S 414-029-C00
(2)
Close the fan cowl panel (AMM 71-11-02/201).
S 444-021-C00
(3)
Do the activation procedure for the thrust reverser
(AMM 78-31-00/201).
S 864-035-C00
(4)
Remove the DO-NOT-CLOSE tag and close this circuit breaker.
(a) P6 Main Power Distribution Panel
1) ENG VIB MON
S 714-020-C00
(5) Do an operational test of the AVM system (AMM 77-31-00/501).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
77-31-02
ALL ú ú C03 Page 405 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TRF VIBRATION (CORE) SENSOR - INSPECTION/CHECK
______________________________________________
1. General
_______
A. This procedure has one task. This task gives the procedure for the visual examination of the TRF vibration (core) sensor.
B. This sensor is a high speed rotor vibration accelerometer.
TASK 77-31-02-206-001-C00
2. Core Sensor Inspection
______________________
A. References
(1)
AMM 71-11-02/201, Fan Cowl Panels
(2)
AMM 78-31-00/201, Thrust Reverser System
B. Access
(1)
Location Zone
5700, Engine No. 1
5800, Engine No. 2
(2)
Access Panel
5738L, Thrust Reverser, Eng. No. 1
5838R, Thrust Reverser, Eng. No. 2
5746L, Fan Cowl Panel, Eng. No. 1
5846R, Fan Cowl Panel, Eng. No. 2
C. Do the Core Sensor Inspection
S 016-002-C00
(1) Open the left fan cowl panel (AMM 71-11-02/201).
S 046-003-C00
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE THRUST REVERSER TO
_______ PREVENT THE OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO THE EQUIPMENT.
(2) Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
S 016-004-C00
WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO OPEN THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS WHEN YOU OPEN THE THRUST REVERSERS, INJURIES TO PERSONS OR DAMAGE TO THE EQUIPMENT CAN OCCUR.
(3) Open the left thrust reverser (AMM 78-31-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
77-31-02
ALL ú ú C01 Page 601 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 216-005-C00
(4) Visually examine the body of the accelerometer for cracks, dents and
deformations.
(a) If the depth of the damage is more than 0.04 inch, replace the
accelerometer.
S 216-006-C00
(5) Visually examine the electrical connector for bent pins, cracks or
crossed threads.
(a) Replace the accelerometer if damage is found.
NOTE:____ Clean the electrical connectors before you connect the
connectors again (WDM 20-60-01).
S 416-007-C00
WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS WHEN YOU CLOSE THE THRUST REVERSERS, INJURIES TO PERSONS OR DAMAGE TO THE EQUIPMENT CAN OCCUR.
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本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 發(fā)動(dòng)機(jī)指示 ENGINE INDICATIN(94)
