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2. Remarks and/or Exceptions
DFM0801_008
APPENDIX 1
Configuration Deviation List
08−01−53−2
REV 66, Feb 01/07
SYSTEM 53 FUSELAGE
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
55−11 Seals between Elevator and
Horizontal Stabilizer Upper
Surface
Item A
2 One or both seals between elevator and
horizontal stabilizer upper surface may be
missing provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–18 kg / seal –40 lb / seal
LANDING WEIGHT
–14 kg / seal –30 lb / seal
ENROUTE CLIMB
–34 kg / seal –75 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.35% / seal +0.35% / seal
55−31 Seals between Rudder and
Vertical Stabilizer
Item B
2 One or both seals between rudder and
vertical stabilizer may be missing provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–20 kg / seal –45 lb / seal
LANDING WEIGHT
–16 kg / seal –35 lb / seal
ENROUTE CLIMB
–36 kg / seal –80 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.35% / seal +0.35% / seal
APPENDIX 1
Configuration Deviation List
08−01−55−1
REV 66, Feb 01/07
SYSTEM 55 STABILIZERS
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_009
APPENDIX 1
Configuration Deviation List
08−01−55−2
REV 66, Feb 01/07
SYSTEM 55 STABILIZERS
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
55−32 Horizontal Stabilizer Forward
Rubber Seal
Item C
2 One or both horizontal stabilizer forward
rubber seals may be missing provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–38 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
+0.75% / seal +0.75% / seal
APPENDIX 1
Configuration Deviation List
08−01−55−3
REV 66, Feb 01/07
SYSTEM 55 STABILIZERS
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_010
APPENDIX 1
Configuration Deviation List
08−01−55−4
REV 66, Feb 01/07
SYSTEM 55 STABILIZERS
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
56−11 P-Static Probes.
Item A
10 One probe may be missing with no
performance penalty.
APPENDIX 1
Configuration Deviation List
08−01−56−1
REV 66, Feb 01/07
SYSTEM 56 WINDOWS
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_011
APPENDIX 1
Configuration Deviation List
08−01−56−2
REV 66, Feb 01/07
SYSTEM 56 WINDOWS
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
57−32 Seal between Aileron Side End
and Wing
Item A
2 One or both seals between aileron side
end and wing may be missing provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–16 kg / seal –35 lb / seal
LANDING WEIGHT
–11 kg / seal –25 lb / seal
ENROUTE CLIMB
–29 kg / seal –65 lb / seal
– the mission fuel requirements are
increased by:
FUEL CONSUMPTION
+0.3% / seal +0.3% / seal
57−51 Bute Door Seals – Inboard Flap
Item B
6 One or any combination of bute door seals
may be missing from the inboard flaps
provided:
– the performance and structurally limited
weights are reduced by:
TAKE-OFF WEIGHT
–11 kg / seal –25 lb / seal
LANDING WEIGHT
–9 kg / seal –20 lb / seal
　
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