| Part Number: 16T7469-9 | Manufacturer: Cyclone Aviation Services 1972 Ltd |
| NSN : 1560-01-355-5954 (1560013555954) | Item Name : spar aircraft |
| CAGE Code: S5503 | FSC : 1560 Airframe Structural Components |
| Alternate P/N : 16T74699 | INC Code: 41028 |
| NIIN : 01-355-5954 (013555954) | FSG : 15 Aircraft and Airframe Structural Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-355-5954 Item Description: Spar Aircraft | 1560 | 013555954 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 16t7469-9 | 6 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 84.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 3.750 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CZDJ | AIRCRAFT LOCATION | HORIZONTAL STABILIZER |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-16A/B/C/D |
| FEAT | SPECIAL FEATURES | FORM,FIT,FUNCTION |
| MATT | III MATERIAL | ALUMINUM ALLOY 2124 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FMS-3002-T851 MFR REF SINGLE MATERIAL RESPONSE |
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