73-21-06
ALL ú ú N03 Page 408 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
3) Discard the key washer used with the nut.
CAUTION: DO NOT TRY TO TURN THE EEC SPEED TRANSDUCER UNTIL IT IS
_______ DISENGAGED FROM THE INNER BRACKET. IF YOU TURN THE SPEED TRANSDUCER WHEN IT IS ENGAGED WITH THE INNER BRACKET, YOU CAN CAUSE DAMAGE TO THE EEC SPEED TRANSDUCER.
(e) Use the jackscrews to break the interface between the flange of the EEC speed transducer and the intermediate case and remove the EEC speed transducer from the engine.
NOTE: The jackscrew holes are 0.190-32 UNJF thread.
____
(f)
Discard the three packings from the EEC speed transducer.
(g)
Install a protection cap on the opening in the intermediate case.
TASK 73-21-06-404-015-N00
3. Install the EEC Speed Transducer (N1) (Fig. 401)
_____________________________________
A. Standard Tools and Equipment
(1)
Mats - Protective, Rubber Manufacturers Association Grade SC43, Neoprene Sponge, 1 inch (25 mm) thick, approximately 3 X 4 feet (90 X 120 cm) with warning streamers attached (three are necessary)
(2)
M303, M305, or M307 Bergen Mechanical Crimper
Bergen Cable Technologies Inc
170 Gregg St
P.O.
Box 1300
Lodi, NJ 07644-9982
B.
Consumable Materials
(1)
D00045 Beeswax
(2)
D00250 Petrolatum White, VV-P-236
(3)
D00390 Oil - Engine
(4)
G02334 Lockwire - AS3214-02
(5)
G02332 Ferrule - P05-292 (Optional)
(6)
G02335 Cable - Safety - P05-291 (Optional)
C.
References
(1)
AMM 70-24-05/201, Electrical Harnesses
(2)
AMM 71-00-00/501, Power Plant
(3)
AMM 71-11-04/201, Fan Cowl Panels
(4)
AMM 71-11-06/201, Core Cowl Panels
(5)
AMM 72-34-03/401, Fan Exit Liner Segment
(6)
AMM 78-31-00/201, Thrust Reverser System
(7)
IPC 73-21-06 Fig. 5
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-21-06
ALL ú ú N03 Page 409 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
D. Access
(1)
Location Zone
412 Engine 1 - Intermediate Case 5 o'clock
422 Engine 2 - Intermediate Case 5 o'clock
432 Engine 3 - Intermediate Case 5 o'clock
442 Engine 4 - Intermediate Case 5 o'clock
(2)
Access Panel
416 Right Thrust Reverser Half - Engine 1
426 Right Thrust Reverser Half - Engine 2
436 Right Thrust Reverser Half - Engine 3
446 Right Thrust Reverser Half - Engine 4
E.
Procedure
S 864-016-N00
(1)
Install the DO-NOT-OPERATE tag on the applicable FUEL CONTROL switch.
S 824-019-N00
(2)
Examine the tip clearance for the EEC speed transducer.
(a)
Apply the beeswax to the flat surface on the end of the shaft for the EEC speed transducer, approximately 0.07 inch (1.8 mm) in thickness.
(b)
Put the Class 1 shim on the end of the shaft, against the shoulder.
NOTE: Do not install the three packings on the EEC speed
____
transducer at this time.
CAUTION: INSTALL THE EEC SPEED TRANSDUCER WITH THE LARGER
_______ ELECTRICAL CONNECTOR TO THE REAR. DO NOT TRY TO TURN THE EEC SPEED TRANSDUCER WHEN IT IS ENGAGED WITH THE INNER BRACKET. IF YOU TURN THE SPEED TRANSDUCER WHEN IT IS ENGAGED WITH THE INNER BRACKET, YOU CAN CAUSE DAMAGE TO THE EEC SPEED TRANSDUCER.
(c)
Carefully install the EEC speed transducer in the intermediate case with the larger electrical connector to the rear.
(d)
Install the EEC speed transducer with the steps that follow:
1) Lubricate the threads of the bolts, which attach the EEC speed transducer, with engine oil.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 發動機燃油和控制 2(34)
