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Steady state idle 25 psi minimum
Take-off power 45 psi minimum
Maximum continuous 110 psi maximum
Maximum transient
After cold start 115 psi (transmitter limit)
(10 minutes maximum) NOTE: Engine must remain at idle until oil
pressure returns to normal range.
LIMITATIONS Power Plant Vol. 1 02.05.3
Oct 05/06
4. CONTINUOUS ENGINE IGNITION
Continuous engine ignition must be used during the following:
.
Take-offs and landings on contaminated runways;
.
Take-offs with high crosswind components;
.
Flight through moderate or heavier intensity rain;
.
Flight through moderate or heavier intensity turbulence;
.
Flight in the vicinity of thunderstorms.
5. AUTOTHROTTLE (ATS)
.
ATS operation is restricted to two-engine operation only.
.
ATS operation is prohibited during category II approach operations.
.
Crew must confirm engine power is set to appropriate take-off N1 limit prior to reaching 80 KIAS during take-off.
.
At first indication of stall (stall buffet, stick shaker, or stick pusher), the crew must disengage the ATS and set thrust levers as required.
.
ATS operation with APR selected on FMS performance thrust limit page is prohibited.
.
If a DISENG’D or FAIL message occurs on the ATS MSD, the crew must position the thrust levers as required. Press either thrust lever ATS DISC switch to cancel ATS message.
.
Selection of AFCS FLC mode following go-around mode is prohibited, unless the altitude preselector is set higher than current altitude when ATS is engaged.
.
The AFM engine limits must not be exceeded when manually entering FMS thrust target (TGT) limit. The ATS will set engine thrust to this target without regard to engine operating limits.
.
ATS operation during take-off with thrust target (TGT) selected on FMS performance thrust limit page is prohibited.
.
ATS operation with maximum continuous thrust (MCT) selected as the FMS performance thrust limit is prohibited.
.
If both mode status displays (MSDs) fail, the crew must disengage the ATS and consider the system inoperative.
.
N1 thrust limit data is required and must be available from the FMS for ATS operation.
.
The radio altimeter must be valid for the ATS retard mode operation. If radio altitude is
unavailable or invalid, the ATS must be disengaged prior to reaching 100 feet AGL.
.
Use of the ATS during touch and go landings is prohibited. ATS must be disengaged if
system engages during touch and go landings.
.
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公务机翻译 www.aviation.cn
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