OPERATIONAL EVALUATION BOARD (OEB) REPORT
Cessna Citation 560 XLS+ to XL / XLS
Report Prepared and Submitted by: Len Kaufman
Operational Evaluation Board Transport Canada Civil Aviation
Commercial & Business Aviation
9300 Airport Road Unit 450
Mount Hope ON L0R 1W0
Telephone: (905) 679-2612
Fax -0033
E-Mail: len.kaufman@tc.gc.ca
DATE: August 27, 2009
Roman Marushko
Program Manager, Flight Technical
Transport Canada, Safety and Security
Certification and Operational Standards
Standards Branch
Place de Ville, Tower C, 330 Sparks Street
Ottawa, ON K1A 0N8
Telephone: (613) 993-4692
Fax: (613) 954-1602
E-Mail: roman.marushko@tc.gc.ca
Arlo Speer
Chief, Certification & Operational Standards
Standards Branch
Transport Canada, Civil Aviation
Table of Contents
- 1. Executive Summary
- 2. Purpose and Applicability
- 3. Acronyms
- 4. Background
- 5. Pilot "Type Rating" Requirements
- 6. Master Common Requirements (MCRs)
- 7. Master Difference Requirements (MDRs)
- 8. Acceptable "Operator Difference Requirements" (ODRs) Tables
- 9. Specifications for Training
- 10. Specifications for Checking
- 11. Specifications for Currency
- 12. Aircraft Regulatory Compliance Checklist
- 13. Specifications for Devices and Simulators
- 14. Application of Report
- 15. Alternate Means of Compliance To This Report
- 16. References
- 17. OPERATOR DIFFERENCE REQUIREMENTS TABLES
- APPENDIX 1. REGULATORY COMPLIANCE CHECKLISTS
Revision Record
| Revision No. | Section | Page # | Date |
| Original | All | All | August 27, 2009 |
Part 1 - OEB Report
1. Executive Summary
During the period of September 20, to November 21, 2008, Transport Canada and EASA conducted a joint operational evaluation (JOE) of the Cessna Citation 560 XLS+.
Beginning with aircraft serial number 560-6001, Cessna introduced a modified configuration of the Citation 560 XLS as the new production aircraft. The older Citation 560 XLS configuration will be discontinued and the new production configuration is marketed as the 560 XLS+. As stated, the Citation 560 XLS+ is not a new aircraft but an upgrade of a certified aircraft that has been in service for several years. Both the 560XL and the 560XLS aircraft are listed on TCCA Type Certificate Data Sheet (TCDS) A-130 and they share the same model number. The nomenclature 560XL, 560XLS, and 560XLS+ will be used in this report to distinguish between the Cessna Citation 560 variants.
Since the most restrictive training, checking, and currency differences are proposed at Level C/C/C, Cessna has requested that all the benefits associated with Same Type Rating be granted to the 560XLS+. The application also proposed Operator Differences Requirements (ODR) tables to identify the training checking and currency requirements for pilots transitioning from one of the three variants to another.
The Transport Canada / EASA joint operational evaluation was conducted in accordance with the procedures described in the Common Procedures Document (CPD) for Conducting Operational Evaluation Boards dated 10 June, 2004.
This report details the findings of the joint operational evaluation board (JOEB) and accepts Cessna’s proposal that the 560XL, 560XLS, and the 560XLS+ should share the same type rating. This report will help Canadian commercial air operators in the development of training programs and Principal Operations Inspectors (POI) in the approval of operator training programs pursuant to Canadian Aviation Regulations Part VII Subpart 4.
2. Purpose and Applicability
The primary purpose of this report is to specify Transport Canada master training, checking, and currency requirements applicable to crews operating the Cessna 560XL, 560XLS, and 560XLS+ aircraft. This report will help commercial air operators in the development of training programs and POIs in the approval of operator training programs pursuant to Canadian Aviation Regulations Part VII Subpart 4. Provisions of this report are effective until amended, superseded, or withdrawn by subsequent operational evaluation determinations.
This report does not address the operation of this aircraft under a CAR 604 Canadian Business Aircraft Association Private Operator Certificate.
3. Acronyms
| AARTF | Certification and Operational Standards |
| AFCS | Automatic Flight Control System |
| AFM | Aircraft Flight Manual |
| C&BA | Commercial and Business Aviation |
| CAR | Canadian Aviation Regulation |
| CASS | Canadian Aviation Regulation Standard |
| CPD | Common Procedures Document for Conducting Operational Evaluation Boards, 10 6 2004. |
| CRT | Cathode ray tubes |
| EASA | European Aviation Safety Agency |
| EFIS | Electronic Flight Information system |
| EIS | Engine Indicating System |
| EVS | Enhanced Vision System |
| FAA | Federal Aviation Administration |
| FAR | Federal Aviation Regulation |
| FCOM | Flight Crew Operating Manual |
| FMS | Flight Management System |
| FSB | Flight Standardization Board |
| HUD | Head Up Display |
| JAA | Joint Aviation Authorities |
| JOEB | Joint Operational Evaluation Board |
| LCD | Liquid crystal displays |
| LOF | Line-oriented flying |
| LOFT | Line-oriented flying training |
| MCR | Master Common Requirements |
| MFF | Mixed Fleet Flying |
| MLW | Maximum Landing Weight |
| MMEL | Master Minimum Equipment List |
| NSEP | National Simulator Evaluation Program |
| ODR | Operator Differences Requirements |
| OE | Operational Evaluation |
| OEB | Operational Evaluation Board |
| ORI | Operational Review Item |
| POI | Principal Operations Inspectors |
| PPC | Pilot Proficiency Check |
| QRH | Quick Reference Handbook |
| SID | Standard Instrument Departure |
| SLD | Super cooled liquid droplet |
| STAR | Standard Terminal Arrival |
| SVS | Synthetic Vision System |
| TCCA | Transport Canada Civil Aviation |
| TCDS | Type Certificate Data Sheet |
| VNAV | Vertical Navigation |
4. Background
Transport Canada (TCCA) Type Certificate Data Sheet (TCDS) A-130 identifies the Citation 560XLS (serial number 560-5501 and on).
