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 (CRJ100/200/440) |
CL65 |
A-276 |
CL-600-2C10 |
CRJ700 (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
- 2. Introduction
- 3. Highlights of change
- 4. General
- 5. Acronyms
- 6. Definitions
- 7. Pilot type rating
- 8. Related aircraft
- 9. Pilot training
- 10. Pilot checking
- 11. Pilot currency
- 12. Operational suitability
- 13. Miscellaneous
- 14. References
- Appendix 1 - Differences legend
- Appendix 2 - Master differences requirements (MDR) table
- Appendix 3 - Differences tables
- Appendix 4 - Transition line indoctrination (TLI)
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
- 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.
- 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
- 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.
- 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.
- 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.
- 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
- The corporate name «Bombardier» has been removed from the marketing names of the CRJ aircraft series and is reflected as follows:
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
- The CRJ100/200/440 is comprised of three separate aircraft variants: the CRJ100, CRJ200 and the CRJ440 respectively.
- 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
- The CRJ1000 was type certified in Canada dated November 01, 2010, and is therefore included on the TCCA TCDS A-276; and
- 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
- 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.
- The following training provider was contracted during OEs:
- 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
- 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;
- 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
- References to “pilots” in this section include both pilots in command (PIC) and second in command (SIC) unless otherwise specified.
- 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
- 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.
- 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
- 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.
- 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.
- The currency requirements detailed at sections 11 of this report shall be maintained.
- 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
- 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.
- 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
- 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.
- 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.
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.
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
-
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).
-
FAA Flight Standardization Board (FSB) Report for the Bombardier CRJ1000 series aircraft Original dated 11/08/2011 (November 08, 2011) or later revision.
-
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).
-
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).
-
JOEB OPS/FCL Common procedures for conducting Operational Evaluation Boards, dated June 10, 2004.
-
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).
-
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.
-
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.
-
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).
-
TCCA Type Certificate Data Sheet (TCDS) A-276, Issue No. 7, dated December 22, 2022 or later issue.
Appendix 1 – Differences legend
Differences level |
Type |
Training method examples |
Conditions |
---|---|---|---|
A | Self-instruction |
|
|
B | Aided instruction |
|
|
C | Systems devices |
|
|
D | Maneuvers devices |
|
|
E | Level C/D FFS or aircraft |
|
|
Differences level |
Checking method examples |
Conditions |
---|---|---|
A | None | None |
B |
|
|
C |
|
|
D |
|
|
E |
|
|
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.
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 |
n/a |
Appendix 3 - Differences tables
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.
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tail span: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-8C1 or |
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; |
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.
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; |
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 |
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) |
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.
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 CRJ700 |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-3B1 |
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 |
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 |
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; |
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.
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; |
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 |
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. |
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 |
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) |
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.
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 |
Yes Normals |
n/a |
n/a |
ICBI, CSS, CPT, PTT, FTD 2-5 |
n/a |
B |
Approach |
Approach Attitude Comparison CRJ700 CRJ200 |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-8C5 |
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; |
No |
Yes Limits |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
B |
Limitations |
MMO above FL340 is 0.84M |
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.
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; |
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 |
No |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
A |
ATA 52 Doors |
Four over wing emergency exits |
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) |
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.
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 CRJ900 |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-3B1 |
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 |
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; |
No |
Yes Limits |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
B |
Limitations |
MMO above FL340 is 0.85M |
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.
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; |
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 |
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. |
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. |
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 |
No |
Yes Normals Abnormal Emergency |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
B |
ATA 52 Doors |
Two over wing emergency exits |
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) |
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.
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 |
Yes Normals |
n/a |
n/a |
ICBI, CSS, CPT, PTT, FTD 2-5 |
n/a |
B |
Approach |
Approach Attitude Comparison CRJ900 CRJ200 |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-8C5 |
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 |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Limitations |
Engine parameters; |
No |
Yes Limits |
HO |
n/a |
n/a |
n/a |
A |
Limitations |
MMO above FL340 is 0.84M |
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.
System |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 27 Flight Controls |
Slat/flap relationship: |
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.
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-8C1 or |
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 |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Limitations |
Engine parameters; |
No |
Yes Limits |
HO |
n/a |
n/a |
n/a |
A |
Limitations |
MMO is 0.85M above FL340 |
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.
System |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 27 Flight Controls |
Slat/flap relationship: |
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.
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-8C5 |
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; |
No |
Yes Limits |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
B |
Limitations |
MMO above FL340 is 0.84M |
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.
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; |
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 |
No |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
A |
ATA 52 Doors |
Four overwing emergency exits. |
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) |
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.
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 CRJ705 |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-3B1 |
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 |
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; |
No |
Yes Limits |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
B |
Limitations |
MMO above FL340 is 0.85M |
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.
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; |
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 |
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 |
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; |
No |
Yes Normals Abnormal Emergency |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
B |
ATA 52 Doors |
Two overwing emergency exits |
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) |
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.
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 |
Yes Normals |
n/a |
n/a |
ICBI, CSS, CPT, PTT, FTD 2-5 |
n/a |
B |
Approach |
Approach Attitude Comparison CRJ705 CRJ200 |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-8C5 |
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) |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Limitations |
Engine parameters; |
No |
Yes |
HO |
n/a |
n/a |
n/a |
A |
Limitations |
MMO above FL340 is 0.84 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.
