NSN 1560-01-162-1008 35822010, 35-8220-10, 01-162-1008
Product Details | AIRCRAFT FORMER
1560-01-162-1008 A light, secondary structural member that does not completely partition various components such as the fuselage, boom, wing, and the like. It is designed to give cross-sectional shape and strength to the item of which it is a part.
Part Alternates: 35822010, 35-8220-10, 1560-01-162-1008, 01-162-1008, 1560011621008, 011621008
Aircraft and Airframe Structural Components | Airframe Structural Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | 01-162-1008 | 41023 ( FORMER, AIRCRAFT ) |
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Technical Data | NSN 1560-01-162-1008
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-25043 MIL STD SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | USED AS ANGLE-UPPER INNER ON FRAME-CANTED BODY COWL PANEL |
| AIRCRAFT MISSION DESIGN SERIES | B-52 AIRCRAFT |
| OVERALL LENGTH | 12.500 INCHES NOMINAL |
| OVERALL WIDTH | 2.400 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.032 INCHES NOMINAL |
| SPECIAL FEATURES | OPPOSITE 35-8220-9 |
| MANUFACTURERS CODE | 81205 |
| DESIGN CONTROL REFERENCE | 35-8220-10 |
Restrictions/Controls & Freight Information | NSN 1560-01-162-1008
| 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 | ||