The 560XL, 560XLS, and XLS+ are all metal, pressurized, low-wing, turbofan-powered aircraft. Thrust is provided by two pod-mounted PW545 A / B / C turbofan engines manufactured by Pratt and Whitney Canada, Inc. Each engine delivers 4119 lb. of thrust at sea level. Engine-driven hydraulic pumps supply hydraulic power for extending and retracting the landing gear, wing flaps, air brakes, thrust reversers, and to operate the stabilizer. Lateral and directional trim is accomplished by mechanically actuated trim tabs installed on the left aileron and the rudder. Longitudinal trim is accomplished by mechanically or electrically changing the angle of the trim tabs on the trailing edge of each elevator. Aircraft environmental systems provide heating, cooling, and pressurization for the crew and passengers.
The 560XLS+ aircraft is capable of maintaining a cruise speed of up to 0.75 Mach. The aircraft maximum operating altitude is 45,000 ft. The maximum operating range is 1858 nm (3441 km) with full fuel, maximum takeoff weight and IFR reserves.
The FAA in their evaluation identified that transitioning from the 560XL or 560XLS to the Pro Line 21 equipped 560XLS+ can be addressed by differences training. As of the date of signing this report, the final FSB report has not been completed. The draft FSB report indicates the minimum training requirements are satisfied at Level C.
The FAA FSB Chairman is a qualified 560XL captain. Accordingly, he evaluated the differences course provided by Flight Safety Wichita from the 560XL and 560XLS to the 560XLS+. The representatives from EASA and TCCA received an initial 560XLS+ course and subsequently they evaluated the differences training to the 560XLS and 560XL respectively.
This operational evaluation is primarily based on a 560XLS+ to 560XL differences ground and simulator training provided by Flight Safety. The training requirements for the transition to the 560XLS have been included under cooperation between TCCA and EASA. The ground school was conducted in Wichita, while the simulator training for the 560XL was conducted at the Flight Safety Columbus facility. Operational Suitability flights were conducted on the 560 XLS+ aircraft between Wichita and Columbus. The Flight training consisted of 5 landings with one ILS approach, followed by a GPS approach, an engine failure on take off with single engine landing followed by a partial flap landing. The aircraft was then flown from Wichita to Columbus for 560XL simulator training.
5. Pilot "Type Rating" Requirements
With reference to Canadian Aviation Regulation CAR 401.06 a new pilot type rating is assigned to the Cessna Citation 560XL and the designated licence endorsement is: C56XL. This operational evaluation, with the consensus of the FAA and EASA, has determined that the same type rating can be awarded and that the 560XLS+ should share the C56XL licensing designator with the older production aircraft. The Canadian Type Certificate Data Sheet (A-130) for the C56XL specifies the needs for one pilot and one copilot. The issuance of a type rating would require a completion of a Pilot Proficiency Check for Commercial Operations in accordance with CASS 421.40(3)(a)(iii)(A). Due to the design of this aircraft, the type shall not be eligible for PPC grouping in accordance with CAR Part VII. The concept of grouping is not applicable in the context of the three variants as they are the same type-rating.
6. Master Common Requirements (MCRs)
The new 560XLS+ differs from the 560XL and 560XLS primarily in the following manner.
- Immediate Action items are identical for both aircraft
- Abnormal and emergency procedures are presented in Quick Reference Handbooks (QRH). The QRH’s for the three variant aircraft share an identical presentation format and direct the pilots to carry out emergency or abnormal procedures in a methodical and structured manner.
- None of the 3 variant aircraft are equipped with a forward observer’s seat. Checking should be conducted in a full motion simulator with an observer seat that provides the check pilot a suitable view of the flight deck for the purpose of checking.
- Compliance with CASS 720.16(2)(a) for the extension of duty day with an additional crew member cannot be demonstrated because of the lack of a forward observer's seat on the flight deck or suitable forward passenger seat.
- normal final landing flap setting is the same for all variants
- handling and performance are similar for all aircraft with a slight variance in V speeds
- pilot operation of the primary flight controls is the same for all variants
- take off climb descent and approach profiles are the same for all variants
- incorporation of the Collins Pro Line 21 avionics package
- full authority digital engine controls including a new throttle quadrant
- modified instrument panel
- replacement of toggle switches with 2 position switch lights
- repositioned electrical, air conditioning, pressurization and other controls
7. Master Difference Requirements (MDRs)
Master Difference Requirements (MDRs) for the 560XL, 560XLS, and the 560XLS+ are shown in the table below. The requirements apply to operators whose crews operate 2 or 3 variants, or apply for conversion between variants. The Difference Level Definitions (e.g. A/A/A) are specified in accordance with the criteria contained in, Common Procedures Document for Operational Evaluation Board (OEB) FAA - JAA - TCCA where the first letter refers to training requirements, the second to checking requirements, and the third to currency requirements.
Level C differences training is the highest level required for the 560XL, 560XLS, and the 560XLS+. It is the responsibility of the operator and the training facility to ensure pilots moving from one variant to the other are given sufficient training to become fully cognizant of the differences in flight deck layout and avionics controls
Master Differences Requirements (MDR) Table
| AIRPLANE TYPE RATING: CE-560XL |
FROM AIRPLANE | |||
| CESSNA MODEL CE-560XL | CESSNA MODEL CE-560XLS | CESSNA MODEL CE-560XLS+ | ||
| CESSNA MODEL CE-560XL | A/A/B* | A/A/B | C/C/C*** | |
| TO AIRPLANE | CESSNA MODEL CE-560XLS | A/A/B | A/A/B* | C/C/C*** |
| CESSNA MODEL CE-560XLS+ | C/C/C** | C/C/C** | A/A/B* | |
NOTES*
Differences to accommodate optional equipment and aircraft modifications.
** The currency level for flight crews, who are trained and qualified in both the CE 560XL/XLS and the CE-560XLS+, or who are engaged in mixed fleet flying, is Level C if they have not operated the CE-560XLS+ in the preceding 180 days. If flight crews have not operated the CE-560XLS+ in the preceding 180 days, operators and training providers must ensure they receive the minimum training required by this report to re-establish currency in the CE-560XLS+ avionics system and FMS. If flight crews have operated the CE-560XLS+ in the preceding 180 days and have retained systems proficiency with the Pro Line 21 System and the FMS, the currency level will be Level B.
*** The currency level for flight crews, who are trained and qualified in CE-560XLS+ and the CE 560XL/XLS, or who are engaged in mixed fleet flying, is Level C if they have not operated the CE-560XL/XLS in the preceding 180 days. If flight crews have not operated the CE-560XL/XLS in the preceding 180 days, operators and training providers must ensure they receive the minimum training required by this report to reestablish currency in the CE-560XL/XLS avionics system and FMS. If flight crews have operated the CE-560XL/XLS in the preceding 180 days and have retained systems proficiency with the Honeywell Avionics System and applicable FMS, the currency level will be Level B.
