At NSN Unlimited, we maintain a large database of parts 1S11 2024 T3 ALCLAD, 1S11 2024-T3, AMS QQ A 200 3, AMS QQ A 250 5, AMS-QQ-A-200 3 with NSN 9540-01-353-4627 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Boeing Company The, Federal Specifications, Society Of Automotive Engineers Inc, Sae International. Utilize our interface to browse items by part number, part type, manufacturer, and more. Obtain insights on top MRO and FBO services, Manufacturer profiles, and part catalogs.
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| Alternative NSN: 9540-01-353-4627 |
| Item Name: Angle Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 013534627 |
| NCB Code: USA (01) |
| Manufacturers: Boeing Company The , Federal Specifications , Society Of Automotive Engineers Inc , Sae International |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 1S11 2024 T3 ALCLAD | 9540-01-353-4627 | angle structural | boeing company the | Avl | RFQ |
| 1S11 2024-T3 | 9540-01-353-4627 | angle structural | boeing company the | Avl | RFQ |
| 1S11 2024-T3 | 9540-01-353-4627 | angle structural | federal specifications | Avl | RFQ |
| 1S11 2024-T3 | 9540-01-353-4627 | angle structural | society of automotive engineers inc | Avl | RFQ |
| AMS QQ A 200 3 | 9540-01-353-4627 | angle structural | society of automotive engineers inc | Avl | RFQ |
| AMS QQ A 250 5 | 9540-01-353-4627 | angle structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 3 | 9540-01-353-4627 | angle structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 3 | 9540-01-353-4627 | angle structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 3 | 9540-01-353-4627 | angle structural | sae international | Avl | RFQ |
| AMS-QQ-A-250 5 | 9540-01-353-4627 | angle structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-250 5 | 9540-01-353-4627 | angle structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-250 5 | 9540-01-353-4627 | angle structural | boeing company the | Avl | RFQ |
| QQ A 200 3 | 9540-01-353-4627 | angle structural | federal specifications | Avl | RFQ |
| QQ A 250 5 | 9540-01-353-4627 | angle structural | federal specifications | Avl | RFQ |
| QQ-A-200 3 | 9540-01-353-4627 | angle structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 3 | 9540-01-353-4627 | angle structural | boeing company the | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ANY ACCEPTABLE |
| ABKW | OVERALL HEIGHT | 0.250 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 0.594 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| AGTA | BASIC SHAPE STYLE | ANGLE |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL |
| AJGP | BASE FLANGE THICKNESS | 0.032 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/3, ALLOY 2024 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3511 TEMPER |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| ADXL | LEFT SIDE FLANGE THICKNESS | 0.032 INCHES NOMINAL |
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