(2)  
AMM 51-21-04/701, Alodine Surfaces

 (3)  
AMM 52-36-02/401, Bulk Cago Door Balance Mechanism

 (4)  
AMM 52-71-00/510, Door Warning System

 (5)  
SSM 52-71-01

 (6)  
WDM 52-71-14

 F.
Access

 (1)  
Location Zone
 146 Bulk Cargo Compartment, RH

 (2)  
Access Panel
 823R Door - Bulk Cargo Compartment

 G.
Procedure

 S 494-010
 (1)  
Attach the door sling and the fishpole hoist to the door.

 S 414-036

 (2)  
Put the door in its position in the door opening.

 S 214-028

 (3)  
Make sure the door stop pin centers touch the frame stop pad centers in a 0.30-inch diameter circle (Fig. 401, View A-A).

 S 824-039

 (4)  
If you will install a new door, trim the door outer skin to get the correct clearance between the door and body skin.

 S 824-040

 (5)
The clearance and flushness tolerances for the zones shown in

 Fig. 403 are listed in Table I. ~.............................................................................. | TABLE I | | BULK CARGO DOOR CLEARANCE AND FLUSHNESS TOLERANCES | ................................................................................ | AIRPLANE | | | | | EFFECTIVITY | ZONE | CLEARANCE | FLUSHNESS |
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 ~.............................................................................. | TABLE I | | BULK CARGO DOOR CLEARANCE AND FLUSHNESS TOLERANCES | ................................................................................ | AIRPLANE | | | | | EFFECTIVITY | ZONE | CLEARANCE | FLUSHNESS | ................................................................................ | ALL | A | 0.10 to 0.18 inch | -0.03 to 0.06 inch | | | | (2.54 to 4.57) mm | (-0.76 to 1.52) mm | ................................................................................ | EXCEPT | A | | -0.04 to -0.10 inch | | GEF 003 | | | (-1.01 to -2.54) mm| ................................................................................ | ALL | B | 0.10 to 0.22 inch | -0.09 to 0.03 inch | | | | (2.54 to 5.58) mm | (-2.28 to 0.76) mm | ................................................................................ | ALL | C | | -0.03 to -0.12 inch | | | | | (-0.76 to -3.04) mm| ................................................................................ | EXCEPT | C | | -0.05 to -0.08 inch | | GEF 003 | | | (-1.27 to -2.03) mm| ................................................................................ | ALL | D | | -0.13 to 0.00 inch | | | | | (-3.30 to 0.00) mm | 2.............................…......…...................….....................1
 (6)  S 374-012If the new bulk cargo door was trimmed, apply clear Alodine to the trimmed edges (AMM 51-21-04/701).
 (7)  S 864-029Put the door in the correct position.
 (8)  S 214-030Make sure the clearances between the door and the fuselage contour are correct.

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MAINTENANCE MANUAL

FWD
CLEARANCE TOLERANCES
Bulk Cargo Door Flushness and Gap Tolerances
Figure 403 (Sheet 1)

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MAINTENANCE MANUAL

FWD
UNPRESSURIZED FLUSHNESS TOLERANCES
A POSITIVE TOLERANCE SHOWS THE DOOR IS OUTBOARD OF THE FUSELAGE CONTOUR. A NEGATIVE TOLERANCE SHOWS THE DOOR IS INBOARD OF THE FUSELAGE.
　
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