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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 液壓 CHAPTER 29 - HYDRAULIC POWER 2(172)
