N2 Control Alternator Connector Grommet Inspection
Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-08
ALL ú ú C01 Page 602 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A10058
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
EXAMPLE OF A GROMMET THAT IS NOT DAMAGED B-B EXAMPLE OF A DAMAGED GROMMET B-B
GMM-1101067-00-B
N2 Control Alternator Connector Grommet Inspection
Figure 601 (Sheet 2)
A10093
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-08
ALL ú ú C01 Page 603 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(5) S 726-005-C00Do an operational test of the alternator stator to make sure it operates correctly (AMM 77-12-00/501).
NOTE:____ If a failure of the J2 connector has occurred, a PMC INOP light will not come on in the control cabin.
(6) S 416-007-C00Close the right fan cowl panel (AMM 71-11-02/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-08
ALL ú ú C01 Page 604 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
T2 TEMPERATURE SENSOR - REMOVAL/INSTALLATION
____________________________________________
1. General_______
A. The T2 temperature sensor is found on the left side of the fan case at
the 10:30 o'clock position.
TASK 73-21-09-004-001-C00
2. Remove the T2 Temperature Sensor________________________________
A. Equipment
(1) Container - 1 gallon (4 liter) capacity, for fuel
B. References
(1) AMM 71-11-02/201, Fan Cowl Panels
C. Access
(1)
Location Zones
506 Engine No. 1 - 10:30 o'clock position
606 Engine No. 2 - 10:30 o'clock position
(2)
Access Panels
5746L Engine No. 1 - Left Fan Cowl Panel
5846R Engine No. 2 - Left Fan Cowl Panel
D. Procedure
S 014-002-C00
(1)
Open the left fan cowl panel (AMM 71-11-02/201).
S 024-003-C00
(2)
Remove the sensor element (Fig. 401).
(a)
Cut the sealant around the inside inlet cowl of the sensor element base.
(b)
Remove the sensing element from the fan inlet duct.
NOTE: To do this, remove the four bolts and washers.
____
(c)
Cover the sensor element inlet and exit holes with a protective cover.
(d)
Disconnect the capillary tube from the two clamps on the fan case brackets.
S 034-004-C00
(3) Remove the housing.
(a)
Put a funnel below the fuel line connections on the housing. Do this to cause fuel that is released to flow into the container.
CAUTION:_______USE TWO WRENCHES TO REMOVE THE COUPLING NUTS. USE ONE WRENCH TO HOLD THE NIPPLE. USE THE OTHER WRENCH TO LOOSEN THE NUT. THIS IS TO PREVENT DAMAGE TO THE HARDWARE.
(b)
Disconnect the P7 and the PB fuel tubes.
(c)
Put caps on the open fuel tubes and the fittings.
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(134)
