Shock Strut
Figure 2
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757 MAINTENANCE MANUAL
NOSE GEAR - REMOVAL/INSTALLATION
________________________________
1. General
_______
A. This procedure contains two tasks. The first task removes the nose landing gear. The second task installs the nose landing gear.
TASK 32-21-01-004-001
2. Remove the Nose Landing Gear (Fig. 401)
____________________________
A. Equipment GUN (1) Transportation Dolly for the Nose Landing GUN Gear - A32038-23 or P/N 0-32-58070
(2)
Nose Landing Gear Shock Strut Lock - B32019-1
(3)
Nose Landing Gear Overhead Removal/Installation Equipment - B32005-68
(4)
Fishpole Hoist - Commercially Available
(5)
Trunnion Pin Puller - B32003-1
B.
References
(1)
AMM 06-41-00/201, Fuselage (Major Zones 100 and 200) Access Doors and Panels
(2)
AMM 07-11-02/201, Jacking Airplane Nose
(3)
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
(4)
AMM 32-00-15/201, Landing Gear Door Locks
(5)
AMM 32-00-20/201, Landing Gear Downlocks
(6)
AMM 32-21-06/401, Nose Gear Lock Link Assembly
(7)
AMM 32-22-03/401, Nose Gear Aft Door
(8)
AMM 32-51-00/501, Nose Wheel Steering System
(9)
AMM 32-51-14/401, Nose Wheel Steering Upper Pulley Support Bracket
C.
Access
(1)
Location Zones
119/120 Main Equipment Center
211/212 Control Cabin
711 Nose Landing Gear (NLG)
713/714 Forward NLG Door
715/716 Aft NLG Door
(2)
Access Panel
119BL Main Equipment Center
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757
MAINTENANCE MANUAL
SEE A
A
A
SEE B
SEQUENCE VALVE
LINK A
10.
BOLT
11.
WASHER (UNDER HEAD)
12.
WASHER (UNDER NUT)
13.
NUT
14.
BUSHING
15.
LINK B FWD
16.
SUPPORT
37. BOLT
BRACKET17. CONTROL
38.
WASHER
ROD
39.
WASHER
40.
NUT
19.
BOLT
20.
WASHER (UNDER HEAD)
21.
WASHER (UNDER NUT)
18. CRANK 22. NUT FWD (4 LOCATIONS)
A
RETRACT
ACTUATOR
1.
WASHER
2.
WASHER
9. PACKING 3. NUT
(2 LOCATIONS)
8. LUBRICATION
INSERT
7. PIN
4.
BOLT
5.
WASHERS
6.
NUT
SHOCK STRUT
OF THE NOSE
LANDING GEAR
SHOCK STRUT INBD
OF THE NOSE LANDING GEAR
A-A
Nose Landing Gear Installation
Figure 401 (Sheet 1)
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757 MAINTENANCE MANUAL
34. BOLT
31. TANG
LEFT TRUNNION PIN
D-D
C-C
Nose Landing Gear Installation
Figure 401 (Sheet 2)
32-21-01
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