NO
DO A CHECK FOR WORN AREAS AMM 52-41-11/401). ON THE CONTROL CAM AND THE CAM FOLLOWER ROLLERS.
ARE THE CONTROL CAM AND
NO
CAM FOLLOWER ROLLERS WORN? 46 LUBRICATE THE CONTROL CAM TRACKS AND THE CAM FOLLOWER ROLLERS FOR THE APPLICABLE DOOR (AMM 12-25-11/301, AMM 12-25-21/301, AMM 12-25-41/301).
YES
47 DO THIS PROCEDURE: THE
UNLATCHED POSITION TO THE
5 MOVE THE DOOR FROM THE YES
FAULT IS IN THE DOOR COCKING LATCHED POSITION.
CYCLE (FIG. 106).
NO
DO THE LATCH ROLLERS HIT, RUB, OR NOT ENGAGE THE LATCH FITTINGS?
48 ADJUST THE LATCHINGNO
MECHANISM FOR THE APPLICABLE
DOOR (AMM 52-11-00/501,
AMM 52-13-00/501,
AMM 52-41-00/501).
YES YES
6 OPERATE THE DOOR GATES.
24 REMOVE THE LINING FOR THE
49 REPLACE THE DAMAGED OR
DO THE GATES TOUCH THE APPLICABLE DOOR WORN COMPONENTS FOR THE CUTOUT COMPONENTS DURING (AMM 52-11-31/401, APPLICABLE DOOR (OHM 52-16-01 OPERATION?
AMM 52-13-21/401, FWD ENTRY DOOR, OHM 52-16-03 AMM 52-41-31/401). AFT ENTRY DOOR, OHM 52-46-05
NO
ARE THERE ANY DAMAGED AFT GALLEY DOOR, OHM 52-46-06 COMPONENTS OR WORN COMPONENTS? FWD GALLEY DOOR). SEE SHEET 3
NO
(BLOCK 7)
50 ADJUST THE LATCHING
MECHANISM FOR THE APPLICABLE
DOOR (AMM 52-11-00/501,
AMM 52-13-00/501,
AMM 52-41-00/501).
The Fault Is In the Door Latch/Unlatch Cycle
Figure 107 (Sheet 2)
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737-300/400/500MAINTENANCE MANUAL
FROM SHEET 2 (BLOCK 6)
NO
YES
7
DO A CHECK OF THE FUSELAGE
51 DO THIS PROCEDURE: THE
CUTOUT FOR DAMAGE.
DO THE DOOR STOP FITTINGS HIT THE BODY STOP FITTINGS?
NO
YES
8
MAKE SURE ALL THE STOP
PINS ARE INSTALLED.
DO THE DOOR STOP PINS HAVE MORE THAN 0.030 INCH OR LESS THAN 0.015 INCH CLEARANCE BETWEEN THE PIN AND THE FITTING?
NO
GUIDE ARM CAM FOLLOWER PIN BINDS IN THE CAM PLATE TRACKS (FIG. 104).
52 ADJUST THE STOP PINS
FOR THE APPLICABLE DOOR
(AMM 52-11-00/501,
AMM 52-13-00/501,
AMM 52-41-00/501).
L15289
The Fault Is In the Door Latch/Unlatch Cycle
Figure 107 (Sheet 3)
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ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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737-300/400/500MAINTENANCE MANUAL
DOOR SEALS - APPROVED REPAIRS
_____________________________
1. General
_______
A. This procedure contains instructions to repair the pressure seals on the doors and the hatches. You can also use this procedure to repair the pressure seals on all pressure sealed access doors.
B. These are the usual types of damage to the seals:
(1)
The joints where the mechanical blade seal joins the diaphragm seal can pull apart (Fig. 801)
(2)
There can be holes, nicks and splits in the seal
(3)
Splices can be unsatisfactory on the continuous blade seals.
C.
These three types of adhesives are used for repairs to the seals:
(1)
Type I adhesive has two parts and cures in the air. You can handle this adhesive after 8 hours. Do not put force on the adhesive until after 24 hours. General Electric SR-529 or PSA-529 adhesive with SRC-18 catalyst is a Type I adhesive.
(2)
Type II adhesives have one part and dry in the air. It is a clear, flexible adhesive that stays flexibile when it is cold. You can handle this adhesive after 24 hours. Do not put force on the adhesive until after 48 hours. Use this adhesive for repairs to the blade seals where flexibility makes a good seal. Dow Corning 732 RTV Clear, General Electric RTV 108, and Dow Corning Q3-7063 are Type II adhesives.
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