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PFD and replaced by an electronic slip indication just below the roll pointer on
each PFD ADI.
(2) If flight instruments are inoperative, check AOA indicator. If a high angle-ofattack
is indicated, briefly pressing the respective AOA test button will slew the
AOA probe to lower angle-of-attack returning flight instruments to normal
operation.
NOTE: If taxi operations are conducted with engine bleed air as source for ECS pack during
warm weather operations it is recommended that one throttle be advanced above idle
with ISOL VLV OPEN and opposite engine bleed air OFF to provide cooling air flow
to the cabin.
5. Thrust Reverser Operational Check (first flight of the day) .................................COMPLETE
6. Thrust Reverser Lights............................................................................CHECK (every flight)
a) REV ARM ..................................................................................................................... ON
b) REV Unlock/Deploy....................................................................................................OUT
NOTE: If either or both Unlock or Deploy lights are ON, maintenance is required before flight.
7. Fuel Temperature ..........................................................................................................CHECK
8. Crew Briefing/EPR/V Speeds....................................................................................BRIEFED
9. Trim Settings (3) .................................................................................................................SET
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-28 FAA APPROVED
11 October 2001
10. 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.
11. Flaps/Stabilizer ................................................................................................ SET TAKEOFF
12. Engine Instruments .......................................................................................................CHECK
13. Hydraulic Pressure ............................................................................ CHECK (3000-3000-0-0)
14. APU..................................................................................................................... AS DESIRED
15. Flight Guidance Panel......................................................................................................... SET
16. Warn Inhibit ......................................................................................................................... ON
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-29
31 May 2000
2-04-30: Line Up:
1. Engine Bleed Air Switches .................................................................................................. ON
2. APU AIR/ISOL VLV......................................................................................... OFF/CLOSED
3. Exterior Lights .................................................................................................AS REQUIRED
4. Ground Spoilers ...........................................................................................................ARMED
5. Transponder/TCAS........................................................................................................ON/ON
6. Crew Alerting System...................................................................................................CHECK
7. Air Start Ignition..............................................................................................AS REQUIRED
NOTE: It is recommended that Air Start Ignition be selected ON for takeoff on a runway with
standing water, slush, or snow.
8. Autothrottle................................................................................ ARM/ENGAGED (if desired)
NOTE: Autothrottle will annunciate “HOLD” at approximately 60 knots and will maintain
power lever "HOLD" unless selected to another mode after attaining 400 ft. AGL.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-30 FAA APPROVED
30 May 2002
2-05-00: INFLIGHT PROCEDURES
2-05-10: Climb:
1. Landing Gear.........................................................................................................................UP
2. Flaps.....................................................................................................................................UP
3. Flight Guidance Panel......................................................................................................... SET
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(38)
