NSN 1560-01-528-1016 Parts of Panel Structural Ai
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| Alternative NSN: 1560-01-528-1016 |
| Item Name: Panel Structural Ai |
| Federal Supply Class (FSC): 1560 Airframe Structural Components |
| NIIN: 015281016 |
| NCB Code: USA (01) |
| Manufacturers: Fleet Readiness Center Southwest |
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| 71091-13 | fleet readiness center southwest | panel structural ai | Avl | RFQ |
| 71091 | fleet readiness center southwest | panel structural ai | Avl | RFQ |
Characteristics Data of NSN 1560015281016
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | Overall Length | 46.000 INCHES NOMINAL |
| FEAT | Special Features | SURFACE TREATMENT SPECIFICATION ALSO INCLUDES LPS-409. |
| MRC | Decoded Requirement | Clear Text Reply |
| ABMK | Overall Width | 6.000 INCHES NOMINAL |
| CXCY | Part Name Assigned By Controlling Agency | INAVY:STRIP |
| MDCL | Material Document And Classification | QQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE |
| AGAV | End Item Identification | C-2A AND E-2A |
| CZDJ | Aircraft Location | WING CENTER SECTION TRAILING EDGE |
| STDC | Surface Treatment Document And Classification | MIL-STD-130 MIL STD SINGLE TREATMENT RESPONSE |
| RTSE | Relationship To Similar Equipment | 71091-11 CAP STRIP REPAIR, FOR WING CENTER SECTION TRAILING EDGE |
| SFTT | Surface Treatment | PRIMER EPOXY |
| CZEK | Aircraft Mission Design Series | C-2A |
| MATT | Material | ALUMINUM ALLOY 2024 |
| BWJF | Side For Which Designed | BOTH SIDES |
| ABNM | Thickness | 0.250 INCHES NOMINAL |
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