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92. Air Stair Door/Seal .......................................................................................................CHECK
93. Standby Pitot Probe .....................................................................COVER REMOVE/CHECK
94. Left Angle of Attack Probe....................................................... COVER REMOVED/CHECK
Check that probe cover is removed and check probe for damage. Verify that sensing ports
are oriented in the direction of flight.
95. Door Pins/Gear Pins/Pitot Covers .............................................................................STOWED
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-9
31 May 2000
2-01-30: Interior Preflight Inspection:
1. Baggage Compartment Door ....................................................................... CHECK/SECURE
2. Baggage Door Seal Control Valve Selector......................................................NORMAL OPS
For airplanes SN 1156 and subs. and airplanes SN 1000 thru 1155 with ASC 157.
3. Windows.....................................................................................................................SECURE
4. Fuel Tank Caps ...........................................................................................................SECURE
5. SPZ-8000 Shutoff Switch (RH Radio Rack) ......................................................................OFF
For airplanes SN 1156 and subs. and airplanes SN 1000 thru 1155 with ASC 92.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-10 FAA APPROVED
31 May 2000
2-02-00: APU GROUND OPERATION
2-02-10: APU Start:
1. HP Fuel Cocks .................................................................................................................SHUT
2. Circuit Breakers ............................................................................................................CHECK
3. Standby Attitude Indicator........................................................................................... CAGED
4. EPMP Bus Switches (6)..................................................................................................AUTO
5. Battery 1 and 2 Switches...................................................................................................... ON
6. Exterior Lights .................................................................................................AS REQUIRED
7. Electric Master Auxiliary Power ........................................................................................OFF
8. APU Fire Warning........................................................................................................CHECK
9. APU Air.............................................................................................................................OFF
10. APU Master Switch ............................................................................................................. ON
11. APU Oil Pressure Low Light.......................................................................... ON (10 seconds)
For airplanes SN 1156 and subs. check the following on first start of the day:
a. APU Overspeed Test Switch ................................................................................... PRESS
b. APU RPM indicator in the Overhead Panel shows a momentary increase and its
Overspeed LED momentarily illuminates.
NOTE: The Overspeed LED will not illuminate in airplanes with ASC 374 or SN 1310 and
subs.
c. APU Oil Pressure Low Light........................................................................................OFF
d. APU Master Switch ......................................................................................................OFF
e. APU Master Switch ....................................................................................................... ON
f. APU Oil Pressure Low Light................................................................... ON (10 Seconds)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-11
30 May 2002
12. Left Main Fuel Boost Pump.................................................................... ON/MESSAGE OUT
13. APU Start Button........................................................................................................... PRESS
14. APU Start Light ......................................................................................OUT (BEFORE 60%)
15. APU Oil Pressure Low Light.............................................................OUT (Before 95% RPM)
16. RPM......................................................................................................................... 100% +3%
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(31)
