrafts prior to Serial No. 7457 have main passenger entry doors that open somewhat slower than main passenger entry doors on aircraft Serial No. 7457 and subsequent. The aircraft Serial No. 7457 and subsequent door design is known as a “Phase IV” door (FAA), which will touch the ground approximately 10 seconds after being opened.
    2. All CRJ700/701/702, CRJ550, CRJ900, CRJ705 and CRJ1000 aircraft have Phase IV passenger doors (FAA).
  • 12.1.3 CRJ1000

    For CRJ1000, an additional (third) flight attendant (FA) is required. The 3rd FA is located in a forward facing jump seat adjacent to the forward right galley service door (GSD).

13. Miscellaneous

13.1 Normal final landing flap setting

The normal final landing flap setting is 45 degrees.

13.2 Landing minima categories

The approach aircraft category and resultant approach minima are determined by the airspeed at which the aircraft is to be maneuvered during the final approach segment for a straight-in or circling approach.

Table 3 Aircraft approach categories
Aircraft Landing Flap Category

CRJ100/200/440

45°

D

CRJ700/701/702

45°

C

CRJ550

45°

C

CRJ900

45°

C/DFootnote 1

CRJ705

45°

C/DFootnote 1

CRJ1000

45°

C

13.3 Approach profiles and speed

The approach profiles are the same for all CRJ variants.

Approach speeds are dependent upon aircraft weight. Landing weights for the CRJ705 and the CRJ900 are the heaviest while the CRJ100/200/440 is the lightest in the series of aircraft. Nevertheless, critical speeds are presented to the pilot in a standardized manner for all CRJ variants. Refer to the Footnote in Table 3 above for more details regarding the relation between approach speed and landing minima categories.

13.4 Abnormal & emergency procedures

Immediate action items are with minor exceptions, identical for all CRJ variants. Abnormal and emergency procedures are presented in quick reference handbooks (QRH) of an identical format for all aircraft. Although individual steps may differ, the steps are carried out under the guidance of the handbook in a logical decision-making manner.

13.5 Maximum flap extension speed VFE

Although the CRJ700/701/702, CRJ550, CRJ900, CRJ705 and the CRJ1000 have flaps and slats while the CRJ100/200/440 has flaps only; the slat/flap or flap extension speeds are similar for all CRJ aircraft series.

Table 4 Maximum Flap Speed VFE
Flap Setting (degrees) CRJ100/200/440 CRJ700/701/702/ CRJ550 CRJ900 CRJ705 CRJ1000

1

n/a

230 KIAS

230 KIAS

230 KIAS

230 KIAS

8

230 KIAS

230 KIAS

230 KIAS

230 KIAS

230 KIAS

20

230 KIAS

230 KIAS

220 KIAS

220 KIAS

220 KIAS

30

185 KIAS

185 KIAS

185 KIAS

185 KIAS

185 KIAS

45

170 KIAS

170 KIAS

170 KIAS

170 KIAS

170 KIAS

13.6 Minimum height for use of the autopilot

The minimum height for the use of the autopilot is 600 feet AGL following takeoff for all CRJ aircraft series.

13.7 Procedural knowledge

  • 13.7.1 Takeoff profiles

    The takeoff profiles are similar for all CRJ aircraft series. The only difference between the CRJ aircraft series is that the CRJ700/701/702, CRJ550, CRJ900, CRJ705 and CRJ1000 have one additional callout for flap retraction: «Flaps 1».

13.8 Optional equipment

Reserved.

Note

Operator specific optional equipment items have not been evaluated under the scope of OEs. Operators should note that the CRJ has a wide range of optional equipment which may require additional flight crew training. TCCA approved training programs for initial, recurrent, transition and upgrade training, as applicable, must include training on TCCA certified optional equipment.

13.9 Scope of CRJ1000 OE

The CRJ1000 OE scope did not include an evaluation of differences training from the CRJ1000 (as base aircraft) to the other CRJ aircraft series (as related aircraft). In addition, the OEB did not evaluate cabin crew training, maintenance training, or the use of equipment or functions such as the electronic flight bag (EFB), head up display (HUD), enhanced/synthetic flight vision systems (E/SFVS), RNP AR or steep approaches, etc.

14. References

  1. FAA Flight Standardization Board (FSB) Report for the Bombardier CRJ series aircraft Revision 7 dated 12/11/2019 (December 11, 2019) or later revision (https://drs.faa.gov/browse/FSB_REPORTS/doctypeDetails).

  2. FAA Flight Standardization Board (FSB) Report for the Bombardier CRJ1000 series aircraft Original dated 11/08/2011 (November 08, 2011) or later revision.

  3. FAA Advisory Circular AC120-53B, Change 1, Guidance for Conduction and Use of Flight Standardization Board Evaluations, dated 10/24/16 (October 24, 2016) or later revision (https://drs.faa.gov/browse/FSB_REPORTS/doctypeDetails).

  4. FAA Type Certificate Data Sheet (TCDS) A21EA-1 Revision 4 dated 02/02/2023 (February 02, 2023) or later revision (https://drs.faa.gov/browse/FSB_REPORTS/doctypeDetails).

  5. JOEB OPS/FCL Common procedures for conducting Operational Evaluation Boards, dated June 10, 2004.

  6. EASA Type Certificate Data Sheet (TCDS) IM.A.673 Issue 3.0 dated September 18, 2023 or later revision (https://www.easa.europa.eu/document-library/type-certificates).

  7. EASA Operational Suitability Data (OSD) Flight Crew for CRJ Aircraft Series 100/200/550/700/705/900/1000 – Revision 3, dated September 01, 2023 or later revison.

  8. Transport Canada Advisory Circular, AC 700-035, Special Authorization for Take-off Operations below RVR 600 down to and including RVR 300, at Issue 01, dated February 12, 2016 or later Issue.

  9. TCCA Policy Letter AARX No. 173, Flight Crew Member Qualification Credits for Transition Programs and Mixed Fleet Flying Programs, Original issue, dated July 25, 2005 (RDIMS # 1040396).

  10. TCCA Type Certificate Data Sheet (TCDS) A-276, Issue No. 7, dated December 22, 2022 or later issue.

Appendix 1 – Differences legend

Training differences legend

Differences level

Type

Training method examples

Conditions

A Self-instruction
  • Operating manual revision (HO)
  • Flight crew operating bulletin (HO)
  • Crew has already demonstrated understanding on base aircraft (e.g., updated version of engine).
  • Minor or no procedural changes required.
  • No safety impact if information is not reviewed or is forgotten (e.g., different engine vibration damping mount).
  • Once called to attention of crew, the difference is self-evident.
B Aided instruction
  • Audiovisual presentation (AV)
  • Tutorial computer-based instruction (TCBI)
  • Stand-up instruction (SU)
  • Systems are functionally similar.
  • Crew understanding required.
  • Issues need emphasis.
  • Standard methods of presentation required.
C Systems devices
  • Interactive (full-task) computer based instruction (ICBI)
  • Cockpit procedures trainers (CPT)
  • Part task trainers (PTT)
  • Level 4 or 5 flight training device (FTD 4-5)
  • Training can only be accomplished through systems training devices.
  • Training objectives focus on mastering individual systems, procedures or tasks versus highly integrated flight operations or “real-time” operations.
  • Training devices are required to assure attainment or retention of crew skills to accomplish more complex tasks usually related to aircraft systems.
D Maneuvers devices
  • Level 6 or 7 flight training device (FTD 6-7)
  • Level A or B full flight simulator (FFS A-B)
  • Training can only be accomplished in flight maneuver devices in a real-time environment.
  • Training requires mastery of interrelated skills versus individual skills.
  • Motion, visual, control loading and specific environmental conditions may be required.
E Level C/D FFS or aircraft
  • Level C or D full flight simulator (FFS C-D)
  • Aircraft (ACFT)
  • Motion, visual, control loading, audio and specific environmental conditions are required.
  • Significant full task differences that require a high fidelity environment.
  • Usually correlates with significant differences in handling qualities.
Checking differences legend

Differences level

Checking method examples

Conditions

A None None
B
  • Oral or written exam
  • Tutorial computer based instruction (TCBI) self-test
  • Individual systems or related groups of systems.
C
  • Interactive (full-task) computer based instruction (ICBI)
  • Cockpit procedures trainers (CPT)
  • Part task trainers (PTT)
  • Level 4 or 5 flight training device (FTD 4-5)
  • Checking can only be accomplished using systems devices.
  • Checking objectives focus on mastering individual systems, procedures or tasks.
D
  • Level 6 or 7 flight training device (FTD 6-7)
  • Level A or B full flight simulator (FFS A-B)
  • Checking can only be accomplished in flight maneuver devices in a real-time environment.
  • Checking requires mastery of interrelated skills versus individual skills.
  • Motion, visual, control loading and specific environmental conditions may be required.
E
  • Level C or D full flight simulator (FFS C-D)
  • Aircraft (ACFT)
  • Significant full task differences that require a high fidelity environment.

Appendix 2 - Master differences requirements (MDR) table

These are the minimum levels of training and checking required, derived from the highest level in the differences tables in Appendix 3. Differences levels are arranged as training/checking.

Table 1 Aircraft master differences requirements (MDR)

To related aircraft

From base aircraft

CRJ100/200/440

CRJ700/701/702

CRJ550

CRJ705

CRJ900

CRJ1000

CRJ100/200/440

n/a

CFootnote */C

CFootnote */C

CFootnote */C

Not evaluated

CRJ700/701/702

CRJ550

CFootnote */C

A/A

A/A

A/A

Not evaluated

CRJ705

CFootnote */C

A/A

n/a

A/A

Not evaluated

CRJ900

CFootnote */C

A/A

A/A

n/a

Not evaluated

CRJ1000

DFootnote */D Footnote 1 Footnote 2

DFootnote */D Footnote 1 Footnote 2

DFootnote */D Footnote 1 Footnote 2

DFootnote */D Footnote 1 Footnote 2

n/a

Appendix 3 - Differences tables

Table of contents – Appendix 3
From Base Aircraft To Related Aircraft Page
From CRJ100, CRJ200, CRJ440 To CRJ700, CRJ701, CRJ702 43
From CRJ700, CRJ701, CRJ702 To CRJ100, CRJ200, CRJ440 52
From CRJ100, CRJ200, CRJ440 To CRJ900 62
From CRJ900 To CRJ100, CRJ200, CRJ440 73
From CRJ700, CRJ701, CRJ702 To CRJ900 83
From CRJ900 To CRJ700, CRJ701, CRJ702 87
From CRJ100, CRJ200, CRJ440 To CRJ705 91
From CRJ705 To CRJ100, CRJ200, CRJ440 101
From CRJ700, CRJ701, CRJ702 To CRJ705 109
From CRJ705 To CRJ700, CRJ701, CRJ702 113
From CRJ705 To CRJ900 117
From CRJ900 To CRJ705 118
From CRJ700, CRJ701, CRJ702 To CRJ550 119
From CRJ100, CRJ200, CRJ440 To CRJ1000 120
From CRJ700, CRJ701, CRJ702 To CRJ1000 131
From CRJ705 To CRJ1000 136
From CRJ900 To CRJ1000 140

Footnote to table of contents – Appendix 3:

Each “Differences tables” indicated above (i.e., CRJ100/200/440 to CRJ700/701/702) refer to a design, a system and a maneuver differences table.

Table 1 Appendix 3 Differences tables terminology
Definitions Training Level

(HO) = Handout

A

(ST) = Slide/tape presentations

(TCBI) = Tutorial computer based instruction

(SU) = Stand-up Instructors

(VT) = Video tapes

B

(ICBI) = Interactive computer based instruction

(CSS) = Cockpit system simulators

(CPT) = Cockpit procedures trainers

(PTT) = Part task trainers

(FTD 2-5) = Flight training devices (level 2-5)

C

(FTD 6-7) = Flight training devices (level 6-7)

(FFS A-B) = Simulators (level A or B)

D

(FFS C-D) = Simulators (level C or D)

(ACFT) = Aircraft

E

Note:

C* in the “CHK LVL” column of a Differences Table requires use of training devices specified in “Training level” C column of the respective Differences Table.

From CRJ100, CRJ200, CRJ440 To CRJ700, CRJ701, CRJ702

This design differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
106 ft, 8 in. (32.51 m)
Increase of 18 ft, 10 in. (5.74 m)

Wingspan:
76 ft, 3 in. (23.25 m)
Increase of 6 ft, 9 in. (2.04 m)

Tail span:
28 ft (8.54 m)
Increase of 7 ft, 8 in. (2.34 m)

Height:
24 ft, 10 in. (7.57 m)
Increase of 4 ft, 2 in. (1.27 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
75,000 lb. (34,020 kg)
Increase of 22,000 lb. (9,979 kg)

Max Landing Weight:
67,000 lb. (30,390 kg)
Increase of 20,000 lb. (9,072 kg)

Fuel Capacity:
2902 U.S. gal. (10,977 L)
Increase of 751 gal (2,835 L)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
13 ft, 6 in. (4.0 m)
Increase of 3 ft, 2 in. (0.96 m)

Nose to Main Wheels:
40 ft, 10 in. (12.44 m)
Increase of 4 ft, 6 in. (1.37 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-8C1 or
GE CF34-8C5B1
13,790 lb. of thrust, APR
Increase of 4,570 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Forward cargo bay

No

Yes Emerg.