8. Acceptable "Operator Difference Requirements" (ODRs) Tables
ODR tables are used to show an operator's compliance method. Acceptable ODR tables for operators conducting mixed fleet flying (MFF) operations, or operators converting between one of the 3 variants, begin on page 14. MFF is defined as operations in which crews alternately fly 2 or 3 variants between PPC /training events.
The ODR tables represent an acceptable means to comply with MDR provisions for the aircraft evaluated based on those differences and compliance methods shown. The tables do not necessarily represent the only acceptable means of compliance for operators with aircraft having other differences, where compliance methods (e.g., devices, simulators, etc.) are different, or for combinations of aircraft not evaluated. For operators flying variants, which are the same as the aircraft used for the ODR table development, and using the same compliance methods, the ODR tables have been found acceptable by TCCA. Equivalent tables, therefore, may be approved by the POI for a particular operator.
Operators flying variants with differences not shown in, or addressed by, the acceptable ODR tables or operators seeking a different means of compliance, must prepare and seek TCCA approval of specific ODR tables applicable to their fleet. New ODR tables proposed by operators should be coordinated with the Program Manager, Flight Technical in Certification and Operational Standards (AARTF) to ensure consistent treatment of variants between various operators’ ODR tables and compatibility of the MDR table with MDR provisions. The operator retains the originals of the approved ODR tables. The Program Manager Flight Technical will retain copies of approved Cessna aircraft ODR tables.
9. Specifications for Training
Initial, Transition and Upgrade Training:
The Flight Safety Wichita Training Center 560XLS+ training program was closely modeled upon the original 560XL, and 560XLS training programs and shares the same philosophy in use of resource material and courseware presentation whenever possible. Minimum training time requirements specified in CASS 724.115(31) Table 1 apply. Commercial operators must ensure that their approved training programs requirements are met when contracting their crew member training to another organization.
Recurrent Training:
Annual recurrent training is accomplished in accordance with the operators approved training program that meets the standards of CASS 724.115. Minimum Ground and Flight (Simulator) specified in CASS 724.115(31) Table 2 apply.
Differences Training:
When any combination of the 560XL, 560XLS, and the 560XLS+ are flown, appropriate instruction in design and systems differences will be required for any airplane consistent with MDR provisions detailed in Section 7. In the future, when significant hardware or software product improvements are introduced for a single aircraft variant or for all variants, a reassessment of the differences training requirements may be undertaken by TCCA.
- Operator training from 560XL or the 560XLS to the 560XLS+ should emphasize the differences between the Primus 1000 / Universal or Honeywell FMS installation and the upgraded Pro Line 21 system.
- The OEB recommends that the amount of differences ground school training and systems integration training when transitioning from 560XLS+ to or from the 560XL and or 560XLS is:
| DIFFERENCES TRAINING HOURS SUMMARY | ||||||
| From | To | Modules | Gnd. Tng. |
Sim. Tng. |
SIT Tng. * |
Check |
| INITIAL TRAINING | ||||||
| XL | XLS | ALL | 4.0 | |||
| XLS | XL | ALL | 4.0 | |||
| XL / XLS |
XLS+ | Avionics | 6.0 | 4.0 | As Req. | |
| Lighting & Master Caution Powerplant |
2.0 | |||||
| XLS+ | XL / XLS |
Avionics | 6.0 | 4.0 | As Req. | |
| Lighting & Master Caution Powerplant |
2.0 | |||||
| RECURRENT TRAINING | ||||||
| XL | XLS | ALL | 2.0 | |||
| XLS | XL | ALL | 2.0 | |||
| XL / XLS |
XLS+ | Avionics Lighting & Master Caution Powerplant |
2.0 | As Req. | ||
| XLS+ | XL / XLS |
Avionics Lighting & Master Caution Powerplant |
2.0 | As Req. | ||
* Must be conducted in a Level 5 FTD, or higher.
- The OEB recommends that systems integrations training be at level C using the minimum devices that meet the level C requirements specified by the MDR table.
- Special Event Training
Special event training is recommended. Such training should be conducted to improve basic crew understanding and confidence regarding aircraft handling qualities, options and procedures as these relate to design characteristics and limitations. Examples of this training should include the following:- Recovery from unusual attitudes;
- Handling qualities and procedures during recovery from an upset condition (e.g., wake vortex encounter);
- Operation of aircraft in icing environments including super cooled liquid droplet (SLD) events;
- Low Energy Awareness Training;
- High Altitude Stall Recovery;
- Engine Failure/Malfunction Recognition Training;
- The OEB also found that early exposure to the automatic flight control system (AFCS), and flight management system (FMS) is important, particularly for pilots with no previous Pro Line 21 experience. Establishing early confidence in manually flying the aircraft, converting from manual to automatic (FMS controlled) flight mode and back is equally important due to heavy reliance on the AFCS. In the event of a flight path deviation due to input error or system malfunction, the flight crew must be able to comfortably transition from automatic to manual mode and back in an orderly fashion.
- Similarly, exposure to the use of VNAV in the terminal environment including SIDs, STARs and LNAV/VNAV approaches is important. Establishing confidence in converting from basic autopilot modes to FMS VNAV controlled flight modes and back is equally important in order to cope with ATC clearance amendments to speed and altitude constraints.
- The differences training program can be found in Appendix 2.
Display of Jeppesen Approach Charts on MFD:
- Jeppesen approach and airport charts that can be displayed on the MFD do not meet requirements for an electronic flight bag because these charts cannot be displayed during all phases of flight. In particular, when the battery is placed in the “EMER” position, the MFD display is not powered. This constraint would require that valid charts in another approved format be available during IFR flight. CBAAC 0231 dated 2004.07.20 provides guidance to operators on the use of Electronic Flight Bags.
10. Specifications for Checking
Checking conducted shall be in accordance with CASS 724.108 schedule 1, as required.
11. Specifications for Currency
Currency will be maintained, or re-established, in accordance with CASS 724.115 through the approved Company training program.
The assessment of currency was not restricted to take-off and landing currency as the scope of this OEB was to specifically evaluate the differences in avionics between the 560XL, 560XLS, and the 560XLS+. The differences in avionics form the primary differences between the three aircraft. Please review the notes regarding currency under the Master Differences Requirements table..
