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| 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) | 01-370-7163 (013707163) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 17P2A6015-4 | boeing company the | panel structural aircraft | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | LAMINATED AND COMPOSITE |
| SR-5 | MANUFACTURERS CODE | 88277 |
| CZEJ | AIRCRAFT STATION NUMBER | FS 981.500 TO FS 1045.750 |
| SR-5 | DESIGN CONTROL REFERENCE | 17P2A6015-4 |
| CZDJ | AIRCRAFT LOCATION | CENTER FUSELAGE FILLET,UPPER |
| BWJF | SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| SFTT | SURFACE TREATMENT | PRIMER EPOXY |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-17A |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | DMS1974 MFR REF 1ST MATERIAL RESPONSE AND DMS2288 MFR REF 2ND MATERIAL RESPONSE |
| SR-5 | THE MANUFACTURERS DATA | |
| FEAT | SPECIAL FEATURES | NHA 17P2A6015-2 & -502;PANEL INSTL-FILLET,UPR,Y 981.50 - Y 1045.75 |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE |
| MATT | MATERIAL | PLASTIC POLYAMIDE AND PLASTIC ARAMID |
| Relevant Components for NSN - 1560-01-370-7163, 1560013707163 | ||||
| 1560-01-554-4660 (1560015544660) | 1560-01-465-6016 (1560014656016) | 1560-00-873-3011 (1560008733011) | 1560-01-445-9850 (1560014459850) | |
| 1560-00-098-0168 (1560000980168) | 1560-00-251-5490 (1560002515490) | 1560-01-621-9290 (1560016219290) | 1560-01-544-3961 (1560015443961) | |
| 1560-00-531-6887 (1560005316887) | 1560-00-146-2205 (1560001462205) | 1560-00-870-4445 (1560008704445) | 1560-01-611-0493 (1560016110493) | |
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