Sling Assembly Installation
Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
55-30-00
ALL ú ú B01 Page 402 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
TO THE OVERHEAD CRANE
REAR SPAR
SLING ASSEMBLY C55004-1
Sling Assembly Installation
Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
55-30-00
ALL ú ú B01 Page 403 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FUSELAGE FITTING
INBD
AFT
INCH
FRONT SPAR FITTING
REAR SPAR FITTING
MAKE SURE THERE IS NO CLEARANCE BETWEEN THE BOLT HEAD AND THE WASHER WHEN YOUEXAMINE THE NECCESSARY CLEARANCE BETWEEN THE FITTING AND THE NUT.
Vertical Fin-to-Fuselage Fitting Figure 402 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
55-30-00
ALL ú ú B01 Page 404 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FIN
FITTING MAXIMUM TOTAL CLEARANCE OF
0.012 INCH BEFORE THE NUT FWD
IS TIGHTENED (OUTBOARD AND INBOARD FITTINGS) (2 LOCATIONS)
FUSELAGE FITTING
LOCKWIRE
FIN
HOLE
FUSELAGE
ANTIRATTLE
FITTINGS
WASHER
Vertical Fin-to-Fuselage Fitting
Figure 402 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
55-30-00
ALL ú ú B01 Page 405 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E07040
C.
D.
E.
A
737-300/400/500MAINTENANCE MANUAL
(5)
F70207-69 Rig Pin Kit (Centering Unit Output Crank R-5)References
(1)
AMM 27-21-00/201, Rudder and Rudder Trim Control System
(2)
SRM 51-70-00, Repairs (Example)Access
(1)
Location Zones 201/202 Control Cabin 700 Empennage
(2)
Access Panels 3701 Stab Trim Access Door 9503/9504 Front Spar Access Door 9505/9506 Rear Spar Access Door
Prepare for the Removal
S 864-002-B00
(1) Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
P6 Load Control Center - Right
1) VHF NAV-2 VOR/ILS
2) INSTR XFMR-2
(b)
P6-1 Panel
1) HF AC
2) HF DC
(c)
P18 Load Control Center - Left
1) VHF NAV-1 VOR/ILS
2) INSTR XFMR-1
(d)
P18-2 Panel
1) HF AC
2) HF DC
S 864-003-B00
WARNING:_______RELEASE THE PRESSURE IN THE RUDDER HYDRAULIC SYSTEM. THE RUDDER CAN MOVE IF YOU PRESSURIZE THE SYSTEM. IF THE RUDDER MOVES, THE RUDDER CAN CAUSE INJURY TO PERSONS.
(2)
Do this task: "Remove the Pressure from Rudder Hydraulic Systems A and B" (AMM 27-21-00/201).
S 414-004-B00
(3)
Open the vertical fin access doors.
(a)
Open the Stab Trim Access Door 3701.
(b)
Open the Front Spar Access Doors 9503 and 9504.
(c)
Open the Rear Spar Access Doors 9505 and 9506.
(4)
Install a rudder gust lock with a warning streamer.
S 494-005-B00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 安定面 STABILIZERS(8)