C. Remove the PMC
S 014-009-C00
(1)
Open the right fan cowl panel (AMM 71-11-02/201).
S 024-003-C00
(2)
Do the steps that follow to remove the PMC (Fig. 401):
(a)
Disconnect the PS12 line from the connector on top of the PMC.
(b)
Disconnect the control alternator (dark blue) cable, N2 from the connector J2 on the bottom of the PMC.
(c)
Disconnect the signal input cable from the connector J3 on the bottom of the PMC.
(d)
Disconnect the signal cable for the flight compartment from the connector J4 on the bottom of the PMC.
(e)
Disconnect the monitor signal cable from the connector J5 on the bottom of the PMC, if you do use this cable.
(f)
Remove the bolt and nut that attaches the grounding strap to the aft mounting flange for the PMC.
(g)
Remove 4 mounting bolts from the PMC and remove the PMC.
NOTE: Hold PMC as bolt aree removed to prevent it from falling
____ from mounting brackets.
(h) Install the protective caps on the connectors.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-04
ALL ú ú C01 Page 401 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
PS12
CONNECTION
PMC
GROUND
STRAP
MOUNTING BOLTS
(4 LOCATIONS)
J2 CONNECTOR J5 CONNECTOR
J4 CONNECTOR
J3 CONNECTOR
FWD
A
PMC Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-04
ALL ú ú C01 Page 402 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TASK 73-21-04-404-004-C00
3. Install the Power Management Control
____________________________________
A. Equipment
(1) Pliers - Soft Jawed, Type 8493-03, CODE BP
B. Consumable Materials
(1) Grease - Graphite (CP2101) (AMM 70-10-01/201).
C. References
(1)
AMM 71-00-00/201, Power Plant
(2)
AMM 71-11-02/201, Fan Cowl Panel
(3)
AMM 73-21-00/501, Fuel Control System
D. Access
(1) Location Zones
506 - Engine 1
606 - Engine 2
E. Procedure
S 424-005-C00
(1) Do the steps that follow to install the PMC (Fig. 401):
(a)
Apply a thin layer of grease to the threads and pressure faces of the 4 mounting bolts.
(b)
Put the PMC on the mounting bracket.
NOTE: Make sure that the 4 connectors side is facing down.
____
(c)
Install the mounting bolts which attach the PMC to the bracket.
1) Tighten the mounting bolts to 100-110 pound-inches (11-13 Newton meters).
(d)
Apply a thin layer of grease to the threads and pressure face of bolt.
(e)
Install the bolt and nut which attaches the grounding strap to the PMC aft flange. 1) Tighten the bolt to 100-110 pound-inches
(11-13 Newton meters).
(f)
Connect the P12 sensing line to the connector on top of the PMC. 1) Tighten the connector to 65-75 pound-inches
(7.5-8.5 Newton meters), and lockwire.
CAUTION: MAKE SURE THAT THE PIN POSITIONS ON CONECTORS ARE CORRECT
_______
WITH MATING RECEPTACLE.
(g) Connect the N2 cable for the control alternator (dark blue) to the PMC connector J2. 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 發(fā)動機燃油和控制(122)
