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Figure 1.
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TB-1-1520-238-20-88 AH-64 Inspection of Fusleage Station (FS) 176 Frame for Cracking Around the Web on Aircraft Manufactured Prior to Tail Number 84-25351 Manual
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Figure 3

TB 1-1520-238-20-88
NOTES:
1.
MS21266-3N GROMMET SHOULD BE USED IN HOLE. USE OF SMALLER -2N GROMMET WILL RESTRICT
USEABLE DIAMETER AND CAUSE INTERFERENCE.
2.
THE CONFIGURATION IN AMB97-04, FIG.  2 WILL RESTRICT THE AMOUNT OF USEABLE HOLE SPACE.
REPLACE AN742-4 CLAMP FOR ELECTRICAL BUNDLE WITH MS21919WDF4 OR HS4271-3510 TO PREVENT
CHAFING FOR THE AMB CONFIGURATION.
3.
USE MS21 266-2N GROMMET AS SHOWN ON FORWARD PLATE CONTACT SURFACE TO PREVENT
CHAFING.
4.
CENTER PLATE AS SHOWN AND POSITION SPACER HOLES TO ALLOW CLAMP POSITIONING AS SHOWN
MS017S12
Figure 2.
9

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