7.
ATTACHMENT LINK FWD INBD BOLT
A
1. ACTUATOR
BEAM
BRACKET ON STRUCTURE
BOLT 7
2. ACTUATOR
A
15. BEAM HANGER INBD 2B
FWD
AB
INBD3. ACTUATOR BEAM
OUTBOARD ATTACHMENT BOLT18. STUD ASSEMBLY
B-B
B
THE BOLT CAN BE INSTALLED WITH THE HEAD ON THE
INBOARD OR THE OUTBOARD SIDE.
Main Landing Gear Beam Hanger Shaft Installation
Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-32-93
ALL ú ú 01 Page 402 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
15.
BEAM HANGER
16.
SPACER 16. SPACER 2
18. STUD ASSEMBLY
4. BEAM HANGER SHAFT
1
0.001-0.135 INCH 0.016-0.060 INCH
5 6
A-A3
15. BEAM HANGER
18. STUD ASSEMBLY
2
4. BEAM HANGER
SHAFT
1
0.01-0.110 INCH
A-A 4
OUTER WING
10. STABILIZING
DOOR HINGE BEAM
BRACKET ON
11. TRUNNION
STRUCTURE
LINK
12. OUTER WING DOOR PUSHROD
BRACKET ON
STRUCTURE
14. OUTER
SEEF
WING DOOR
13. BONDING 9. WING DOOR CABLE FWD HINGE BOLT 10. STABILIZING
E
BEAM
1 THE BEAM HANGER SHAFT 4 FOR 737-400 AIRPLANES ONLY
F
IS ALSO KNOWN AS THE
5 TOTAL ALLOWABLE GAP BETWEEN
TUBE ASSEMBLY.
THE BEAM HANGER SHAFT/STUD
2
THE BEAM HANGER IS ALSO
ASSEMBLY AND THE BEAM HANGER.
KNOWN AS THE SUPPORT LINK.
6TOTAL ALLOWABLE GAP BETWEEN
3
FOR 737-300/-500
THE STUD ASSEMBLY AND THE
AIRPLANES ONLY
TUBE ASSEMBLY.
Main Gear Beam Hanger Shaft Installation
Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-32-93
ALL ú ú 01 Page 403 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 014-006
(5)
Disconnect the inboard end of the actuator beam (1) from the actuator beam arm (8).
S 024-007
(6)
Remove the beam hanger shaft (4).
(a)
Hold the actuator assembly and remove the bolts that attach the ends of the beam hanger shaft (4) and stud assembly (18) to the brackets on the structure.
(b)
Lower the outboard end of the actuator assembly to get access to the beam hanger shaft (4).
(c)
Write the quantity and locations of spacers (16) at the ends of the beam hanger shaft (4) and the stud assembly (18) for use on the installation.
(d)
Loosen the stud assembly (18) and remove it from the beam hanger shaft (4).
(e)
Remove the beam hanger shaft (4) from the beam hanger (15).
TASK 32-32-93-404-008
3. Main Gear Beam Hanger Shaft Installation (Fig. 401)________________________________________
A. Consumable Materials
(1)
G01395 Compound - Corrosion Inhibiting, BMS 3-27, Mastinox 6856K
(2)
D00633 Grease - BMS 3-33
(3)
D00013 Grease - MIL-PRF-23827
(4)
C00259 Primer - BMS 10-11, Type I (Ref 20-30-41)
B.
References
(1)
AMM 07-11-11/201, Jack Airplane
(2)
AMM 32-32-00/501, Main Gear Extension and Retraction - Adj/Test
(3)
AMM 32-32-11/401, Main Gear Actuator Assembly
C.
Access
(1)
Location Zone
101,102 Control Cabin
310,410 Main Landing Gear
(2)
Access Panel
8401,8501 Hydraulic Access Panel
D.
Installation
S 144-009
(1) Clean the surfaces of the beam hanger shaft (4), spacers (16), stud assembly (18), and beam hanger (15).
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