曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專(zhuān)營(yíng)店坑蒙拐騙欺詐消費(fèi)者

only.
3. Brakes ........................................................................................................CHECK
OPERATING MANUAL
03-04-00 EXPANDED NORMAL PROCEDURES
Page 2
May 30/02
Revision 7
4. Slip Indicators / Compasses / Flight Instruments.................................CHECK
NOTE:
On SPZ-8400 equipped aircraft, the external slip
indicator is removed from the PFD and replaced by an
electronic slip indication just below the roll pointer on
each PFD ADI.
NOTE:
If flight instruments are inoperative, check AOA
indicator. If high angle-of-attack is indicated, briefly
pressing the respective AOA test button will slew the
AOA probe to lower angle of attack, returning flight
instruments to normal operation.
NOTE:
If taxi operations are conducted with engine bleed air
as the source for the ECS packs during warm weather
operations, it is recommended that with one power
lever be advanced above idle with the ISOLATION
valve OPEN and the opposite engine bleed air OFF to
provide cooling air flow to the cabin.
5. Thrust Reversers Operational Check (First Flight of Day) ...........COMPLETE
6. Thrust Reverser Lights (Every Flight) ....................................................CHECK
A. REV ARM................................................................................................ON
B. REV Unlock / Deploy...........................................................................OUT
NOTE:
If either or both Unlock or Deploy lights are ON,
maintenance is required before flight.
7. Fuel Temperature ......................................................................................CHECK
8. Crew Briefing / EPR / V-Speeds ...........................................................BRIEFED
9. Trim Settings (3) .............................................................................................SET
10. BTMS / OVHT Message .................................................................CHECK / OUT
For airplanes with Brake Temperature Monitoring System installed.
NOTE:
SPZ-8000 equipped airplanes SN 1156 and subs and
SN 1000 through 1155 having ASC 167. For SPZ-
8400 equipped airplanes, BTMS display is
incorporated in the BRAKES synoptic page.
11. Flaps / Stabilizer ...........................................................................SET TAKEOFF
12. Engine Instruments ..................................................................................CHECK
13. Hydraulic Pressure.................................................CHECK (3000 - 3000 - 0 - 0)
14. APU ...................................................................................................AS DESIRED
OPERATING MANUAL
EXPANDED NORMAL PROCEDURES 03-04-00
Page 3
May 30/02
Revision 7
15. Flight Guidance Panel....................................................................................SET
16. Warn Inhibit.......................................................................................................ON
03-04-30: Line Up
1. Engine Bleed Air Switches..............................................................................ON
2. APU Air / ISOLATION Valve.........................................................OFF / CLOSED
3. Exterior Lights ..............................................................................AS REQUIRED
4. Ground Spoilers .......................................................................................ARMED
5. Transponder / TCAS................................................................................ON / ON
6. Crew Alerting System...............................................................................CHECK
7. Air Start Ignition ...........................................................................AS REQUIRED
NOTE:
It is recommended that Air Start Ignition be selected
ON for takeoff on a runway with standing water, slush
or snow.
8. Autothrottle.......................................................ARM / ENGAGED (IF DESIRED)
NOTE:
Autothrottle will annunciate “HOLD” at approximately
60 knots and will maintain power lever “HOLD” unless
selected to another mode after attaining 400 ft AGL.
OPERATING MANUAL
03-04-00 EXPANDED NORMAL PROCEDURES
Page 4
May 30/02
Revision 7
INFLIGHT PROCEDURES
03-05-10: Climb
1. Landing Gear.....................................................................................................UP
2. Flaps...................................................................................................................UP
3. Flight Guidance Panel....................................................................................SET
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：灣流4操作手冊(cè) Gulfstream IV Operating Manual 3(34)