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时间:2011-04-02 16:31来源:蓝天飞行翻译 作者:航空
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 ú  a) 6A17, HYD SYSTEM BRAKE PRESS IND
 ú  4) On the P42 panel
 ú  a) LTG 5V AC SEC
 ú  (b) Remove the windshield wiper assembly (AMM 30-42-11/401).
 ú  (c) Loosen screws that attach P3-1 instrument panel and move
 ú  slightly aft.
 (d) Disconnect the following electrical connectors that are
 connected to the P3-1 panel mounted indicators and lights:
 1) Radio Digital Distance Magnetic Indicator
 (AMM 34-28-81/401)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 30-42-21
 ALL  ú ú 03.1 Page 403 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 ú 2) AIRPLANES WITH EFIS;
 ú Autoflight Status Annunciator (AMM 22-11-32/401)
 ú (e) Disconnect the following electrical connectors:
 ú 1) D2678 (Brake Pressure Indicator)
 ú 2) D3328 and D3332 (Brake Temperature Indicators, if
 ú installed)
 ú 3) D477 electrical connector
 ú (f) Remove the P1-3 instrument panel. If necessary remove the EADI
 ú display unit (AMM 34-22-21/401).
 ú (g) Disconnect electrical connector D64 from the right drive motor.
 ú (h) Remove the bolts that attach the support fitting to the
 ú structure.
 ú (i) Remove the ground wire from the drive motor.

 TASK 30-42-21-404-002
 3. Windshield Wiper Drive Assembly Installation (Fig. 401)
____________________________________________
 A. References ú (1) AMM 22-11-32/401, Autoflight Status Annunciator ú (2) AMM 28-41-51/401, Fuel Quantity Indicator ú (3) AMM 30-42-11/401, Windshield Wiper Assembly ú (4) AMM 34-12-21/401, Air Data System Indicators
 (5)
AMM 34-22-21/401, EADI Display Unit ú (6) AMM 34-25-11/201, Standby Horizon Indicator ú (7) AMM 34-28-81/401, Radio Digital Distance Magnetic Indicator ú (8) AMM 34-28-91/401, Vertical Speed Indicator

 (9)
AIPC 30-40-00 Fig. 10

 (10)
 SSM 30-42-00

 (11)
 WDM 30-42-01


 B. Access
 (1)  Location Zone
 101 Control Cabin - Left
 102 Control Cabin - Right


 C.
Procedure ú ú S 424-007 ú (1) Do these steps to install the left wiper drive assembly: ú (a) Install lockwire on the cap on the end of the drive assembly. ú (b) Connect the ground wire to the drive motor. ú (c) Install the bolts that attach the support fitting to the ú structure. ú (d) Connect electrical connector D62 to the left drive motor.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 30-42-21
 ALL  ú ú 03.1 Page 404 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 ú  (e) Install the windshield wiper assembly if it was removed
 ú  (AMM 30-42-11/401).
 ú  (f) Close this circuit breaker and remove the DO-NOT-CLOSE tag:
 ú  1) On the P18 panel
 ú  a) WIPER-L
 ú  (g) Do a test of the windshield wiper system (AMM 30-42-00/501).
 ú
 ú  S 424-028
 ú  (2)  Do these steps to re-install the P1-3 instrument panel if it was
 ú  removed to get access to the left wiper drive assembly.
 ú  (a) Open these circuit breakers and attatch DO-NOT-CLOSE tags:
 ú  1) On the P6-3 panel
 ú  a) 6D15, MASTER DIM SECT 6
 ú  b) 6C14, MASTER DIM SECT 2
 ú  c) 6C12, DIM & TEST
 ú  2) On the P6-2 panel
 ú  a) 6B09, AUTO SPEED BRAKE
 ú  3) On the P18 panel
 ú  a) 18A01, STAB TRIM SERVO
 ú  (b) Connect the following electrical connectors and pitot/static
 
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