(e)
Put the springs (1) and (5) on the spring retainer bolts.
(f)
Install the washers and the nuts (7).
(g)
Tighten the nuts with your hand.
(h)
Install the cotter pins.
(i)
Extend the springs (1, 5).
(j)
Move the connections above each end of the lock spring shaft (19).
(k)
Install the washers and nuts.
(l)
Tighten the nuts with your hand.
(m)
Install the cotter pins.
(n)
AIRPLANES THE THE HOSE GUARD; Install the hose guard on the lock brace (3) as far aft as possible without against the radius.
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A 737-300/400/500MAINTENANCE MANUAL
(o) Install the lock sensor in the support bracket.
NOTE:____ Adjust it if it is necessary (AMM 32-61-41/401).
(p) (q) Do a check of the operation of the nose landing gear (AMM 32-33-00/501).Lower the airplane and remove the jack (AMM 07-11-21/201).
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A
737-300/400/500MAINTENANCE MANUAL
NOSE LANDING GEAR LOCK MECHANISM - INSPECTION/CHECK
___________________________________________________
1. General
_______
A. This procedure only has illustration and a wear limits table which shows the data for wear limits. There are no procedures for the access, the removal, or the installation of the parts. Refer to the Nose Landing Gear Lock Mechanism - Removal/Installation for procedures to do these tasks.
TASK 32-33-51-206-001
2. Wear Limits for the Lock Mechanism of the Nose Landing Gear (Fig./601)
___________________________________________________________
A. Wear Limits for the Lock Mechanism
S 226-002
(1) Refer to Fig. 601 for the inspection points and the wear limits table.
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A 737-300/400/500MAINTENANCE MANUAL
UPPER DRAG BRACE ASSEMBLY
SEE A
FORWARD LOCK LINK ASSEMBLY
LOWER DRAG
BRACE ASSEMBLY
SHOCK STRUT OUTER CYLINDER ASSEMBLY
FWD
C
UPPER DRAG
BRACE ASSEMBLY
A
B
B
AFT LOCK BRACE ASSEMBLY
FORWARD LOCK
LINK ASSEMBLY LOCK ACTUATOR
LOWER DRAG
BRACE ASSEMBLY
A
11. BEARING/BOLT
A
Nose Gear Lock Mechanism Wear Limits Figure 601 (Sheet 1)
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737-300/400/500MAINTENANCE MANUAL
UPPER DRAG 7. BUSHING/ BRACE ASSEMBLY BUSHING
C-C
1
SUM OF A AND B
Nose Gear Lock Mechanism Wear Limits Figure 601 (Sheet 2)
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A
