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4. Exterior Lights .................................................................................................AS REQUIRED
5. Ignition ...............................................................................................................................OFF
6. Ground Spoilers ..................................................................................................................OFF
7. BTMS/OVHT Message....................................................................................... CHECK/OUT
For airplanes with Brake Temperature Monitoring System installed.
NOTE: For SPZ 8400 equipped airplanes, BTMS display is incorporated on the BRAKES
System page.
8. Pressurization................................................................................................................CHECK
9. Engine Climb Power/Autothrottle ...........................................................SET/AS REQUIRED
10. Engine Synchronizer ........................................................................................AS REQUIRED
11. Altimeters (3) ..........................................SET & CROSS-CHECKED (at Transition Altitude)
12. APU........................................................................................SHUTDOWN prior to 30,000 ft.
NOTE: Shutdown APU prior to 30,000 ft. if not required for electrical power.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-31
11 October 2002
2-05-20: Cruise:
1. Power .......................................................................................................... SET FOR CRUISE
2. Pressurization................................................................................................................CHECK
3. Panel Sweep..........................................................................................................COMPLETE
NOTE: A panel sweep or a check for normal system operation and indication should be
accomplished at top-of-climb, top-of-descent, and at regular intervals between top-ofclimb
and top-of-descent.
4. FMS Fuel Quantity .................................................................................................... UPDATE
NOTE: Crew should perform hourly updates to the FMS fuel quantity using data from the
FQMS. On FMS PERF INIT Page 5/5, perform a delete to line select key 2L.
2-05-30: Descent:
1. Crew Briefing (VREF/Go-Around Power) ..................................................................BRIEFED
2. Pressurization.....................................................................................................................SET
CAUTION: IF ON MANUAL PRESSURE CONTROL, MONITOR CLOSELY TO ENSURE
LANDING UNPRESSURIZED WITH THE OUTFLOW VALVE FULLY OPEN.
3. Circuit Breakers ............................................................................................................CHECK
4. Fuel Boost Pumps ........................................................................................................ALL ON
5. Nosewheel Steering ............................................................................................................. ON
6. Parking Brake/Accumulator ...............................................................................OFF/3000 PSI
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-32 FAA APPROVED
30 May 2002
2-05-40: Approach - In Range:
1. Altimeters (3).............................................. SET & CROSS-CHECKED (at Transition Level)
2. Engine Synchronizer...........................................................................................................OFF
3. Flaps.................................................................................................................AS REQUIRED
4. VREF/Go-Around Power.......................................................................................... CHECKED
5. Hydraulic Pressure ........................................................................................................CHECK
6. Exterior Lights .................................................................................................AS REQUIRED
7. Auxiliary Hydraulic Pump...........................................................................................ARMED
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-33
31 May 2000
2-05-50: Before Landing:
1. Landing Gear .................................................................................................................DOWN
2. Crew Alerting System...................................................................................................CHECK
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(39)