HO

n/a

n/a

n/a

A

ATA 00 General

Increase of 20 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Addition of second Flight Attendant position

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical power

Revised architecture

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight controls

Three panel slats on each wing

Minor

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 49 APU

Tail cone mounted

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Forward cargo bay door

No

Minor Normals

HO

n/a

n/a

n/a

A

Limitations

APU operating limits;
Engine parameters;
Gear extension speed;
These are not all inclusive.

No

Yes Limits

n/a

ST, TCBI, SU, VT

n/a

n/a

B

This system differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 21 Air Conditioning

Recirculated air distribution system with fan control switch

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

No dedicated fan for avionics bay cooling

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

No dedicated standby fan for EFIS cooling. Backup cooling is via ECS airflow.

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Selected and actual temp displayed on ECS synoptic page

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Revised architecture. No dedicated cargo bay fan

No

No

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Revised architecture. One electrically operated outflow valve, two safety valves, one ground valve

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

CB panels 3 and 4 removed;
40 KVA generator (no load shedding for failed generator);
Generator switches (3) always left in auto;
AC utility buses removed;
ACPC controls switching automatically;
4 - 120A TRUs instead of 5 - 100A TRUs;
Bus Ties are automatic (controlled by DCPC). Switchlights removed on electrical power panel;
Service bus powered from DC bus 2;
One DC utility bus;
DC external power plug and DC External switchlight removed;
New ADG bus installed.
AC electric synoptic changes
ADC (no lamp test)
Battery chargers and battery location

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 26 Fire Protection

Simplified testing procedure. Automatic Bite and MDC interface

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 26 Fire Protection

No jetpipe overheat detection

No

No

HO

n/a

n/a

n/a

A

ATA 26 Fire Protection

Fire suppression for forward cargo area. Common Halon system used to supply both compartments. Three cargo smoke detectors.

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No dedicated spoiler on control surface. Multifunction spoilers act as flight spoiler or spoiler on or ground lift dump.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

No flutter dampers on elevators

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Rudder limiter incorporated, function of speed and flap position controlled by SSCU

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

The power up Bite test starts only when all three hydraulic systems are fully powered. A SPLR/Stab in test advisory message is posted on EICAS during this test - All flight control systems are inoperative during the test

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

For redundancy, emergency slat/flap switch added to drive slats to 25 degrees and flaps to 20 degrees with a slat/flap selector failure

No

Yes Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 27 Flight Controls

Slat/Flap lever has 6 positions

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

No gravity refuel capability on center tank

No

Yes

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Dedicated cross-flow pump

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Bulk fuel temperature sensor in right main tank

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Fuel synoptic changes

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

1B/2B pump is not load shed when respective engine GEN is not operating

No

Minor Abnormal

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

Thrust reversers are powered by hydraulics

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

Hydraulic SOV switches added to isolate EDP during low pressure condition without shutting down the engine

No

Minor Normals Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

No cowl anti-ice blow out plug on engines

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for cowl anti-icing duct leak detection in pylon area

No

Minor New msg.

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Simplified cowl and wing anti-ice synoptic page

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Air data probes and sensor anti-icing tested before flight with ICE DET switchlight

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for wing OVHT protection. No STBY mode for wing anti-ice required.

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Windshield wiper has intermittent position.

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Variable white arcs on the N2 gauges. Range of arc varies with engine bleed condition.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Wing anti-ice system tested continuously. No test switch (automatic function)

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Nose doors are mechanical

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Cantilever assemblies on main gear with shimmy dampers

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No main gear dust pin covers

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No FLT/NORM switch installed on forward external service panel

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No anti-skid test switch. Revised anti-skid test procedure.

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

NWS deflection is +/- 80 degrees with tiller and rudder pedal movement will deflect NW +/- 8 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Overhead panel dome lights installed

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Single nose landing light

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Three exterior lights per side for emergency exit lighting

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

No emer LTS Off light on panel. emer LTS Off caution message only

No

Minor Normals Abnormal

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

No mach transducer or selector valves in Pitot Static system

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

One electronic integrated standby instrument provides airspeed, altitude, attitude, slip/skid, and localizer/glideslope information

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 35 Oxygen

Overboard discharge indicator located on left side of fuselage

No

No

HO

n/a

n/a

n/a

A

ATA 36 Pneumatic

New flight deck bleed air panel. Engine bleed air taken from either 6th or 10th stage to supply common manifold.

Bleed air selection is automatic when in auto mode. Provisions for manual switching.

No

Yes Normals/ Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

Power On automatic bleed air leak detection test

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 49 APU

40 KVA generator
No APU Intake Door 'MID' EICAS indication
Dedicated APU fuel pump
APU Fuel supply, left collector tank
AVAIL light = ready for electrical loading, ECU determines when pneumatic loading is available. No fire horn. Start cycle.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 70 Powerplant

FADEC controlled

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, FTD 2-5

n/a

B

ATA 70 Powerplant

N1 and N2 sync control panel

No

Minor Normals Abnormal

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

FADEC controlled start cycle for ATS and windmill starts

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, FTD 2-5

n/a

B

ATA 70 Powerplant

Thrust reversers hydraulically-actuated. No thrust lever retarder control system

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

No emergency stow PBAs

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

High power schedule PBA

No

Yes

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

FADEC generated thrust limits for: (automatic with thrust levers in respective detent)

Takeoff (TO)
Flex (FLX)
Climb (CLB)
Go Around (GA)
Max Continuous Thrust (MCT)
Cruise (CRZ) - manually set in the cruise range

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

Engine oil test panel removed. Engine oil level quantities provided on menu page

No

Minor Normals

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

AFCS

Initial take off pitch target is optimized to takeoff V speeds entered

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Takeoff

Rotation rate is 3-5 degrees per second towards target FD

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

Takeoff

Throttles placed in "TOGA" detent and thrust is set into N1 caret by FADEC

Throttles placed in "CLB" detent and thrust is set into N1 caret by FADEC

No

No

n/a

n/a

CSS, PTT, FTD 2-5

n/a

B

Takeoff

Flap retraction:

Flaps 8 takeoff - Flaps retracted to '1' from '8' at V2 + 12 and to '0' from '1' at VT -15 kts.

Flaps 20 takeoff - Flaps retracted to '8' from '20' at V2 + 12 and to '1' from '8' at V2 + 20 and then to '0' from '1' at VT -15.

No

Yes Normals

n/a

n/a

CSS, PTT, FTD 2-5

n/a

C*Note: C* in the “CHK LVL” column of a Differences Table requires use of training devices specified in “TRAINING LEVEL” C column of the respective Differences Table. End note

Approach

Approach Attitude Comparison

CRJ200
Single Engine
N/A
Normal
Flapless

 

CRJ700
Normal
Flapless (Slats 25)
Slatless (Flaps 45)
Single Engine

Yes

No

n/a

VT

n/a

n/a

B

Landing

More pronounced flare

Yes

No

n/a

VT

n/a

n/a

B

From CRJ700, CRJ701, CRJ702 To CRJ100, CRJ200, CRJ440

This design differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ100/200/440 (CL-600-2B19)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
87 ft, 10 in. (26.77 m)
Decrease of 18 ft, 10 in. (5.74 m)

Wingspan:
69 ft, 6 in. (21.21 m)
Decrease of 6 ft, 9 in. (2.04 m)

Tailspan:
20 ft, 4 in. (6.2 m)
Decrease of 7 ft, 8 in. (2.34 m)

Height:
20 ft, 8 in. (6.3 m)
Decrease of 4 ft, 2 in. (1.27 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
53,000 lb. (24,041 kg)
Decrease of 22,000 lb. (9,979 kg)

Max Landing Weight:
47,000 lb. (21,319 kg)
Decrease of 20,000 lb. (9,072 kg)

Fuel Capacity:
2151 U.S. gal. (8,142 L)
Decrease of 751 gal. (2,835 L)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
10 ft, 4 in. (3.1 m)
Decrease of 3 ft, 2 in. (0.96 m)

Nose to Main Wheels:
36 ft, 4 in. (11.07 m)
Decrease of 4 ft, 6 in. (1.37 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-3B1
9,220 lb. of thrust, APR
Decrease of 4,570 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

No forward cargo bay

No

Minor

HO

n/a

n/a

n/a

A

ATA 00 General

Decrease of 20 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

One Flight Attendant position

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

Architectural differences

No

Minor
(Ext. DC)

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

No slats on wings

Minor

Yes Normals

HO

n/a

n/a

n/a

A

ATA 49 APU

Located in aft equipment bay
Intake/exhaust/Hazard areas

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

No forward cargo bay door

No

Minor Normals

HO

n/a

n/a

n/a

A

Limitations

APU operating limits;
Engine parameters, Gear extension speed, windshield wipers, single pack ops., crosswind, cargo (fire), cold soak (T/R’s). These are not all inclusive.

No

Yes Limits

n/a

ST, TCBI, SU, VT

n/a

n/a

B

This system differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ100/200/440 (CL-600-2B19)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 21 Air Conditioning

No recirculation feature

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Dedicated avionics bay cooling system with fan control

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 21 Air Conditioning

Cabin actual temperature indications only

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Dedicated cargo bay fan

No

Minor Msg.

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Architectural differences: two pneumatically controlled outflow/safety valves, overboard and inboard ground valves

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

CB panels 3 and 4 in Flight Deck;
30 KVA generator (load shedding for failed generator);
Generator switches (3) manually selected from Off to ON after engine start;
Two AC utility busses, load shed under certain conditions;
No ACPC installed, individual relays accomplish switching;
5 - 100A TRUs instead of 4 - 120A TRUs;
Bus Ties 1 and 2 are automatic. ESS Tie is manually selected. Switchlights on electrical power service panel;
Service bus powered from SERV TRU;
Two DC utility busses;
DC external power plug with External DC Switchlight on electrical panel;
ADG feeds directly to AC Essential Bus.
System affected during AC power transfer (loss of AC Bus 2).
Battery charger; battery location.

No

Minor Normals, Abnormal, Emergency

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 26 Fire Protection

Non-automated testing procedure.

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 26 Fire Protection

JETPIPE OVHT detection
Emergency Procedure (Recall)

No

Msg.

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 27 Flight Controls

Dedicated spoileron control surface and dedicated flight spoiler control surface

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Flutter dampers on elevators

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No rudder limiter

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No power up Bite test or SPLR/Stab in test advisory message

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No emergency flap switch

No

Yes Abnorm

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Flap lever has 5 positions

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Gravity refuel capability on center tank

No

Yes

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Shared APU and crossflow fuel pump

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Bulk fuel temperature sensor in left main tank

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

1B/2B pump is load shed when opposite GEN is not operating

No

Minor Abnorm

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

No hydraulic SOV switches

No

Minor Abnorm

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Cowl anti-icing valves pressure regulated with overpressure protection (anti-ice blow out plug on engines)

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for cowl anti-icing duct leak detection in pylon area

No

Minor

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Air data probes and sensor anti-icing not tested

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Wing anti-icing two operating temperature modes NORM and STBY are manually selectable

No

Minor Abnorm

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Amber arcs on the N2 gauges. Range from 0 -78%

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Wing anti-ice system test switch

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Architectural differences on synoptic page

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Cowl and wing anti-ice deactivated during thrust reverser deployment

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Nose doors are powered by hydraulics

No

Minor Normals

n/a

n/a

FTD 2-5

n/a

B

ATA 32 Landing Gear

Trailing link assemblies on main gear without shimmy dampers

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Main gear pin dust cover

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

FLT/NORM switch on forward external service panel

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

Anti-skid test switch.
Parking brake Off.

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

NWS deflection is +/- 70 degrees with tiller and rudder pedal movement will deflect NW +/- 5 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

No overhead panel dome lights

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Dual nose landing lights

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Four exterior lights per side for emergency exit lighting

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

emer LTS Off light on the emer LTS panel illuminates coincident with the emer LTS Off caution message

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

Mach transducer and selector valves in pitot static system

No

Minor Abnorm

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

Two separate standby instruments provide airspeed, altitude, attitude, slip/skid, and localizer/glideslope information

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 35 Oxygen

Overboard discharge indicator located on right side of fuselage

No

No

HO

n/a

n/a

n/a

A

ATA 36 Pneumatic

Thrust reversers are powered by 14th stage bleed air

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

10th and 14th stage bleed air systems controlled by manual manipulation of bleed air switches with APU interlock protection system

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 36 Pneumatic

10th stage manifold services: air conditioning, engine starting.