12. Aircraft Regulatory Compliance Checklist
Any Canadian operator wishing to operate the 560XL, 560XLS, or 560XLS+ aircraft will have to demonstrate to Transport Canada that the aircraft fully complies with all applicable CAR 605/704 parts before that aircraft enters service. A sample compliance checklist is included in Appendix 1 of this report.
POIs may contact the Program Manager of Flight Technical in Certification and Operational Standards, Flight Technical to obtain a sample checklist for guidance in determining an operator’s compliance with all applicable CAR 605/704 regulations.
13. Specifications for Devices and Simulators
Device and simulator characteristics are designated in Aeroplane and Rotorcraft Simulator Manual (TP 9685). The acceptability of differences between devices, simulators, and aircraft must be addressed by the POI. Requests for device approval should be made to the POI. The POI may approve those devices for that operator if their characteristics clearly meet the established TC criteria and have been qualified by the National Simulator Evaluation Program (NSEP).
14. Application of Report
All relevant parts of this report are applicable to operators on the effective date of this report.
15. Alternate Means of Compliance To This Report
The TCCA Program Manager Flight Technical should be consulted by the POI when alternate means of compliance, other than those specified in this report, are proposed. If an alternate means of compliance is sought, operators will be required to submit a proposed alternate means of compliance for approval that provides an equivalent level of safety to the provisions of CPD and this OEB report. Analysis, demonstrations, proof of concept testing, differences documentation, and/or other evidence may be required.
In the event that an alternate means of compliance is sought, training program hour reductions, simulator approvals, and device approvals may be significantly limited and reporting requirements may be increased to ensure an equivalent level of training, checking, and currency. TCCA will generally not consider relief through an alternate means of compliance unless sufficient lead-time has been planned by an operator to allow for any necessary testing and evaluation.
16. References
- Common Procedures Document (CPD) for Conducting Operational Evaluation Boards dated 10 June 2004;
- Transport Canada Commercial and Business Aviation Advisory Circular (CBAAC) No. 231; Electronic Flight Bags; dated 2004.07.20.
17. OPERATOR DIFFERENCE REQUIREMENTS TABLES
| Definitions used in the ODR Tables: |
| X = Pilot’s Operating Handbook and or Flight Manual Supplement FTD 5 = Flight training devices (level 5) |
CE-560XL to CE-560XLS
| DIFFERENCE AIRCRAFT: CE-560XLS BASE AIRCRAFT: CE-560XL APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| DESIGN | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| Citation 560XLS | More Engine Thrust, Hyd. and Brake System differences, Larger Cockpit Displays, added Body Fairings, Max Gross Weight change (20,200 lbs to 20,400 lbs. ramp load) | None | Minor | X | A | B | |||
| DIFFERENCE AIRCRAFT: CE-560XLS BASE AIRCRAFT: CE-560XL APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| MANEUVER | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| None | No Changes | None | None | ||||||
Note: There is no systems differences in this report as there are no systems differences between the XL & XLS.
CE-560XLS to CE-560XL
| DIFFERENCE AIRCRAFT: CE-560XL BASE AIRCRAFT: CE-560XLS APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| DESIGN | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| Citation 560XL | Less Engine Thrust, Hyd. and Brake System differences, Smaller Cockpit Displays, no Body Fairings, Max Gross Weight change (20,400 lbs to 20,200 lbs. ramp load) | None | Minor | X | A | B | |||
| DIFFERENCE AIRCRAFT: CE-560XLS BASE AIRCRAFT: CE-560XL APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| MANEUVER | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| None | No Changes | None | None | ||||||
Note: There is no systems differences in this report as there are no systems differences between the XL & XLS.
CE-560XL TO CE-560XLS+
| DIFFERENCE AIRCRAFT: CE-560XLS+ BASE AIRCRAFT: CE-560XL APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| DESIGN | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| Engine PW545C replaces PW545A | FADEC controlled. more Engine Thrust. Thrust reverser deployment emergency procedures changed. |
None | Minor | X | B | B | |||
| Avionics | Collins Pro Line 21 replaces Honeywell P-1000. | None | Major | FTD 5 | C/ FTD 5 |
C/B | |||
| Cockpit Structure | Full span tilt panel added. Emergency gear release controls changed. | None | Minor | X | A | B | |||
| DIFFERENCE AIRCRAFT: CE-560XLS+ BASE AIRCRAFT: CE-560XL APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| MANEUVER | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| None | No Changes | None | None | ||||||
| DIFFERENCE AIRCRAFT: CE-560XLS+ BASE AIRCRAFT: CE-560XL APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| SYSTEM | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| ATA-21 Air conditioning |
Relocated temperature and pressurization controllers. | No | Minor | X | A | A | |||
| Auto Flight ATA-22 |
Collins autopilot and flight guidance control panel. Single flight guidance panel located below Glareshield replaces dual flight guidance panels located above PFDs. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Communications ATA-23 |
Collins radios. Radio tuning through Control Display Units or Cursor Control Panels instead of Radio Management Units. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Electrical Power ATA-24 |
Relocated controls and ammeters. | No | Minor | X | A | A | |||
| Indicating/ Recording Systems ATA-31 |
CAS on display unit 3 replaces annunciator panel. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Landing Gear ATA-32 |
Relocated emergency gear release and blow down handles. | No | Minor | X | B | B | |||
| Lights ATA-33 |
Lighting controls relocated. | No | Minor | X | A | A | |||
| Navigation ATA-34 |
4 tube Collins displays and controllers replace 3 tube Honeywell displays and controllers. Collins radios and FMS. Radio tuning through CDUs and CCPs instead of RMUs. Electronic standby HSI replaces mechanical HSI. | No | Major | FTD 5 | C/ FTD 5 |
