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weights are reduced by:
TAKE-OFF WEIGHT
–23 kg / brush seal –50 lb / brush seal
LANDING WEIGHT
–16 kg / brush seal –35 lb / brush seal
ENROUTE CLIMB
–41 kg / brush seal –90 lb / brush seal
– and the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.4% / brush seal +0.4% / brush seal
32−22 Nose Landing Gear Door Seal
Item B
1 The seal of the nose landing gear door
may be missing. The effect on the
performance is negligible.
APPENDIX 1
Configuration Deviation List
08−01−32−1
REV 66, Feb 01/07
SYSTEM 32 LANDING GEAR
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. Number required for all flight conditions
SUB except as provided in column 2
SYSTEM ITEM
2. Remarks and/or Exceptions
DFM0801_003
APPENDIX 1
Configuration Deviation List
08−01−32−2
REV 66, Feb 01/07
SYSTEM 32 LANDING GEAR
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
33−42 Navigation Light Covers: ∗
− Vertical Stabilizer
Item A
1 May be missing with no performance
penalty.
− Tail Boom
Item B
1 May be missing with no performance
penalty.
33−43 Wing Inspection Light Covers ∗
Item C
2 One or two wing inspection light covers
may be missing. The effect on the
performance is negligible.
NOTE
Lights must be operative for flight in
icing conditions.
33−43 Beacon Light Covers ∗
(optional) Item D
2 One or both beacon light covers may be
missing provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–23 kg / cover –50 lb / cover
LANDING WEIGHT
–18 kg / cover –40 lb / cover
ENROUTE CLIMB
–43 kg / cover –95 lb / cover
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.4% / cover +0.4% / cover
33−51 Exterior Emergency Light
Covers ∗
Item E
4 One or any combination of exterior
emergency light covers may be missing for
daytime operations only. The effect on the
performance is negligible.
APPENDIX 1
Configuration Deviation List
08−01−33−1
REV 66, Feb 01/07
SYSTEM 33 LIGHTS
∗ Only one flight is permitted, to an airport where the necessary repairs or replacements can be made. This
flight must not be carried out in known or forecast lightning conditions.
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. Number required for all flight conditions
SUB except as provided in column 2
SYSTEM ITEM
2. Remarks and/or Exceptions
DFM0801_004
APPENDIX 1
Configuration Deviation List
08−01−33−2
REV 66, Feb 01/07
SYSTEM 33 LIGHTS
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
51−00 Aerodynamic Sealant
Item A
– Any length of aerodynamic sealant may be
missing in areas other than the wing
leading edge/winglet and zone 1 (as
defined in the CL–604 Structural Repair
Manual, section 51–14–01, Figure 1)
provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–14 kg / 10 ft –30 lb / 10 ft
LANDING WEIGHT
–11 kg / 10 ft –25 lb / 10 ft
ENROUTE CLIMB
–25 kg / 10 ft –55 lb / 10 ft
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.25% / 10 ft +0.25% / 10 ft
NOTE
If less than 10 ft are missing, apply
the correction for 10 ft.
APPENDIX 1
Configuration Deviation List
08−01−51−1
REV 66, Feb 01/07
SYSTEM 51 STRUCTURES - GENERAL
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. Number required for all flight conditions
SUB except as provided in column 2
SYSTEM ITEM
2. Remarks and/or Exceptions
DFM0801_005
APPENDIX 1
Configuration Deviation List
08−01−51−2
REV 66, Feb 01/07
SYSTEM 51 STRUCTURES - GENERAL
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
52−45 Main Pressure Refueling
Control Panel Door ∗
Item A
1 The main pressure refueling control panel
door may be missing. The effect on the
performance is negligible.
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(104)