14th stage manifold services: anti-ice systems.

Single pack ops.

No

Yes Abnorm

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

Bleed air leak detection test conducted first flight of the day

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 49 APU

30KVA generator
APU intake door EICAS indications: CLSD, MID and OPEN
Shared APU and Crossflow fuel pump
Fuel supply, both wing tanks
AVAIL light = ready for pneumatic loading, APU GCU determines when electrical loading is available.
Fire horn; Start cycle.

No

Yes Normals Abnorm & Emerg

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

Hydro-mechanically and N1 speed governing

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 70 Powerplant

APR and ENG Speed control panel

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 70 Powerplant

Thrust lever retarder control system

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

Emergency stow PBAs for thrust reversers

No

Yes Normals Emergency

n/a

n/a

FTD 2-5

n/a

C

ATA 70 Powerplant

Pilot-managed start cycles for ATS and windmill starts

No

Yes Normals

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

FMS generated thrust limits for: manually set, no detents

Takeoff (TO)
Flex (FLX)
Climb (CLB)
Go Around (GA)
Max Continuous Thrust (MCT)
Cruise (CRZ)

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 70 Powerplant

No high power schedule PBA

No

Yes

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

Oil level test panel

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

This maneuver differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ100/200/440 (CL-600-2B19)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

AFCS

FD target pitch attitude on takeoff is 15 degrees up and GA or SE takeoff is 10 degrees up

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Takeoff

Rotation rate is 3 degrees per second towards target FD

No

No

HO

n/a

n/a

n/a

A

Takeoff

Throttles manually placed in thrust caret, set by FMS

No

No

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

B

Takeoff

No Flap 1 position:
No requirement to monitor Vt -15 airspeed for flap retraction from flap 8 to flap 1

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

B

Approach

Approach Attitude Comparison

CRJ700
Normal
Flapless (Slats 25)
Slatless (Flaps 45)
Single Engine

 

CRJ200
Single Engine
N/A
Normal
Flapless

Yes

No

n/a

VT

n/a

n/a

B

Landing

Minimal flare required

Yes

No

n/a

VT

n/a

n/a

B

From CRJ100, CRJ200, CRJ440 To CRJ900

This design differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ900 (CL-600-2D24), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ900 (CL-600-2D24)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
118 ft, 11 in. (36.24 m)
Increase of 31 ft, 1 in. (9.47 m)

Wingspan:
81 ft, 7 in. (24.87m)
Increase of 12 ft, 1 in. (3.66 m)

Tailspan:
28 ft. (8.54 m)
Increase of 7 ft, 8 in. (2.23 m)

Height:
24 ft, 7 in. (7.49 m)
Increase of 3 ft, 11 in. (1.19 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
84,500 lb. (38,329 kg)
Increase of 31,500 lb. (14,288 kg)

Max Landing Weight:
75,100 lb. (34,065 kg)
Increase of 28,100 lb. (12,746 kg)

Fuel Capacity:
2902 U.S. gal. (10,977 L)
Increase of 751 gal. (2,835 L)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
13 ft, 6in. (4.0 m)
Increase of 3 ft, 2 in. (0.96 m)

Nose to Main Wheels:
48 ft, 4 in. (14.73 m)
Increase of 12 ft. (3.66 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-8C5
14,510 lb. of thrust, APR
Increase of 5,290 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Forward cargo bay

No

Yes Emerg.

HO

n/a

n/a

n/a

A

ATA 00 General

Increase of 40 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Addition of second Flight Attendant position

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

Revised architecture

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

Three panel slats on each wing

Minor

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 49 APU

Tailcone mounted

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Two additional forward cargo bay doors

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Four overwing emergency exits

No

No

HO

n/a

n/a

n/a

A

Limitations

APU operating limits;
Engine parameters;
Gear extension speed.
Taxi turning radius.
These are not all inclusive.

No

Yes Limits

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Limitations

MMO above FL340 is 0.84M
Decrease of 0.01 m

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ900 (CL-600-2D24), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ900 (CL-600-2D24)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 21 Air Conditioning

Recirculated air distribution system with fan control switch

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

No dedicated fan for avionics bay cooling

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

No dedicated standby fan for EFIS cooling. Backup cooling is via ECS airflow.

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Selected and actual temp displayed on ECS synoptic page

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Revised architecture. No dedicated cargo bay fan

No

No

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Revised architecture. One electrically operated outflow valve, two safety valves, one ground valve

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

CB panels 3 and 4 removed;
40 kVA generator (no load shedding for failed generator);
Generator switches (3) always left in auto;
AC Utility buses removed;
ACPC controls switching automatically;
4 - 120A TRUs instead of 5 - 100A TRUs;
Bus Ties are automatic (controlled by DCPC). Switchlights removed on electrical power panel;
Service bus powered from DC bus 2;
One DC utility bus;
DC external power plug and DC External switchlight removed;
New ADG bus installed.
AC Electric synoptic changes
ADC (no lamp test)
Battery chargers and battery location

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 26 Fire Protection

Simplified testing procedure. Automatic Bite and MDC interface

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 26 Fire Protection

No jetpipe overheat detection

No

No

HO

n/a

n/a

n/a

A

ATA 26 Fire Protection

Fire suppression for forward cargo area. Common Halon system used to supply both compartments. Three cargo smoke detectors.

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No dedicated spoileron control surface. Multifunction spoilers act as flight spoiler or spoileron or ground lift dump.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

No flutter dampers on elevators

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Rudder limiter incorporated, function of speed and flap position controlled by SSCU

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

The power up Bite test starts only when all three hydraulic systems are fully powered. A SPLR/Stab in test advisory message is posted on EICAS during this test - All flight control systems are inoperative during the test

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

For redundancy, emergency slat/flap switch added to drive slats to 20 degrees and flaps to 20 degrees with a slat/flap selector failure

No

Yes Abnorm

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 27 Flight Controls

Slat/Flap lever has 6 positions

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

No gravity refuel capability on centre tank

No

Yes

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Dedicated cross-flow pump

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Bulk fuel temperature sensor in right main tank

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Fuel synoptic changes

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

1B/2B pump is not load shed when respective engine GEN is not operating

No

Minor Abnorm

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

Thrust reverser are powered by hydraulics

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

Hydraulic SOV switches added to isolate EDP during low pressure condition without shutting down the engine

No

Minor Normals Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

No cowl anti-ice blow out plug on engines

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for cowl anti-icing duct leak detection in pylon area

No

Minor New msg.

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Simplified cowl and wing anti-ice synoptic page

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Air data probes and sensor anti-icing tested before flight with ICE DET switchlight

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for wing OVHT protection. No STBY mode for wing anti-ice required.

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Windshield wiper has intermittent position.

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Variable white arcs on the N2 gauges. Range of arc varies with engine bleed condition.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Wing anti-ice system tested continuously. No test switch (automatic function)

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Nose doors are mechanical

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Cantilever assemblies on main gear with shimmy dampers

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No main gear dust pin covers

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No FLT/NORM switch installed on forward external service panel

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No anti-skid test switch. Revised anti-skid test procedure.

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

NWS deflection is +/- 80 degrees with tiller and rudder pedal movement will deflect NW +/- 8 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Increased tire speed limit

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Overhead panel dome lights installed

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Single nose landing light

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Three exterior lights per side for emergency exit lighting

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

No emer LTS Off light on panel. emer LTS Off caution message only

No

Minor Normals Abnormal

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

No mach transducer or selector valves in Pitot Static system

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

One electronic integrated standby instrument provides airspeed, altitude, attitude, slip/skid, and localizer/glideslope information

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 35 Oxygen

Overboard discharge indicator located on left side of fuselage

No

No

HO

n/a

n/a

n/a

A

ATA 36 Pneumatic

New flight deck bleed air panel. Engine bleed air taken from 6th or 10th stage to supply common manifold.

Bleed air selection is automatic when in auto mode. Provisions for manual switching.

No

Yes Normals/ Abnorm

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

Power On automatic bleed air leak detection test

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 49 APU

40 kVA generator
No APU Intake Door 'MID' EICAS indication
Dedicated APU fuel pump
APU Fuel supply, left collector tank
AVAIL light = ready for electrical loading, ECU determines when pneumatic loading is available. No fire horn. Start cycle.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 52 Doors

Four over wing emergency exits
Minor changes to Doors synoptic page and EICAS messages

No

Minor Messages

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

FADEC controlled

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, FTD 2-5

n/a

B

ATA 70 Powerplant

N1 and N2 sync control panel

No

Minor Normals Abnormal

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

FADEC controlled start cycle for ATS and windmill starts

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, FTD 2-5

n/a

B

ATA 70 Powerplant

Thrust reversers hydraulically actuated. No thrust lever retarder control system

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

No emergency stow PBAs

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

High power schedule PBA

No

Yes

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

FADEC generated thrust limits for: (automatic with thrust levers in respective detent)

Takeoff (TO)
Flex (FLX)
Climb (CLB)
Go Around (GA)
Max Continuous Thrust (MCT)
Cruise (CRZ) – manually set in the cruise range

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

Engine oil test panel removed. Engine oil level quantities provided on menu page

No

Minor Normals

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ900 (CL-600-2D24), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ900 (CL-600-2D24)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

AFCS

Initial take off pitch target is optimized to takeoff V speeds entered

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Taxi

Turning radius increased

No

No

HO

n/a

n/a

n/a

A

Takeoff

Rotation rate is 3-5 degrees per second towards target FD

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

Takeoff

Throttles placed in "TOGA" detent and thrust is set into N1 caret by FADEC

Throttles placed in "CLB" detent and thrust is set into N1 caret by FADEC

No

No

n/a

n/a

CSS, PTT, FTD 2-5

n/a

B

Takeoff

Flap retraction:

Flaps 8 takeoff - Flaps retracted to '1' from '8' at V2 + 12 and to '0' from '1' at VT -15 kts.

Flaps 20 takeoff - Flaps retracted to '8' from '20' at V2 + 12 and to '1' from '8' at V2 + 20 and then to '0' from '1' at VT -15.

No

Yes Normals

n/a

n/a

CSS, PTT, FTD 2-5

n/a

C*Note: C* in the “CHK LVL” column of a Differences Table requires use of training devices specified in “TRAINING LEVEL” C column of the respective Differences Table. End note

Approach

Approach Attitude Comparison

CRJ200
Single Engine
N/A
Normal
Flapless

 

CRJ900
Normal
Flapless (Slats 20)
Slatless (Flaps 45)
Single Engine

Yes

No

n/a

VT

n/a

n/a

B

Landing

More pronounced flare

Yes

No

n/a

VT

n/a

n/a

B

From CRJ900 To CRJ100, CRJ200, CRJ440

This design differences table, from the CRJ900 (CL-600-2D24) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: crj100/200/440 (CL-600-2B19

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
87 ft, 10 in. (26.77 m)
Decrease of 31 ft, 1 in. (9.47 m)

Wingspan:
69 ft, 6 in. (21.21 m)
Decrease of 12 ft, 1 in. (3.66 m)

Tailspan:
20 ft, 4 in (6.20 m)
Decrease of 7 ft, 8 in. (2.23 m)

Height:
20 ft, 8 in. (6.30 m)
Decrease of 3 ft, 11 in. (1.19 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
53,000 lb. (24,041 kg)
Decrease of 31,500 lb. (14,288 kg)

Max Landing Weight:
47,000 lb. (21,319 kg)
Decrease of 28,100 lb. (12,746 kg)

Fuel Capacity:
2151 U.S. gal. (8,142 L)
Decrease of 751 gal. (2,835L)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
10 ft, 4 in. (3.15 m)
Decrease of 3ft, 2 in. (0.96 m)

Nose to Main Wheels:
36 ft, 4 in. (11.07 m)
Decrease of 12 ft. (3.66 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-3B1
9,220 lb. of thrust, APR
Difference of 5,290 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

No forward cargo bay

No

Minor

HO

n/a

n/a

n/a

A

ATA 00 General

Decrease of 40 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

One Flight Attendant position

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

Architectural differences

No

Minor (Ext. DC)

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

No slats on wings

Minor

Yes Normals

HO

n/a

n/a

n/a

A

ATA 49 APU

Located in aft equipment bay
Intake/exhaust/Hazard Areas

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

No forward cargo bay door

No

No

HO

n/a

n/a

n/a

A

ATA 52 Doors

2 fewer over wing emergency exits

No

No

HO

n/a

n/a

n/a

A

Limitations

APU operating limits;
Engine parameters, Gear extension speed, windshield wipers, single pack ops., crosswind, cargo (fire), cold soak (T/R’s).
These are not all inclusive

No

Yes Limits

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Limitations

MMO above FL340 is 0.85M
Increase of 0.01 M

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ900 (CL-600-2D24) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ100/200/440 (CL-600-2B19)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 21 Air Conditioning

No recirculation feature

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Dedicated avionics bay cooling system with fan control

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 21 Air Conditioning

Cabin actual temperature indications only

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Dedicated cargo bay fan

No

Minor Msg.

