Mfg Part Number: 17P2A6011-5
Alternate P/N: 17P2A60115
NSN : 1560-01-370-4087
NIIN : 013704087
CAGE Code : 88277
Manufacturer: Boeing Company The
Item Name : Panel Structural Ai Panel Structural Ai
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-370-4087 Item Description: Panel Structural Ai | 1560 | 013704087 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
17p2a6011-5 | 6 | 1 | C | A |
MRC | Criteria | Characteristic |
---|---|---|
SR-5 | Design Control Reference Or Manufacturers Code | |
SFTT | Surface Treatment | PRIMER EPOXY |
CZDJ | Aircraft Location | CENTER FUSELAGE FILLET,LOWER |
MDCL | Material Document And Classification | DMS1974 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 |
SR-5 | Design Control Reference Or Manufacturers Code | 17P2A6011-215 |
STDC | Surface Treatment Document And Classification | MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE |
MDCL | Material Document And Classification | DMS2288 MFR REF 3RD MATERIAL RESPONSE |
CZEK | Aircraft Mission Design Series | C-17A |
MATT | Material | PLASTIC ARAMID |
MATT | Material | ALUMINUM ALLOY 1145 AND |
CZEJ | Aircraft Station Number | FS 910.500 TO FS 981.500 |
FEAT | Special Features | NHA 17P2A6011-213;PANEL INSTL-FILLET,LWR Y=910.500 THRU Y=981.500 |
MATT | Material | PLASTIC POLYAMIDE AND |
MDCL | Material Document And Classification | DMS2502 MFR REF 2ND MATERIAL RESPONSE AND |
MRC | Decoded Requirement | Clear Text Reply |
AARN | Fabrication Method | COMPOSITE |
AARN | Fabrication Method | LAMINATED AND |
BWJF | Side For Which Designed | LEFT SIDE |
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