(2)
AMM 32-12-00/501, Main Gear Doors
D.
Access
(1)
Location Zones
211/212 Control Cabin
731/741 Main Landing Gear (MLG)
732/742 MLG Body Doors
733/743 MLG Oleo Doors
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E. Install the Trunnion Fairing Door
S 424-009
(1)
Install the hinge bolts (9), the washers (8 and 10), the bushings (11), and the nuts (12) to connect the door hinges to the support beam. Tighten the nuts to 95-100 pound-inches (Detail B).
S 824-015
(2)
If you will install a new operating rod, do the steps that follow to adjust the length of the rod:
(a)
Loosen the adjust bolts on the pushrod adjust tool so that the slotted plates can move freely
(b)
Install the rod ends of the old rod on the pins on the slotted plates
(c)
Tighten the adjust bolts so that the slotted plates cannot move
(d)
Remove the old rod from the pushrod adjust tool
(e)
Adjust the length of the new operating rod to match the two pin locations on the pushrod adjust tool. The fit of the new rod on the pins of the adjust tool should be tight.
(f)
Tighten the jamnut on the new rod
(g)
Install lockwire on the jamnut
(h)
Remove the new pushrod from the pushrod adjust tool.
S 434-013
(3)
Install the bolts (3), the washers (4 and 6), the bushings (5) and the nuts (7) to connect the pushrod (2) to the strut door and the fairing door.
F.
Put the Airplane Back to Its Usual Condition
S 094-012
(1)
Remove the downlocks on the nose and main landing gear
(AMM 32-00-20/201).
S 864-010
(2)
Remove the DO-NOT-OPERATE tag from the control lever for the landing gear.
S 824-011
(3)
If you replaced the door or changed the rigged length of the pushrod, then do the task "Adjust the Trunnion Fairing Door" (AMM 32-12-00/501).
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MAINTENANCE MANUAL
S 824-020
(4) Adjust the trunnion fairing door (AMM 32-12-00/501).
NOTE: Adjustment of the trunnion fairing door is not necessary if
____ the same door, attaching hardware and adjustment rod that was removed is reinstalled and the jamnut on the adjustment rod is not loosened.
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MAIN GEAR TRUNNION FAIRING DOOR - INSPECTION/CHECK
__________________________________________________
1. General_______
A. This procedure only has illustrations, and a wear limit table which shows the data for wear limits. There are no procedures for access, removal, or installation of the parts. Refer to the Main Gear Trunnion Fairing Door - Removal/Installation for the procedures to do these tasks.
TASK 32-12-10-206-001
2. Wear Limits for the Trunnion Fairing Door of the Main Landing Gear__________________________________________________________________ (Fig. 601)
A. Wear Limits for the Trunnion Fairing Door
S 226-002
(1) Refer to Fig. 601 for the inspection points and the wear limits table.
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