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Architectural differences: two pneumatically controlled outflow/safety valves, overboard and inboard ground valves

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

CB panels 3 and 4 in flight deck;
30 kVA generator (load shedding for failed generator);
Generator switches (3) manually selected from Off to ON after engine start;
Two AC utility busses, loadshed under certain conditions;
No ACPC installed, individual relays accomplish switching;
5 - 100A TRUs instead of 4 - 120 A TRUs;
Bus Ties 1 and 2 are automatic. ESS Tie is manually selected. Switchlights on electrical power service panel;
Service bus powered from SERV TRU;
Two DC utility busses;
DC external power plug with external DC Switchlight on electrical panel;
ADG feeds directly to AC essential bus.
System affected during AC power transfer (loss of AC Bus 2).
Battery and battery charger location.

No

Minor Normals, Abnormal, Emergency

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 26 Fire Protection

Non-automated testing procedure.

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 26 Fire Protection

JETPIPE OVHT detection
Emergency Procedure (Recall)

No

Msg.

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 27 Flight Controls

Dedicated spoileron control surface and dedicated flight spoiler control surface

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Flutter dampers on elevators

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No rudder limiter

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No power up Bite test or SPLR/Stab in test advisory message

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No emergency flap switch

No

Yes Abnormal

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Flap lever has 5 positions

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Fuel synoptic changes

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Gravity refuel capability on center tank

No

Yes

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Shared APU and crossflow fuel pump

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Bulk fuel temperature sensor in left main tank

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

1B/2B pump is load shed when opposite GEN is not operating

No

Minor Abnormal

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

No hydraulic SOV switches

No

Minor Abnormal

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Cowl anti-icing valves pressure regulated with overpressure protection (Anti-ice blow out plug on engines)

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for cowl anti-icing duct leak detection in pylon area

No

Minor

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Air data probes and sensor anti-icing not tested

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Wing anti-icing two operating temperature modes NORM and STBY are manually selectable

No

Minor Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Amber arcs on the N2 gauges. Range from 0 -78%

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Wing anti-ice system test switch

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Architectural differences on synoptic page

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Cowl and wing anti-ice deactivated during thrust reverser deployment

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Nose doors are powered by hydraulics

No

Minor Normals

n/a

n/a

FTD 2-5

n/a

B

ATA 32 Landing Gear

Trailing link assemblies on main gear without shimmy dampers

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Decreased tire speed limit

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Main gear pin dust cover

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

FLT/NORM switch on forward external service panel

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

Anti-skid test switch.
Parking brake Off.

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

NWS deflection is +/- 70 degrees with tiller and rudder pedal movement will deflect NW +/- 5 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

No overhead panel dome lights

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Dual nose landing lights

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Four exterior lights per side for emergency exit lighting

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

emer LTS Off light on the emer LTS panel illuminates coincident with the emer LTS Off caution message

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

Mach transducer and selector valves in pitot static system

No

Minor Abnormal

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

Two separate standby instruments provide airspeed, altitude, attitude, slip/skid, and localizer/glideslope information

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 35 Oxygen

Overboard discharge indicator located on right side of fuselage

No

No

HO

n/a

n/a

n/a

A

ATA 36 Pneumatic

Thrust reversers are powered by 14th stage bleed air

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

10th and 14th stage bleed air systems controlled by manual manipulation of bleed air switches with APU Interlock Protection System

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 36 Pneumatic

10th stage manifold services: air conditioning, engine starting.
14th stage manifold services: anti-ice systems.
Single pack ops.

No

Yes Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

Bleed air leak detection test conducted first flight of the day

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 49 APU

30 kVA generator
APU Intake Door EICAS Indications: CLSD, MID and OPEN
Shared APU and Crossflow fuel pump
Fuel supply, both wing tanks
AVAIL light = ready for pneumatic loading, APU GCU determines when electrical loading is available

No

Yes Normals Abnormal Emergency

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 52 Doors

Two over wing emergency exits
Minor changes to Doors synoptic page and EICAS messages

No

Minor Messages

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

Hydro-mechanically and N1 speed governing

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 70 Powerplant

APR and ENG Speed control panel

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 70 Powerplant

Thrust Lever retarder control system

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

Emergency stow PBAs for thrust reversers

No

Yes Normals Emergency

n/a

n/a

FTD 2-5

n/a

C

ATA 70 Powerplant

Pilot-managed start cycles for ATS and windmill starts

No

Yes Normals

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

FMS generated thrust limits for: manually set, no detents

Takeoff (TO)
Flex (FLX)
Climb (CLB)
Go Around (GA)
Max Continuous Thrust (MCT)
Cruise (CRZ)

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 70 Powerplant

No high power schedule PBA

No

Yes

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

Oil level test panel

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

This maneuver differences table, from the CRJ900 (CL-600-2D24) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ100/200/440 (CL-600-2B19)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

AFCS

FD target pitch attitude on takeoff is 15 degrees up and GA or SE takeoff is 10 degrees up

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Taxi

Turning radius decreased

No

No

HO

n/a

n/a

n/a

A

Takeoff

Rotation rate is 3 degrees per second towards target FD

No

No

HO

n/a

n/a

n/a

A

Takeoff

Throttles manually placed in thrust caret, set by FMS

No

No

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

B

Takeoff

No Flap 1 position:
No requirement to monitor Vt -15 airspeed for flap retraction from flap 8 to flap 1

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

B

Approach

Approach Attitude Comparison

CRJ900
Normal
Flapless (Slats 20)
Slatless (Flaps 45)
Single Engine

 

CRJ200
Single Engine
N/A
Normal
Flapless

Yes

No

n/a

VT

n/a

n/a

B

Landing

Minimal flare required

Yes

No

n/a

VT

n/a

n/a

B

From CRJ700, CRJ701, CRJ702 To CRJ900

This design differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ900 (CL-600-2D24), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ900 (CL-600-2D24)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
118 ft, 11 in. (36.24 m)
Increase of 12 ft, 3 in. (3.73 m)

Wingspan:
81 ft, 7 in. (24.87m)
Increase of 5 ft, 4 in. (1.62 m)

Tailspan:
28 ft. (8.54 m)
No Change

Height:
24 ft, 7 in. (7.49 m)
Decrease of 0 ft, 3 in. (0.08 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
84,500 lb. (38,329 kg)
Increase of 9,500 lb. (4,309 kg)

Max Landing Weight:
75,100 lb. (34,065 kg)
Increase of 8,100 lb. (3,674 kg)

Fuel Capacity:
2902 U.S. gal. (10,977 L)
No Change

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
13 ft, 6 in. (4.0 m)
No Change

Nose to Main Wheels:
48 ft, 4 in. (14.73 m)
Increase of 7 ft, 6 in. (2.29 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-8C5
14,255 lb. of thrust, APR
Increase of 720 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Increase of 20 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 52 Doors

Two forward cargo bay door (2 total)

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Four over wing emergency exits
Minor EICAS changes

No

No

HO

n/a

n/a

n/a

A

Limitations

Engine parameters;
Flap 20 VFE
Tire speed
Ground turning radius
These are not all inclusive.

No

Yes Limits

HO

n/a

n/a

n/a

A

Limitations

MMO above FL340 is 0.84M
Decrease of 0.01 m

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ900 (CL-600-2D24), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ900 (CL-600-2D24)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 27 Flight Controls

Slat/flap relationship:
When flap lever is selected to 20 degrees, slats are at 20 degrees and flaps are at 20 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Emergency Flap when selected, slats move to 20 degrees and flaps are at 20 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Increase in tire speed

No

No

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ900 (CL-600-2D24), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ900 (CL-600-2D24)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Taxi

Increase in taxi turning radius

No

No

HO

n/a

n/a

n/a

A

Landing

More pronounced flare

No

No

HO

n/a

n/a

n/a

A

From CRJ900 To CRJ700, CRJ701, CRJ702

This design differences table, from the CRJ900 (CL-600-2D24) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
106 ft, 8 in. (32.51 m)
Decrease of 12 ft, 3 in. (3.73 m)

Wingspan:
76 ft, 3 in. (23.25 m)
Decrease of 5 ft, 4in. (1.62 m)

Tailspan:
28 ft, 0 in. (8.54 m)
No Change

Height:
24 ft, 10 in. (7.57 m)
Increase of 0 ft, 3 in. (0.08 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
75,000 lb. (34,020 kg)
Decrease of 9,500 lb. (4,309 kg)

Max Landing Weight:
67,000 lb. (30,390 kg)
Decrease of 8,100 lb. (3,674kg)

Fuel Capacity:
2902 U.S. gal. (10,977 L)
No change

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
13 ft, 6 in. (4.0 m)
No Change

Nose to Main Wheels:
40 ft, 10 in. (12.44 m)
Decrease of 7 ft, 6 in. (2.29 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-8C1 or
GE CF34-8C5B1
13,790 lb. of thrust, APR
Decrease of 720 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Decrease of 20 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 52 Doors

One forward cargo bay door

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Two over wing emergency exits
Minor EICAS changes

No

No

HO

n/a

n/a

n/a

A

Limitations

Engine parameters;
Flap 20 VFE
Tire speed
Ground turning radius
These are not all inclusive.

No

Yes Limits

HO

n/a

n/a

n/a

A

Limitations

MMO is 0.85M above FL340
Increase of 0.01M

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ900 (CL-600-2D24) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 27 Flight Controls

Slat/flap relationship:
When flap lever is selected to 20 degrees, slats are at 25 degrees and flaps are at 20 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Emergency Flap when selected, slats move to 25 degrees and flaps are at 20 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Tire speed reduced

No

No

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ900 (CL-600-2D24) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Taxi

Decrease in taxi turning radius

No

No

HO

n/a

n/a

n/a

A

Landing

Less pronounced flare

No

No

HO

n/a

n/a

n/a

A

From CRJ100, CRJ200, CRJ440 To CRJ705

This design differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ705 (CL-600-2D15), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ705 (CL-600-2D15)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
118 ft, 11 in. (36.24 m)
Increase of 31 ft, 1 in. (9.47 m)

Wingspan:
81 ft, 7 in. (24.87 m)
Increase of 12 ft, 1 in. (3.66 m)

Tailspan:
28 ft (8.54 m)
Increase of 7 ft, 8 in. (2.23 m)

Height:
24 ft, 7 in. (7.49 m)
Increase of 3 ft, 11 in. (1.19 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
84,500 lb. (38,329 kg)
Increase of 31,500 lb. (14,288 kg)

Max Landing Weight:
75,100 lb. (34,065 kg)
Increase of 28,100 lb. (12,746 kg)

Fuel Capacity:
2902 U.S. gal. (10,977 L)
Increase of 751 gal. (2,835 L)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
13 ft, 6 in. (4.0 m)
Increase of 3 ft, 2 in. (0.96 m)

Nose to Main Wheels:
48 ft, 4 in. (14.73 m)
Increase of 12 ft. (3.66 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-8C5
14,510 lb. of thrust, APR
Increase of 5,290 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Forward cargo bay

No

Yes Emerg.

HO

n/a

n/a

n/a

A

ATA 00 General

Increase of 25 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Addition of second Flight Attendant position

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

Revised architecture

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

Three panel slats on each wing

Minor

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 49 APU

Tailcone mounted

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Two forward cargo bay doors

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Two additional overwing emergency exits

No

No

HO

n/a

n/a

n/a

A

Limitations

APU operating limits;
Engine parameters;
Gear extension speed;
Taxi turning radius;
These are not all inclusive

No

Yes Limits

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Limitations

MMO above FL340 is 0.84M
Decrease of 0.01 m

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ705 (CL-600-2D15), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ705 (CL-600-2D15)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 21 Air Conditioning

Recirculated air distribution system with fan control switch

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

No dedicated fan for avionics bay cooling

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

No dedicated standby fan for EFIS cooling. Backup cooling is via ECS airflow.

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Selected and actual temp displayed on ECS synoptic page

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Revised architecture. No dedicated cargo bay fan

No

No

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Revised architecture. One electrically operated outflow valve, two safety valves, one ground valve

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

CB panels 3 and 4 removed;
40 kVA generator (no load shedding for failed generator);
Generator switches (3) always left in auto;
AC Utility buses removed;
ACPC controls switching automatically;
4 - 120A TRUs instead of 5 - 100A TRUs;
Bus Ties are automatic (controlled by DCPC). Switchlights removed on electrical power panel;
Service bus powered from DC bus 2;
One DC utility bus;
DC external power plug and DC external switchlight removed;
New ADG bus installed;
AC Electric synoptic changes;
ADC (no lamp test);
Battery chargers, battery location.

