1) Manually tighten the connnector nut with your hand until fully engaged.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-04
ALL ú ú C01 Page 403 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(h)
Connect the signal input cable to the PMC connector J3.
1) Manually tighten the connector nut with your hand until fully engaged.
(i)
Connect the signal cable for the flight compartment to the PMC connector J4. 1) Manually tighten the connector nut with your hand until
fully engaged.
(j)
Connect the monitor signal cable to the PMC connector J5, if you do use this cable. 1) Manually tighten the connector nut with your hand until
fully engaged.
(k)
Examine all the connectors for correct installation.
NOTE: Make sure that there is no movement.
____
(l) Install the protective cap to the PMC, if you do not use the monitor signal cable. 1) Tighten the protective cap to 40-60 pound-inches
(4.5-5.0 Newton meters).
S 414-007-C00
(2)
Close the right fan cowl panel (AMM 71-11-02/201).
S 724-008-C00
(3)
Do the test for the PLA transducer gain adjustment (AMM 73-21-00/501).
S 714-011-C00
(4)
Do a test for the MEC Trim (part power trim check) (AMM 71-00-00/501, Test No. 6).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-04
ALL ú ú C01 Page 404 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
POWER MANAGEMENT CONTROL - INSPECTION/CHECK
___________________________________________
1. General
_______
A. This procedure contains one task. This task is used to do a check on the power management control (PMC).
TASK 73-21-04-206-001-C00
2. Power Management Control Inspection/Check
_________________________________________
A. References
(1) AMM 71-11-02/201, Fan Cowl Panel
B. Access
(1)
Location Zones
503/603 Fan Cowl - Right
(2)
Access Panels
5746 Fan Cowl Assy - Left
5846 Fan Cowl Assy - Right
C. Procedure (Fig. 601)
S 016-003-C00
(1)
Open the right fan cowl panel (AMM 71-11-02/201).
S 206-004-C00
(2)
Do a check on the PMC parts and areas as identified in the table that follows:
(a) Do the corrective action shown in the table.
(3)
Close the right fan cowl panel (AMM 71-11-02/201).
S 416-002-C00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-04
ALL ú ú C01 Page 601 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
PMC COVER
ADJUSTMENT
WELL COVER
PMC CHASSIS
J5 CONNECTOR
SHOCK MOUNTS
(4 LOCATIONS) J3 CONNECTOR
J4 CONNECTOR
J2 CONNECTOR
A
G-M56-SM-0394(1)-01-C
PMC Inspection Areas
Figure 601
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:737-300 400 500 AMM 飞机维护手册 发动机燃油和控制(123)