NSN 1560-01-333-2588 01-333-2588, 013332588
Product Details | AIRCRAFT FRAME
1560-01-333-2588 A principal transverse structural member of the fuselage, hull, nacelle, pod, and the like. It follows the periphery and provides shape and support by attachment to the longitudinal members or skin.
Part Alternates: 1560-01-333-2588, 01-333-2588, 1560013332588, 013332588
Aircraft and Airframe Structural Components | Airframe Structural Components
Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
---|---|---|---|
15 | 01-333-2588 | 41024 ( FRAME, AIRCRAFT ) |
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Related Products | NSN 1560-01-333-2588
Technical Data | NSN 1560-01-333-2588
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY 2024 |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4-T62 FED SPEC SINGLE MATERIAL RESPONSE |
AIRCRAFT LOCATION | CANOPY |
SIDE FOR WHICH DESIGNED | LEFT SIDE |
AIRCRAFT MISSION DESIGN SERIES | F-16C |
OVERALL LENGTH | 13.000 INCHES NOMINAL |
OVERALL WIDTH | 13.000 INCHES NOMINAL |
MATERIAL THICKNESS | 0.100 INCHES NOMINAL |
MANUFACTURERS CODE | 81755 |
DESIGN CONTROL REFERENCE | 16K0522-47 |
Restrictions/Controls & Freight Information | NSN 1560-01-333-2588
Category | Code | Description |
---|---|---|
Hazardous Material Indicator Code | P | There is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product |
Category | Code | Description |
---|---|---|
No Freight Information |