(2)
Open the core cowl panel (AMM 71-11-06/201).
(3)
Remove the bolt which attaches the latch to the latch fitting.
(4)
Remove the latch from the core cowl panel.
S 014-003-N00
S 034-004-N00
S 024-005-N00
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////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE A
CORE COWL PANEL
1 WASHER
1 NUT
LATCH FITTING
2 FWD A BOLT 1 LATCH
1 BOLT DIRECTION IS REARWARD
2 BOLT DIRECTION IS FORWARD
Figure 401 Core Cowl Panel Latch Installation
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TASK 71-11-07-404-006-N00
3. Install the Core Cowl Panel Latch (Fig. 401)
_________________________________
A. References
(1)
AMM 71-11-06/201, Core Cowl Panel
(2)
AMM 71-11-07/501, Core Cowl Panel Latch
(3)
AMM 78-31-00/201, Thrust Reverser System
(4)
IPC 71-11-07 Fig. 1
B.
Access
(1)
Location Zone
417 and 418 Core Cowl Panel - Engine 1
427 and 428 Core Cowl Panel - Engine 2
437 and 438 Core Cowl Panel - Engine 3
447 and 448 Core Cowl Panel - Engine 4
C.
Procedure
S 424-007-N00
(1)
Install the latch in the latch fitting.
S 424-012-N00
(2)
Attach the latch with the bolt, washer, nut, and cotter pin.
S 824-008-N00
CAUTION: MAKE SURE THE LATCHES ON THE CORE COWL PANEL ARE ADJUSTED
_______ CORRECTLY. WHEN THE ENGINE IS IN OPERATION, IT MOVES AND BECOMES LARGER. IF THE LATCHES ARE NOT CORRECTLY ADJUSTED, DAMAGE TO THE ENGINE OR THE CORE COWL PANEL CAN OCCUR.
(3)
Adjust the latches (AMM 71-11-07/501).
(4)
Close the core cowl panel (AMM 71-11-06/201).
S 864-010-N00
(5)
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
S 414-009-N00
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CORE COWL PANEL LATCH - ADJUSTMENT/TEST
_______________________________________
1. General
_______
A. This procedure gives the instructions to adjust the latches for the core cowl panel.
B. You must adjust the latches to get the correct aerodynamic smoothness and latch tension.
C. You must adjust the latches and shims when you replace the engine, core cowl panel, thrust reverser or core cowl latch.
D. You must install the thrust reverser with all latches adjusted and closed, before you adjust the latches for the core cowl panels.
TASK 71-11-07-825-024-N00
2. Adjust the Core Cowl Panel Latch
________________________________
A. Standard Tools and Equipment
(1)
Hex Wrench - 3 millimeter or 7/64 inch standard long series
(2)
Scale - Push Pull, 60 pound (267-N) capacity
B.
Consumable Materials
(1)
G02020 Clay - Modeling
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本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 動(dòng)力裝置 POWER PLANT 2(81)
