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limitations specified in the AFM, as amended by this appendix.
3. The associated limitations must be listed on a placard affixed in the cockpit on the pilot’s
instrument panel in clear view of the pilot.
4. The pilot shall be notified of each operation with a missing part(s) by listing the missing
part(s) in the flight or dispatch release.
5. No more than three (3) parts evaluated as having negligible penalties may be missing for
takeoff without taking a further performance penalty at the rate of the threshold weight
reduction per each additional negligible item.
6. Takeoff performance penalties are applicable to takeoff gross weights that are limited by
structural limit, field length, second segment climb, final segment climb, or takeoff flight
path.
7. Landing performance penalties are applicable to landing gross weights that are limited by
structural limit, landing field length, landing climb, or approach climb.
8. En route performance penalties are applicable to operations that are limited by one engine
inoperative en route climb performance.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
FAA APPROVED B-3
31 May 2001
INDEX Page
ATA - 21 Air Conditioning B-4
21 - 1 Baggage Door Seal
21 - 2 Main Entrance Door Seal
ATA - 23 Communications B-5
23 - 1 Static Dischargers
23 - 2 Wing Trailing Edge Static Dischargers
23 - 3 Elevator Static Dischargers
ATA - 53 Fuselage B-6
53 - 1 Canopy Boundary Layer Energizers (BLE’s)
53 - 2 Safety Relief Valve Vortex Generators
53 - 3 RACAL Satphone Antenna Vortex Generators
ATA - 56 Windows B-7
56 - 1 Windshields
ATA - 57 Wings B-8
57 - 1 Vortex Generators
57 - 2 Winglets
ATA - 78 Engine Exhaust B-9
78 - 1 Door Flap Seals
78 - 2 Sugar Scoop Flap Seals
78 - 3 Boot Seals
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
B-4 FAA APPROVED
31 May 2001
ATA SYSTEM OR UNIT NO.
INST
NO.
REQD
REQUIREMENTS FOR FLIGHT
21 - Air Conditioning
21 -1 Baggage Door Seal 1 0 Aircraft must be operated in an
unpressurized configuration below
10,000 feet MSL.
21 -2 Main Entrance Door Seal 1 0 Aircraft must be operated in an
unpressurized configuration below
10,000 feet MSL.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
FAA APPROVED B-5
31 May 2001
ATA SYSTEM OR UNIT NO.
INST
NO.
REQD
REQUIREMENTS FOR FLIGHT
23 - Communications
23 -1 Static Dischargers
With RACAL or other tail
mounted satphone antenna
installed
17
16
0
0
None required where ADF, Loran
or HF communications are not
required.
None required where ADF, Loran
or HF communications are not
required.
23
For flights where ADF,
Loran or HF
communications are
required, only wing and
elevator static dischargers
may be missing as noted:
-2 Wing Trailing Edge
Static Dischargers
6 4 Two (2) may be missing, however
only one (1) may be missing from
each wing.
23 -3 Elevator Static
Dischargers
6 4 Two (2) may be missing, however
only one (1) may be missing from
each elevator.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
B-6 FAA APPROVED
31 May 2001
ATA SYSTEM OR UNIT NO.
INST
NO.
REQD
REQUIREMENTS FOR FLIGHT
53 - Fuselage
53 -1 Canopy Boundary
Layer Energizers
(BLE’s)
15 0
53 -2 Safety Relief
Valve Vortex
Generators (if
installed)
2 0
53 -3 RACAL or other tailmounted
Satphone
Antenna Vortex
Generators (if installed)
8 0
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
FAA APPROVED B-7
31 May 2001
ATA SYSTEM OR UNIT NO.
INST
NO.
REQD
REQUIREMENTS FOR FLIGHT
56 - Windows
56 -1 Windshields 2 2 With the outer windshield
heating/protective ply cracked, one
takeoff to a base of maintenance is
permitted.
With either main structural
windshield ply cracked, a takeoff is
permitted for ferry purposes only.
NOTE: If a cracked windshield
occurs in-flight, continued flight
to destination is permitted. If the
crack is in the outer windshield
heating/protective ply, turn
windshield heat OFF on the
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 2(135)
