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A
737-300/400/500
MAINTENANCE MANUAL
ELEV ELEV
STA STA
213.32 195.00 176.64 149.12 121.59 94.07 66.54 39.02
ELEVATOR TAB
ELEV ELEV ELEV ELEV
STA STA STA STA
149.12 121.59 94.07 ELEVATOR BALANCE 66.54
ELEVATOR TAB ADJUST WEIGHTS
1
INBD
B-B
ADD OR REMOVE WEIGHTS IF REQUIRED AND TAB ADJUSTINSTALL BOLTS IN HOLES NOT USED FOR WEIGHTSWEIGHT ATTACHMENT IN UPPER SURFACE
A-A
ONLY
Elevator Tab Adjust Weights Location Diagram Figure 403
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A 737-300/400/500MAINTENANCE MANUAL
9) Seal the nutplate, the edge of the elevator tab skin and the hinge fitting with sealant.
(5) S 864-019Manually turn all the hinge fittings through full travel. (a) Make sure that the hinge fittings move freely.
(6) S 434-021Install the elevator tab and the hinge fittings at the elevator rear spar. (a) Install the bolt, the washer, the bushings and the nut. (b) Tighten the nut to 50 to 80 pound-inches. (c) Align the cotter pin holes on the nut and bolt and install the cotter pin.
(7) S 864-020Move the elevator tab through full travel. (a) Make sure that the elevator tab moves freely.
(8) S 434-017At the hinge fittings of the inboard and outboard elevator tab, install the bonding jumpers to the elevator tab. (a) Clean the mating surfaces for the bonding jumpers. (b) Use the milliohmmeter to make sure the resistance of the bonding jumper connection is less than 0.010 ohms. (c) Seal the bonding jumpers with sealant.
(9) S 434-018Connect the elevator tab pushrods to the elevator tab. (a) AIRPLANES WITH THE ALUMINUM TAB PUSHRODS; Make sure you install the bushings. 1) Install the bolts with the threaded ends pointed toward each other. (b) AIRPLANES WITH THE TITANIUM TAB PUSHRODS; Make sure you install the bushings. 1) Install the bolts with the threaded ends pointed towards each other. (c) Do not install the nut and the washer until you align the elevator tab.
CAUTION:_______ IF NUTS ARE NOT TORQUED PROPERLY THEN THE PUSHRODS CAN BECOME DETACHED AND CAUSE DAMAGE TO THE ELEVATORS AND STABILIZERS.
(d) Tighten the nut to 30 - 50 pound-inches.
NOTE:____ Make sure that a new nut is installed.
1) Make sure that torque remains at 30 - 50 pound-inches after alignment of the nut castallations and bolt cotter pin holes.
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737-300/400/500MAINTENANCE MANUAL
S 094-009
(10)
Remove the rig pin E-5 from the aft control quadrant.
S 864-008
(11)
Do this task: "Put the Elevator Hydraulic Systems A and B Back to the Condition Before the Pressure Removal" (AMM 27-31-00/201).
S 824-010
(12)
Adjust the elevator tab:
(a)
If you install the same tab that you removed and the measurements for elevator tab positon were not recorded in the "Remove elevator tab" step of this procedure: Adjust the elevator tab system per AMM 27-31-00/501.
(b) 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 2(158)
