(6)
Make sure that the circuit breakers that follow are closed:
(a)
P6 Load Control Center
1) IDLE CONT
(b)
P18 panel
1) FLT RCDR AC
2) FLT RCDR DC
S 734-017-C00
S 724-018-C00
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(7) S 214-008-C00Make sure that the OFF LIGHT on the flight recorder test module on the P5 panel is ON.
(8) S 864-020-C00Prepare and start engine No. 1 (AMM 71-00-00/201). (a) Make sure these circuit breakers on the P18 panel stay closed during this procedure. 1) FLT RCDR AC 2) FLT RCDR DC
(9) S 214-009-C00Make sure that the OFF LIGHT on the flight recorder test module on the P5 panel is OFF.
S 864-039-C00
(10)
Prepare and start engine No. 2 (AMM 71-00-00/201).
S 864-040-C00
(11)
Let the engines become stable (two minutes are necessary).
S 864-024-C00
(12)
For the two engines, open this circuit breaker and attach a DO-NOT-CLOSE tag:
(a) P6 Load Control Center 1) IDLE CONT
S 724-025-C00
(13) Do a check that the engine speed for the two engines increase to high idle.
NOTE: The difference between low idle and high idle is a change in
____ N1 of 4 to 8 percent.
S 864-026-C00
(14) For the two engines, remove the DO-NOT-CLOSE tag and close this circuit breaker:
(a) P6 Load Control Center 1) IDLE CONT
S 724-027-C00
(15) Do a check that the engine speed for the two engines goes to low idle after approximately 4 seconds.
NOTE: The difference between low idle and high idle is a change in
____ N1 of 4 to 8 percent.
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S 864-028-C00
(16)
Stop the engine No. 1 (AMM 71-00-00/201).
S 214-010-C00
(17)
Make sure that the OFF LIGHT on the flight recorder test module on the P5 panel is OFF.
S 864-030-C00
(18)
Stop the engine No. 2 (AMM 71-00-00/201).
S 214-011-C00
(19)
Make sure that the OFF LIGHT on the flight recorder test module on the P5 panel is ON.
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THRUST REVERSER VOLUMETRIC HYDRAULIC FUSES - REMOVAL/INSTALLATION
_________________________________________________________________
1. General
_______
A. This procedure contains the tasks to remove and install the thrust reverser volumetric hydraulic fuses.
B. There is no on-airplane test for the volumetric hydraulic fuses for the thrust reversers.
NOTE: The volumetric hydraulic fuses may be tested after removal
____ from the airplane to find out if they are operational. Use the functional test procedures contained in the Vendor CMM.
TASK 78-34-07-004-001-C00
2. Volumetric Hydraulic Fuse Removal
_________________________________
A. References
(1)
AMM 29-09-00/201, Hydraulic Reservoir Pressurization System
(2)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 EXHAUST(180)
