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52−45 Refueling Adaptor Door ∗
Item B
1 The refueling adaptor door may be missing
provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–226 kg –500 lb
LANDING WEIGHT
–171 kg –375 lb
ENROUTE CLIMB
–421 kg –930 lb
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+4.10% +4.10%
52−45 Hydraulic System Service
Doors ∗
Item C
2 One or both hydraulic system service
doors may be missing provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–31 kg / door –70 lb / door
LANDING WEIGHT
–23 kg / door –50 lb / door
ENROUTE CLIMB
–57 kg / door –125 lb / door
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.55% / door +0.55% / door
APPENDIX 1
Configuration Deviation List
08−01−52−1
REV 66, Feb 01/07
SYSTEM 52 DOORS
∗ 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_006
APPENDIX 1
Configuration Deviation List
08−01−52−2
REV 66, Feb 01/07
SYSTEM 52 DOORS
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
52−45 APU Control and Ground Air
Start Door ∗
Item D
1 The APU control and ground air start door
may be missing. The effect on the
performance is negligible.
52−45 DC Ground Power Door ∗
Item E
1 The DC ground power door may be
missing. The effect on the performance is
negligible.
52−45 Water Fill Access Door ∗
Item F
1 The water fill access door may be missing.
The effect on the performance is
negligible.
52−45 Toilet Service Compartment
Door ∗
Item G
1 The toilet service compartment door may
be missing. The effect on the performance
is negligible.
APPENDIX 1
Configuration Deviation List
08−01−52−3
REV 66, Feb 01/07
SYSTEM 52 DOORS
∗ 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_007
APPENDIX 1
Configuration Deviation List
08−01−52−4
REV 66, Feb 01/07
SYSTEM 52 DOORS
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
53−65 Main Landing Gear Door Seals
Item A
8 One or any combination of main landing
gear door seals may be missing. The
effect on the performance is negligible.
53−65 Main Landing Gear Bin Brush
Seals
Item B
6 One or any combination of brush seals
may be missing provided:
– the performance and structurally limited
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
53−66 Tail Tank Fairing Access
Panels:
− Forward Panel * Item C 1 May be missing. The effect on the
performance is negligible.
− Aft Panel * Item D 1 May be missing. The effect on the
performance is negligible.
APPENDIX 1
Configuration Deviation List
08−01−53−1
REV 66, Feb 01/07
SYSTEM 53 FUSELAGE
∗ 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
　
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