AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| Alternative NSN: 9540-01-072-9576 |
| Item Name:Angle Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 010729576 |
| NCB Code: USA (01) |
| Manufacturers: Alcoa Reynolds Metals Company , American Society For Testing And , Federal Specifications , Inspektorat Wsparcia Sil Zbrojnych , Sae International , Society Of Automotive Engineers Inc , Transtar Metals Corp |
ASAP Aerospace, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Customers can easily search our database to find NSN parts like Angle Structural 26873, 60-7239, 9540PL0905376, AMS QQ A 200 3, AMS-QQ-A-200 3 of Alcoa Reynolds Metals Company, Transtar Metals Corp, Inspektorat Wsparcia Sil Zbrojnych, Sae International, Society Of Automotive Engineers Inc with NSN 9540-01-072-9576.
NSN 9540-01-072-9576, National Stock Number, is a 13-digit serial number assigned by the US DLA to an item that is bought, stored, and sold via the federal supply chain. Unlike part numbers, NSNs are not arbitrary and follow a specific classification system.
| Part No | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|
| 26873 | Angle Structural | Alcoa Reynolds Metals Company | Avl | RFQ |
| 60-7239 | Angle Structural | Transtar Metals Corp | Avl | RFQ |
| 9540PL0905376 | Angle Structural | Inspektorat Wsparcia Sil Zbrojnych | Avl | RFQ |
| AMS QQ A 200 3 | Angle Structural | Sae International | Avl | RFQ |
| AMS-QQ-A-200 3 | Angle Structural | Society Of Automotive Engineers Inc | Avl | RFQ |
| ASTM B221 | Angle Structural | American Society For Testing And | Avl | RFQ |
| QQ-A-200 3 | Angle Structural | Federal Specifications | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.200 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 2.750 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXL | LEFT SIDE FLANGE THICKNESS | 0.080 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | F-16 AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | ANGLE |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| AJGM | OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.030 INCHES NOMINAL |
| AJGP | BASE FLANGE THICKNESS | 0.080 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.374 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.030 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.030 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
| ZZZK | SPECIFICATION/STANDARD DATA | 81755-K10 MANUFACTURERS STANDARD |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3511 TEMPER |
| 9505-00-004-3522 | 9505-00-006-5050 | 9505-00-020-6766 | 9505-00-023-4467 | 9505-00-027-2485 | 9505-00-027-7789 | 9505-00-044-2161 | 9505-00-051-1088 | 9505-00-054-7077 |
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