NSN 9520-01-718-4305 · NIIN 017184305 · FSC 9520
NO DASHES 9520017184305
In Stock
ANGLE,STRUCTURAL
Structural Shapes
Application: C-17A AIRCRAFT
Technical characteristics
9 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| SUPP | SUPPLEMENTARY FEATURES | EXTRUDED ALUMINUM USED FOR REPAIRS ON THE VERTICAL STABILIZERS AND THE MAIN LANDING GEAR POD |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE QQ-A-200 TO 11 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| AGAV | END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| ABRY | LENGTH | INCHES NOMINAL 4.000 |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 1.700 |
| ALBY | USAGE DESIGN | AIRCRAFT AND STRUCTURAL |
| FEAT | SPECIAL FEATURES | CONTRACT NO.: FA852621D0001; F33657-81-C-2108; F33657-96-C-2059 |
| MATT | MATERIAL | ALUMINUM ALLOY |