NSN 1560-01-520-8775 160D611501127, 160D611501-127, 01-520-8775
Product Details | AIRFOIL RIB
1560-01-520-8775 A principal chordwise rib that gives cross-sectional shape, strength and rigidity to a portion of a wing, stabilizer, and the like. See also RIB (1), STIFFENER, AIRCRAFT
Part Alternates: 160D611501127, 160D611501-127, 1560-01-520-8775, 01-520-8775, 1560015208775, 015208775
Aircraft and Airframe Structural Components | Airframe Structural Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | 01-520-8775 | 41026 ( RIB, AIRFOIL ) |
Cross Reference | NSN 1560-01-520-8775
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 160D611501-117 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATION DIV NORTHROP GRUMMAN AEROSPACE |
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Technical Data | NSN 1560-01-520-8775
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | LEADING EDGE INSTL-CENTER PANEL |
| AIRCRAFT MISSION DESIGN SERIES | A-10 ACFT |
| OVERALL LENGTH | 19.000 INCHES NOMINAL |
| OVERALL WIDTH | 14.000 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.080 INCHES NOMINAL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RIB, AIRFOIL |
| MANUFACTURERS CODE | 98747 |
| DESIGN CONTROL REFERENCE | 160D611501-127 |
Restrictions/Controls & Freight Information | NSN 1560-01-520-8775
| 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 | ||