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4. V2 Speed ..................................................................MAINTAIN TO 1500 FT AGL
NOTE:
If engine failure should occur after passing V2on
takeoff, it is recommended that the speed at the time
of engine failure (up to V2+10 knots) be maintained. A
speed of V2+10 knots in a single engine takeoff
configuration will produce the maximum climb gradient
available.
5. Flaps ........................................................................UP WHEN VFSIS ATTAINED.
Maintain speed for adequate stall margin.
6. Power ............................................................MAXIMUM CONTINUOUS POWER
7. ENGINE FAILURE / SHUTDOWN IN FLIGHT Checklist..................COMPLETE
See Section 05-10-10, Engine Failure / Shutdown In Flight.
05-09-40: Dual Engine Flameout
IF FLAMEOUT IS THE RESULT OF VOLCANIC ASH ENCOUNTER, AN IMMEDIATE
RELIGHT IS NOT RECOMMENDED. REVERSE COURSE TO CLEAR ASH CLOUD
AND PROCEED WITH STEP 3.
1. Power Levers .................................................................................................IDLE
2. AIR START Ignition ..........................................................................................ON
OPERATING MANUAL
05-09-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 2
October 11/02
Revision 8
3. Airspeed / Altitude .....DESCEND AT VMO/MMO TO 25,000 FT, THEN SLOW TO
210 KCAS, NOT TO EXCEED MACH LIMITATIONS
IF ENGINES FAIL TO RELIGHT:
4. CREW OXYGEN Masks / Regulators....................DON / 100% (IF REQUIRED)
5. PASSENGER OXYGEN Masks ....................................DEPLOY (IF REQUIRED)
6. Power Levers .................................................................................................IDLE
7. HP Fuel Cocks..............................................................................................SHUT
IF BELOW 28,000 FT, PROCEED TO STEP 15
8. AIR START Ignition ........................................................................................OFF
9. Battery Switches (BATT 1 / BATT 2) ................................................VERIFY ON
10. Essential AC / DC Buses ..........................................VERIFY CONFIGURATION
A. ESS AC BUS ........................................................................VERIFY E INV
B. ESS DC BUS ........................................................................VERIFY BATT
11. ELECTRIC MASTER LEFT PWR / RIGHT PWR Switches...........................OFF
12. Crossflow / Fuel Boost Pumps ..........................OPEN / ONE MAIN PUMP ON
13. Electrical Load ............................................REDUCE AS SITUATION PERMITS
14. BLEED AIR Switches......................................................................................OFF
15. Symbol Generators 2 and 3...........................................................................ALT
16. EICAS Display......................................................TOP COMPACT (IF DESIRED)
WHEN WITHIN AIRSTART ENVELOPE (BELOW 25,000 FT / 200-324 KCAS):
17. Fire Handles........................................................................................................IN
18. Crossflow / Fuel Boost Pumps ..........................OPEN / ONE MAIN PUMP ON
19. AIR START Ignition ..........................................................................................ON
20. Engine RPM (HP and LP) .................................................................INDICATING
21. HP Fuel Cocks (One at a Time) ..................OPEN (CHECK FOR FUEL FLOW)
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. AIR START Ignition ........................................................................................OFF
ALLOW ENGINES TO DRAIN FOR THIRTY (30) SECONDS, THEN:
25. Airstart Procedure.................................................................BEGIN AT STEP 17
AFTER RELIGHT OF ONE OR BOTH ENGINES OCCURS:
26. Electrical Power............................................................................AS REQUIRED
27. BLEED AIR Switches / ISOLATION Valve ..................................AS REQUIRED
WITH BOTH ENGINES RUNNING:
A. Both BLEED AIR Switches ...................................................................ON
OPERATING MANUAL
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湾流4操作手册 Gulfstream IV Operating Manual 3(94)
