Attachment A - Bombardier Challenger Acquisition Requirements_2019-10-31.pdf

Attachment A: Bombardier Challenger Requirements

1 Challenger Aircraft Designations The FAA is assessing three used Challenger options to meet requirements:

CL-605: Challenger 605 aircraft without Avionics Upgrade Service Bulletins (SB). Serial numbers 5701 to 5990.

CL-605(SB): Challenger 605 aircraft with one to all of the Avionics Upgrade SBs installed.

CL-650: All the Avionics Upgrade SBs. Newly manufactured via block point change on the assembly line and denoted as serial number 6050 and subsequent.

The age of the aircraft and flight hours will also be considered and weighed against the avionics equipment installed.

The Avionics Upgrade SBs are estimated between $1.2 and $2 million per CL-605 depending on the number of SB to be installed. The effort is estimated to take 45-60 days to install. Section 3 of this document contains a list of all Service Bulletins installed on existing FAA Challenger 605 aircraft. Any acquired CL-605 will need to be updated with all of these Service Bulletins.

2 Challenger Requirements The Challenger 605/650 aircraft must have the following capabilities:

Propulsion: Turbojet

Min Cruise: 0.77M

Minimum Range: 3,500NM

Min Service Ceiling: FL410

Cabin Configuration: The FAA does not require aircraft with highly customized interiors.

Flight Deck Avionics: Rockwell Collins Pro Line 21 Advanced Package

Additional Avionics Requirements:

• Dual Channel Iridium Satellite System o 605-23-004 R5; 605-23-004 R6; 605-23-011 R3

• FANS 1A/+ Link 2000 + o 605-23-008

• Triple Honeywell Inertial Reference Unit (IRU) o 605-34-004 R3

• Triple Flight Management System (FMC-6200) with V-Speed database o 605-34-007 R2

• Third VHF Comm. Radio o 605-23-001 R1

• Second Radio Altimeter o 605-34-005 R2; 605-34-029

• 3D MAP/Long Range Cruise (LRC) o 605-34-002; 605-34-032 R1

• Cockpit Defuel/Refuel Panel o 605-11-002

• Honeywell Mark V EGPWS with Runway Awareness Advisory System (RAAS)/Smart Runway o 605-34-022 R1

• ADS-B Out TCAS 7.1 o 605-34-018

• RNP Approach Certification o 605-34-021 R1

• Multi Scan Weather Radar o 605-34-023 R2

• Synthetic Vision System o 605-34-020 R3

• XM Graphical Weather Option o 605-46-003 R4

Additional Avionics Desired Options

• Provisioned for HUD/EVS (Desirable for military equipped AC)

• FMS Search Pattern Capability

3 CL-605 Service Bulletin Requirements

SB NUMBER TITLE

605-11-001 R1 Modification – Nose Landing Gear (NLG) – Towing Strap Placard Installation

605-11-002 Modification – Service Doors and Flight Compartment, Placards and Markings – Install Fuel Spillage Prevention

605-21-003 R1 Modification – Temperature Control – Prevention of Ice Formation Downstream of Air Conditioning Units (ACU) Serial No. 5701 – 5990

605-22-002 R1 Part Number verification for both YAW Damper Linear Actuators. If one of both of the YAW Damper Linear Actuator installed is Part No. 622- 9968-002

605-22-002 R1 Part B YAW Damper System – Automatic Flight Control System (AFCS) Wiring Change to Prevent Un-Commanded YAW Damper/Linear Actuator Motion After Power Supply Failure

605-23-001 R1 Modification – Very High Frequency (VHF) Communication System – Installation of the Third VHF Communication System (VHF 3) Serial No. 5701 – 6999

605-23-002 R1 Modification – Datalink System – Installation of the Datalink System Serial No. 5701 – 5990

605-23-002 R4 Modification – Datalink System – Installation of the Datalink System Serial No. 5701 – 5990

POST SB 605−34−019

605-23-004 R5 Install the Dual-Channel Iridium Communication System Antenna 605-23-004 R6 Install the Dual-Channel Iridium Communication System Antenna

605-23-008 Future Air Navigation System (FANS)

605-23-011 R3 Satellite Communication System (SATCOM), Installation of Iridium Satellite Communication System