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 26 Fire Protection

Simplified testing procedure. Automatic Bite and MDC interface

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 26 Fire Protection

No jetpipe overheat detection

No

No

HO

n/a

n/a

n/a

A

ATA 26 Fire Protection

Fire suppression for forward cargo area. Common Halon system used to supply both compartments. Three cargo smoke detectors.

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No dedicated spoileron control surface. Multifunction spoilers act as flight spoiler or spoileron or ground lift dump.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

No flutter dampers on elevators

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Rudder limiter incorporated, function of speed and flap position controlled by SSCU

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

Power up Bite test starts only when all three hydraulic systems are fully powered. A SPLR/Stab in test advisory message is posted on EICAS during this test - All flt control systems are inoperative during the test

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

For redundancy, emergency slat/flap switch added to drive slats to 20 degrees and flaps to 20 degrees with a slat/flap selector failure

No

Yes Abnorm

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 27 Flight Controls

Slat/flap lever has 6 positions

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

No gravity refuel capability on center tank

No

Yes

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Dedicated cross-flow pump

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Bulk fuel temperature sensor in right main tank

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Fuel synoptic changes

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

1B/2B pump is not load shed when respective engine GEN is not operating

No

Minor Abnorm

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

Thrust reversers are powered by hydraulics

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

Hydraulic SOV switches added to isolate EDP during low pressure condition without shutting down the engine

No

Minor Normals Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

No cowl anti-ice blowout plug on engines

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for cowl anti-icing duct leak detection in pylon area

No

Minor New msg.

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Simplified cowl and wing anti-ice synoptic page

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Air data probes and sensor anti-icing tested before flight with ICE DET switchlight

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for wing OVHT protection. No STBY mode for wing anti-ice required.

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Windshield wiper has intermittent position.

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Variable white arcs on the N2 gauges. Range of arc varies with engine bleed condition.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Wing anti-ice system tested continuously. No test switch (automatic function)

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Nose doors are mechanical

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Cantilever assemblies on main gear with shimmy dampers

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No main gear dust pin covers

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No FLT/NORM switch installed on forward external service panel

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

No anti-skid test switch. Revised anti-skid test procedure.

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

NWS deflection is +/- 80 degrees with tiller and rudder pedal movement will deflect NW +/- 8 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Increased tire speed limit

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Overhead panel dome lights installed

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Single nose landing light

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Three exterior lights per side for emergency exit lighting

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

No emer LTS Off light on panel. emer LTS Off caution message only

No

Minor Normals Abnormal

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

No mach transducer or selector valves in pitot static system

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

One electronic integrated standby indicator provides airspeed, altitude, attitude, slip/skid, and localizer/glideslope information

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 35 Oxygen

Overboard discharge indicator located on left side of fuselage

No

No

HO

n/a

n/a

n/a

A

ATA 36 Pneumatic

New flight deck bleed air panel. Engine bleed air taken from either 6th or 10th stage to supply common manifold.

Bleed air selection is automatic when in auto mode. Provisions for manual switching.

No

Yes Normals/ Abnorm

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

Power On automatic bleed air leak detection test

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 49 APU

40 kVA generator;
No APU intake door 'MID' EICAS indication;
Dedicated APU fuel pump;
APU Fuel supply, left collector tank;
AVAIL light = ready for electrical loading, ECU determines when pneumatic loading is available;
No fire horn;
Start cycle.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 52 Doors

Four overwing emergency exits.
Minor changes to doors synoptic page and EICAS messages

No

Minor Messages

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

FADEC controlled

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, FTD 2-5

n/a

B

ATA 70 Powerplant

N1 and N2 sync control panel

No

Minor Normals Abnormal

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

FADEC controlled start cycle for ATS and windmill starts

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, FTD 2-5

n/a

B

ATA 70 Powerplant

Thrust reversers hydraulically-actuated. No thrust lever retarder control system

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

No emergency stow PBAs

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

High power schedule PBA

No

Yes

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

FADEC generated thrust limits for: (automatic with thrust levers in respective detent)

Takeoff (TO)
Flex (FLX)
Climb (CLB)
Go Around (GA)
Max Continuous Thrust (MCT)
Cruise (CRZ) – manually set in the cruise range

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

Engine oil test panel removed. Engine oil level quantities provided on menu page

No

Minor Normals

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ705 (CL-600-2D15), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ705 (CL-600-2D15)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

AFCS

Initial takeoff pitch target is optimized to takeoff V speeds entered

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Taxi

Turning radius increased

No

No

HO

n/a

n/a

n/a

A

Takeoff

Rotation rate is 3-5 degrees per second towards target FD

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

Takeoff

Throttles placed in "TOGA" detent and thrust is set into N1 caret by FADEC.

Throttles placed in "CLB" detent and thrust is set into N1 caret by FADEC.

No

No

n/a

n/a

CSS, PTT, FTD 2-5

n/a

B

Takeoff

Flap retraction:

Flaps 8 takeoff - Flaps retracted to '1' from '8' at V2 + 12 and to '0' from '1' at VT -15 kts.

Flaps 20 takeoff - Flaps retracted to '8' from '20' at V2 + 12 and to '1' from '8' at V2 + 20 and then to '0' from '1' at VT -15 kts.

No

Yes Normals

n/a

n/a

CSS, PTT, FTD 2-5

n/a

C*Note: C* in the “CHK LVL” column of a Differences Table requires use of training devices specified in “TRAINING LEVEL” C column of the respective Differences Table. End note

Approach

Approach Attitude Comparison

CRJ200
Single Engine
N/A
Normal
Flapless

 

CRJ705
Normal
Flapless (Slats 20)
Slatless (Flaps 45)
Single Engine

Yes

No

n/a

VT

n/a

n/a

B

Landing

More pronounced flare

Yes

No

n/a

VT

n/a

n/a

B

From CRJ705 To CRJ100, CRJ200, CRJ440

This design differences table, from the CRJ705 (CL-600-2D15) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ100/200/440 (CL-600-2B19)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
87 ft, 10 in. (26.77 m)
Decrease of 31 ft, 1 in. (9.47 m)

Wingspan:
69 ft, 6 in. (21.21 m)
Decrease of 12 ft, 1 in. (3.66 m)

Tailspan:
20 ft, 4 in (6.20 m)
Decrease of 7 ft, 8 in. (2.23 m)

Height:
20 ft, 8 in. (6.30 m)
Decrease of 3 ft, 11 in. (1.19 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
53,000 lb. (24,041 kg)
Decrease of 31,500 lb. (14,288 kg)

Max Landing Weight:
47,000 lb. (21,319 kg)
Decrease of 28,100 lb. (12,746 kg)

Fuel Capacity:
2151 U.S. gal. (8,142 L)
Decrease of 751 gal. (2,835L)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
10 ft, 4 in. (3.15 m)
Decrease of 3 ft, 2 in, (0.96 m)

Nose to Main Wheels:
36 ft, 4 in. (11.07 m)
Decrease of 12 ft. (3.66 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-3B1
9,220 lb. of thrust, APR
Decrease of 5,290 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

No forward cargo bay

No

Minor

HO

n/a

n/a

n/a

A

ATA 00 General

Decrease of 25 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

One Flight Attendant position

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

Architectural differences

No

Minor (Ext. DC)

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 27 Flight Controls

No slats on wings

Minor

Yes Normals

HO

n/a

n/a

n/a

A

ATA 49 APU

Located in aft equipment bay
Intake/exhaust/hazard areas

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Two overwing emergency exits

No

No

HO

n/a

n/a

n/a

A

Limitations

APU operating limits;
Engine parameters; Gear extension speed; Windshield wipers; Single pack ops.; Crosswind; Cargo (fire); Cold soak (T/R’s);
These are not all inclusive

No

Yes Limits

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Limitations

MMO above FL340 is 0.85M
Increase of 0.01 m

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ705 (CL-600-2D15) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ100/200/440 (CL-600-2B19)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 21 Air Conditioning

No recirculation feature

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Dedicated avionics bay cooling system with fan control

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 21 Air Conditioning

Cabin actual temperature indications only

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Dedicated cargo bay fan

No

Minor Msg.

HO

n/a

n/a

n/a

A

ATA 21 Air Conditioning

Architectural differences: two pneumatically controlled outflow/safety valves overboard and inboard ground valves

No

No

HO

n/a

n/a

n/a

A

ATA 24 Electrical Power

CB panels 3 and 4 on flight deck;
30 kVA generator (load shedding for failed generator);
Generator switches (3) manually selected from Off to ON after engine start;
Two AC Utility busses, loadshed under certain conditions;
No ACPC installed, individual relays accomplish switching;
5 - 100A TRUs instead of 4 - 120A TRUs;
Bus Ties 1 and 2 are automatic. ESS Tie is manually selected. Switchlights on electrical power service panel;
Service bus powered from SERV TRU;
Two DC utility busses;
DC external power plug with external DC switchlight on electrical panel;
ADG feeds directly to AC essential bus;
System affected during AC power transfer (loss of AC Bus 2).
Battery chargers, Battery location.

No

Minor Normals, Abnormal, Emergency

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 26 Fire Protection

Non-automated testing procedure.

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 26 Fire Protection

JETPIPE OVHT detection
Emergency Procedure (Recall)

No

Msg.

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 27 Flight Controls

Dedicated spoileron control surface and dedicated flight spoiler control surface

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Flutter dampers on elevators

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No rudder limiter

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No power up Bite test or SPLR/Stab in test advisory message

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

No emergency flap switch

No

Yes Abnorm

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

Flap lever has 5 positions

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Gravity refuel capability on center tank

No

Yes

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Shared APU and crossflow fuel pump

No

No

HO

n/a

n/a

n/a

A

ATA 28 Fuel System

Bulk fuel temperature sensor in left main tank

No

No

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

1B/2B pump is load shed when respective GEN is not operating

No

Minor Abnormal

HO

n/a

n/a

n/a

A

ATA 29 Hydraulics

No hydraulic SOV switches

No

Minor Abnormal

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Cowl anti-icing valves pressure regulated with overpressure protection (Anti-ice blowout plug on engines)

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Revised architecture for cowl anti-icing duct leak detection in pylon area

No

Minor

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Air data probes and sensor anti-icing not tested

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Wing anti-icing two operating temperature modes NORM and STBY are manually selectable

No

Minor Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Amber arcs on the N2 gauges. Range from 0 -78%

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Wing anti-ice system test switch

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 30 Ice and Rain Protection

Architectural differences on synoptic page

No

No

HO

n/a

n/a

n/a

A

ATA 30 Ice and Rain Protection

Cowl and wing anti-ice deactivated during thrust reverser deployment

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Nose doors are powered by hydraulics

No

Minor Normals

n/a

n/a

FTD 2-5

n/a

B

ATA 32 Landing Gear

Trailing link assemblies on main gear without shimmy dampers

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Decreased tire speed limit

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Main gear pin dust cover

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

FLT/NORM switch on forward external service panel

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

Anti-skid test switch
Parking brake Off.

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 32 Landing Gear

NWS deflection is +/- 70 degrees with tiller and rudder pedal movement will deflect NW +/- 5 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

No overhead panel dome lights

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Dual nose landing lights

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

Four exterior lights per side for emergency exit lighting

No

No

HO

n/a

n/a

n/a

A

ATA 33 Lights

emer LTS Off light on the emer LTS panel illuminates coincident with the emer LTS Off caution message

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

Mach transducer and selector valves in pitot static system

No

Minor Abnormal

HO

n/a

n/a

n/a

A

ATA 34 Navigation Equipment

Two separate standby instruments provide airspeed, altitude, attitude, slip/skid, and localizer/glideslope information

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 35 Oxygen

Overboard discharge indicator located on right side of fuselage

No

No

HO

n/a

n/a

n/a

A

ATA 36 Pneumatic

Thrust reversers are powered by 14th stage bleed air

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

10th and 14th stage bleed air systems controlled by manual manipulation of bleed air switches with APU interlock protection system

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 36 Pneumatic

10th stage manifold services: air conditioning, engine starting.

14th stage manifold services: anti-ice systems.

Single pack ops.

No

Yes Abnormal

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 36 Pneumatic

Bleed air leak detection test conducted first flight of the day

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 49 APU

30kVA generator;
APU Intake Door EICAS Indications: CLSD, MID and OPEN;
Shared APU and Crossflow fuel pump;
Fuel supply, both wing tanks;
AVAIL light = ready for pneumatic loading, APU GCU determines when electrical loading is available.
Fire horn; start cycle.

