S 722-028-C00
(18)
Do a check that continuity is kept between the C and NO terminals.
S 862-029-C00
(19)
Move the lever to the stow position.
S 082-030-C00
(20)
Disconnect the ohmmeter leads from the switch.
S 432-004-C00
WARNING:_______ USE ONLY APPROVED HEAT SOURCES WHEN YOU HEAT THE HEAT SHRINK
TUBING. OTHER EQUIPMENT CAN GIVE OFF SPARKS OR OPEN FLAMES
WHICH COULD CAUSE A FIRE. THIS WOULD CAUSE SEVERE INJURY TO
PERSONS AND DAMAGE TO EQUIPMENT.
(21) At each connection, install a sleeve made from 0.5 inch (12.7 mm) of heat shrink tubing.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-34-04
ALL ú ú C03 Page 209 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 432-031-C00
(22) Connect the leads to the switch as follows:
-red to NC
-green to C
-black to NO
-white is a spare.
S 412-032-C00
(23)
Install the cover on the thrust lever (Fig. 203).
S 092-033-C00
(24)
Remove the protractor from the reverser thrust lever (Fig. 202).
S 862-038-C00
(25)
Close the applicable THR REV CONTR SYS circuit breaker on the circuit breaker panel P6.
S 862-043-C00
(26)
Close the THR REV CONT SYS ALTN circuit breaker on the P6 panel.
S 862-039-C00
(27)
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
S 862-034-C00
(28)
Manually retract the thrust reverser (AMM 78-31-00/201).
S 712-036-C00
(29)
Do the Normal Operation Test (AMM 78-31-00/501).
TASK 78-34-04-782-049-C00
5. AIRPLANES WITH THE THRUST REVERSER SYNC-LOCK; Adjust the Sync Lock Switch S5 of the Thrust Reverser
______________________________________________________
A. Equipment
(1)
F70044-500, Protractor for the Reverse Thrust Lever
(2)
F70207-108, Kit Rig Pin
B. Consumable Materials
(1) G01148 Tubing - Heat Shrink, Raychem RT-876, 1/16-inch diameter
C. References
(1)
AMM 78-31-00/201, Thrust Reverser System
(2)
AMM 78-31-00/501, Thrust Reverser System
D. Access
(1) Location Zones
101/102 Control Cabin
502/503 Engine No. 1 - Fan Cowl Panels
602/603 Engine No. 2 - Fan Cowl Panels
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-34-04
ú ALL ú
ú ú ú C04.101 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. Page 210Jul 12/02
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2)
Access Panels
5737L/5746L Engine No. 1 - Fan Cowl Panels
5837R/5846R Engine No. 2 - Fan Cowl Panels
E.
Procedure
S 862-062-C00
(1)
Make sure the adjustment of the engine control system is correct
(AMM 76-11-00/501).
S 862-061-C00
(2)
Put the applicable forward thrust lever and reverse thrust lever in
the idle stop position and hold the levers in this position during
the next check.
S 862-060-C00
(3)
Check the rig pin 1 (F70207-23) can be inserted freely in the torque switch mechanism of the autothrottle.
S 862-059-C00
(4)
If the rig pin cannot be inserted freely refer to cable rigging
checks in AMM 76-11-00/501 for reverse thrust lever clearance.
S 862-058-C00
(5)
Install the protractor on the reverse thrust lever.
S 862-057-C00
(6) 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 EXHAUST(169)