605-24-003 Modification – Emergency AC Generation System – Replace the Air Driven Generator (ADG) Generator Control Unit (GCU) Serial No. 5701 – 5856

605-24-007

Special Check/Rework – Integrated Drive Generator (IDG) and Hydraulic Systems No.1 and No. 2 – Aft Equipment Bay Right IDG Power Cable and Adjacent Hydraulic Lines Support Brackets Serial No. 5701 – 5990

605-24-009 R1

Special Check/Rework – Integrated Drive Generator (IDG) and Electrical Harness – Possible Fouling between the Right Engine IDG Power Cable and the Fuel Flow Meter Serial No. 5701 – 5875, 5877, 5878, 5880, 5882, 5889 and 5895

605-25-001 Modification – Insulation – Installation of the Entry Headliner Structure, the Cabin Primary Insulation Blankets and the Top Cover Serial No. 5718 – 5990

605-27-001 R1 Modification – Stall Protection System – Introduction of a New Configuration Angle-of-Attack Sensor Serial No. 5701 – 5827

605-27-002 R2

Modification – Horizontal Stabilizer Trim-Actuating System – Replace the Horizontal Stabilizer Trim Actuator (HSTA) Part Number 604- 92305-3 or -5 (8454-1 or 8454-2) with Part Number 604-92305-7 (8454- 3) Serial No. 5701 – 5907

605-27-003 Special Check/Modification – Flaps – Relocation of Inboard Stop Brackets Serial No. 5701 – 5857

605-27-005 Modification – Horizontal Stabilizer Trim-Actuating System (HSTA) – Serialization of the Actuator Pins and Trunnions Serial No. 5701 – 5926

605-27-006

Modification – Flap Position and Indicating System – Installation for the Flap On-Board Recorder (FOBR) Serial No. 5701 – 5990 +5.62 pounds

605-28-006 Special Check/Modification – Motive Flow System – Collector Tank Ejector Line inside of the Auxiliary Center Fuel Tanks Serial No. 5701 – 5846, 5848 to 5865, 5867 – 5872, and 5875

605-28-007 R2 Fuel Quantity Indicating System-Electrical Harness Installation Inside the Main and Center Fuel Tanks

605-28-009

Special Check/Modification – Auxiliary Power Unit (APU) Fuel-Feed System – Possible Chafing of the APU Negative-G Fuel-Feed Drain Line Serial No. 5701 – 5970

605-28-010

Special Check – Standby Fuel Feed System and Auxiliary Power Unit (APU) Fuel Feed System – Engine and APU Electrical Fuel Pump Cartridge/Canister Fuel Leakage Serial No. 5701 – 5995

605-28-010

Make sure that fuel quantity in each main tank is minimum 500 lbs. and that you continuously monitor the RHS and LHS main tanks fuel quantity on the EICAS while operating any boost pump to prevent the pump from running dry.

605-31-001 R1 Modification – Flight Data System – Installation of the FAR 135 Enhancement Package Serial No. 5701 – 6999

605-31-003

Modification – Electronic Flight Display (EFD) System – Upgrade the Adaptive Flight Displays (AFD) to “–204” and Incorporation of Rockwell Collins Service Bulletins for Reliability Improvements Serial No. 5701 – 5799, 5801 – 5803, 5805 – 5810, and 5812 – 5824

605-31-004 Modification – Electronic Flight Display (EFD) System– Installation of Insulation Blankets to Control Condensation Serial No. 5701 – 5990

605-33-005 R2 Floodlight Panel – Cockpit Floodlight Gasket Installation to Prevent Water Ingress

605-34-001 R3

Modification – Flight Management System – Installation of the Third Flight Management System (FMS) Serial No. 5701 – 5990

POST SB 605−34−019

605-34-002 Modification – Flight Management System (FMS) – Installation of the 3D Map and Long-Range Cruise (LRC) Serial No. 5701 – 5990

605-34-003 Modification – Flight Management System (FMS) – Installation of Search Patterns Serial No. 5701 – 5990

605-34-004 R3 Modification – Inertial Reference System – Installation of the Third Inertial Reference (IRS 3) Serial No. 5701 – 6999

605-34-005 R2 Modification – Radio Altimeter System – Installation of the Second Radio Altimeter Serial No. 5701 – 5990

605-34-005 R9

For action applicable to aircraft on which the Basic Issue Revision 01, Revision 02, Revision 03, Revision 04, Revision 05, Revision 06, Revision 07 or Revision 08 of this Service Bulletin was done, refer to the retroactive action box on Page 1 of this Service Bulletin.