C/B | |||
| Oxygen ATA-35 |
Relocated oxygen controls and gauge. | No | Minor | X | A | A | |||
| Engine Fuel & Control ATA-73 |
Dual channel FADEC Engines with new throttles. | No | Minor | X | B | B | |||
| Engine Indicating ATA-77 | Engine Information System on display unit 2. New standby engine gauge. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
CE-560XLS TO CE-560XLS+
| DIFFERENCE AIRCRAFT: CE-560XLS+ BASE AIRCRAFT: CE-560XLS APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| DESIGN | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| Engine PW545C replaces PW545B | FADEC controlled. | None | Minor | X | B | B | |||
| Avionics | Collins Pro Line 21 replaces Honeywell P-1000 | None | Major | FTD 5 | C/ FTD 5 |
C/B | |||
| Cockpit Structure | Full span tilt panel added. Emergency gear release controls changed. | None | X | A | B | ||||
| DIFFERENCE AIRCRAFT: CE-560XLS+ BASE AIRCRAFT: CE-560XLS APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| MANEUVER | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| None | No Changes | None | None | ||||||
| DIFFERENCE AIRCRAFT: CE-560XLS+ BASE AIRCRAFT: CE-560XLS APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| SYSTEM | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| ATA-21 Air conditioning |
Relocated temperature and pressurization controllers. | No | Minor | X | A | A | |||
| Auto Flight ATA-22 |
Collins autopilot and flight guidance control panel. Single flight guidance panel located below Glareshield replaces dual flight guidance panels located above PFDs. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Communications ATA-23 |
Collins radios. Radio tuning through Control Display Units or Cursor Control Panels instead of Radio Management Units. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Electrical Power ATA-24 |
Relocated controls and ammeters. | No | Minor | X | A | A | |||
| Indicating/ Recording Systems ATA-31 |
CAS on display unit 3 replaces annunciator panel. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Landing Gear ATA-32 |
Relocated emergency gear release and blow down handles. | No | Minor | X | B | B | |||
| Lights ATA-33 |
Lighting controls relocated. | No | Minor | X | A | A | |||
| Navigation ATA-34 |
4 tube Collins displays and controllers replace 3 tube Honeywell displays and controllers. Collins radios and FMS. Radio tuning through CDUs and CCPs instead of RMUs. Electronic standby HSI replaces mechanical HSI. | No | Major | FTD 5 | C/ FTD 5 |
C/B | |||
| Oxygen ATA-35 |
Relocated oxygen controls and gauge. | No | Minor | X | A | A | |||
| Engine Fuel & Control ATA-73 |
Dual channel FADEC Engines with new throttles. | No | Minor | X | B | B | |||
| Engine Indicating ATA-77 | Engine Information System on display unit 2. New standby engine gauge. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
CE-560XLS+ TO CE-560XL
| DIFFERENCE AIRCRAFT: CE-560XL BASE AIRCRAFT: CE-560XLS+ APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| DESIGN | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| Engine PW545A replaces PW545C | EEC controlled instead of FADEC controlled, and less thrust. | None | Minor | FTD 5 | C/ FTD 5 |
B | |||
| Avionics | Honeywell P-1000 replaces Collins Pro Line 21 | None | Major | FTD 5 | C/ FTD 5 |
C/B | |||
| Cockpit Structure | Full span tilt panel removed. Emergency gear release controls changed. | None | Minor | X | A | B | |||
| DIFFERENCE AIRCRAFT: CE-560XL BASE AIRCRAFT: CE-560XLS+ APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| MANEUVER | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| None | No Changes | None | None | ||||||
| DIFFERENCE AIRCRAFT: CE-560XL BASE AIRCRAFT: CE-560XLS+ APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| SYSTEM | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| ATA-21 Air conditioning |
Relocated temperature and pressurization controllers. | No | Minor | X | A | A | |||
| Auto Flight ATA-22 |
Honeywell autopilot and flight guidance control panel. Dual flight guidance panels located above PFDs replace single flight guidance panel located below glareshield. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Communications ATA-23 |
Honeywell radios. Radio tuning through Radio Management Units instead of Control Display Units or Cursor Control Panels. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Electrical Power ATA-24 |
Relocated controls and ammeters. | No | Minor | X | A | A | |||
| Indicating/ Recording Systems ATA-31 |
Annunciator Panel replaces CAS on display unit 3. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Landing Gear ATA-32 |
Relocated emergency gear release and blow down handles. | No | Minor | X | A | A | |||
| Lights ATA-33 |
Lighting controls relocated. | No | Minor | X | B | B | |||
| Navigation ATA-34 |
3 tube Honeywell displays and controllers replace 4 tube Collins displays and controllers. Honeywell radios and FMS. Radio tuning through RMUs instead of CDUs and CCPs. Mechanical standby HSI replaces electrical HSI. | No | Major | FTD 5 | C/ FTD 5 |
C/B | |||
| Oxygen ATA-35 |
Relocated oxygen controls and gauge. | No | Minor | X | A | A | |||
| Engine Fuel & Control ATA-73 |
Single channel EEC Engines with different throttles and AUTO/MANUAL switches. | No | Minor | FTD 5 | C/ FTD 5 |
B | |||
| Engine Indicating ATA-77 | AMLCD or mechanical tape gauges. Standby engine gauge is half of AMLCD or just mechanical N1 tapes. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
CE-560XLS+ TO CE-560XLS
| DIFFERENCE AIRCRAFT: CE-560XLS BASE AIRCRAFT: CE-560XLS+ APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| DESIGN | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| Engine PW545B replaces PW545C | EEC controlled instead of FADEC controlled | None | Minor | FTD 5 | C/ FTD 5 |
B | |||
| Avionics | Honeywell P-1000 replaces Collins Pro Line 21 | None | Major | FTD 5 | C/ FTD 5 |
C/B | |||
| Cockpit Structure | Full span tilt panel removed. Emergency gear release controls changed. | None | Minor | X | A | B | |||
| DIFFERENCE AIRCRAFT: CE-560XLS BASE AIRCRAFT: CE-560XLS+ APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| MANEUVER | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| None | None | None | |||||||
