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GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-17
31 May 2000
13. Electrical Load............................................................................... Reduce as situation permits
14. Bleed Air Switches .............................................................................................................OFF
15. Symbol Generators 2 and 3 ................................................................................ALTERNATE
16. EICAS Display............................................................................TOP COMPACT (If Desired)
When within Airstart envelope (Below 25,000 ft., 200-324 KCAS):
17. Fire Handles.......................................................................................................................... IN
18. Crossflow/Boost Pumps.......................................................................... OPEN/One Main-ON
19. Airstart Ignition ................................................................................................................... ON
20. Engine RPM (HP and LP) .................................................................................. INDICATING
21. HP Fuel Cocks (one at a time) .................................................... OPEN (Check for Fuel Flow)
NOTE: Use clock to time measurements of thirty (30) second airstart attempts and engine drain
time cycles.
22. Engine Parameters ................................................................................................MONITOR
CAUTION: ENGINE DAMAGE MAY RESULT IF RPM IS NOT ALLOWED TO
STABILIZE AT IDLE BEFORE ADVANCING POWER LEVERS.
If engine does not relight within thirty (30) seconds or if engine does not reach idle:
23. HP Fuel Cocks .................................................................................................................SHUT
24. Airstart Ignition ..................................................................................................................OFF
Allow engines to drain for thirty (30) seconds.
25. Begin Airstart procedure with Step 17.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-18 FAA APPROVED
31 May 2000
After relight of one or both engines occurs:
26. Electrical Power...............................................................................................AS REQUIRED
27. Bleed Air Switches/Isolation Valve.................................................................AS REQUIRED
NOTE: With both engines running the configuration is Both Bleeds – ON, Both ECS Packs –
ON, and ISOL VLV – CLOSED.
With one engine running the configuration is Operating Engine Bleed – ON, Both ECS
Packs – ON, and ISOL VLV – OPEN.
28. Pressurization .....................................................................................RESET AS REQUIRED
29. “E” Batts ...........................................................................................................................ARM
30. Airstart Ignition...................................................................................................................OFF
31. Cowl/Wing Anti-Ice ........................................................................................AS REQUIRED
32. Windshield Heat ............................................................................................CYCLE OFF/ON
33. Fuel Balance.............................................................................................................MONITOR
34. APU .....................................................................................................START-IF REQUIRED
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-19
31 May 2000
4-09-50: Dual Engine Out Approach and Landing Procedure:
1. APU (if available) ........................................................................... START (one attempt only)
2. Starting Point ...............................................................................ESTABLISH 5,000 FT AGL
OVER LANDING AREA
3. Flaps................................................................................. 10° (EXTEND WITH AUX PUMP)
4. Airspeed ..............................................................................VREF FOR 10° FLAPS +20 KCAS
5. 180° Position...................................................................................... BANK TO ESTABLISH
A 25 degree bank will bring the airplane to a 180 degree position at about 2,500 ft AGL.
6. Flaps................................................................................. 20° (EXTEND WITH AUX PUMP)
　
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