| Item Name | Panel Structural Aircraft |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-478-0839 (014780839) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 17P2A6519-4 | boeing company the | panel structural aircraft | 88277 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| CZDJ | AIRCRAFT LOCATION | WG TO FUS PANEL INSTL, FILLET-OUTBD, UPR, AFT |
| SR-5 | MANUFACTURERS CODE | 88277 |
| SR-5 | DESIGN CONTROL REFERENCE | 17P2A6519-4 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-17 |
| FEAT | SPECIAL FEATURES | CONSISTS OF 1(-6) PANEL, 1(-8) CORE, 1(-10) CORE, 2 RETAINERS, 2 SEALS AND 44 RIVETS. PANEL MATERIAL GLASS FIBER WOVEN FABRIC AND CARBON FIBER WOVEN FABRIC; CORE MATERIAL HONEYCOMB POLYMIDE PAPER, OVEREXPANDED |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | DMS 2288 TYPE 2,CLASS 2,GRADE D MFR REF 1ST MATERIAL RESPONSE AND DMS 1974 TYPE 2,CLASS 2,GRADE B,DENSITY- 3 PCF MFR REF 2ND MATERIAL RESPONSE |
| SR-5 | THE MANUFACTURERS DATA | |
| MATT | MATERIAL | PLASTIC EPOXY AND PLASTIC POLYIMIDE |
| Relevant Components for NSN - 1560-01-478-0839, 1560014780839 | ||||
| 1560-00-213-3123 (1560002133123) | 1560-01-523-1268 (1560015231268) | 1560-00-966-6107 (1560009666107) | 1560-01-600-6748 (1560016006748) | |
| 1560-00-216-1469 (1560002161469) | 1560-00-678-4848 (1560006784848) | 1560-01-151-6707 (1560011516707) | 1560-01-477-0410 (1560014770410) | |
| 1560-01-605-2013 (1560016052013) | 1560-00-427-9181 (1560004279181) | 1560-01-322-5302 (1560013225302) | 1560-00-412-9723 (1560004129723) | |
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