EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 CAUTION: IF NUTS ARE NOT TORQUED PROPERLY THEN THE PUSHRODS
_______ CAN BECOME DETACHED AND CAUSE DAMAGE TO THE ELEVATOR AND STABILIZER.
 4)  Torque nut 30 - 50 pound-inches. Make sure that torque remains at 30 - 50 pound-inches after alignment of the nut castellations and bolt cotter pin holes.
 NOTE: A minimum gap of 0.010 inch is required between
____ the thread ends of the bolts used at the attachment of the aft end of the elevator tab push rods. Operators are permitted to install up to two washers under each bolt head to obtain this minimum clearance.
 5)  Make sure that each bolt has proper protrusion through the nut.
 (c) Install the pin retainer.
____ 1 "B" DIMENSION IS MEASURED BETWEEN CENTER OF UPPER AND LOWER GIMBAL PINS NOTE: STABILIZER TRIM JACKSCREW SHOWN WITH STABILIZER LEADING EDGE AT ZERO DEGREES  "B" DIM  1  TRAMMEL BAR 
FWD 

Stabilizer Trim Jackscrew Setting
Figure 407

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 714-026
 (7) Use the spring scale and a loading block to measure the breakaway
 force (Fig. 405):
 (a) Slowly turn the elevator by hand through full travel.
 1) Make sure the elevator moves freely.
 (b) Apply a force to the elevator rear spar, adjacent to the
 inboard rib.
 1) If the elevator moves after you release it at the neutral
 position (index mark), write down the maximum force needed
 to slowly move it back to the neutral position.
 2) Measure the force at the time the elevator reaches the
 neutral position (index mark).
 3) The difference between these forces must not be more than
 1.0 pound.
 S 434-018
 (8) Attach the elevator control pushrod to the elevator (Fig. 405):
 (a) Move the elevators to the neutral position.
 (b) With the bolt head inboard, install the bolt from the inner
 side of the tail cone.
 (c) Tighten the inner nut to 500-600 pound-inches.
 (d) Tighten the outer nut to 150-220 pound-inches.
 NOTE: Do not tighten the inner nut again after you tighten the____
 outer nut.
 S 094-012
 (9) Remove the rig pin E-5 from the aft control quadrant.
 S 864-013
 (10) Do this task: "Put the Elevator Hydraulic Systems A and B Back to
 the Condition Before the Pressure Removal" (Ref 27-31-00/201).
 S 824-014
 (11) If the elevator tab position measurements were not recorded before
 removal, do this task: "Adjustment - Elevator and Tab Control
 ú  System" (AMM 27-31-00/501).
 ú
 ú  NOTE: If you install the same elevator that you removed, and____
 ú  no adjustments to the elevator system have been made, then it
 ú  is not necessary to do the adjustment of the elevator system.
 ú  Only the adjustment of the tab control system is required.
 ú
 ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 824-034
 ú ú  (12) If the elevator tab position measurements were recorded in the elevator removal steps, adjust the elevator and tab control system(AMM 27-31-00/501), except adjust the tab pushrods as follows:
　
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