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24. Hydraulic Pressure .................................................................................................. CHECKED
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-25
31 May 2001
2-04-00: BEFORE TAKEOFF PROCEDURES
2-04-10: After Starting Engines:
1. Start Master.........................................................................................................................OFF
2. Electrical Power................................................................................................................... ON
3. External Electrical Power/Air..........................................................OFF/CARTS REMOVED
4. Auxiliary Electrical Power/Air/Engine Bleed Air .............................................. AS DESIRED
NOTE: Only one source of Bleed Air, either APU or engines should be selected after engines
are started. This is to prevent thermal transients on the APU or possible damage to the
APU when the power levers are moved from idle. With engines as source of bleed air,
ensure ISOL VLV is CLOSED.
5. Battery Ammeters .........................................................................................................CHECK
6. ESS DC Bus Power Source ..........................................AUTO/LEFT MAIN ILLUMINATED
CAUTION: DO NOT DISPATCH WITH ESS DC POWERED BY BATTERIES.
7. Emergency Power .............................................................................................................ARM
8. Doors.............................................................................................................................CLOSE
NOTE: Check that the orange dot position indicators on each of the six locking pins is visible.
9. Anti-Ice Heaters ................................................................................................................... ON
For airplanes SN 1096 and subs. (5), and airplanes SN 1000 thru 1095 (4)
10. Cowl/Wing Anti-Ice ......................................................................... CHECK/AS REQUIRED
NOTE: Check or select cowl/wing anti-ice ON using engine bleed air only to prevent excessive
APU EGT.
11. Pressurization Control .............................................................................AUTO/FLIGHT/SET
12. Fuel Boost Pumps/Crossflow Valve....................................................................ON/CLOSED
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-26 FAA APPROVED
30 May 2002
13. Nose Wheel Steering ..........................................................................................................OFF
14. Ground Spoilers ............................................................................................................CHECK
NOTE: Check first flight of the day.
15. Stall Barrier.......................................................................................................................TEST
NOTE: Check first flight of day. If flight time for the day exceeds 8 hours, a second stall
barrier check is required prior to the second flight of the day.
16. Flight Controls/Rudder Torque Limiter........................................................................CHECK
17. Yaw Damper........................................................................................................................ ON
18. Nose Wheel Steering ........................................................................................................... ON
19. Pedal Steering Disconnect Switch ...............................................................ON/LIGHTS OUT
20. Auxiliary Hydraulic Pump...........................................................................................ARMED
21. Brake Test Switch (BITE)/Anti-Skid Test Switch.......................... PRESS, THEN RELEASE
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-27
31 May 2001
2-04-20: Taxi/Before Takeoff:
1. Exterior Lights .................................................................................................AS REQUIRED
NOTE: Limit ground operation of landing lights to five (5) minutes.
2. Cowl/Wing Anti-ice.........................................................................................AS REQUIRED
NOTE: Select cowl/wing anti-ice ON using engine bleed air only.
3. Brakes ...........................................................................................................................CHECK
4. Slip Indicators/Compasses/Flight Instruments..............................................................CHECK
NOTE: (1) For SPZ 8400 equipped airplanes, the external slip indicator is removed from the
　
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