| DIFFERENCE AIRCRAFT: CE-560XLS BASE AIRCRAFT: CE-560XLS+ APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
| TRAINING | CHKG/CURR | ||||||||
| SYSTEM | REMARKS | FLT CHAR |
PROC CHNG |
LVL A |
LVL B |
LVL C |
LVL D |
CHK | CURR |
| ATA-21 Air conditioning |
Relocated temperature and pressurization controllers. | No | Minor | X | A | A | |||
| Auto Flight ATA-22 |
Honeywell autopilot and flight guidance control panel. Dual flight guidance panels located above PFDs replace single flight guidance panel located below glareshield. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Communications ATA-23 |
Honeywell radios. Radio tuning through Radio Management Units instead of Control Display Units or Cursor Control Panels. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Electrical Power ATA-24 |
Relocated controls and ammeters. | No | Minor | X | A | A | |||
| Indicating/ Recording Systems ATA-31 |
Annunciator Panel replaces CAS on display unit 3. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
| Landing Gear ATA-32 |
Relocated emergency gear release and blow down handles. | No | Minor | X | A | A | |||
| Lights ATA-33 |
Lighting controls relocated. | No | Minor | X | A | B | |||
| Navigation ATA-34 |
3 tube Honeywell displays and controllers replace 4 tube Collins displays and controllers. Honeywell radios and FMS. Radio tuning through RMUs instead of CDUs and CCPs. Mechanical standby HSI replaces electrical HSI. | No | Major | FTD 5 | C/ FTD 5 |
C/B | |||
| Oxygen ATA-35 |
Relocated oxygen controls and gauge. | No | Minor | X | A | A | |||
| Engine Fuel & Control ATA-73 |
Single channel EEC Engines with different throttles and AUTO/MANUAL switches. | No | Minor | FTD 5 | C/ FTD 5 |
B | |||
| Engine Indicating ATA-77 | AMLCD or mechanical tape gauges. Standby engine gauge is half of AMLCD or just mechanical N1 tapes. | No | Minor | FTD 5 | C/ FTD 5 |
C/B | |||
APPENDIX 1. REGULATORY COMPLIANCE CHECKLISTS
Reserved ... Cessna Aircraft to completed prior to first 560XLS+ importation
| CAR | Amendment | Requirement | Applicant Position | Remarks | TCCA Finding |
| 605.01 | 2004-2 | Application | Noted | ||
| 605.02 | 2004-2 | Reserved | Noted | ||
| Division I - Aircraft Requirements - General | |||||
| 605.03 | 2004-2 | Flight authority | -- | ||
| 605.04 | 2004-2 | Availability of Aircraft Flight Manual | Operator Responsibility | ||
| 605.05 | 2004-2 | Markings and placards | |||
| 605.06 | 2004-2 | Aircraft equipment standards and serviceability | -- | ||
| 605.07 | 2004-2 | Minimum Equipment List | |||
| 605.08 | 2004-2 | Unserviceable and removed equipment - General | . | Operator responsibility | |
| 605.09 | 2004-2 | Unserviceable and removed equipment - Aircraft with a Minimum Equipment List | Operator responsibility | ||
| 605.10 | 2004-2 | Unserviceable and removed equipment - Aircraft without a Minimum Equipment List | Operator responsibility | ||
| 605.11 | 2004-2 | Reserved | Noted | ||
| 605.12 | 2004-2 | Reserved | Noted | ||
| 605.13 | 2004-2 | Reserved | Noted | ||
| *Division II - Aircraft Equipment Requirements* | |||||
| 605.14 | 2004-2 | Power-driven aircraft - Day VFR | |||
| 605.15 | 2004-2 | Power-driven aircraft - VFR OTT | . | ||
| 605.16 | 2004-2 | Power-driven aircraft - Night VFR | |||
| 605.17 | 2004-2 | Use of position and anti-collision lights | Use of these lights is operator ‘s responsibility | ||
| 605.18 | 2004-2 | Power-driven aircraft - IFR | . | ||
| 605.19 | 2004-2 | Balloons - Day VFR | Not applicable | √ | |
| 605.20 | 2004-2 | Balloons - Night VFR | Not applicable | √ | |
| 605.21 | 2004-2 | Gliders - Day VFR | Not applicable | √ | |
| 605.22 | 2004-2 | Seat and safety belts requirements | |||
| 605.23 | 2004-2 | Restraint system requirements | |||
| 605.24 | 2004-2 | Shoulder harness requirements | |||
| (1) | Flight deck seats equipped with shoulder harness | ||||
| (2) | Flight attendant seats equipped with shoulder harness | ||||
| (3) | Small airplane requirements | Not applicable | √ | ||
| (4) | Helicopter requirements | Not applicable | √ | ||
| (5) | Special flight operations requirements | Not applicable | √ | ||
| 605.25 | 2004-2 | General use of safety belts and restraint system | -- | Operator responsibility | |
| 605.26 | 2004-2 | Use of passenger safety belts and restraint system | -- | Operator responsibility | |
| 605.27 | 2004-2 | Use of crew member safety belts | -- | Operator responsibility | |
| 605.28 | 2004-2 | Child restraint system | -- | Operator responsibility | |
| 605.29 | 2004-2 | Flight control locks | |||
| 605.30 | 2004-2 | De-icing or anti-icing equipment | |||
| 605.31 | 2004-2 | Oxygen equipment and supply | |||
| (1) | Unpressurized aircraft | Not applicable | √ | ||
| (2) | Pressurized aircraft | ||||
| 605.32 | 2004-2 | Use of oxygen | -- | Operator responsibility | |
| 605.33 | 2004-2 | Flight data recorder and cockpit voice recorder | |||
| (1) | Flight data recorder | ||||
| (2) | Cockpit voice recorder | ||||
| 605.34 | 2004-2 | Use of Flight Data Recorder and Cockpit Voice Recorder | . | Operator responsibility | |
| 605.35 | 2004-2 | Transponder and automatic pressure-altitude reporting equipment | |||
| (1) | Equipment installed | ||||
| (2) | Operation with unserviceable equipment | Operator responsibility | |||
| (3) | Operation of aircrafts with no equipment installed | ||||
| 605.36 | 2004-2 | Altitude alerting system or device | |||
| 605.37 | 2004-2 | Ground proximity warning system | |||
| (1) | Equipment requirement | ||||
| (2) | Operation with unserviceable equipment | Operator responsibility | |||
| (3) | Equipment deactivation | Operator responsibility | |||
| 605.38 | 2004-2 | ELT | |||
| 605.39 | 2004-2 | Use of ELT’s | -- | Operator responsibility | |
| 605.40 | 2004-2 | ELT activation | -- | Operator responsibility | |
| 605.41 | 2004-2 | Standby attitude indicator | |||
| 605.42 to 605.83 | 2004-2 | Reserved | Noted | ||
| *Division III - Aircraft Maintenance Requirements* | |||||
| 605.84 | 2004-2 | Aircraft maintenance - General | The operator is responsible to perform the required maintenance in accordance with the approved maintenance program. | ||
| 605.85 | 2004-2 | Maintenance release and elementary work | -- | Operator responsibility | |
