At NSN Unlimited, we maintain a large database of parts 40-029-1, 60 12152, 60-12152, AMS-QQ-A-200 11, QQ-A-200 11 with NSN 9540-01-166-2657 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Federal Specifications, Bell Helicopter Textron Inc, Society Of Automotive Engineers Inc, Transtar Metals Corp, 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: 9540-01-166-2657 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 011662657 |
| NCB Code: USA (01) |
| Manufacturers: Federal Specifications , Bell Helicopter Textron Inc , Society Of Automotive Engineers Inc , Transtar Metals Corp , Sae International |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 40-029-1 | 9540-01-166-2657 | beam structural | federal specifications | Avl | RFQ |
| 40-029-1 | 9540-01-166-2657 | beam structural | bell helicopter textron inc | Avl | RFQ |
| 40-029-1 | 9540-01-166-2657 | beam structural | society of automotive engineers inc | Avl | RFQ |
| 60 12152 | 9540-01-166-2657 | beam structural | transtar metals corp | Avl | RFQ |
| 60-12152 | 9540-01-166-2657 | beam structural | society of automotive engineers inc | Avl | RFQ |
| 60-12152 | 9540-01-166-2657 | beam structural | federal specifications | Avl | RFQ |
| 60-12152 | 9540-01-166-2657 | beam structural | bell helicopter textron inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-166-2657 | beam structural | bell helicopter textron inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-166-2657 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-166-2657 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-166-2657 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-166-2657 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-166-2657 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-166-2657 | beam structural | bell helicopter textron inc | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 0.993 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.050 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.205 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.295 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.500 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.215 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 83.30 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 96.30 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
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