Subtask 52-32-11-820-055
C. Adjustment of the Drift Pins
**ON A/C 001-049, 051-099, 101-105, 201-220,
(Ref. Fig. 502/TASK 52-32-11-991-009)
**ON A/C 106-149, 221-299, 301-399,
(Ref. Fig. 502A/TASK 52-32-11-991-009-B)
**ON A/C 151-199,
(Ref. Fig. 502B/TASK 52-32-11-991-009-A) R **ON A/C 401-499,
R (Ref. Fig. 502C/TASK 52-32-11-991-009-C) **ON A/C ALL
(1)
Open the cargo door (Ref. TASK 52-30-00-860-001) to get access to the fuselage pockets of the drift pins.
(2)
Measure the distance X between the external contour of the cargo door to the flat of the drift pin (16).
(3)
Measure the distance Y between the outer skin of the fuselage and the plate (17) in the fuselage pockets.
(4)
Put shim(s) (15) under the plate (17) until the dimension of the distance Y is the same as the distance X.
NOTE : A tolerance of 0.0 +0.5 -0.0 mm (0.0000 +0.0196 -0.0000 in.)
____
is permitted.
(5) Close the cargo door (Ref. TASK 52-30-00-860-002).
1EFF : ALL 1 52-32-11Page 518 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
Subtask 52-32-11-220-056
D. Dimensional Check **ON A/C 001-049, 053-099, 101-105, 201-220,
(Ref. Fig. 502/TASK 52-32-11-991-009) **ON A/C 106-149, 221-299, 301-399,
(Ref. Fig. 502A/TASK 52-32-11-991-009-B) **ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
(1) Make sure that the clearances of latching hooks (3) and the roller
(4) between FR53A and FR55 are correct.
NOTE : The permitted clearance is 0.2 mm (0.0078 in.)
____
(2)
Install the access panel 826AR on the cargo door.
(3)
Make sure that the access panel is in line with the fuselage contour of the door sill area.
NOTE : The permitted tolerance of the skin offset is -1.5 mm (-0.0590
____
in.).
(4)
Make sure that the subsequent clearances are correct (Ref. TASK 52-32-00-710-001) during the cargo door starts to open:
-
between the latching hooks and the door frame fittings,
-
between the latching hooks and the door sill.
(5)
Measure the gap "G" between the access panel of the cargo door and the door sill edge of the fuselage.
**ON A/C 001-049, 053-099, 101-105, 201-220,
(Ref. Fig. 501/TASK 52-32-11-991-008-A)
R 1EFF : 001-049, 053-099, 101-149, 201-299, 1 52-32-11Page 519 1301-399, 1Aug 01/05 1 1 1CES 1 **ON A/C 106-149, 221-299, 301-399,
(Ref. Fig. 501A/TASK 52-32-11-991-008-C)
**ON A/C 051-052,
Subtask 52-32-11-220-056-B
D. Dimensional Check
(Ref. Fig. 502/TASK 52-32-11-991-009)
(1) Make sure that the clearances of locking hooks (3) and the roller (4) between FR53A and FR55 are correct.
NOTE : The permitted clearance is 0.2 mm (0.0078 in.)
____
(2)
Install the access panel 826AR on the cargo door.
(3)
Make sure that the access panel is in line with the fuselage contour of the door sill area.
NOTE : The permitted tolerance of the skin offset is -1.5 mm (-0.0590
____
in.).
(4)
Make sure that the subsequent clearances are correct (Ref. TASK 52-32-00-710-001) during the cargo door starts to open:
-
between the locking hooks and the door frame fittings,
-
between the locking hooks and the door sill.
(5)
Measure the gap "G" between the access panel of the cargo door and the door sill edge of the fuselage (Ref. Fig. 501/TASK 52-32-11-991-008-A)
R **ON A/C 151-199, 401-499,
Subtask 52-32-11-220-056-A
D. Dimensional Check R **ON A/C 151-199,
(Ref. Fig. 502B/TASK 52-32-11-991-009-A)
R 1EFF : 051-052, 106-149, 151-199, 221-299, 1 52-32-11Page 520 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 401-499,
R (Ref. Fig. 502C/TASK 52-32-11-991-009-C)
R **ON A/C 151-199, 401-499,
(1) Make sure that the clearances of latching hooks (3) and the roller (4) between FR56A and FR58 are correct.
NOTE : The permitted clearance is 0.2 mm (0.0078 in.)____
(2) Install the access panels 826AR, 826BR and 826CR on the cargo door.
(3) Make sure that the access panels is in line with the fuselage contour of the door sill area.
NOTE : The permitted tolerance of the skin offset is -1.5 mm (-0.0590____ in.).
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