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OPERATING MANUAL
03-06-00 EXPANDED NORMAL PROCEDURES
Page 2
October 11/02
Revision 8
23. Gust Lock..........................................................................................................ON
CAUTION
ENSURE HYDRAULIC PRESSURE IS DEPLETED
PRIOR TO ENGAGING GUST LOCK. IT IS NOT POSSIBLE
TO READ HYDRAULIC PRESSURES AS THE
AIRPLANE IS POWERED DOWN. CYCLE THE
CONTROLS WITH THE CONTROL COLUMN,
CONTROL YOKE AND RUDDER PEDALS TO
DEPLETE THE RESIDUAL PRESSURE. FAILURE TO
ALLOW HYDRAULIC PRESSURE TO DISSIPATE
PRIOR TO ENGAGING THE GUST LOCK MAY
CAUSE DAMAGE TO AIRPLANE STRUCTURE.
24. Chocks...................................................................................................IN PLACE
25. Parking Brake .................................................................................................OFF
03-06-30: Postflight
1. Engine Oil ..................................................................................................CHECK
NOTE:
For accurate readings, engine oil quantity must be
checked within thirty (30) minutes after shutdown.
2. Brakes / Landing Gear .................................................................INSPECT / PIN
3. Thrust Reversers...............................................CHECK / PROPERLY STOWED
NOTE:
If the lower thrust reverser door leading edge is
sagged out of normal contour, report for maintenance
action before next flight.
4. Exterior....................................................................................................INSPECT
5. Forms And Records ..........................................................................COMPLETE
6. Interior........................................................................................................CHECK
7. Doors ..........................................................................................................CLOSE
NOTE:
For an expanded postflight inspection procedure, see
Section 09-02-90, Expanded Postflight Inspection.
OPERATING MANUAL
EXPANDED NORMAL PROCEDURES 03-06-00
Page 3
October 11/02
Revision 8
OPERATING MANUAL
THIS PAGE IS INTENTIONALLY LEFT BLANK.
03-06-00 EXPANDED NORMAL PROCEDURES
Page 4
October 11/02
TRAFFIC PATTERN PROCEDURES
03-07-10: Traffic Pattern
TAKEOFF
1. Gear....................................................................................................................UP
2. Flaps...................................................................................................................UP
3. Guidance Panel...............................................................................................SET
4. Climb Power....................................................................................................SET
5. Ground Spoilers .............................................................................................OFF
PATTERN
6. Approach Briefing ....................................................................ACCOMPLISHED
7. FMS..................................................................................................ARRIVAL SET
8. Flight Instruments ..............................................................SET / AS REQUIRED
9. Flight Observer Seat Position .................................................................CHECK
LANDING
10. Gear ..........................................................................................DOWN / 3 GREEN
11. Nutcracker .....................................................................................................TEST
12. Ground Spoilers .......................................................................................ARMED
13. Brakes / Hydraulics .............................................................................CHECKED
14. Flaps ......................................................................................SET FOR LANDING
CAUTION
DONOTMOVEREVERSETHRUSTLEVERS OUTOF
THE FORWARD THRUST POSITION PRIOR TO
TOUCHDOWN.
NOTE:
Maintain a minimum 67% HP RPM until landing.
15. WARN INHIBIT...........................................................................................INHIBIT
TAXI-BACK
16. Ground Spoilers .............................................................................................OFF
17. Flaps......................................................................................SET FOR TAKEOFF
18. LDG / STROBE Lights....................................................................................OFF
19. Brake Temps.........................................................................................CHECKED
For airplanes with Brake Temperature Monitoring System installed.
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湾流4操作手册 Gulfstream IV Operating Manual 3(39)