(d)
Remove the C78004-2 Lockpin from the No. 1(2) control valve module (AMM 78-31-00/201).
S 865-231-C00
(13) Move the engine No. 1(2) reverse thrust lever forward and down to the retracted position.
(a) AIRPLANES WITH THE SIXTEEN LIGHT ENGINE ACCESSORY UNIT; Press and release the No. 1(2) reset switch. 1) Make sure that all the lights on the sixteen light engine
accessory unit are off.
S 735-163-C00
(14)
Do the Valve Disagreement Test for the engine No. 2 thrust reverser with the ENG 2 circuit breakers and monitor the lights for engine No. 2.
S 865-164-C00
(15)
Close the circuit breaker:
(a) On the P6 panel:
1) ENG 2 SYNC LOCK - ALTN
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CFM56 ENGINES
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S 845-232-C00
(16) Put the airplane back to its usual configuration (or continue with the tests).
TASK 78-31-00-735-166-C00
10. Put the Airplane Back to its Usual Configuration
________________________________________________
A. Equipment
(1) C75001 Switch, Detent System Test
B. Access
(1) Location Zones
504/604 Thrust Reverser - Left
505/605 Thrust Reverser - Right
101 Control Cabin - Left
102 Control Cabin - Right
205 Electronic Compartment
C. Procedure
S 095-167-C00
(1)
Make sure that the lockpins C78004-2 are removed from both control valve modules for the thrust reverser (AMM 78-31-00/201).
S 865-168-C00
(2)
Make sure that the forward thrust levers are at the idle position.
S 215-169-C00
(3)
Make sure that the reverse thrust levers are fully forward and down.
S 865-170-C00
(4)
Remove electrical power (AMM 24-22-00/201).
(a) Set the BAT switch on the Electrical Meters Battery and Galley Power Module (P5-13) to the OFF position and install a DO-NOT-OPERATE tag.
S 865-171-C00
(5)
Remove hydraulic power (AMM 29-15-00/201).
S 845-172-C00
(6)
Make sure airplane is in ground mode.
(a) Make sure the Air Sensing Switch, S1, on the E11 landing gear logic shelf is released.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST REVERSER SYSTEM - INSPECTION/CHECK
_________________________________________
1. General
_______
A. This procedure is a scheduled maintenance task and gives instructions to do a visual inspection of the thrust reverser components that follow:
-Thrust reverser actuators
-Cascades
-Blocker doors and attaching drag links
-Translating sleeve
-Track liners and sliders
-Inner and outer ducts
-Fire seals in upper bifurcation area
-Bull nose seal and fairing.
TASK 78-31-00-206-001-C00
2. Thrust Reverser System Inspection
_________________________________
A. Equipment
(1)
Rig Pin Assembly - F70207-8; MS20392-4C pins
(or equivalent 0.311 +0.000/-0.002-inch
diameter, 3-inch long rod or bolt)
(2)
Mirror, Inspection (approximately 6 inches (150 mm) square or round)
(3)
Flashlight
(4)
Rod, Extension (approximately 3 feet long to hold the mirror)
B.
References
(1)
AMM 29-15-00/201, Hydraulic System A, B, and Standby
(2)
AMM 78-31-00/201, Thrust Reverser System
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