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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
GIV-SP 31 May 2000
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 2000 GIV-SP
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
affected panel and avoid flight into
known icing conditions. With a
crack in either the main structural
windshield ply, a reduction of
cabin pressure differential to 7.5
psi is recommended for the
remainder of the flight. If flight
conditions permit descend to
35,000 feet or below and maintain
a cabin altitude of 8000 feet or less
at the reduced differential pressure
of 7.5 psi. It is recommend that the
pilot adjacent to the cracked area
wear an eye protection device such
as smoke goggles.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
B-8 FAA APPROVED
GIV-SP 31 May 2000
ATA SYSTEM OR UNIT NO.
INST
NO
REQD
REQUIREMENTS FOR FLIGHT
57 - Wings
57 -1 Wing Vortex Generators 100 0 With any Vortex Generators
missing the maximum
recommended speed is Mach 0.80.
At speeds above Mach 0.80 some
aileron buffet may be felt but is
considered normal.
57 -2 Winglets 2 0 One or both may be missing.
Increase VR to V2 speed. Increase
takeoff distance by 1,000 feet.
Cruise performance must be
reduced by: 3.7% with one
missing; 7.5 % with both missing.
Maximum recommended airspeed
is M.80.
Increase VREF by 5 knots. Increase
landing distance by 1,000 feet.
Ferry permit is required.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
FAA APPROVED B-9
31 May 2000 GIV-SP
ATA SYSTEM OR UNIT NO.
INST
NO.
REQD
REQUIREMENTS FOR FLIGHT
78 – Engine Exhaust
78 -1 Door Flap Seals 2 0 One or both may be missing for a
period not to exceed 90 days.
78 -2 Sugar Scoop Flap Seals 2 0 One or both may be missing for a
period not to exceed 90 days.
78 -3 Boot Seals 2 0 One or both may be missing for a
period not to exceed 90 days.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
CONFIGURATION
DEVIATION LIST
APPENDIX B
B-10 FAA APPROVED
GIV-SP 31 May 2000
THIS PAGE INTENTIONALLY LEFT BLANK.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
BRAKE KINETIC ENERGY &
CARBON BRAKE COOLING
APPENDIX C
FAA APPROVED C-1
31 May 2000 GIV-SP
BRAKE KINETIC ENERGY (BKE) AND CARBON BRAKE COOLING
For airplanes SN 1000 thru 1213 with ASC 190 / ASC 266 and SN 1214 and Subs.
INTRODUCTION
To stop an airplane in motion, the brakes along with other drag forces, must be capable of
dissipating the airplane’s kinetic energy. The energy dissipated by the brakes accounts for most
of this energy and generates heat, which is absorbed by the brakes and surrounding equipment.
High levels of heat will cause the fusible plugs in the wheels to release tire pressure to avoid
equipment failure. Excessive heat can result in fire and equipment damage.
This section contains a discussion of how to estimate Brake Kinetic Energy (BKE) and how to
determine brake cooling times required for safe operations. The purpose of this discussion is to
　
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