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the necessary repairs or replacements can be made.
An asterisk (*) against a part indicates that only one flight is permitted to an airport when the
necessary repairs or replacements can be made. This flight must not be carried out in known or
forecast lightning conditions.
No more than one part for any one sub-system in this appendix may be missing unless
specifically designated combinations are indicated herein. Unless otherwise specified herein,
parts from different sub-systems may be missing. The performance penalties are cumulative
unless specifically designated penalties for combination of missing parts are indicated.
Where performance penalties are listed as negligible, no more than three negligible items may be
missing for take-off unless the following performance penalties are applied for each additional
negligible item:
Take-Off and Landing Weight: Reduce by 46 Kg (100 lb).
Enroute Climb Limited Weight: Reduce by 46 Kg (100 lb).
Take-off performance decrements are applicable to take-off gross weight which are limited by
structural limit, field length, first segment climb, second segment climb, final segment climb, or
take-off flight path. The actual take-off weight must not exceed the normal take-off weight limit
minus the CDL take-off weight penalty.
Enroute performance decrements are applicable to operations which are limited by enroute,
one-engine-inoperative climb performance.
Landing performance decrements are applicable to landing gross weights which are limited by
structural limit, landing field length, landing climb, or approach climb. The maximum allowable
landing weight must not exceed the normal landing weight limit minus the CDL landing weight
penalty.
The numbering and designation of systems in this appendix is based on ATA Spec. 100. The
parts within each system are identified by functional description and, when necessary, by part
numbers.
APPENDIX 1
Configuration Deviation List
08−01−01−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
APPENDIX 1
Configuration Deviation List
08−01−01−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
23−61 Static Dischargers
Items A to K (without Service
Bulletin 604–23–006
incorporated)
24
or
26*
Certain static dischargers may be
damaged or missing, as detailed in the
deviation table.
23−61 Static Dischargers
Items A to H and items L to O
(with Service Bulletin 604–23–006
incorporated)
26
or
28*
Certain static dischargers may be
damaged or missing, as detailed in the
deviation table.
DFM0801_014
Item Quantity Installed Deviation
A 1 –
B 1 –
B* 3 One may be damaged or missing.
C 1 –
D 1 –
E 2 (1 per side) –
F 4 (2 per side) One may be damaged or missing from each side.
G 2 (1 per side) –
APPENDIX 1
Configuration Deviation List
08−01−23−1
REV 71, Oct 31/07
SYSTEM 23 COMMUNICATIONS
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_002
Item Quantity Installed Deviation
H 6 (3 per side) One may be damaged or missing from each side.
I 2 (1 per side) One may be damaged or missing from each side.
Items J and K must be intact.
J 2 (1 per side) One may be damaged or missing from each side.
Items I and K must be intact.
K 2 (1 per side) One may be damaged or missing from each side.
Items I and J must be intact.
L 2 (1 per side) One may be damaged or missing from each side.
Item M and either item N or O must be intact.
M 2 (1 per side) One may be damaged or missing from each side.
Item L and either item N or O must be intact.
N 2 (1 per side) One may be damaged or missing from each side.
Item O and either item L or M must be intact.
O 2 (1 per side) One may be damaged or missing from each side.
Item N and either item L or M must be intact.
APPENDIX 1
Configuration Deviation List
08−01−23−2
REV 66, Feb 01/07
SYSTEM 23 COMMUNICATIONS
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
32−12 Main Landing Gear Door Brush
Seal
Item A
2 One or both brush seals may be missing
provided:
– the performance and structurally limited
　
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