| Mfg Part Number: 74A342535-2001 | Alternate P/N: 74A3425352001 | Manufacturer: Boeing Company The | Item Name : web structural component aircraf |
| NSN : 1560-01-502-4671 (1560015024671) | CAGE Code : 76301 | FSC : 1560 Airframe Structural Components |
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NSN Information for Part Number 74A342535-2001 with NSN 1560-01-502-4671, 1560015024671
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-502-4671 Item Description: Web Structural Component Aircraf | 1560 | 015024671 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 74a342535-2001 | 5 | 2 | 3 |
Characteristics Data of NSN 1560-01-502-4671, 1560015024671
| MRC | Criteria | Characteristic |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | WEB,STRUCTURAL COMPONENT (INAVY); KEEL WEB, LOWER 591.500 TO 631.250, AFT FUS (DRAWING NAME) |
| ASXK | HOLE QUANTITY | 31 |
| ABMK | OVERALL WIDTH | 4.750 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F/A18-E/F FIGHTER AIRCRAFT |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZDJ | AIRCRAFT LOCATION | AFT FUSELAGE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F/A18-E/F |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE |
| ABHP | OVERALL LENGTH | 13.000 INCHES NOMINAL |
| CZEJ | AIRCRAFT STATION NUMBER | FS 570.0 TO FS 695.0 |
| MATT | MATERIAL | TITANIUM ALLOY |
| ABPX | MATERIAL THICKNESS | 0.063 INCHES NOMINAL |
