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ENROUTE CLIMB
–20 kg / seal –45 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.2% / seal +0.2% / seal
APPENDIX 1
Configuration Deviation List
08−01−57−1
REV 66, Feb 01/07
SYSTEM 57 WINGS
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
57−51 Bute Door Seals – Outboard
Flap
Item C
6 One or any combination of bute door seals
may be missing from the outboard flaps
provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–7 kg / seal –15 lb / seal
LANDING WEIGHT
–5 kg / seal –10 lb / seal
ENROUTE CLIMB
–11 kg / seal –25 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.1% / seal +0.1% / seal
APPENDIX 1
Configuration Deviation List
08−01−57−2
REV 66, Feb 01/07
SYSTEM 57 WINGS
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_012
APPENDIX 1
Configuration Deviation List
08−01−57−3
REV 66, Feb 01/07
SYSTEM 57 WINGS
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
57−53 Inboard Flaps – Inboard Seals
Item D
2 One or both seals between inboard flaps
and fuselage fairing may be missing
provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–39 kg / seal –85 lb / seal
LANDING WEIGHT
–29 kg / seal –65 lb / seal
ENROUTE CLIMB
–70 kg / seal –155 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.7% / seal +0.7% / seal
57−53 Inboard Flaps – Outboard Seals
Item D
2 One or both seals between inboard flaps
and wing structure may be missing
provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–36 kg / seal –80 lb / seal
LANDING WEIGHT
–27 kg / seal –60 lb / seal
ENROUTE CLIMB
–68 kg / seal –150 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.65% / seal +0.65% / seal
APPENDIX 1
Configuration Deviation List
08−01−57−4
REV 66, Feb 01/07
SYSTEM 57 WINGS
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
57−55 Outboard Flaps – Inboard Seals
Item E
2 One or both seals between outboard flaps
and wing structure may be missing
provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–30 kg / seal –65 lb / seal
LANDING WEIGHT
–23 kg / seal –50 lb / seal
ENROUTE CLIMB
–57 kg / seal –125 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.55% / seal +0.55% / seal
57−55 Outboard Flaps – Outboard
Seals
Item E
2 One or both seals between outboard flaps
and wing structure may be missing
provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–23 kg / seal –50 lb / seal
LANDING WEIGHT
–16 kg / seal –35 lb / seal
ENROUTE CLIMB
–41 kg / seal –90 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.4% / seal +0.4% / seal
APPENDIX 1
Configuration Deviation List
08−01−57−5
REV 66, Feb 01/07
SYSTEM 57 WINGS
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_013
APPENDIX 1
Configuration Deviation List
08−01−57−6
REV 66, Feb 01/07
SYSTEM 57 WINGS
DOT Approved
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(107)
