APPENDIX 1
CONFIGURATION
DEVIATION LIST
AIRPLANE
F
LIGHT
AP1-00 ANAC APPROVED
Page 4 code 01 REVISION 14
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Takeoff performance penalties should be applied to the takeoff weights
that are limited by performance considerations (i.e., takeoff field length,
first, second, or final segment climb, or takeoff flight path).
If the performance-limited takeoff weight is greater than the maximum
certified takeoff weight, the takeoff performance penalties should be
applied to the maximum certified takeoff weight to ensure compliance
with the noise requirements.
Landing performance penalties should be applied to the landing
weights that are limited by performance considerations (i.e., landing
field length, landing climb, or approach climb). If the performance-
limited landing weight is greater than the maximum certified landing
weight, the landing performance penalties should be applied to the
maximum certified landing weight to ensure compliance with the noise
requirements.
En route performance penalties apply only to operations that are
limited by the one-engine inoperative en route climb performance.
Refer to the Aircraft Maintenance Manual TASK 51-22-01-910-801A
for speed tape application, inspection procedure, and replacement
instructions information. The use of speed tape is time limited to 120
days.
If the CDL item refers to a MMEL item, the MMEL conditions,
limitations and repair interval must be applied.
COMPONENT LOCATION
The numbering and designation of each system in this Appendix is
b
ased on ATA Spec. 2200. The parts within each system are identified
by its functional description and, when necessary, by door or panel
identification. See Maintenance Manual, Chapter 06, for panel
identification.
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