A B
SEE B
FWD
B
INBD BODY GEAR SHOCK STRUT INBOARD DOOR
A
Body Gear Shock Strut Inboard Door Adjustment Figure 505 (Sheet 1)
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A
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BODY STRUCTURE (REF)
0.75
INCH
0.17
LIMITS OF MISMATCH OF THE BODY GEAR DOOR INSIDE THE CONTOUR OF THE BODY STRUCTURE:
OUTSIDE MISMATCH
B-B
0.06 INCH (30% OF THE INBOARD DOOR EDGE)
0.03 INCH (70% OF THE INBOARD DOOR EDGE)
INSIDE MISMATCH
BODY GEAR BODY GEAR SHOCK STRUT SHOCK STRUT DOORSTOP STOP
CLEARANCE MAX MISMATCH
C-C D-D

Body Gear Shock Strut Inboard Door Adjustment
Figure 505 (Sheet 2)

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SHIMS BODY GEAR
DOORSTOP WHEEL WELL INBOARD DOOR
AFT STOP PAD
BODY GEAR WHEEL BODY GEAR SHOCK WELL OUTBOARD DOOR STRUT INBOARD DOOR
SUPPORT STRUCTURE (REF)
SEE C
E-E
BODY GEAR SHOCK STRUT INBOARD DOOR FWD
LIMITS OF MISMATCH OF THE BODY GEAR DOOR INSIDE THE CONTOUR OF THE BODY STRUCTURE:
0.12 INCH (30% OF THE INBOARD DOOR EDGE)
0.06 INCH (70% OF THE INBOARD DOOR EDGE)
G-G

INSIDE MISMATCH
BODY GEAR SHOCK STRUT INBOARD DOOR LINKAGE ROD
FWD
DOOR OPEN POSITION
B

BODY GEAR SHOCK STRUT INBOARD DOOR BODY GEARSHIMS SHOCK STRUT INBOARD DOOR
0.35  0.50 0.20  INCH 
|0.12 INCH  CLEARANCE 
MAX MISMATCH  F-F 

STOP PAD
0.65
0.50 INCHSUPPORT 0.30
STRUCTURE CLEARANCE
(REF)
LIMITS OF MISMATCH OF THE BODY GEAR DOOR
OUTSIDE THE CONTOUR OF THE BODY STRUCTURE:
0.06 INCH (30% OF THE INBOARD DOOR EDGE)
0.03 INCH (70% OF THE INBOARD DOOR EDGE)
OUTSIDE MISMATCH
BODY GEAR SHOCK STRUT INBOARD DOOR LINKAGE ROD
DRAG STRUT
C

Body Gear Shock Strut Inboard Door Adjustment
Figure 505 (Sheet 3)

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 ~............................................................................... | BODY GEAR SHOCK STRUT INBOARD DOOR FLUSHNESS AND CLEARANCE DEVIATIONS | | TABLE 502 | ................................................................................. | | | TYPE OF | MISMATCH | | | AIRPLANE | ZONE | MISMATCH | (FLUSHNESS) | CLEARANCE | .................................................................................
 |ABD 001  |  B-B  |Outside  |-0.16 inch (30% of|  |
 |  |  |  |the inboard door  |  |
 |  |  |  |edge)  |  |
 |  |  |  |  |  |
 |  |  |Inside  |+0.08 inch (30% of|  |
 |  |  |  |the inboard door  |  |
 |  |  |  |edge)  |  |

 2............…........….............…..................…........................1
 S 825-282
 (2)  Table 503 (for Fig. 506) shows expanded tolerances which were permitted at delivery. Use these tolerances only if you cannot get the usual tolerances.
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