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3. Power ....................................................................................... Go Around Thrust (if required)
4. Flaps........................................................... 20° (Once the Go Around Attitude is Established)
5. Landing Gear ......................................RETRACT (When Positive Rate of Climb is Attained)
6. Flaps................... UP (When VREF +20 is Attained, Maintain speed for adequate stall margin)
7. Power ..................................................................................................................... As Required
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-37
31 May 2000
2-06-00: AFTER LANDING PROCEDURES
2-06-10: After Landing:
1. Ignition...............................................................................................................................OFF
2. Transponder ............................................................................................................ STANDBY
3. Flaps.................................................................................................................... AS DESIRED
4. Anti-Ice and Anti-Ice Heaters .............................................................................................OFF
5. Fuel Boost Pumps......................................................................................OFF (one each side)
6. Landing Lights ....................................................................................................................OFF
7. Ground Spoilers ..................................................................................................................OFF
8. BTMS/OVHT Light............................................................................................ CHECK/OUT
For airplanes SN 1156 and subs and airplanes SN 1000 thru 1155 with ASC 167.
NOTE: (1) For SPZ 8400 equipped airplanes, BTMS display is incorporated on the BRAKES
System page.
(2) If landing required hard braking, monitor temperatures to ensure brake
temperatures have peaked and are decreasing. Note peak temperature for use in
determining turn around time and brake cooling requirements. See Appendix C
for Brake Kinetic Energy and Brake Cooling Chart data.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-38 FAA APPROVED
31 May 2000
9. APU .................................................................................................................... AS DESIRED
10. Auxiliary Power/APU Air/Engine Bleeds .......................................................... AS DESIRED
NOTE: 1. With APU Alternator selected ON and Yaw Damper selected OFF, RIGHT
Converter may be selected OFF and RIGHT engine may be shut down for taxi
operations. Refer to Section 2-08-60: Single Engine Taxi.
2. If APU air is selected ON after landing, select both Engine Bleed Air Switches
OFF. This will prevent thermal transients on the APU or possible damage to the
APU when the power levers are moved above idle.
11. Radar (BOTH) .................................................................................................................STBY
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-39
31 May 2000
2-06-20: Shutdown:
1. Parking Brake/Pressure..........................................................................................ON/3000 psi
2. Emergency Power Switch ...................................................................................................OFF
3. Radar..................................................................................................................................OFF
4. Electrical Master Left and Right Power..............................................................................OFF
5. HP Fuel Cocks .................................................................................................................SHUT
NOTE: It is required to run the engine(s) at idle for one minute before shutting down (taxi time
may be credited).
6. TGT..........................................................................................................................MONITOR
7. Radios ................................................................................................................................OFF
8. BTMS ...........................................................................................................................CHECK
For airplanes with Brake Temperature Monitoring System installed.
NOTE: For SPZ 8400 equipped airplanes, BTMS display is incorporated on the BRAKES
System page.
9. IRS’s ...................................................................................................................................OFF
　
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