(2)
Measure the part
(3)
Compare the dimensions with the correct dimensions in the table.
(4)
Install, repair or replace the part.
TASK 52-36-01-206-001
2. Examine the Condition of the Bulk Cargo Door (Fig. 601)____________________________________________
A. References
(1)
AMM 52-36-00/001, Bulk Cargo Door
(2)
AMM 52-36-03/401, Bulk Cargo Door Uplatch Hook
(3)
AIPC 52-36-01 Fig. 2, AIPC 52-36-03 Fig. 2, AIPC 52-36-04 Fig. 1
B.
Access
(1)
Location Zone
146 Bulk Cargo Compartment, RH
(2)
Access Panel
823R Door - Bulk Cargo Compartment
C.
Procedure
(1)
Open the bulk cargo door sufficiently for access (AMM 52-36-00/001).
(2)
Remove the lining from the bulk cargo door.
S 216-010
(3)
Examine the latch mechanism for corrosion, deterioration and general condition.
S 016-002
S 036-003
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-36-01
ALL ú ú 01 Page 601 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
B B
SEE C
SEE A
SEE B
A
A
A
FWD
B
Bulk Cargo Wear Limits
Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-36-01
ALL ú ú 01 Page 602 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
2. INSERT/PROBE 1. BUSHING/PROBE
A-A 5. BUSHING/BOLT
4. FITTING/BUSHING SNUBBER FITTING
B-B
C
C
3. BUSHING/SPACER
C Bulk Cargo Door Wear Limits Figure 601 (Sheet 2) C-C
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-36-01
ALL ú ú 01 Page 603 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
INDEX NO. PART NAME DIM. DESIGN LIMITS WEAR LIMITS REPLACE PART WORN REPAIR WORN PART REPAIR INSTR.
DIAMETER WEAR DIM. ALLOWED DIAM CLEAR-ANCE MAX
MIN MAX
1 BUSHING ID 1.5015 1.5025 1.512 0.022 X
PROBE OD 1.498 1.499 1 X
2 INSERT ID 0.225 0.235 2 X
PROBE OD 0.838 0.843 1 X
3 BUSHING ID 0.261 0.263 0.290 0.080 X
SPACER OD 0.240 0.260 0.210 X
4 FITTING ID 0.3761 0.3766 0.0000 0.0010 X
BUSHING OD 0.3756 0.3761 0.0005 X
5 BUSHING ID 0.2500 0.2515 0.0000 0.0030 X
BOLT OD 0.2485 0.2495 0.0005 X
DAMAGE THROUGH THE CHROME LAYER IS NOT SATISFACTORY REPLACE THE INSERT IF IT IS LESS THAN 0.210 INCHES THICK
NOTE:REFER TO OVERHAUL MANUAL 52-36-35 TO REPLACE THE BUSHINGS.
Bulk Cargo Door Wear Limits
Figure 601 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-36-01
ALL ú ú 01 Page 604 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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 4(15)
