Alternative NSN: 1560-01-497-5366 |
Item Name: Panel Structural Ai |
CAGE Code : 88277 |
NIIN: 014975366 |
FSG: 15 Aircraft and Airframe Structural Components |
FSC Name: 1560 Airframe Structural Components |
NCB Code: USA (01) |
Manufacturers: boeing company the |
Part No Part No
|
Manufacturer |
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
17P2A6015-53 | boeing company the | panel structural ai | Avl |
MRC | Criteria | Characteristic |
---|---|---|
SR-5 | Design Control Reference Or Manufacturers Code | |
SFTT | Surface Treatment | PRIMER EPOXY-POLYAMIDE |
MDCL | Material Document And Classification | DMS1974-2-2B-3 MFR REF 1ST MATERIAL RESPONSE AND |
SR-5 | Design Control Reference Or Manufacturers Code | 88277 |
STDC | Surface Treatment Document And Classification | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND |
CZEJ | Aircraft Station Number | Y981.500 TO Y1045.750 |
SR-5 | Design Control Reference Or Manufacturers Code | 17P2A6015-53 |
STDC | Surface Treatment Document And Classification | MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE |
AARN | Fabrication Method | COMPOSITE |
MDCL | Material Document And Classification | DMS2288-3-4E MFR REF 3RD MATERIAL RESPONSE |
CZEK | Aircraft Mission Design Series | C-17A |
MATT | Material | PLASTIC ARAMID |
CZDJ | Aircraft Location | WING TO FUSELAGE FILLET |
MDCL | Material Document And Classification | DMS2288-2-2D MFR REF 2ND MATERIAL RESPONSE AND |
AARN | Fabrication Method | LAMINATED AND |
FEAT | Special Features | USED ON THE FOLLOWING NHA:17P2A6015-1, -501, -503, -505, -507, -509 AND -521 CONFIGURATIONS |
AARN | Fabrication Method | HONEYCOMB AND |
MRC | Decoded Requirement | Clear Text Reply |
BWJF | Side For Which Designed | LEFT SIDE |
MATT | Material | PLASTIC POLYAMIDE AND |
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