No

Yes Normals Abnormal Emergency

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 52 Doors

Two overwing emergency exits
Minor changes to doors synoptic page and EICAS messages

No

Minor Messages

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

Hydro-mechanical and N1 speed governing

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 70 Powerplant

APR and ENG Speed control panel

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

ATA 70 Powerplant

Thrust lever retarder control system

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

ATA 70 Powerplant

Emergency stow PBAs for Thrust Reversers

No

Yes Normals Emergency

n/a

n/a

FTD 2-5

n/a

C

ATA 70 Powerplant

Pilot-managed start cycles for ATS and windmill starts

No

Yes Normals

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

FMS generated thrust limits for: manually set, no detents

Takeoff (TO)
Flex (FLX)
Climb (CLB)
Go Around (GA)
Max Continuous Thrust (MCT)
Cruise (CRZ)

No

Minor Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

C

ATA 70 Powerplant

High power schedule PBA

No

Yes

HO

n/a

n/a

n/a

A

ATA 70 Powerplant

Oil level test panel

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

This maneuver differences table, from the CRJ705 (CL-600-2D15) to the CRJ100/200/440 (CL-600-2B19), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15) To related aircraft: CRJ100/200/440 (CL-600-2B19)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

AFCS

FD target pitch attitude on takeoff is 15 degrees up and GA or SE takeoff is 10 degrees up

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Taxi

Turning radius decreased

No

No

HO

n/a

n/a

n/a

A

Takeoff

Rotation rate is 3 degrees per second towards target FD

No

No

HO

n/a

n/a

n/a

A

Takeoff

Throttles manually placed in thrust caret, set by FMS

No

No

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

B

Takeoff

No Flap 1 position:
No requirement to monitor Vt -15 airspeed for flap retraction from flap 8 to flap 1

No

Yes Normals

n/a

n/a

ICBI, CSS, CPT, PTT, FTD 2-5

n/a

B

Approach

Approach Attitude Comparison

CRJ705
Normal
Flapless (Slats 20)
Slatless (Flaps 45)
Single Engine

 

CRJ200
Single Engine
N/A
Normal
Flapless

No

No

n/a

VT

n/a

n/a

B

Landing

Minimal flare required

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

From CRJ700, CRJ701, CRJ702 To CRJ705

This design differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ705 (CL-600-2D15), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ705 (CL-600-2D15)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
118 ft, 11 in. (36.24 m)
Increase of 12 ft, 3 in. (3.73 m)

Wingspan:
81 ft, 7 in. (24.87 m)
Increase of 5 ft, 4 in. (1.62 m)

Tailspan:
28 ft. (8.54 m)
No change

Height:
24 ft, 07 in. (7.49 m)
Decrease of 3 in. (0.08 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
84,500 lb. (38,329 kg)
Increase of 9,500 lb. (4,309 kg)

Max Landing Weight:
75,100 lb. (34,065 kg)
Increase of 8,100 lb. (3,674 kg)

Fuel Capacity:
2902 U.S. gal. (10,977 L)
No change

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
13 ft, 6 in. (4.0 m)
No change

Nose to Main Wheels:
48 ft, 4 in. (14.73 m)
Increase of 7 ft, 6 in. (2.29 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-8C5
14,510 lb. of thrust, APR
Increase of 720 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Increase of 5 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 52 Doors

Additional forward cargo bay doors (2 total)

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Two additional overwing emergency exits (4 total)
Minor EICAS changes

No

No

HO

n/a

n/a

n/a

A

Limitations

Engine parameters;
Flap 20 VFE;
Tire speed;
Ground turning radius;
These are not all inclusive

No

Yes
Limits

HO

n/a

n/a

n/a

A

Limitations

MMO above FL340 is 0.84 M
Decrease of 0.01 M

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ705 (CL-600-2D15), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ705 (CL-600-2D15)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Larger winglets

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

New slat/flap 20 relationship.
When flap 20 selected, slats are 20 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

When emergency slats/flaps switch selected, slats are driven to 20 degrees and flaps to 20 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Tire speed increased

No

No

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ705 (CL-600-2D15), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ705 (CL-600-2D15)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Taxi

Increased taxi turning radius

No

No

HO

n/a

n/a

n/a

A

Landing

More pronounced flare

No

No

HO

n/a

n/a

n/a

A

From CRJ705 To CRJ700, CRJ701, CRJ702

This design differences table, from the CRJ705 (CL-600-2D15) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Fuselage

Length:
106 ft, 8 in. (32.51 m)
Decrease of 12 ft, 3 in. (3.73 m)

Wingspan:
76 ft, 3 in. (23.24 m)
Decrease of 5 ft, 4 in. (1.62 m)

Tailspan:
28 ft, 0 in. (8.54 m)
No change

Height:
24 ft, 10 in. (7.57 m)
Increase of 3 in. (0.08 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Performance

Max T.O. Weight:
75,000 lb. (34,020 kg)
Decrease of 9,500 lb. (4,309 kg)

Max Landing Weight:
67,000 lb. (30,390 kg)
Decrease of 8,100 lb. (3,674 kg)

Fuel Capacity:
2902 U.S. gal. (10,977 L)
No change

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Wheel Base

Main Wheel Track:
13 ft, 2 in. (4.0 m)
No Change

Nose to Main Wheels:
40 ft, 10 in. (12.44 m)
Decrease of 7 ft, 6 in. (2.29 m)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Powerplant

GE CF34-8C1 or
GE CF34-8C5B1
13,790 lb. of thrust, APR
Decrease of 720 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Decrease of 5 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

ATA 52 Doors

One forward cargo bay door

No

Minor Normals

HO

n/a

n/a

n/a

A

ATA 52 Doors

Two fewer overwing emergency exits (2 total)
Minor EICAS changes

No

No

HO

n/a

n/a

n/a

A

Limitations

Engine parameters;
Flap 20 VFE;
Tire speed;
Ground turning radius;
These are not all inclusive

No

Yes Limits

HO

n/a

n/a

n/a

A

Limitations

MMO is 0.85M above FL340
Increase of 0.01M

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ705 (CL-600-2D15) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Smaller winglets

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

New slat/flap 20 relationship.
When flap 20 selected, slats are 25 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 27 Flight Controls

When emergency slats/flaps switch is selected, the slats are driven to 25 degrees and flaps to 20 degrees

No

No

HO

n/a

n/a

n/a

A

ATA 32 Landing Gear

Tire speed reduced

No

No

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ705 (CL-600-2D15) to the CRJ700/701/702 (CL-600-2C10), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ700/701/702 (CL-600-2C10)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Taxi

Decreased taxi turning radius

No

No

HO

n/a

n/a

n/a

A

Landing

Less pronounced flare

No

No

HO

n/a

n/a

n/a

A

From CRJ705 To CRJ900

This design differences table, from the CRJ705 (CL-600-2D15) to the CRJ900 (CL-600-2D24), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ900 (CL-600-2D24)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Increase of 15 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

From CRJ900 To CRJ705

This design differences table, from the CRJ900 (CL-600-2D24) to the CRJ705 (CL-600-2D15) lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ705 (CL-600-2D15)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

Decrease of 15 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

From CRJ700, CRJ701, CRJ702 To CRJ550

This design differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ550 (CL-600-2C11), lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ550 (CL-600-2C11)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

ATA 00 General

New aircraft Model CL-600-2C11 (CRJ550)

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Limitation to fifty (50) or fewer passenger seats.

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Maximum certified gross takeoff weight (GTOW) of 65,000 lb.

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Three class cabin.

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

New aircraft data plate identifying the aircraft Model (CL-600-2C11) and Series (CRJ550).

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

New MTOW placard on FS280 bulkhead at the entrance of the flight deck, to reflect 65,000 lb.

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

New airspeed limits placard inside flight deck, to reflect design maneuvering speed (VA) at 65,000 lb.

No

No

HO

n/a

n/a

n/a

A

ATA 00 General

Revision 27 (RS-347) to existing CL-600-2C10 AFM (CSP B-012) to introduce two new option codes:

  • Option code <1550> to introduce the new CL-600-2C11 aircraft Model and CRJ550 branding, and 50 passenger limitation.

  • Option code <1251> for Customer Option CR670-00-255 with new Maximum Ramp Weight (MRW)/MTOW/MLW/Maximum Zero Fuel Weight (MZFW) values and weight/center of gravity (CG) envelope, Supplement 1 noise data, and performance data.

No

No

HO

n/a

n/a

n/a

A

From CRJ100, CRJ200, CRJ440 To CRJ1000

This design differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ1000 (CL-600-2E25)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Aircraft General

Fuselage

Length:
128 ft, 4 in. (39.13 m)
Increase of 40 ft, 6 in. (12.36 m)

Wingspan:
85 ft, 10 in. (26.17 m)
Increase of 16 ft, 2 in. (4.95 m)

Tailspan:
28 ft. (8.54 m)
Increase of 7 ft, 8 in. (2.23 m)

Height:
24 ft, 5 in. (7.43 m)
Increase of 4 ft. (1.19 m)

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Performance

Max T.O. Weight:
91,800 lb. (41,640 kg)
Increase of 38,800 lb. (17,599 kg)

Max Landing Weight: 81,500 lb. (36,968 kg)
Increase of 34,500 lb. (15,649 kg)

Fuel Capacity:
2941 U.S. gal. (11,132 L)
Increase of 790 gal. (2,990 L)

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Powerplant

GE CF34-8C5
14,510 lb. of thrust, APR
Increase of 5,290 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Forward cargo bay

No

Yes Emerg

HO

n/a

n/a

n/a

A

Aircraft General

Increase of 46-54 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Addition of second or third Flight Attendant position

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Larger passenger cabin windows

No

No

HO

n/a

n/a

n/a

A

Limitations

APU operating limits;
Engine parameters;
Gear extension speed.
Taxi turning radius.
These are not all inclusive.

No

Yes Limits

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Limitations

MMO above FL340 is 0.84M
Decrease of 0.01 m

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ1000 (CL-600-2E25)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

21 ECS

Recirculated air distribution system with fan control switch

No

Minor Normals

HO

n/a

n/a

n/a

A

21 ECS

No dedicated fan for avionics bay cooling

No

Minor Normals

HO

n/a

n/a

n/a

A

21 ECS

No dedicated standby fan for EFIS cooling. Backup cooling is via ECS airflow.

No

Minor Normals

HO

n/a

n/a

n/a

A

21 ECS

Selected and actual temp displayed on ECS synoptic page

No

Minor Normals

HO

n/a

n/a

n/a

A

21 ECS

Revised architecture. No dedicated cargo bay fan

No

No

HO

n/a

n/a

n/a

A

21 ECS

Revised architecture. One electrically operated outflow valve, two safety valves, one ground valve

No

No

HO

n/a

n/a

n/a

A

21 ECS

Revised flight deck control panel

No

Yes Normals Abnormals

HO

n/a

n/a

n/a

A

21 ECS

Single pack operations
New limitations

No

Yes Abnormals

HO

n/a

n/a

n/a

A

23 COMM

Smaller LCD radio tuning units (RTU) will minor changes to functionality.

No

Minor Normals

HO

n/a

n/a

n/a

A

24 Electrics

Revised architecture

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

24 Electrics

CB panels 3 and 4 removed;
40 kVA generator (no load shedding for failed generator);
Generator switches (3) always left in auto;
AC Utility buses removed;
ACPC controls switching automatically;
4 - 120A TRUs instead of 5 - 100A TRUs;
Bus Ties are automatic (controlled by DCPC). Switchlights removed on electrical power panel;
Service bus powered from DC bus 2;
One DC utility bus;
DC external power plug and DC External switchlight removed;
New ADG bus installed;
AC Electric synoptic changes ADC (no lamp test);
Battery chargers and battery location

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

26 Fire/OVHT

Simplified testing procedure. Automatic Bite and MDC interface

No

Minor Normals

HO

n/a

n/a

n/a

A

26 Fire/OVHT

Redesigned flight deck panels

No

No

HO

n/a

n/a

n/a

A

26 Fire/OVHT

APU: new messages

No

No

HO

n/a

n/a

n/a

A

26 Fire/OVHT

No jetpipe overheat detection

No

No

HO

n/a

n/a

n/a

A

26 Fire/OVHT

Fire suppression for forward cargo area. Common Halon system used to supply both compartments. Three cargo smoke detectors.

No

Minor Normals

HO

n/a

n/a

n/a

A

27 Flight Controls

No flutter dampers on elevators

No

No

HO

n/a

n/a

n/a

A

27 Flight Controls

Three panel slats on each wing Changes on flt controls synoptic page

Minor

Yes Normals Abnormals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

27 Flight Controls

Architecture changes: SSCU, SFECU Changes in limitations

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

27 Flight Controls

No dedicated spoileron control surface. Multifunction spoilers act as flight spoiler or spoileron or ground lift dump.

No

Yes

n/a

ST, TCBI, SU, VT

n/a

n/a

A

27 Flight Controls

Command by wire (CBW) rudder system.

