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时间:2011-10-11 13:08来源:蓝天飞行翻译 作者:航空
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 S 684-007

 (6)  
Close the drain valve when the reservoir is empty.


 D. Remove the Temperature Transmitter (Fig. 401)
 S 034-008
 (1)  
Remove the electrical connector.

 S 024-009

 (2)  
Remove the transmitter (1) from the reservoir and discard the O-ring (2).

 S 034-010

 (3)  
Install a cap on the open reservoir port.


 TASK 29-32-03-404-027
 3. Install the Temperature Transmitter
___________________________________
 A. Consumable Materials
 (1)  D00054 Hydraulic System Lubricant - MCS 352
 B. Parts ~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ...............................................................................| | 401 | 1 | Temperature Transmitter | 29-11-20 | 04 | 157 | | | | | | | 145 | | | | | | | 107 | | | 2 | Packing (O-ring) | | | 160 | | | | | | | 150 | | | | | | | 109 | 2.......….......…...................................…...........….....…........1
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 29-32-03
 ALL  ú ú 01 Page 403 ú Sep 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 C. References
 (1)  
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)  
AMM 12-12-01/301, Hydraulic Systems

 (3)  
AMM 12-25-01/301, Exterior Cleaning

 (4)  
AMM 24-22-00/201, Electrical Power

 (5)  
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems

 (6)  
AMM 32-00-15/201, Landing Gear Door Locks

 D.
Access

 (1)  
Location Zones
 197 Wing to Body - Aft Lower Half (Left)
 211/212 Control Cabin
 732/742 MLG Body Door


 (2)  
Access Panel
 197KL Hydraulic Service Bay


 E.
Install the Temperature Transmitter (Fig. 401)


 S 644-011
 (1)  
Apply a layer of hydraulic lubricant or hydraulic fluid on the new O-ring (2) and the temperature transmitter threads.

 S 434-012

 (2)  
Remove the cap from the reservoir port.

 S 424-013

 (3)
Install the O-ring (2) and the transmitter (1) in the reservoir.

 S 434-014

 (4)  
Connect the electrical connector.

 S 614-015

 (5)  
Fill the hydraulic reservoir (AMM 12-12-01/301).

 S 864-016

 (6)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11:


 (a)  11K15, HYDRAULICS ELEC PUMP C1
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 29-32-03
 ALL  ú ú 01 Page 404 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 (b)  
11K16, HYDRAULICS ELEC PUMP RIGHT

 (c)  
11K24, HYDRAULICS ELEC PUMP C2
 
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