R. Autopilot Disconnect Warning Signals Test
S 865-551
(1) Make sure that these P11 panel circuit breakers are closed:
(a) 11E16, MODE CONT PNL LEFT
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(b)
11E17, FLT CONT COMPUTER POWER LEFT
(c)
11E18, FLT CONT COMPUTER SERVO LEFT
(d)
11E20, FLT CONT CMPTR PWR CTR
(e)
11E21, FLT CONT CMPTR SERVO CTR
(f)
11E34, MODE CONT PNL RIGHT
(g)
11E35, FLT CONT CMPTR PWR RIGHT
(h)
11E36, FLT CONT CMPTR SERVO RIGHT
(i)
11S15, LANDING GEAR AIR/GND SYS 1
(j)
11S19, LANDING GEAR AIR/GND SYS 2
S 865-552
(2) Open this P11 panel circuit breaker:
(a) 11A17, AUTO FLIGHT WARN
S 865-553
(3)
Make sure that the MCDP is off.
S 865-554
(4)
Push and hold the autopilot disconnect switch on the captain's control column.
(a)
Make sure that the left side of the A/P DISC light comes on.
(b)
Make sure that a siren aural warning comes from the left and right speakers.
S 865-555
(5) Release the autopilot disconnect switch.
(a)
Make sure that the A/P DISC light goes off.
(b)
Make sure that the aural warning goes off.
S 865-556
(6) Close this P11 panel circuit breaker:
(a) 11A17, AUTO FLIGHT WARN
S. Put the Airplane Back to Its Usual Condition
S 865-637
(1) Return the flaps and slats to their usual position.
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(2) S 865-015Put the R STAB TRIM switch to its NORM position.
(3) S 865-638Push the POWER SUPPLY RESET switch on the P51 panel.
(4) S 865-639Remove electrical power if it is not necessary (Ref 24-22-00).
TASK 31-51-00-725-010
3. Takeoff Configuration Warning Test
__________________________________
NOTE: This is a scheduled maintenance task.
____
A. References
(1)
AMM 24-22-00/201, Electrical Power - Control
(2)
AMM 27-48-00/501, Stabilizer Trim Position Indicating System
(3)
AMM 27-61-00/201, Spoiler/Speedbrakes System
(4)
AMM 29-11-00/201, Pressurize/Depressurize Main Hydraulic System
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本文鏈接地址：757 AMM 飛機維護手冊 儀表 CHAPTER 31 - INSTRUMENTS 2(125)
