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a) Loosen the screws securing the stop.
b) Move the stop towards the aircraft centerline until full alignment is obtained.
c) Tighten the screws.
NOTE : The deviation value must be measured at points A, B, ...I.
Access doors - Removal / Installation
Figure 201 (1/2)
PAGE INTENTIONALLY LEFT BLANK
WA
Validity : S / N 1 - 9999 Pre-MOD. 151 52 10 Page 206
00 (BA) JUN 01
ACCESS DOORS
MAINTENANCE PRACTICES
NOTE : This procedure is applicable to L.H. and R.H. installations. Information specific to R.H. installation are given in square brackets.
1. SERVICING
None
2. REMOVAL / INSTALLATION - ACCESS DOOR (Figure 201)
A. Tools and consumable materials
- Grease (TB 04-004A)
- Cleaning agent (TB 11-003)
- Clean, lintfree cloths
B. Removal of the access door
1) Hold access door (22) [23] open, remove and discard washer (9), remove pin (10).
2) Disconnect gas strut (8).
3) Close access door (22) [23]. Remove protective caps (11), remove and discard nuts (12), retain the fitting and, if installed, shim (30).
4) Remove screws (21) and washers (20).
5) Remove door (22) [23] and remove adjustment shims (18).
6) If necessary, remove gas strut (8)
a) Remove the upholstery panel of access door (22) [23].
b) Remove and discard washer (7) and remove pin (6).
c) Remove gas strut (8).
7) If necessary, remove and disassemble the hinge fittings
a) Remove screws (16) and (15). Remove the hinge fittings.
b) Remove hinge pin (17) and remove door fitting (14) and upper fuselage panel fitting (19).
8) If necessary, remove hook (4) assy
a) Remove screws (3) and washers (2).
b) Remove hook (4) assy and retain washers (1).
C. Installation of the access door
1) Inspect parts for condition, replace as required.
2) Clean the parts with clean, lintfree cloths moistened with cleaning agent (TB 11-003).
3) If removed, install hook (4) assy
a) Assemble screws (3), washers (2), hook (4) and washers (1).
b) Secure hook assy onto access door (22) [23]. Tighten - refer to 20-00-01.
4) If removed, assemble and secure the hinge fittings
a) Lubricate hinge pin (17) with grease (TB 04-004A).
b) Assemble door fitting (14) and upper fuselage panel fitting (19) using hinge pin (17). For front hinge fitting, the knurled section of the hinge pin must be located at the front. For rear hinge fitting, the knurled section of the hinge pin must be located at the rear.
c) Secure the hinge fittings onto access door (22) [23] with screws (16) and (15). Tighten - refer to 20-00-01.
5) If removed, secure gas strut (8) onto access door (22) [23] with pin (6) and washer (7). Install the upholstery panel of access door (22) [23].
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