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 | 1560-01-541-7391 | SUPPORT,STRUCTURAL COMPONENT,AIR | 07/10/2006 |
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 | 1560-01-541-7391 | SUPPORT,STRUCTURAL COMPONENT,AIR | | 0 |
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 | OVERALL LENGTH | 2.500 INCHES NOMINAL | | OVERALL WIDTH | 2.100 INCHES NOMINAL | | MATERIAL THICKNESS | 0.040 INCHES NOMINAL | | END ITEM IDENTIFICATION | A-10 | | PART NAME ASSIGNED BY CONTROLLING AGENCY | CLIP | | AIRCRAFT LOCATION | ELECTRICAL INTERFACE | | AIRCRAFT MISSION DESIGN SERIES | A-10A | | SPECIAL FEATURES | HEAT TREAT T3 | | MATERIAL | ALUMINUM ALLOY 2024 | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
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