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

Exxon 2389 Mobil Jet Oil II
Mobil Jet Oil 254
Castrol 5000 Gas Turbine Oil
Refer to the following manuals for oils approved for specific usage in the engine, starter
and APU:
• Engine: U.K. CAAApproved Rolls-Royce Tay Operating Instructions (F-TAY-1RR)
and associated Service Bulletins
• Starter: Garrett Starter Maintenance Manual 80-10-53
• APU: Garrett Maintenance Manual No. 49-21-89 for APU Model No. GTCP36-
100(G)
OPERATING MANUAL
01-12-00 EXPANDED LIMITATIONS
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AIR CONDITIONING AND BLEED AIR
01-21-10: Cabin Pressurization Control System
1. Maximum Cabin Pressure Differential Permitted: 9.80 psi
2. Maximum Cabin Pressure Differential Permitted For Taxi, Takeoff Or
Landing: 0.3 psi
01-21-20: Bleed Air System
Do not operate above 41,000 ft without both engine bleeds ON and each engine being
bled by either the air conditioning system or engine cowl anti-ice. See Section 05-01-10:
Air Conditioning System Shut Down Or Inoperative.
OPERATING MANUAL
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AUTO FLIGHT
01-22-10: Mach Trim Compensation / Electric Elevator Trim
1. Use of Mach Trim Compensation:
Mach trim compensation must be ON during all flight operations except as
provided for in Section 05-03-40: Mach Trim Compensation Failure.
2. If Mach Trim Compensation Failure is Coupled with Yaw Damper Failure:
When mach trim compensation failure is coupled with yaw damper failure,
observe speed limitations for both failures and limit altitude to 41,000 ft.
01-22-20: Autothrottle
1. Use During Takeoff or Go-Around:
Use of autothrottle is not permitted for takeoff or go-around when wing anti-ice is
used.
2. Disengage Height:
The autothrottle must be disengaged by 50 ft (AGL) on approach.
01-22-30: Autopilot
1. Minimum Engage Height:
Do not engage below 200 ft (AGL) on takeoff.
2. Disengage Height:
Must be disengaged on approach by 50 ft (AGL).
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ELECTRICAL POWER
01-24-10: Standby Electrical System
WHEN THE STANDBY ELECTRICAL SYSTEM IS IN OPERATION, THE FOLLOWING
LIMITATIONS APPLY:
1. Minimum HP RPM: 67 percent
2. Use of Speed Brakes:
Speed brakes may be used, however, operation should be slow (approximately
five (5) seconds for full range movement).
3. Landing with Standby Electrical System Operating:
Landing is approved provided automatic ground spoilers and thrust reversers are
not used for landing. See Section 05-17-50: Landing With Standby Electrical
Power System Operating.
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FLIGHT CONTROLS
01-27-10: Angle-Of-Attack System (AOA)
1. Use As A Reference:
Angle-Of-Attack (AOA) may be used as reference, but does not replace airspeed
as the primary reference.
2. Indication Parameters:
AOA indication must be within white band once forward airspeed is attained
during takeoff roll.
3. Use As A Speed Reference:
AOA shall not be used as a speed reference for takeoff rotation.
01-27-20: Stall Warning / Stall Barrier System
1. Takeoff Requirements:
Both stall warning / stall barrier systems must be operative for takeoff.
2. Use Of System:
Stall barrier systems must be ON during all flight operations except as noted in
Section 05-15-40, Stall Barrier Malfunction. See Section 2A-27-20, Pitch Flight
Control System, for a description of the stall warning / stall barrier system
checkout procedure.
01-27-30: Yaw Damper
1. If Yaw Damper Fails Prior ToTakeoff:
Maximum fuel quantity permitted for takeoff is 9000 lb (4082 kg).
2. If Yaw Damper Fails In Flight:
A. Above 18,000 Feet:
Maintain airspeed at or above 220 KCAS.
B. Below 18,000 Feet:
Maintain airspeed as a function of fuel quantity at or above that shown on
the following table until ready to configure for approach and landing.
Fuel Qty -
1000 Lb
8 10 12 14 16 18 20 22 24 26 28 30
Minimum
Airspeed -
KCAS
96 107 117 126 135 143 151 158 165 172 178 184
01-27-40: Speed Brakes
1. Use Of Speed Brakes:
　
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