605-34-007 R2 Modification – Flight Management System – Installation of the FAA V- Speed Database

POST SB 605−34−019

605-34-009 R6 Part B Flight Management System (FMS) – Installation of the DBU 5000

605-34-013 R1

Modification – Air Traffic Control Transponder System (ATC) – Incorporation of ATC Transponder Part No.622-9210-409 with Automatic Dependent Surveillance Broadcast (ADS-B) Out Capability Serial No. 5701 – 6049

605-34-018 Modification – Traffic Alert and Collision Avoidance System (TCAS) – “Change 7.1” Upgrade to Meet the New Regulation Requirement Serial No. 5701 – 5895

605-34-019 R2 This is the foundational Service Bulletin defining if the Advanced Avionics package is installed.

605-34-020 R3 Synthetic Vision System (SVS) – Installation of the Synthetic Vision System

605-34-021 R1 Flight Management System (FMS) - Introduction of Required Navigation Performance (RNP) AR 0.3 Capability

605-34-022 R1 PART

A

Terrain Awareness Warning System (TAWS), Introduction of The Runway Awareness and Advisory System (RAAS)

605-34-023 R2 Weather Radar System - Introduction of Multi-Scan Weather Radar

605-34-027 R2

Modification – Pitot-Static and Temperature Sensing System – Replacement of Pitot-Static Visual Drain Bottles to larger Capacity Bottles Serial No. 5701 – 5918

605-34-029 Modification – Radio Altimeter System – Protective Cover Installation Serial No. 5701 – 5976

605-34-030 R1 Automatic Dependent Surveillance – Broadcast (ADS-B) out V2

605-34-032 R1 Flight Management System (FMS) – Installation of The Long Range Cruise (LRC)

605-35-001

Special Check/Modification – Oxygen Supply System – Inspection and Replacement of Oxygen Cylinder and Regulator Assembly (CRA) and Regulator Assemblies with Specific Serial Numbers Serial No. 5701 – 5802, 5804 – 5808, 5810 – 5816, 5819, 5822 – 5823

605-35-001 R1 Oxygen Supply System – Inspection and Replacement of Oxygen Cylinder and Regulator Assembly

605-35-002 Special Check/Modification – Crew Oxygen System – Verification and Replacement of Crew Oxygen Mask Inflatable Harness Serial No. 5701 – 5834

605-36-001 R1 Modification – Bleed-Air Leak Detection System – 10th Stage Bleed-Air Pressure Transducers Relocation Serial No. 5701 – 5849

605-46-003 R4

Modification – Flight Deck Information Systems – Installation of the XM Graphical Weather Option Serial No. 5701 –599 POST SB 605−34−019 Rework

605-49-002 Special Check/Modification – Auxiliary Power Unit (APU) Engine Oil System – Replacement of the APU Oil Filter Element Serial No. 5701 – 5836

605-52-001 R3 Special Check/Modification – Passenger Door – Epoxy Ramp Removal and Corrosion Prevention Serial No. 5701 – 5868

605-52-003 Modification - Passenger Door - Improve the Support Leg Mechanism Serial No.5701 – 5990

605-53-004 Modification – Floors – Inspection of Seat Tracks for Corrosion Serial No. 5701 – 5885

605-53-004 R1 Floors – Inspection of Seat Tracks for Corrosion 605-53-004 R1 Part C Part C: Inspection of Seat Track at All Other Locations

A605-57-004 R3 Inboard Flap Hinge Box – Forward Attachment Fittings Fasteners

605-57-005 Special Check – Flap Hinge Box – Forward Lugs Edge to Edge Distance Serial No. 5701 – 5953

605-57-005 R1 Flap Hinge Box – Forward Lugs Edge to Edge Distance

605-71-002 Modification – Core Cowl Doors – Installation of a Hold Open Rod Bracket to Prevent Malfunction of the L/H Engine Fuel Control Unit Serial No. 5701 – 5884

605-79-001 Modification – Engine Oil Indication Board – Add an On/Off Power Switch for the Engine Oil Indicating Board in Junction Box JB5 Serial No. 5815 and 5817