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17. EGT..................................................................................................988°C Maximum (0-60%)
821°C to 732°C (60% to 100% during start (linear decrease)
732°C Maximum (Running)
CAUTION: IF APU FAILS TO COME UP TO SPEED OR START SWITCH LIGHT
REMAINS ILLUMINATED, DEPRESS OVERSPEED TEST SWITCH. IF APU
START SWITCH LIGHT STILL REMAINS ILLUMINATED, PLACE APU
MASTER SWITCH AND BATTERY SWITCHES 1 AND 2 OFF.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-12 FAA APPROVED
30 May 2002
2-02-20: APU Operation:
1. Electric Master Auxiliary Power ...........................................................................ON/CHECK
2. Battery Charger FAIL Lights .............................................................................................OUT
3. Battery Amps ........................................................................................................ CHARGING
NOTE: If no charge is indicated on battery immediately after start, battery charger failure may
be indicated.
4. L/R ECS Pack Switches....................................................................................................... ON
5. APU Air............................................................................................ON/CHECK PRESSURE
NOTE: Wait one (1) minute for EGT to stabilize before selecting APU air ON. After six (6)
seconds, verify Isolation Valve is Open. Maximum APU EGT with air ON is 680°C.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
FAA APPROVED 2-13
31 May 2000
2-02-30: APU Shutdown:
1. Electric Master Auxiliary Power ........................................................................................OFF
2. APU Overspeed Test Button..................................................................PRESS (Momentarily)
Note Overspeed Indication
3. APU Air.............................................................................................................................OFF
NOTE: APU Air Switch position should not be changed just prior to shutdown. After
shutdown, wait until RPM indicates less than 95% before changing APU Air Switch
position.
4. APU Master Switch .........................................................................OFF (RPM less than 10%)
CAUTION: CYCLING APU MASTER SWITCH DURING SHUTDOWN WHILE RPM
REMAINS ABOVE 10 PERCENT WILL CAUSE PREMATURE ECU RESET
AND LOW ENERGY RESTART RESULTING IN HIGH EGT INDICATION
AND TORCHING FROM APU TAILPIPE.
5. Fuel Boost Pumps ..........................................................................................OFF/As Required
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 2
NORMAL
PROCEDURES
2-14 FAA APPROVED
11 October 2001
2-03-00: ENGINE STARTING PROCEDURES
2-03-10: Before Starting Engines:
1. Preflight Checklists...............................................................................................COMPLETE
2. Circuit Breakers ............................................................................................................CHECK
3. EPMP Bus Switches (6)..................................................................................................AUTO
4. EPMP L/R Pwr Switches....................................................................................................OFF
5. Battery 1 and 2 Switches...................................................................................................... ON
6. Essential AC/DC Bus Volts.........................................CHECK 115VAC/400HZ/22 - 27VDC
7. Standby Electrical Power ...................................................................................................OFF
8. HP Fuel Cocks .................................................................................................................SHUT
9. Electrical Power/Air ................................ ON (See APU GROUND OPERATION Checklist)
10. Display Switches (3) ............................................................................................................ ON
11. CABIN/GALLEY/RADIO MASTER Switches.................................................................. ON
12. Display Controllers (2) ........................................................................................................ ON
For airplanes SN 1156 and subs. and airplanes SN 1000 thru 1155 with ASC 92.
13. IRS’s ..................................................................................................................................NAV
14. FMS’s .....................................................................................................................INITIALIZE
　
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