| 605.86 | 2004-2 | Maintenance schedule | The operator is responsible to perform the required maintenance in accordance with the approved maintenance program. | ||
| 605.87 | 2004-2 | Transfer of aeronautical products between maintenance schedules | -- | Operator responsibility | |
| 605.88 | 2004-2 | Inspection after abnormal occurrences | The operator is responsible to perform the required maintenance in accordance with the approved maintenance program. | ||
| 605.89 to 605.91 | 2004-2 | Reserved | Noted | ||
| *Division IV - Technical Records* | |||||
| 605.92 | 2004-2 | Requirements to keep technical records | -- | Operator responsibility | |
| 605.93 | 2004-2 | Technical records - General | -- | Operator responsibility | |
| 605.94 | 2004-2 | Journey log requirements | -- | Operator responsibility | |
| 605.95 | 2004-2 | Journey log - carrying on board | -- | Operator responsibility | |
| 605.96 | 2004-2 | Requirements for technical records other than the journey log | -- | Operator responsibility | |
| 605.97 | 2004-2 | Transfer of records | -- | Operator responsibility | |
| 605.98 to 605.110 | 2004-2 | Reserved | Noted | ||
| CAR | Amendment | Requirement | Applicant Position | Remarks | TCCA Finding |
| *Division I - General* | |||||
| 604.01 | Application | Noted | |||
| 604.02 | Aircraft operation | -- | Operator responsibility | ||
| 604.03 to 604.04 | Reserved | Noted | |||
| *Division II - CERtification* | |||||
| 604.05 | Issuance or amendment of Private Operator Certificate | -- | Operator responsibility | ||
| 604.06 | Contents of Air Operator Certificate | -- | Operator Responsibility | ||
| 604.07 | General conditions of Air Operator Certificate | -- | Operator responsibility | ||
| 604.08 and 604.09 | Reserved | Noted | √ | ||
| *Division III - FLIGHT operations* | |||||
| 604.10 | Checklist | ||||
| (1) | Operational checklist | Operator responsibility to make these checklists available to the crew | |||
| (2) | Checklist accomplishment | -- | Operator responsibility | ||
| 604.11 | Operational flight data sheet | -- | Operator responsibility | ||
| 604.12 | VFR flight minimum flight visibility - uncontrolled airspace | -- | Operator responsibility | ||
| 604.13 | No alternate aerodrome - IFR flight | -- | Operator responsibility | ||
| 604.14 | Take-off minima | -- | Operator responsibility | ||
| 604.15 | Instrument approach procedures | It is operator responsibility to comply with operational procedures. | |||
| 604.16 | Flight attendant requirement | ||||
| 604.17 | Cabin safety procedures | -- | Operator responsibility | ||
| 604.18 | Briefing of passengers | -- | Operator responsibility | ||
| 604.19 | Safety features card | It is operator responsibility to decide the final content of the safety features card. | |||
| 604.20 thru 604.25 | Reserved | Noted | - | ||
| *Division IV - Flight time and duty time limitations and rest periods* | |||||
| 604.26 | Flight time limitations | -- | Operator responsibility | ||
| 604.27 | Flight duty time limitations and rest periods | -- | Operator responsibility | ||
| 604.28 | Split flight duty time | -- | Operator responsibility | ||
| 604.29 | Extension of flight duty time | -- | Operator responsibility | ||
| 604.30 | Unforeseen operational circumstances | -- | Operator responsibility | ||
| 604.31 | Delayed reporting time | -- | Operator responsibility | ||
| 604.32 | Requirements for time free from duty | -- | Operator responsibility | ||
| 604.33 | Flight crew positioning | -- | Operator responsibility | ||
| 604.34 thru 604.37 | Reserved | Noted | |||
| *Division V - emergency equipment* | |||||
| 604.38 | Survival equipment | Over land Over water |
Operator Responsibility | √ | |
| 604.39 | First aid kits | Operators Responsibility to mark date of last inspection | |||
| 604.40 | Protective breathing equipment | Operator responsibility to provide PBE on the flight deck, flight attendant station, cargo compartments, and fire extinguishers. | |||
| 604.41 | Hand held fire extinguishers | ||||
| 604.42 thru 604.47 | Reserved | Noted | √ | ||
| *Division Vi - maintenance* | |||||
| 604.48 | Maintenance control system | -- | Operator responsibility | ||
| 604.49 | Description of maintenance control system in operations manual | -- | Operator responsibility | ||
| 604.50 | Person responsible for maintenance control system | -- | Operator responsibility | ||
| 604.51 | Maintenance personnel and facility | -- | Operator responsibility | ||
| 604.52 | Defect reporting and rectification control procedure | -- | Operator responsibility | ||
| 604.53 | Service difficulty report | -- | Operator responsibility | ||
| 604.54 | Technical dispatch instructions | -- | Operator responsibility | ||
| 604.55 | Service information review | -- | Operator responsibility | ||
| 604.56 | Maintenance agreements | -- | Operator responsibility | ||
| 604.57 | Maintenance training | -- | Operator responsibility | ||
| 604.58 thru 604.64 | Reserved | Noted | |||
| *Division Vii - Personnel requirements* | |||||
| 604.65 | Designation of pilot-in-command and second-in-command | -- | Operator responsibility | ||
| 604.66 | Crew member qualifications | -- | Operator responsibility | ||
| 604.67 | Check authority | -- | Operator responsibility | ||
| 604.68 | Validity period | -- | Operator responsibility | ||
| 604.69 thru 604.72 | Reserved | Noted | |||
| *Division Viii - training* | |||||
| 604.73 | Training program | -- | Operator responsibility | ||
| 604.74 | Training and qualification records | -- | Operator responsibility | ||
| 604.75 and 604.79 | Reserved | Noted | |||
| *Division ix - manuals* | |||||
| 604.80 | Requirements related to operations manual | -- | Operator responsibility | ||
| 604.81 | Contents of operations manual | -- | Operator responsibility | ||
| 604.82 | Distribution of operations manual | -- | Operator responsibility | ||
| 604.83 | Aircraft operating manual | Development and approval of Aircraft Operating Manual is operator’s responsibility. | |||
| 604.84 | Standard operating procedures | Development and approval of Standard Operating Procedures (separately or as part of Aircraft Operating Manual) is operator’s responsibility. | |||
| 604.85 thru 604.89 | Reserved | Noted | √ | ||
| CAR | Amendment | Requirement | Applicant Position | Remarks | TCCA Finding |