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. |
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.
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
ATA 00 General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Performance Max T.O. Weight: Max Landing Weight: Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Wheel Base Main Wheel Track: Nose to Main Wheels: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
ATA 00 General |
Powerplant GE CF34-8C1 or |
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) |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Limitations |
Engine parameters; |
No |
Yes Limits |
HO |
n/a |
n/a |
n/a |
A |
Limitations |
MMO is 0.85M above FL340 |
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.
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. |
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.
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.
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.
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.
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:
|
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
Aircraft General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Aircraft General |
Performance Max T.O. Weight: Max Landing Weight: 81,500 lb. (36,968 kg) Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Aircraft General |
Powerplant GE CF34-8C5 |
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; |
No |
Yes Limits |
n/a |
ST, TCBI, SU, VT |
n/a |
n/a |
B |
Limitations |
MMO above FL340 is 0.84M |
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.
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 |
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; |
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 |
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:
|
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 |
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 |
No |
Minor Messages |
HO |
n/a |
n/a |
n/a |
A |
70 Powerplant |
FADEC controlled: |
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: |
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) |
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.
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 |
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 |
D |
Takeoff/ Go-Around |
Enhanced flight director with movable takeoff command bar indications |
Yes |
Yes |
n/a |
n/a |
n/a |
FFS |
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 |
D |
Takeoff |
Engine failure at V1 |
No |
No |
n/a |
n/a |
n/a |
FFS |
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 CRJ1000 |
Yes |
Yes |
n/a |
n/a |
n/a |
FFS |
D |
Landing |
Different procedure, thrust reduction technique may differ |
Yes |
Yes |
n/a |
n/a |
n/a |
FFS |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
Aircraft General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Aircraft General |
Performance Max T.O. Weight: 91,800 lb. (41,640 kg) Max Landing Weight: 81,500 lb. (36,968 kg) Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Aircraft General |
Powerplant GE CF34-8C5 |
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. |
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.
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 |
D |
27 Flight Controls |
Slat/flap relationship: |
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. |
No |
Minor Normals |
n/a |
n/a |
FTD |
n/a |
C |
34 FLT INST |
Smaller FMS CDU(s) with more functionality:
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.
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 |
D |
Takeoff/ Go-Around |
Enhanced flight director with movable takeoff command bar with indications |
No |
Minor Normals |
n/a |
n/a |
n/a |
FFS |
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 |
D |
Landing |
Same procedure, thrust reduction technique may differ |
No |
No |
n/a |
n/a |
n/a |
FFS |
D |
Landing |
More pronounced flare |
No |
Yes |
n/a |
n/a |
n/a |
FFS |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
Aircraft General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Aircraft General |
Performance Max T.O. Weight: 91,800 lb. (41,640 kg) Max Landing Weight: 81,500 lb. (36,968 kg) Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Aircraft General |
Powerplant GE CF34-8C5 |
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. |
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.
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 |
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. |
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:
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 |
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.
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 |
D |
Takeoff/ Go-Around |
Enhanced flight director with moveable takeoff command bar indications |
No |
Yes Normals |
n/a |
n/a |
n/a |
FFS |
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 |
D |
Landing |
Same procedure, thrust reduction technique may differ |
No |
No |
n/a |
n/a |
n/a |
FFS |
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.
Design |
Remarks |
FLT CHAR |
PROC CHNG |
Training Level |
CHK LVL |
|||
---|---|---|---|---|---|---|---|---|
A | B | C | D | |||||
Aircraft General |
Fuselage Length: Wingspan: Tailspan: Height: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Aircraft General |
Performance Max T.O. Weight: 91,800 lb. (41,640 kg) Max Landing Weight: 81,500 lb. (36,968 kg) Fuel Capacity: |
No |
No |
HO |
n/a |
n/a |
n/a |
A |
Aircraft General |
Powerplant GE CF34-8C5 |
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. |
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.
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 |
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 |
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. |
No |
Minor Normals |
n/a |
n/a |
FTD |
n/a |
C |
34 FLT INST |
Smaller FMS CDU (s) with more functionality
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.
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 |
D |
Takeoff/ Go-Around |
Enhanced flight director with moveable takeoff command bar indications |
No |
Minor Normals |
n/a |
n/a |
n/a |
FFS |
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 |
D |
Landing |
Same procedure, thrust reduction technique may differ |
No |
No |
n/a |
n/a |
n/a |
FFS |
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.
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.
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 |
not applicable |
not applicable |
CRJ700/701/702 |
not applicable |
CRJ100/200/440 |
not applicable |
not applicable |
CRJ100/200/440 |
not applicable |
CRJ1000 |
not applicable |
not applicable |
Qualified on aircraft |
Differences training |
TLI as per CARs |
MFF |
---|---|---|---|
CRJ100/200/440 |
CRJ700/701/702 |
not applicable |
not applicable |
CRJ700/701/702 |
CRJ100/200/440 |
not applicable |
not applicable |
CRJ100/200/440 |
CRJ1000 |
not applicable |
not applicable |
Notes
-
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.
-
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.
-
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.
-
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.