S 034-022-B00

 (15)
 Remove the pins that attach the link assembly to the pedestal.

 S 034-023-B00

 (16)
 Remove the seal plate with the attached link assembly.

 S 434-038-B00

 (17)
 At the bench, assemble the (rivet) seal plate, the link assembly, and the corner plates.

 NOTE: Use the holes that are in the tie-bar for the locations to
____
 drill.

 S 214-024-B00
 (18)
 Make sure that the protective Mylar tape stays around the end of the strip.

 (19)
 Put the seal assembly into the tracks.

 S 434-025-B00
 NOTE: The plate must be bent in the opposite direction during the
____
 installation to remove the stabilizer.

 S 434-026-B00
 (20) Move the seal up and down.
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737-300/400/500MAINTENANCE MANUAL
 S 034-027-B00
 (21)
 The force to move the seal must not be more than 20 pounds and the seal must move freely.

 S 434-028-B00

 (22)
 Attach the link assembly to the pedestal with the pins and the markers.

 S 434-029-B00

 (23)
 Install the cotter pins.

 S 434-030-B00

 (24)
 Install the rub guide.

 S 434-039-B00

 (25)
 Adjust and trim the ends of the rub guide where it is necessary to keep 0.03 |0.01 inch clearance between each end of the rub guide and the track.

 S 434-031-B00

 (26)
 On the upper seal only, manually put the leading edge of the stabilizer to the full up position.

 S 214-032-B00

 (27)
 Do a check of the clearance between the uppermost rivet at the corner plates and the body structure.

 NOTE: If the rivet touches the body structure, cut the driven head
____ until it does not touch the body structure.
 D. Put the Airplane to Its Usual Condition:
 S 034-033-B00
 (1)
Remove all the protective tapes and the covers.

 (2)
Clean up the area.

 (3)
Install the center track strips (Fig. 401).

 S 164-034-B00
 S 434-035-B00
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 S 434-036-B00
 (4)  Install the upper and lower clearance panels on the stabilizer where it is necessary (AMM 12-31-81/201).
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 1.

2.

3.

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737-300/400/500MAINTENANCE MANUAL
 STRUCTURE ATTACHMENT FITTINGS - DESCRIPTION AND OPERATION
_________________________________________________________General
_______
 A.  This section describes the fittings on the fuselage used for the
 attachment of landing gear and doors.Landing Gear Attachment Fittings (Fig. 1)
________________________________
 A.  The nose landing gear attachment fittings are incorporated in the nose landing gear wheel well structure.
 B.  The main landing gear attachment fittings included in the fuselage structure consist of the fittings to which the landing gear side struts and support beams are attached. The upper member of the landing gear side struts connect to the fuselage at body stations 685 and 695. Each landing gear support beam is connected to the fuselage by means of a swinging link fitting. The lower end of this link is connected to the landing gear support beam and its upper end is connected to two fuselage fittings, one at station 695 and the other at station 706.
　
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