S 024-036-N00
(1) Do the steps that follow to remove the Fan Exit Fairing:
NOTE: Unless it is specified differently, remove the shoulder
____ screws with a No. 3 cross-drive (Phillips). Remove all of the other screws with a No. 10 Torq-set drive.
(a)
Cut and remove the sealant from around the cover plate (10).
(b)
Remove the screws (11) and the cover plate (10).
(c)
Cut and remove the sealant from around the access covers (6).
(d)
Remove the screws (4) and (5), and the access covers (6).
(e)
Remove the classified washers that are on the inner side of the bolt holes (4), if there are some installed.
(f)
Cut and remove the sealant from around the top of the outer fairing (1).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-34-04
ALL ú ú N01 Page 408 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
FAN EXIT (BIFURCATION) OUTER FAIRING SEE D
SEE A FAN EXIT (BIFURCATION) INNER FAIRING
SEE C
COVER PLATE SEE B
ACCESS COVER (2 LOCATIONS)
SEE C
FAN EXIT (BIFURCATION) FAIRING INSTALLATION
A L-A8017 (000) Fan Exit (Bifurcation) Fairing Installation Figure 402 (Sheet 1)
D04745
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-34-04
ALL ú ú N01 Page 409 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
10.COVER PLATE
3. FAN EXIT
INNER
FAIRING
11.SCREW (8 LOCATIONS)
A A
6. ACCESS COVER FAN EXIT CASE (2 LOCATIONS) (REAR VIEW)
FAN EXIT FAIRING COVER PLATE
B
3. FAN EXIT INNER FAIRING
FAN EXIT (BIFURCATION) INNER FAIRING C
1. FAN EXIT OUTER FAIRING
FAN EXIT (BIFURCATION) OUTER FAIRING D
Fan Exit (Bifurcation) Fairing Installation Figure 402 (Sheet 2)
D04746
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-34-04
ALL ú ú N01 Page 410 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
3. FAN EXIT FAIRING
4. SCREW
(COVER)
V-RAIL 5. SCREW
6. ACCESS (COVER)
COVER
HARNESS HARNESS
A-A
L-A5989 (0292)
Fan Exit (Bifurcation) Fairing Installation
Figure 402 (Sheet 3)
D04747
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-34-04
ALL ú ú N01 Page 411 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
B
SCREW (4 LOCATIONS, EACH SIDE)
SCREW (4 LOCATIONS, EACH SIDE)
10. COVER PLATE
5.
SCREW (3 LOCATIONS, EACH SIDE)
6.
ACCESS COVER (TWO SIDES)
8. SCREW BE BE
(2 LOCATIONS, 9. SCREW 4. SCREW
EACH SIDE) EACH SIDE) (1 LOCATION, (SHOULDER) (2 LOCATIONS, EACH SIDE)
L-A8010 (0000)
Fan Exit (Bifurcation) Fairing Installation Figure 402 (Sheet 4)
D04766
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-34-04
ALL ú ú N01 Page 412 ú Oct 10/94
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 ENGINE 2(60)
