曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

21. AIR START Ignition / IGN Message...........OFF / MESSAGE NOT DISPLAYED
22. Power Lever ...................................................................................................IDLE
BEFORE ATTEMPTING ANOTHER RELIGHT:
23. Engine .................ALLOW TO DRAIN FOR AT LEAST THIRTY (30) SECONDS
THEN:
24. Relight .............................................................ATTEMPT AT LOWER ALTITUDE
OPERATING MANUAL
EXPANDED ABNORMAL / EMERGENCY PROCEDURES 05-10-00
Page 3
September 13/00
Revision 1
Airstart Envelope
Figure 1
OPERATING MANUAL
05-10-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 4
September 13/00
Revision 1
05-10-40: One (1) Engine Inoperative Landing Procedure
1. Normal BEFORE LANDING Checklist..............................................COMPLETE
See Section 03-05-50, Before Landing.
NOTE:
Leave flaps at 20° until landing is assured.
2. Approach Speed .........................................VREF (FOR 20° FLAPS) +10 KNOTS
3. Configuration ...................39° (DOWN) FLAPS WHEN LANDING IS ASSURED
NOTE:
Selecting 39° flaps at this point in the approach
assumes that the landing weight is at or below
maximum landing weight. If IMC (Instrument
Meteorological Conditions), continue the approach at
20° flaps at V REF +10 knots. Refer to the Performance
section of the Airplane Flight Manual or Chapter 13 of
the Operating Manual.
4. Airspeed ......................................................................................VREF 39° FLAPS
AFTER LANDING:
5. Operating Engine Thrust Reverser.............................................AS REQUIRED
05-10-50: One (1) Engine Inoperative Go-Around Procedure
1. Power Lever (Operating Engine) ....................................GO-AROUND POWER
2. Flaps ..................................................................................................................20°
3. Airspeed.........................................................VREF (FOR 20° FLAPS) +5 KNOTS
WHEN POSITIVE RATE OF CLIMB IS ATTAINED:
4. Landing Gear ........................................................................................RETRACT
WHEN VREF (FOR 20° FLAPS) +20 KNOTS IS ATTAINED:
5. Flaps...................................................................................................................UP
Maintain speed adequate for stall margin.
6. Power ............................................................MAXIMUM CONTINUOUS POWER
NOTE:
Final Segment Climb performance is based on setting
Maximum Continuous Power on operating engine.
OPERATING MANUAL
EXPANDED ABNORMAL / EMERGENCY PROCEDURES 05-10-00
Page 5
September 13/00
Revision 1
OPERATING MANUAL
THIS PAGE IS INTENTIONALLY LEFT BLANK.
05-10-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 6
September 13/00
ENGINE STARTING SYSTEM
05-11-10: Engine Failure To Start
Failure of the engine to start or reach idle speed may be caused by:
• No engine rotation.
• No fuel or no ignition of fuel.
Failure of the engine to rotate can be the result of electrical or pneumatic malfunctions.
Check the engine instruments display for presence of the Start Valve Open (SVO) icon.
If no SVO icon is present, see Section 05-11-20: Start Valve Failure.
NOTE:
For airplanes SN 1144 and subsequent, and SN
1000 through 1143 with ASC 151: Engine failure to
start may be the result of a failed igniter. Check the
engine instruments display for presence of the Ignition
(IGN) icon. If no IGN icon is present, the start may be
salvaged by selecting AIR START Ignition to ON prior
to moving the HP fuel cock from SHUT to OPEN.
NOTE:
Verify fuel flow / pressure to the engine. If there is no
fuel flow / pressure, verify the FIRE handle is fully in.
Automatic ignition should occur when the ENG START switch is depressed. Its
availability will be indicated by the IGN icon on the engine instruments display. If
automatic ignition is not indicated, check for proper selection of MASTER START (versus
MASTER CRANK) switch. If MASTER CRANK has inadvertently been selected, the start
may be salvaged by selecting the appropriate AIR START Ignition to ON, or the start may
be terminated, proper selections made, and a second attempt initiated.
Fuel ignition should occur within five (5) to ten (10) seconds after opening the HP fuel
cock.
IF THERE IS NO INDICATION OF IGNITION:
1. HP Fuel Cock................................................................................................SHUT
2. START MASTER Switch.................................................................................OFF
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：灣流4操作手冊 Gulfstream IV Operating Manual 3(97)