No

Yes Normals Abnormals Emerg

n/a

n/a

n/a

FFS
level
C/D

D

27 Flight Controls

The power up Bite test starts only when all three hydraulic systems are fully powered. A SPLR/Stab in test advisory message is posted on EICAS during this test - All flight control systems are inoperative during the test

No

Minor Normals

HO

n/a

n/a

n/a

A

27 Flight Controls

For redundancy, emergency slat/flap switch added to drive slats to 20 degrees and flaps to 20 degrees with a slat/flap selector failure

No

Yes Abnormals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

27 Flight Controls

Slat/Flap lever has 6 positions

No

Minor Normals

HO

n/a

n/a

n/a

A

28 Fuel

No gravity refuel capability on centre tank

No

Yes

HO

n/a

n/a

n/a

A

28 Fuel

Dedicated APU pump

No

Yes

HO

n/a

n/a

n/a

A

28 Fuel

Dedicated cross-flow pump

No

No

HO

n/a

n/a

n/a

A

28 Fuel

Bulk fuel temperature sensor in right main tank

No

No

HO

n/a

n/a

n/a

A

28 Fuel

Fuel synoptic changes

No

No

HO

n/a

n/a

n/a

A

28 Fuel

Minimum fuel quantity procedures

No

Yes Abnormals

HO

n/a

n/a

n/a

A

29 Hydraulics

1B/2B pump is not load shed when respective engine GEN is not operating

No

Minor Abnormals

HO

n/a

n/a

n/a

A

29 Hydraulics

Thrust reverser are powered by hydraulics

No

No

HO

n/a

n/a

n/a

A

29 Hydraulics

Hydraulic SOV switches added to isolate EDP during low pressure condition without shutting down the engine

No

Minor Normals Abnormals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

29 Hydraulics

Revised flight deck panel

No

Yes

HO

n/a

n/a

n/a

A

30 Ice and Rain

Wing A/I cross bleed valve, new architecture

No

Yes

HO

n/a

n/a

n/a

A

30 Ice and Rain

No cowl anti-ice blow out plug on engines

No

Minor Normals

HO

n/a

n/a

n/a

A

30 Ice and Rain

Revised architecture for cowl anti-icing duct leak detection in pylon area

No

Minor New msg.

HO

n/a

n/a

n/a

A

30 Ice and Rain

Simplified cowl and wing anti-ice synoptic page

No

No

HO

n/a

n/a

n/a

A

30 Ice and Rain

Air data probes and sensor anti-icing tested before flight with ICE DET switchlight

No

Minor Normals

HO

n/a

n/a

n/a

A

30 Ice and Rain

Revised architecture for wing OVHT protection. No STBY mode for wing anti-ice required.

No

No

HO

n/a

n/a

n/a

A

30 Ice and Rain

Windshield wiper has intermittent position.

No

No

HO

n/a

n/a

n/a

A

30 Ice and Rain

Windshield wipers, new speed limitations

No

Minor Normals

HO

n/a

n/a

n/a

A

30 Ice and Rain

Variable white arcs on the N2 gauges. Range of arc varies with engine bleed condition.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

30 Ice and Rain

Wing anti-ice system tested continuously. No test switch (automatic function)

No

Minor Normals

HO

n/a

n/a

n/a

A

32 Landing Gear

Nose doors are mechanical

No

No

HO

n/a

n/a

n/a

A

32 Landing Gear

Cantilever assemblies on main gear with shimmy dampers

No

Minor Normals

HO

n/a

n/a

n/a

A

32 Landing Gear

No main gear dust pin covers

No

No

HO

n/a

n/a

n/a

A

32 Landing Gear

No FLT/NORM switch installed on forward external service panel

No

Minor Normals

HO

n/a

n/a

n/a

A

32 Landing Gear

No anti-skid test switch. Revised anti-skid test procedure.

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

32 Landing Gear

NWS deflection is +/- 80 degrees with tiller and rudder pedal movement will deflect NW +/- 8 degrees

No

No

HO

n/a

n/a

n/a

A

32 Landing Gear

Increased tire speed limit

No

No

HO

n/a

n/a

n/a

A

32 Landing Gear

Landing Gear, Electric Alternate Extension System (EAES). Guarded switch versus handle.

No

Minor Normals Abnormals Emerg

HO

n/a

n/a

n/a

A

32 Landing Gear

Carbon Brakes versus steel brakes

No

Minor Normals

HO

n/a

n/a

n/a

A

33 Lighting

Overhead panel dome lights installed

No

No

HO

n/a

n/a

n/a

A

33 Lighting

Single nose landing light

No

No

HO

n/a

n/a

n/a

A

33 Lighting

Three exterior lights per side for emergency exit lighting

No

No

HO

n/a

n/a

n/a

A

33 Lighting

No emer LTS Off light on panel. emer LTS Off caution message only

No

Minor Normals Abnormals

HO

n/a

n/a

n/a

A

34 FLT INSTR.

No mach transducer or selector valves in Pitot Static system

No

Minor Normals

HO

n/a

n/a

n/a

A

34 FLT INSTR.

One electronic integrated standby instrument provides airspeed, altitude, attitude, slip/skid, and localizer/glideslope information

No

Minor Normals

HO

n/a

n/a

n/a

A

34 FLT INSTR.

Enhanced flight director with movable takeoff command bar indications

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

34 FLT INSTR.

Smaller FMS CDU (s) with more functionality:

  • SBAS

  • Frequencies

  • Selectable temperature compensated

No

Minor Normals

n/a

n/a

CSS, CPT, PTT, FTD I

n/a

B

34 FLT INSTR.

FMS Nav to Nav tuning

No

Minor Normals

n/a

n/a

FTD I

n/a

C

35 Oxygen

Overboard discharge indicator located on left side of fuselage

No

No

HO

n/a

n/a

n/a

A

36 Pneumatics

New flight deck bleed air panel. Engine bleed air taken from 6th or 10th stage to supply common manifold.

Bleed air selection is automatic when in auto mode. Provisions for manual switching.

No

Yes Normals Abnormals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

36 Pneumatics

Power On automatic bleed air leak detection test

No

Minor Normals

HO

n/a

n/a

n/a

A

36 Pneumatics

Anti-Ice Leak Detection Controller (AILC)

No

Yes Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

49 APU

Tailcone mounted

No

Minor Normals

HO

n/a

n/a

n/a

A

49 APU

40 kVA generator
No APU Intake Door 'MID' EICAS indication Dedicated APU fuel pump
APU Fuel supply, left collector tank
AVAIL light = ready for electrical loading, ECU determines when pneumatic loading is available. No fire horn. Start cycle.

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

A

52 Doors

Two additional forward cargo bay doors

No

Minor Normals

HO

n/a

n/a

n/a

A

52 Doors

Four over wing emergency exits
Minor changes to Doors synoptic page and EICAS messages

No

Minor Messages

HO

n/a

n/a

n/a

A

70 Powerplant

FADEC controlled:
Ignition, Flameout protection

No

Minor Normals Abnormals

n/a

n/a

ICBI, CSS, CPT, FTD I

n/a

B

70 Powerplant

N1 and N2 sync control panel

No

Minor Normals Abnormals

HO

n/a

n/a

n/a

A

70 Powerplant

FADEC controlled start cycle for ATS and windmill starts:
Start valve new messages

No

Minor Normals Abnormals

n/a

n/a

ICBI, CSS, CPT, FTD I

n/a

B

70 Powerplant

Thrust reversers hydraulically actuated. No thrust lever retarder control system

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

70 Powerplant

No emergency stow PBAs

No

Minor Normals Abnormals Emerg

n/a

ST, TCBI, SU, VT

n/a

n/a

B

70 Powerplant

High power schedule PBA

No

Yes

n/a

ST, TCBI, SU, VT

n/a

n/a

B

70 Powerplant

FADEC generated thrust limits for: (automatic with thrust levers in respective detent)

Takeoff (TO)
Flex (FLX)
Climb (CLB)
Go Around (GA)
Max Continuous Thrust (MCT)
Cruise (CRZ) – manually set in the cruise range

No

Yes Normals Abnormals

n/a

ST, TCBI, SU, VT

n/a

n/a

B

70 Powerplant

Engine oil test panel removed. Engine oil level quantities provided on menu page

No

Minor Normals

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ100/200/440 (CL-600-2B19) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ100/200/440 (CL-600-2B19)

To related aircraft: CRJ1000 (CL-600-2E25)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

AFCS

Initial take-off pitch target is optimized to takeoff V speeds entered

No

No

n/a

ST, TCBI, SU, VT

n/a

n/a

B

Taxi

Turning radius increased

No

No

n/a

n/a

n/a

FFS
level
C/D

D

Taxi

Carbon brakes, technique to reduce brake wear

No

No

HO

n/a

n/a

n/a

A

Takeoff

Rotation rate is 3-5 degrees per second towards target FD

No

No

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff/ Go-Around

Enhanced flight director with movable takeoff command bar indications

Yes

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff

Throttles placed in "TOGA" detent and thrust is set into N1 caret by FADEC

Throttles placed in "CLB" detent and thrust is set into N1 caret by FADEC

No

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff

Engine failure at V1

No

No

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff

Flap retraction:

Flaps 8 takeoff - Flaps retracted to '1' from '8' at V2 + 12 and to '0' from '1' at VT -15 kts.

Flaps 20 takeoff - Flaps retracted to '8' from '20' at V2 + 12 and to '1' from '8' at V2 + 20 and then to '0' from '1' at VT -15.

No

Yes Normals

n/a

n/a

CSS, PTT, FTD I

n/a

C*Note: C* in the “CHK LVL” column of a Differences Table requires use of training devices specified in “TRAINING LEVEL” C column of the respective Differences Table. End note

Approach

Approach Attitude Comparison

CRJ200
Single Engine
N/A
Normal
Flapless

 

CRJ1000
Normal
Flapless (Slats 20)
Slatless (Flaps 45)
Single Engine

Yes

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Landing

Different procedure, thrust reduction technique may differ

Yes

Yes

n/a

n/a

n/a

FFS
level
C/D

D

From CRJ700, CRJ701, CRJ702 To CRJ1000

This design differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ1000 (CL-600-2E25)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Aircraft General

Fuselage

Length:
128 ft, 4 in. (39.13 m)
Increase of 22 ft, 3 in. (6.80 m)

Wingspan:
85 ft, 10 in. (26.17 m)
Increase of 9 ft, 7 in. (2.92 m)

Tailspan:
28 ft. (8.54 m)
No Change

Height:
24 ft, 5 in. (7.43 m)
Decrease of 1 in. (0.03 m)

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Performance

Max T.O. Weight: 91,800 lb. (41,640 kg)
Increase of 16,800 lb. (7,620 kg)

Max Landing Weight: 81,500 lb. (36,968 kg)
Increase of 14,500 lb. (6,577 kg)

Fuel Capacity:
2941 U.S. gal. (11,132 L)
Increase of 39 gal. (148 L)

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Powerplant

GE CF34-8C5
14,510 lb. of thrust, APR
Increase of 720 lb. of thrust

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Increase of 18-26 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

FLT ATT

Third Flight Attendant position may be required for 104 passengers configuration

No

No

HO

n/a

n/a

n/a

A

Limitations

Single pack ops, Engine limits, Engine relight altitude, Flaps extend speeds, Tire limit speeds, MMO Speeds.
These are not all inclusive.

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ1000 (CL-600-2E25)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

23 COMM

Smaller LCD radio tuning units (RTU) with minor functionality changes

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

27 Flight Controls

Command by wire (CBW) rudder system.

No

Yes Normals Abnormals Emerg

n/a

n/a

n/a

FFS
level
C/D

D

27 Flight Controls

Slat/flap relationship:
When flap lever is selected to 20 degrees, slats are at 25 degrees and flaps are at 20 degrees

No

No

HO

n/a

n/a

n/a

A

27 Flight Controls

Emergency Flap when selected, slats move to 25 degrees and flaps are at 20 degrees

No

No

HO

n/a

n/a

n/a

A

32 Landing Gear

Tire speed increased

No

No

HO

n/a

n/a

n/a

A

32 Landing Gear

Landing Gear, Electric Alternate Extension System (EAES). Guarded switch versus handle.

No

Minor Normals Abnormals Emerg

HO

n/a

n/a

n/a

A

32 Landing Gear

Carbon MLG Brakes

No

Minor Normals

HO

n/a

n/a

n/a

A

34 FLT INST

Enhanced flight director with movable takeoff command bar indications

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

34 FLT INST

FMS Nav to Nav tuning for approach.
Optional equipment for 2C10, if installed this is not applicable.

