| Mfg Part Number: 68A332192-2003 | Alternate P/N: 68A3321922003 | Manufacturer: Boeing Company | Item Name : former aircraft |
| NSN : 1560-01-457-6442 (1560014576442) | CAGE Code : 76301 | FSC : 1560 Airframe Structural Components |
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NSN Information for Part Number 68A332192-2003 with NSN 1560-01-457-6442, 1560014576442
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-457-6442 Item Description: Former Aircraft | 1560 | 014576442 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 68a332192-2003 | 5 | 2 | 3 |
Characteristics Data of NSN 1560-01-457-6442, 1560014576442
| MRC | Criteria | Characteristic |
|---|---|---|
| SR-5 | MANUFACTURERS CODE | 76301 |
| ABMK | OVERALL WIDTH | 16.500 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | U/O F-15C 304UP, F-15D 50UP, FMF-15C 10UP, FMF15D 7UP |
| SR-5 | THE MANUFACTURERS DATA | |
| CZDJ | AIRCRAFT LOCATION | EMPENAGE SUPPORT BEAM CLOSURE |
| SR-5 | DESIGN CONTROL REFERENCE | 68A332192-2003 |
| ABHP | OVERALL LENGTH | 17.500 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-15 |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| ABPX | MATERIAL THICKNESS | 0.040 INCHES NOMINAL |
