Side Cargo Door Latch Cam and Pin Adjustment
Figure 408 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-32-01
ALL ú ú 02 Page 422 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
LATCH FITTING
NO. 1 THRU 3 AND 6 THRU 10
A-A
RAMP
DUMMY
LATCH PIN
MODELING
CLAY
INBD
HORIZONTAL
POSITION (CUT
AND MEASURE
CLAY AT THIS
POSITION)
VERTICAL
POSITION (CUT
LATCH AND MEASURE
CAM CLAY AT THIS
POSITION)
USE OF DUMMY LATCH PIN 2 B-B
Side Cargo Door Latch Cam and Pin Adjustment
Figure 408 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-32-01
ALL ú ú 02 Page 423 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
MAIN DECK SIDE CARGO DOOR
10
9
DOORWAY
LOWER SILL
8
SEE D
7
FWD
6
5 4
3 2 DOORWAY LOWER SILL
1
D
ONE OF
FIVE PAIRS
SEE E RETAINING CLIP FITTINGS
1
2, 4, 6, 8, AND 10 DOORWAY LOWER SILL
LATCH PINS FACE TOWARD EACH OTHER IN EACH PAIR
FWD
E
FITTINGS 1, 3, 5, 7, AND 9
____ NUMBERS ADJACENT TO LATCH PIN FITTINGS
NOTE: DENOTE LATCH POSITIONS.
1
A RETAINING CLIP IS ADDED TO THE LATCH PIN FITTING TO
PREVENT REVERSE INSTALLATION OF THE LATCH PIN.
Side Cargo Door Cam and Latch Pin Adjustment
Figure 408 (Sheet 3)
H15673
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-32-01
ALL ú ú 02 Page 424 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
WARNING:_______ DO NOT GET SOLVENTS IN YOUR MOUTH, OR YOUR EYES, OR
ON YOUR SKIN. DO NOT BREATHE THE FUMES FROM
SOLVENTS. SOLVENTS ARE HAZARDOUS MATERIALS.
SOLVENTS MAY BE FLAMMABLE OR HARMFUL TO THE
ENVIRONMENT. REFER TO PRODUCT MATERIAL SAFETY DATA
SHEETS (MSDS) AND LOCAL REQUIREMENTS FOR PROPER
HANDLING PROCEDURES.
2) Clean the parts with solvent, Series 92 (AMM 20-30-92).
NOTE: Use a plastic tool, if it is necessary, to remove
____ all the used sealant.
3) Add or remove shims until you get a 0.020- to 0.030-inch clearance between the forward guide roller ramp and guide roller with the door fully closed.
4) Apply sealant to all mating surfaces of the forward guide roller ramp, ramp channel, shims, and latch fitting. 5) Apply sealant to the fastener threads, shanks, and countersinks and install the parts.
6) Apply sealant to fully cover the nuts.
7) Remove unwanted sealant material from the face of the guide roller ramp with solvent, Series 92 (AMM 20-30-92) . 8) Fully close the door. 9) Measure the clearance between the guide roller ramp and
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 艙門 DOORS 2(124)