No

Minor Normals

n/a

n/a

FTD

n/a

C

34 FLT INST

Smaller FMS CDU(s) with more functionality:

  • Selectable temperature compensated minimums

Optional equipment for 2C10, if installed this is not applicable

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

52 Doors

Two forward cargo bay door (2 total)

No

Minor Normals

HO

n/a

n/a

n/a

A

52 Doors

Four over-wing emergency exits Minor EICAS changes

No

No

HO

n/a

n/a

n/a

A

This maneuver differences table, from the CRJ700/701/702 (CL-600-2C10) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ700/701/702 (CL-600-2C10)

To related aircraft: CRJ1000 (CL-600-2E25)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Taxi

Increase in taxi turning radius

No

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff/ Go-Around

Enhanced flight director with movable takeoff command bar with indications

No

Minor Normals

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff

Engine failure at V1

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

Approach and Landing

Flapless (slats 20)

No

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Landing

Same procedure, thrust reduction technique may differ

No

No

n/a

n/a

n/a

FFS
level
C/D

D

Landing

More pronounced flare

No

Yes

n/a

n/a

n/a

FFS
level
C/D

D

From CRJ705 To CRJ1000

This design differences table, from the CRJ705 (CL-600-2D15) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ1000 (CL-600-2E25)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Aircraft General

Fuselage

Length:
128 ft, 4 in. (39.13m)
Increase of 9ft, 5 in. (2.90 m)

Wingspan:
85 ft, 10 in. (26.17m)
Increase of 4 ft, 3 in. (1.30 m)

Tailspan:
28 ft. (8.54 m)
No Change

Height:
24 ft, 5 in. (7.43 m)
Increase of 4 in. (0.08 m)

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Performance

Max T.O. Weight: 91,800 lb. (41,640 kg)
Increase of 7,300 lb. (3,311 kg)

Max Landing Weight: 81,500 lb. (36,968 kg)
Increase of 6,500 lb. (2,948 kg)

Fuel Capacity:
2,941 U.S. gal. (11,132 L)
Increase of 39 gal (148 L)

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Powerplant

GE CF34-8C5
14,510 lb. of thrust, APR
No change

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Increase of 21 - 29 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Third Flight Attendant position may be required

No

No

HO

n/a

n/a

n/a

A

Limitations

Single pack ops, Engine limits, Engine relight altitude, MMO Speeds.
These are not all inclusive.

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ705 (CL-600-2D15) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ1000 (CL-600-2E25)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

23 COMM

Smaller LCD radio tuning units (RTU)

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

27 Flight Controls

Command by wire (CBW) rudder system.

No

Yes Normals Abnormals Emerg

n/a

n/a

n/a

FFS
level
C/D

D

32 Landing Gear

Landing Gear, Electric Alternate Extension System (EAES). Guarded switch versus handle.

No

Minor Normals Abnormals Emerg

HO

n/a

n/a

n/a

A

32 Landing Gear

Carbon MLG Brakes

No

Minor Normals

HO

n/a

n/a

n/a

A

34 FLT INST

FMS Nav to Nav tuning for approach.
Optional equipment for 2D15, if installed, this finding is not applicable.

No

Minor Normals

n/a

n/a

FTD

n/a

C

34 FLT INST

Enhanced flight director with movable takeoff command bar indications

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

34 FLT INST

Smaller FMS CDU(s) with more functionality:

  • Selectable temperature compensated minimums

Optional equipment for 2D15, if installed, this finding is not applicable.

No

Minor Normals

n/a

n/a

CSS, CPT, PTT, FTD I

n/a

B

34 FLT INST

Coupled VNav
Optional equipment for 2D15. If installed this finding is not applicable.

No

Minor Normals

n/a

n/a

CSS, CPT, PTT, FTD I

n/a

B

This maneuver differences table, from the CRJ705 (CL-600-2D15) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ705 (CL-600-2D15)

To related aircraft: CRJ1000 (CL-600-2E25)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Taxi

Increase in taxi turning radius

No

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff/ Go-Around

Enhanced flight director with moveable takeoff command bar indications

No

Yes Normals

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff

Engine failure at V1

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

Approach and Landing

Flapless approach (slats 20)

No

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Landing

Same procedure, thrust reduction technique may differ

No

No

n/a

n/a

n/a

FFS
level
C/D

D

From CRJ900 To CRJ1000

This design differences table, from the CRJ900 (CL-600-2D24) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ1000 (CL-600-2E25)

Design

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Aircraft General

Fuselage

Length:
128 ft, 4 in. (39.13m)
Increase of 9ft, 5 in. (2.90 m)

Wingspan:
85 ft, 10 in. (26.17m)
Increase of 4 ft, 3 in. (1.30 m)

Tailspan:
28 ft. (8.54 m)
No Change

Height:
24 ft, 5 in. (7.43 m)
Increase of 4 in. (0.08 m)

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Performance

Max T.O. Weight: 91,800 lb. (41,640 kg)
Increase of 7,300 lb. (3,311 kg)

Max Landing Weight: 81,500 lb. (36,968 kg)
Increase of 6,500 lb. (2,948 kg)

Fuel Capacity:
2,941 U.S. gal. (11,132 L)
Increase of 39 US gal (148 L)

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Powerplant

GE CF34-8C5
14,510 lb. of thrust, APR
No change

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Increase of 6-14 passengers in payload capacity

No

No

HO

n/a

n/a

n/a

A

Aircraft General

Third Flight Attendant position may be required for 104 passengers configuration.

No

No

HO

n/a

n/a

n/a

A

Limitations

Fuel quantity, Single pack ops, Engine limits, Engine relight altitude, MMO Speeds.
These are not all inclusive.

No

Yes Limits

HO

n/a

n/a

n/a

A

This system differences table, from the CRJ900 (CL-600-2D24) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ1000 (CL-600-2E25)

System

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

23 COMM

Smaller LCD radio tuning units (RTU).
Later 2D25 aircraft may have the smaller RTUs. In this case there is no difference.

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

27 Flight Controls

Command by wire (CBW) rudder system.
Later 2D25 aircraft may have the CBW upgrade. In this case there is no difference.

No

Yes Normals Abnormals Emerg

n/a

n/a

n/a

FFS
level
C/D

D

32 Landing Gear

Landing Gear, Electric Alternate Extension System (EAES). Guarded switch versus handle.
Later 2D25 aircraft may have the EAES. In this case there is no difference.

No

Minor Normals Abnormals Emerg

HO

n/a

n/a

n/a

A

32 Landing Gear

Carbon MLG Brakes

No

Minor Normals

HO

n/a

n/a

n/a

A

34 FLT INST

Enhanced flight director with movable takeoff command bar indications

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

34 FLT INST

FMS Nav to Nav tuning for approach.
Optional equipment for 2D24, if installed, this finding is not applicable.

No

Minor Normals

n/a

n/a

FTD

n/a

C

34 FLT INST

Smaller FMS CDU (s) with more functionality

  • Selectable temperature compensated minimums

Optional equipment for 2D24, if installed, this finding is not applicable.

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

This maneuver differences table, from the CRJ900 (CL-600-2D24) to the CRJ1000 (CL-600-2E25), was proposed by MHI RJ Aviation ULC and validated by TCCA. It lists the minimum differences levels operators must use to conduct differences training and checking of flight crew members.

From base aircraft: CRJ900 (CL-600-2D24)

To related aircraft: CRJ1000 (CL-600-2E25)

Maneuver

Remarks

FLT CHAR

PROC CHNG

Training Level

CHK LVL

A B C D

Taxi

Increase in taxi turning radius

No

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff/ Go-Around

Enhanced flight director with moveable takeoff command bar indications

No

Minor Normals

n/a

n/a

n/a

FFS
level
C/D

D

Takeoff

Engine failure at V1

No

Minor Normals

n/a

ST, TCBI, SU, VT

n/a

n/a

A

Approach and Landing

Flapless approach (slats 20)

No

Yes

n/a

n/a

n/a

FFS
level
C/D

D

Landing

Same procedure, thrust reduction technique may differ

No

No

n/a

n/a

n/a

FFS
level
C/D

D

Appendix 4 - Transition line indoctrination (TLI)

Under an approved transition/MFF program(s), transition line indoctrination (TLI) must be accomplished in accordance with the table below and, where indicated by a C* or D* for flight crews flying the variants listed.

Table 1 MDR/TLI TABLE

To related aircraft

From base aircraft

CRJ100/200/440

CRJ700/701/702

CRJ550

CRJ705

CRJ900

CRJ1000

CRJ100/200/440

n/a

CFootnote */C

CFootnote */C

CFootnote */C

Not evaluated

CRJ700/701/702

CRJ550

CFootnote */C

A/A

A/A

A/A

Not evaluated

CRJ705

CFootnote */C

A/A

n/a

A/A

Not evaluated

CRJ900

CFootnote */C

A/A

A/A

n/a

Not evaluated

CRJ1000

DFootnote */D

DFootnote */D

DFootnote */D

DFootnote */D

n/a

Transition line indoctrination (TLI) may be required in certain circumstances and is authorized for crew members that have qualified and served in the same capacity on the same group of aeroplanes. TLI is a specific type of initial operating experience (IOE)/initial line indoctrination in which a pilot occupies a specific crew position (not in the observer seat) and performs particular assigned duties related to post qualification skill enhancement while under supervision. Supervision is by a pilot qualified to conduct the TLI and is typically a check pilot. TLI is not accomplished until after a crewmember has completed his training and, if applicable, checked (PPC) to perform duties for that particular crew position.

There are a variety of reasons why the OEB may specify TLI in conjunction with master difference requirements (MDR). One or more of the reasons described below may apply:

  • a) Introduction of new aircraft types or variants;

  • b) Introduction of new systems (e.g., flight management system (FMS), TCAS, Omega, INS);

  • c) Introduction of new operations (e.g., oceanic operations);

  • d) Experience for a particular crew position (e.g., PIC, second-in-command (SIC));

  • e) Post qualification skill refinement (e.g., refining alternate or multiple ways to use particular equipment to increase operating efficiency, operating flexibility, or convenience);

  • f) Special characteristics (e.g., unique airports, mountainous areas, unusual weather, special air traffic control procedures, non-standard runway surfaces, etc.).

In the case of pilots moving from the CRJ100/200/440 to the CRJ700/701/702, CRJ550, CRJ900 or CRJ705, operators should provide TLI in accordance with CARs requirements. Similarly, pilots moving from the CRJ700/701/702, CRJ550, CRJ900 or the CRJ705 to the CRJ100/200/440, operators should provide TLI in accordance with CARs requirements. In the case of pilots moving from the CRJ100/200/440, CRJ700/701/702, CRJ550, CRJ900 or CRJ705 to the CRJ1000, operators should provide TLI in accordance with CARs requirements. This requirement is intended to permit pilots to obtain additional operating experience in order to become fully cognizant of the differences in landing characteristics/techniques as a result of attitude differences related to fuselage length and landing weights and landing gear design differences between the base aircraft and the variant(s). Tables 2 and 3 below summarize the TLI requirements detailed in this paragraph and has detailed in Table 1 above.

Table 2 Example of an acceptable Initial flight training plan for MFF

Newly qualified on aircraft

IOE/Initial line indoctrination as per CARs

Differences training

TLI as per CARs

MFF

CRJ100/200/440

not applicable

CRJ700/701/702
CRJ550
CRJ705
CRJ900

not applicable

not applicable

CRJ700/701/702
CRJ550
CRJ705
CRJ900

not applicable

CRJ100/200/440

not applicable

not applicable

CRJ100/200/440
CRJ700/701/702
CRJ550
CRJ705
CRJ900

not applicable

CRJ1000

not applicable

not applicable

Table 3 Example of an acceptable flight training plan for MFF program

Qualified on aircraft

Differences training

TLI as per CARs

MFF

CRJ100/200/440

CRJ700/701/702
CRJ550
CRJ705
CRJ900

not applicable

not applicable

CRJ700/701/702
CRJ550
CRJ705
CRJ900

CRJ100/200/440

not applicable

not applicable

CRJ100/200/440
CRJ700/701/702
CRJ550
CRJ705
CRJ900

CRJ1000

not applicable

not applicable

Notes

  1. The CRJ700/701/702, CRJ550, CRJ900 and the CRJ705 are considered to be functionally equivalent and minimum differences training when transitioning between those four variants are required.

  2. In certain specific cases whereby the operator’s approved differences training program is immediately followed by level D FFS training and checking on the new variant, the requirement to conduct TLI may be waived.

  3. Pilots transitioning between any CRJ variants (e.g., CRJ100/200/440 to CRJ700/701/702 or CRJ550 or CRJ900 or CRJ705, CRJ100/200/440 or CRJ700/701/702 or CRJ550 or CRJ900 or CRJ705 to CRJ1000) or conducting MFF with different CRJ variants (e.g., CRJ100/200/440 and CRJ700/701/702, CRJ100/200/440 or CRJ700/701/702 and CRJ1000) require exemptions to specific provisions of CAR 705.106, CASS 725.106 and CAR 705.113. This appendix provides the transition credits between all CRJ aircraft series. Appendices 2 and 3 provide the training and checking credits between the CRJ aircraft series. TCCA Policy Letter AARX No. 173, Original issue, dated July 25, 2005 (RDIMS # 1040396) provide guidance on flight crew member qualification credits for transition programs and mixed fleet flying programs.

  4. Line checks conducted in one variant should satisfy the requirements for all CRJ variants. If the operator’s line operations (e.g., route structure, area of operation, ETOPS) of one variant is significantly different from another variant, then separate line checks should be conducted.