S 014-038-N00
(2) Open the applicable fan cowl panel (AMM 71-11-04/201).
S 044-039-N00
WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
(3)
Do this procedure: Thrust Reverser Deactivation for Ground Maintenance (AMM 78-31-00/201).
S 014-037-N00
(4)
Open the applicable core cowl panel (AMM 71-11-06/201).
S 014-040-N00
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU OPEN THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(5)
Open the applicable thrust reverser (AMM 78-31-00/201).
D.
Procedure
S 014-004-N00
(1) For the left control valve (4), remove the pneumatic manifold (AMM 36-11-01/401).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
75-33-01
ALL ú ú N03 Page 405 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 024-050-N00
(2)
Remove the control valves:
(a)
Disconnect the EEC electrical connector (6) from the control valve (4). 1) Install protection caps to the EEC electrical connector (6)
and the receptacle on the control valve (4).
(b)
ENGINES POST-PW-SB 75-91;
Disconnect the air signal tube from the adapter (11).
(c)
Remove the hose clamp (8) which attaches the cooling air hose
(7) to the control valve (4).
(d)
Disconnect the cooling air hose (7) from the control valve (4).
(e)
For the left control valve (4), remove the bolt (16) and nut (15) that attach the No. 3 bearing breather tube to the bracket (14).
(f)
ENGINES POST-PW-SB 73-164; For the right control valve (4), disconnect the bracket (15) from the cover (9) with the steps that follow: 1) Remove the two bolts (1) and washers (16) that attach the
bracket (15) to the cover (9). 2) Move the bracket (15) away from the control valve (4) with the harness attached to it.
(g)
ENGINES POST-PW-SB 79-52; For the left control valve (4), remove the bolt (22) and the nut (24) that attach the clamp (23) of the trim-line oil tube (21).
(h)
For the right control valve (4), remove the control valve (4) from the engine with the steps that follow: 1) Remove the bolts (5) which attach the control valve (4). 2) Remove the control valve (4) and the gasket (3) from the
HPC case.
a) Discard the gasket (3).
(i)
ENGINES PRE-PW-SB 79-52; For the left control valve (4), remove the control valve (4) from the engine with the steps that follow: 1) Remove the bolts (5) which attach the control valve (4).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
75-33-01
ALL ú ú N02 Page 406 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
2) Remove the control valve (4) and the gasket (3) from the HPC case. a) Discard the gasket (3).
(j) ENGINES POST-PW-SB 79-52; For the left control valve (4), remove the control valve (4) from the engine with the steps that follow: 1) Remove the bolts (5) which attach the control valve (4) and
the bracket (20).
2) Remove the control valve (4), the bracket (20) and the gasket (3) from the HPC case. a) Discard the gasket (3).
(k) Install a protection cap on the HPC case pad.
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 大氣 AIR 2(93)
