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71. Elevator Trim................. CHECK/SET (See Table for Recommended Elevator Trim Setting)
72. Stall Barrier......................................................................................................................... ON
73. Anti-Skid............................................................................................................................. ON
74. Ground Spoilers ..................................................................................................................OFF
75. T/REV EMER STOW Switch ............................................................................................OFF
76. Nutcracker Test Switch...................................................................................GUARD DOWN
CAUTION: DO NOT DEPRESS NUTCRACKER TEST SWITCH WHILE THE AIRPLANE
IS ON THE GROUND. DEPRESSING THE SWITCH SIMULATES THE INFLIGHT
CONDITION WHICH AFFECTS AIRPLANE SYSTEMS INCLUDING
MOMENTARY UNLOCKING OF THE LANDING GEAR HANDLE DOWN
LOCK SOLENOID.
77. Parking Brake ...................................................................................................................... ON
78. Brake Accumulator Pressure ...................................................................................... 3000 PSI
79. Flight Power Shutoff Handle .........................................................................................DOWN
80. Radios ................................................................................................................................SET
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-20 FAA APPROVED
30 May 2002
81. TCAS/TCAS MODE/SET UP............................................................. TEST/TA-RA/ABOVE
82. E/GPWS...........................................................................................................................TEST
83. BTMS/Selector Switch ............................................................................................TEST/ALL
For airplanes with Brake Temperature Monitoring System installed.
NOTE: For SPZ 8400 equipped airplanes, BTMS is incorporated in the BRAKES System page.
No test required or selection available.
84. Rudder and Aileron Trim..............................................................................................CHECK
85. EPR/V Speeds/AOA/Radio Altimeter................................................................................SET
NOTE: The AOA indexer on the center post will operate only if an AOA value is set (boxed)
on the Display Controller.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-21
31 May 2000
Figure 2-1: Table of Recommended Elevator Trim Tab Setting
FUEL
LOADING
POUNDS
ELEVATOR TRIM TAB POSITION UNITS
29,000 11 10 9 8 7 6 5 4 3 2
28,000 11 10 9 8 7 6 5 4 3 2
27,000 11 10 9 8 7 7 6 5 4 3
26,000 12 11 10 9 8 7 6 5 4 3
25,000 12 11 10 9 8 7 6 5 4 3
24,000 12 11 10 9 8 7 6 5 4 3
23,000 12 11 10 9 8 7 6 5 4 3
22,000 12 11 10 9 8 7 6 5 4 3
21,000 12 11 10 9 8 7 6 5 4 3
20,000 12 11 10 9 8 7 6 5 4 3
19,000 12 11 10 9 8 7 6 5 4 3
18,000 12 11 10 9 8 7 6 5 4 3
17,000 12 11 10 9 8 7 6 5 3 3
16,000 12 11 10 9 8 7 6 4 3 2
15,000 12 11 10 9 8 6 5 4 3 2
14,000 12 11 10 8 7 6 5 4 3 1
13,000 12 10 9 8 7 6 5 4 2 1
12,000 11 10 9 8 7 5 4 3 2 1
11,000 11 10 9 7 6 5 4 3 1 0
10,000 11 9 8 7 6 5 3 2 1 -1
9,000 10 9 8 6 5 4 3 1 0 -2
8,000 10 8 7 6 5 3 2 1 -1 -3
7,000 9 8 7 5 4 3 1 0 -2 -4
6,000 9 7 6 5 3 2 0 -1 -2 -5
5,000 8 6 5 4 3 1 0 -2 -3 -5
4,000 7 6 5 3 2 0 -1 -3 -4 -6
3,000 7 5 4 2 1 -1 -2 -4 -5 -7
2,000 6 4 3 1 0 -2 -3 -5 -6 -8
1,000 5 3 2 0 -1 -3 -4 -6 -7 -8
36 37 38 39 40 41 42 43 44 45
ZERO FUEL CENTER OF GRAVITY - % MAC
NOTE: A minus sign (-) indicates nose down trim.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-22 FAA APPROVED
30 May 2002
2-03-20: Starting Engines:
1. Start Page ............................................................................................................... SELECTED
NOTE: See cold start procedure when oil temperature is minus 10°C or less.
2. HP Fuel Cocks .................................................................................................................SHUT
3. Power Levers .................................................................................................................... IDLE
4. Gust Lock...........................................................................................................................OFF
　
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