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07−12−01−8
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
DFM0712_002 LFL605_SAL_GS2STOP_MOD_JCR_FEB07
SUPPLEMENT 12
Steep Approaches up to 5.5 Degrees
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REV 70, Jun 08/07
Distance from Glideslope System Position on Runway to Full Stop
Figure 07−12−2
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
SUPPLEMENT 12
Steep Approaches up to 5.5 Degrees
07−12−01−10
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
General Limitations 08−01−01−1
SYSTEM
23 Communications
Static Dischargers 08−01−23−1
32 Landing Gear
Main Landing Gear Door Brush Seal 08−01−32−1
Nose Landing Gear Door Seal 08−01−32−1
33 Lights
Navigation Light Covers 08−01−33−1
Wing Inspection Light Covers 08−01−33−1
Beacon Light Covers 08−01−33−1
Exterior Emergency Light Covers 08−01−33−1
51 Structures − General
Aerodynamic Sealant 08−01−51−1
52 Doors
Main Pressure Refueling Control Panel Door 08−01−52−1
Refueling Adaptor Door 08−01−52−1
Hydraulic System Service Doors 08−01−52−1
APU Control and Ground Air Start Door 08−01−52−3
DC Ground Power Door 08−01−52−3
Water Fill Access Door 08−01−52−3
Toilet Service Compartment Door 08−01−52−3
53 Fuselage
Main Landing Gear Door Seals 08−01−53−1
Main Landing Gear Bin Brush Seals 08−01−53−1
Tail Tank Fairing Access Panels 08−01−53−1
APPENDIX 1
Table of Contents
08−01−00−1
REV 66, Feb 01/07
08−01−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
55 Stabilizers
Seals between Elevator and Horizontal Stabilizer Upper Surface 08−01−55−1
Seals between Rudder and Vertical Stabilizer 08−01−55−1
Horizontal Stabilizer Forward Rubber Seal 08−01−55−3
56 Windows
P-Static Probes. 08−01−56−1
57 Wings
Seal between Aileron Side End and Wing 08−01−57−1
Bute Door Seals – Inboard Flap 08−01−57−1
Bute Door Seals – Outboard Flap 08−01−57−2
Inboard Flaps – Inboard Seals 08−01−57−4
Inboard Flaps – Outboard Seals 08−01−57−4
Outboard Flaps – Inboard Seals 08−01−57−5
Outboard Flaps – Outboard Seals 08−01−57−5
APPENDIX 1
Table of Contents
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REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
Page
CHAPTER 8 − APPENDICES
TABLE OF CONTENTS
Page
APPENDIX 1 − CONFIGURATION DEVIATION LIST 08−01−00−1
APPENDICES
Table of Contents
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REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
APPENDICES
Table of Contents
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REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. GENERAL LIMITATIONS
This Configuration Deviation List (CDL) contains additional limitations for operation of the CL–604
Challenger without certain secondary airframe and/or nacelle parts as listed herein. The
Limitations in the Airplane Flight Manual are applicable except as amended in this appendix.
The associated limitations must be listed on a placard affixed in the flight compartment on the
instrument panel in clear view of both pilots.
The pilot in command will be notified of each operation with a missing part(s) by listing the
missing part(s) in the flight or dispatch release.
The operator will list in the airplane logbook an appropriate notation covering the missing part(s)
on each flight.
If an additional part is lost in flight, the airplane may not depart the airport at which it landed
following this event until it again complies with the limitations of this appendix. This, of course,
does not preclude the issuance of a ferry permit to allow the airplane to be flown to a point where
　
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