| *Division I - General* | |||||
| 704.01 | Application | ||||
| 704.02 | Aircraft operation | -- | Operator responsibility | ||
| 704.03 to 704.06 | Reserved | Noted | |||
| *Division II - CERtification* | |||||
| 704.07 | Issuance or amendment of Air Operator Certificate | -- | Operator responsibility | ||
| (1) | Compliance with regulation | -- | Operator responsibility | ||
| (2)(a) thru (2)(c) | Operator organization requirements | -- | Operator responsibility | ||
| (2)(d) | MMEL/MEL requirement | Approval of applicable MEL is the operator’s responsibility | |||
| (2)(e) thru (2)(j) | Operator organization requirements | -- | Operator responsibility | ||
| 704.08 | Contents of Air Operator Certificate | -- | Operator Responsibility | ||
| 704.09 | General conditions of Air Operator Certificate | -- | Operator responsibility | ||
| 704.10 and 704.11 | Reserved | Noted | |||
| *Division III - FLIGHT operations* | |||||
| 704.12 | Operating instruction | -- | Operator responsibility | ||
| 704.13 | General operational information | -- | Operator responsibility | ||
| 704.14 | Scheduled air service requirements | -- | Operator responsibility | ||
| 704.15 | Operational control system | -- | Operator responsibility | ||
| 704.16 | Flight authorization | -- | Operator responsibility | ||
| 704.17 | Operational flight plan | -- | Operator responsibility | ||
| 704.18 | Maintenance of aircraft | The operator is responsible to perform the required maintenance in accordance with the approved maintenance program. | |||
| 704.19 | Checklist | ||||
| (1) | Operational checklist | Operator responsibility to make these checklists available to the crew | |||
| (2) | Checklist accomplishment | -- | Operator responsibility | ||
| 704.20 | Fuel requirements | -- | Operator responsibility | ||
| 704.21 | Admission to flight deck | -- | Operator responsibility | ||
| 704.22 | Simulation of Emergency situations | -- | Operator responsibility | ||
| 704.23 | VFR flight obstacle clearance requirements | -- | |||
| 704.24 | VFR flight minimum flight visibility - uncontrolled airspace | Not applicable | |||
| 704.25 | VFR flight weather conditions | -- | Operator responsibility | ||
| 704.26 | Take-off minima | -- | Operator responsibility | ||
| 704.27 | No alternate aerodrome - IFR flight | Operator responsibility | |||
| 704.28 | VFR OTT flight | Not applicable | |||
| 704.29 | Routes in uncontrolled airspace | -- | Operator responsibility | ||
| 704.30 | Instrument approach procedures | Operator responsibility | |||
| 704.31 | Minimum altitudes and distances | Not applicable | |||
| 704.32 | Weight and balance control | Operator responsibility to operate the aircraft within the operational envelope. | |||
| 704.33 | Apron and cabin safety procedures | -- | Operator responsibility | ||
| 704.34 | Briefing of passengers | -- | Operator responsibility | ||
| 704.35 | Safety features card | -- | Operator responsibility | ||
| 704.36 thru 704.43 | Reserved | Noted | Operator responsibility | ||
| *Division IV - Aircraft performance operating limitation* | |||||
| 704.44 | Exceptions | Noted | |||
| 704.45 | General requirements | Noted | |||
| 704.46 | Take-off weight limitations | Operator responsibility to operate the aircraft within the operational limits. | |||
| 704.47 | Net take-off flight path | Operator responsibility to operate the aircraft within the operational limits. | |||
| 704.48 | Enroute limitations with one engine inoperative | Operator responsibility to operate the aircraft within the operational limits. | |||
| 704.49 | Dispatch limitations: landing at destination and alternate aerodromes | -- | Operator responsibility | ||
| 704.50 | Dispatch limitations: wet runway - turbo-jet-powered aeroplanes | -- | Operator responsibility | ||
| 704.51 thru 704.61 | Reserved | Noted | |||
| *Division V - Aircraft equipment requirements* | |||||
| 704.62 | General requirements | ||||
| (1) | IMC condition requirement | ||||
| (2) | Multi-engine helicopter requirement | Not applicable | |||
| (3) | Night condition requirement | ||||
| 704.63 | Operation of aircraft in icing condition | ||||
| (1) | Aircraft equipment | ||||
| (2) | Illumination/detection of ice | ||||
| 704.64 | Airborne thunderstorm detection and weather radar equipment | ||||
| 704.65 | Additional equipment for single-pilot operations | Not applicable | |||
| 704.66 | Protective breathing equipment | ||||
| 704.67 | First aid oxygen | ||||
| 704.68 | Shoulder harness | ||||
| 704.69 thru 704.82 | Reserved | Noted | |||
| *Division Vi - emergency equipment* | |||||
| 704.83 | Hand-held fire extinguisher | ||||
| 704.84 | Equipment standards and inspection | -- | Operator responsibility | ||
| 704.85 thru 704.105 | Reserved | Noted | |||
| *Division Vii - Personnel requirements* | |||||
| 704.106 | Minimum crew | Operator responsibility | |||
| 704.107 | Designation of pilot-in-command and second-in-command | -- | Operator responsibility | ||
| 704.108 | Flight crew member qualifications | -- | Operator responsibility | ||
| 704.109 | Qualifications of operational control personnel | -- | Operator responsibility | ||
| 704.110 | Check authority | -- | Operator responsibility | ||
| 704.111 | Validity period | -- | Operator responsibility | ||
| 704.112 thru 704.114 | Reserved | Noted | |||
| *Division Viii - training* | |||||
| 704.115 | Training program | -- | Operator responsibility | ||
| 704.116 | Conditional approval of training program | -- | Operator responsibility | ||
| 704.117 | Training and qualification records | -- | Operator responsibility | ||
| 704.118 and 704.119 | Reserved | Noted | |||
| *Division ix - manuals* | |||||
| 704.120 | Requirements related to company operations manual | -- | Operator responsibility | ||
| 704.121 | Contents of company operations manual | -- | Operator responsibility | ||
| 704.122 | Distribution of company operations manual | -- | Operator responsibility | ||
| 704.123 | Aircraft operating manual | Development and approval of Aircraft Operating Manual is operator’s responsibility. | |||
| 704.124 | Standard operating procedures | Development and approval of Standard Operating Procedures (separately or as part of Aircraft Operating Manual) is operator’s responsibility. | |||
| 704.125 thru 704.127 | Reserved | Noted | |||