S 034-064
(15)
If it is necessary, loosen the four support clamps for the shock strut door (1, 4, 9 and 11).
S 224-061
(16)
Examine the clearance around the shock strut door.
S 034-016
(17)
If the clearance is in or less than the tolerance, loosen the four support clamps for the strut door (1, 4, 9 and 11).
S 824-017
(18)
Hold the outer door.
(a) Adjust the center door until the outer door has an overlap on
the center door 0.50 |0.10 inch.
(b) Examine that a clearance of 0.20 - 0.60 inch is between the
center door and the aft wing skin panels.
NOTE:____ If you move the support clamps (1, 4, 9, 11) during the
door removal, put the clamps at the distances shown.
If not installed, you can apply mylar tape between the
clamps and the shock strut/drag strut. Trim the edges
to match the outer side of the clamps.
S 844-018
(19)
Tighten the four support clamps for the strut door (1, 4, 9 and 11) if they were loosened.
(a)
Put an index stripe mark on the clamp (9) and the outer cylinder of the shock strut (Fig. 401, Sheet 3), if it was removed.
S 824-065
(20)
Adjust the door support link until you align the center door with the wing contour in | 0.06 inch.
S 824-060
(21)
Extend the gear.
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A
737-300/400/500MAINTENANCE MANUAL
S 424-059
(22)
Install the bolt to connect the adjustable rod (7) to the control rod support (6).
S 424-062
(23)
Connect the control rod for the outboard wing door.
S 824-049
(24)
Retract the gear.
S 844-050
(25)
Set the control lever for the landing gear in the neutral position.
S 224-021
(26)
Examine the fit of the inner and the outer doors.
(a)
You must align the outer door with the wing fairing in less than | 0.06 inch.
(b)
You must align the inner door with the body fairing in less than | 0.06 inch.
S 824-022
(27)
Extend the gear.
S 824-023
(28)
Adjust the inner control rods (7) for the wing door to meet the conditions of step above.
(29)
Do the above steps again until you get the necessary tolerances.
S 764-025
(30)
Examine whether the electrical power is necessary on the airplane.
(a)
If the power is not necessary, turn off the power sources.
(31)
Lower the airplane and remove the jacks (AMM 07-11-11/201).
S 824-024
S 844-026
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A
737-300/400/500MAINTENANCE MANUAL
TASK 32-13-11-024-045
4. Shock Strut Inner Door Removal (Fig. 401)______________________________
A. References
(1)
AMM 32-00-01/201, Ground Lock Assemblies
B.
Access
(1)
Location Zone
310 Left Main Landing Gear
410 Right Main Landing Gear
C.
Shock Strut Inner Door Removal
S 494-027
(1)
Make sure that you install the ground lock assemblies (AMM 32-00-01/201).
S 024-063
(2)
Remove the bolt to disconnect the adjustable control rod (7) from the control rod support (6).
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 起落架 LANDING GEAR 2(2)
