(a) R IND LTS 1
S 095-034
(33)
Remove the jumper from the pins 1 and 2 of the electrical connector for the left EDP.
S 435-035
(34)
Connect the electrical connector to the left EDP.
S 865-036
(35)
Remove the DO-NOT-CLOSE tag and close this circuit breaker on the P11 panel:
(a) R IND LTS 1
S 215-037
(36)
Make sure the L ENG HYD OVHT message does not show on the EICAS.
S 215-038
(37)
Make sure the L ENG OVHT light on the hydraulic control panel is not on.
S 865-039
(38)
Open this circuit breaker on the P11 panel and attach a DO-NOT-CLOSE tag:
(a) L IND LTS 1
S 095-040
(39)
Remove the jumper from the pins 1 and 2 of the electrical connector for the right EDP.
(40)
Connect the electrical connector to the right EDP.
S 435-041
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-32-00
ALL ú ú 01 Page 506 ú Sep 20/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
S 865-042
(41) Remove the DO-NOT-CLOSE tag and close this circuit breaker on the P11 panel:
(a) L IND LTS 1
S 215-043
(42)
Make sure the R ENG HYD OVHT message does not show on the EICAS.
S 215-044
(43)
Make sure the R ENG OVHT light on the hydraulic control panel is not on.
E. Put the Airplane Back to Its Usual Condition
S 415-045
WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO REMOVE THE DOOR LOCKS.
_______ THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(1)
Remove the door locks from the landing gear doors and close the doors (AMM 32-00-15/201).
S 415-046
(2)
Close the access panels for the hydraulic bay in the left and right aft struts (Ref 06-43-00/201).
S 865-048
(3)
Close the access panel for the central hydraulic service center (AMM 06-41-00/201).
S 865-049
(4)
Do the activation procedure for the thrust reverser
(AMM 78-31-00/201).
(5)
Remove electrical power, if it is not necessary (AMM 24-22-00/201).
S 865-050
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
TASK 29-32-00-735-077
3. System Test-Temperature Indication for the Hydraulic Reservoir Fluid
____________________________________________________________________
A. Equipment
(1)
Decade Box, Variable Resistance - 10 to 150 |0.5 ohms - commercially available
B.
References
(1)
AMM 06-41-00/201, Fuselage Access Doors and Panels
(2)
AMM 24-22-00/201, Electrical Power
(3)
AMM 32-00-15/201, Landing Gear Door Locks
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本文鏈接地址：757 AMM 飛機維護手冊 液壓 CHAPTER 29 - HYDRAULIC POWER 2(167)
