(a) P6 Overhead Circuit Breaker Panel
1) EIS PRI 2
2) EIS PRI 4
S 864-085-C03
WARNING:_______YOU MUST DO A DEACTIVATION OF THE THRUST REVERSER. IF YOU DO
NOT, THE THRUST REVERSER CAN MOVE AND CAUSE INJURY TO PERSONS
AND DAMAGE TO THE EQUIPMENT.
(3)
Do the deactivation procedure for the thrust reverser
(AMM 78-31-00/201).
S 014-086-C03
(4)
Open the left fan cowl panels (AMM 71-11-02/201).
S 014-087-C03
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU OPEN THE
_______
THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY
TO PERSONS OR DAMAGE TO THE EQUIPMENT CAN OCCUR.
(5) Open the left thrust reverser (AMM 78-31-00/201).
E. Remove the Forward EGT Extension Cable
S 024-015-C03
CAUTION: DO NOT BEND OR MAKE A KINK IN THE EGT HARNESSES AND PROBES.
_______
YOU CAN EASILY CAUSE DAMAGE TO THE EGT HARNESSES AND PROBES.
(1) Do these steps to disconnect the connector or terminals (Fig. 401):
(a)
Remove the bolt, the nut, and the loop clamp that attach the extension cable to the engine brackets at three locations.
(b)
Disconnect the connector (on the lower extension harness) from the main junction box with the fork wrench.
(c)
ENGINES WITH INTERFACE CONNECTORS; Disconnect the connector: 1) Disconnect the connector from the airplane wires. 2) Remove the four screws and the two shims that attach the
connector to the bracket.
(d)
ENGINES WITH INTERFACE TERMINALS; Remove the two nuts and disconnect the two interface terminals.
(e)
Put protective caps on the connectors and the receptacles.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
9 PROBE EGT SYSTEM (SOFT MOUNT) ú 77-21-01
ú CONFIG 3 ú C05 Page 402 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
SEE B INTERFACE CONNECTOR 1 SEE D FORWARD EXTENSION CABLE MAIN JUNCTION BOX
A
1 2 ENGINES WITH TERMINAL AT INTERFACE ENGINES WITH CONNECTOR 2 TERMINAL INTERFACE
LUG/BLOCK AT INTERFACE SEE C
Forward EGT Thermocouple Harness Extension Cable Installation Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
9 PROBE EGT SYSTEM (SOFT MOUNT) ú 77-21-01
ú CONFIG 3 ú C01 Page 403 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
HPT/LPT COOLING AIRTUBE FORWARD EXTENSION LEAD
TERMINAL INTERFACE
INTERFACE CONNECTOR
B C
CLAMP BOLT NUT BOLT CLAMP BOLT
SHIMS (2 LOCATIONS) NUT NUT CLAMP CONNECTOR MAIN JUNCTION BOX
BOLT (4 LOCATIONS) D
Forward EGT Thermocouple Harness Extension Cable Installation
Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
9 PROBE EGT SYSTEM (SOFT MOUNT) ú 77-21-01
ú CONFIG 3 ú C01 Page 404 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
中國航空網 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 發動機指示 ENGINE INDICATIN(39)
