TASK 71-00-00-206-001-C00
2. Power Plant Inspection______________________
A. References
(1)
71-11-02/201, Fan Cowl Panels
(2)
78-31-00/201, Thrust Reverser System
B.
Access
(1)
Location Zone
506 Engine No. 1
606 Engine No. 2
(2)
Access Panels 5738L/5739R Engine No. 1 - Fan Duct Cowl and Thrust Reverser Halves
5838L/5839R Engine No. 2 - Fan Duct Cowl and ThrustReverser Halves
C. Procedure
S 016-002-C00
(1)
Open the fan cowl panels (AMM 71-11-02/201).
S 016-003-C00
(2)
Open the thrust reversers (AMM 78-31-00/201).
S 216-004-C00
(3)
Examine the engine inlet area.
(a)
Examine the inlet cowl and the aft flange. 1) Look for the correct installation. a) Make sure all the bolts, nuts and pins are installed
and not broken. 2) Look for cracks. 3) Look for cracks or delamination in the acoustic panels.
(b)
Examine the front and rear cones of the spinner for dents or gaps.
S 216-005-C00
(4) Examine the fan cowl panels.
(a)
Examine the composite skin for cracks or delamination.
(b)
Examine the aluminum foil on the interior lining for cracks or delamination.
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ALL ú ú C02 Page 601 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(c)
Examine the access doors for cracks, loose fasteners, and loose hinges. 1) Make sure the access doors are in the closed position.
(d)
Examine the hold-open rods for worn areas on the hinge bolts and stowage receivers. 1) Do a check for the correct operation of the double action
lock.
(e)
Examine these components for worn areas, cracks, corrosion and loose fasteners: 1) The hinge fittings and roll pins 2) The latches 3) The latch hooks and keepers
(f)
Make sure the latches operate correctly.
S 216-006-C00
(5)
Examine the exhaust ports and drain holes for blockage.
S 216-007-C00
(6)
Examine the T2 and T12 sensors for dents or cracks, and sealant that has gone away.
S 216-008-C00
(7)
Examine the forward fairing for serviceable condition and the correct installation.
(a)
Make sure the pressure relief door is in the closed position.
S 216-009-C00
(8)
Examine the fan duct cowl and thrust reverser halves:
(a)
Examine the composite skin for cracks or delamination.
(b)
Examine the latches for cracks.
(c)
Make sure the latches operate correctly.
S 216-010-C00
(9)
Examine the engine oil system.
(a)
Examine these components for leakage and the correct
installation.
1) The oil tank
2) The oil filler cap
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 動力裝置 POWER PLANT 1(86)
