At NSN Unlimited, we maintain a large database of parts 1104A, 1503-8813, 6099, AMS QQ A 200 2, AMS-QQ-A-200 2 with NSN 9540-00-145-8447 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Alcoa Reynolds Metals Company, The Boeing Company, Federal Specifications, Bohn Aluminum And Brass Co, Society Of Automotive Engineers Inc. 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: 9540-00-145-8447 |
| Item Name: Angle Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 001458447 |
| NCB Code: USA (00) |
| Manufacturers: Alcoa Reynolds Metals Company , The Boeing Company , Federal Specifications , Bohn Aluminum And Brass Co , Society Of Automotive Engineers Inc , Sae International , American Society For Testing And |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 1104A | 9540-00-145-8447 | angle structural | alcoa reynolds metals company | Avl | RFQ |
| 1503-8813 | 9540-00-145-8447 | angle structural | the boeing company | Avl | RFQ |
| 1503-8813 | 9540-00-145-8447 | angle structural | federal specifications | Avl | RFQ |
| 6099 | 9540-00-145-8447 | angle structural | bohn aluminum and brass co | Avl | RFQ |
| AMS QQ A 200 2 | 9540-00-145-8447 | angle structural | society of automotive engineers inc | Avl | RFQ |
| AMS QQ A 200 2 | 9540-00-145-8447 | angle structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 2 | 9540-00-145-8447 | angle structural | the boeing company | Avl | RFQ |
| AMS-QQ-A-200 2 | 9540-00-145-8447 | angle structural | federal specifications | Avl | RFQ |
| ASTM B221 | 9540-00-145-8447 | angle structural | the boeing company | Avl | RFQ |
| ASTM B221 | 9540-00-145-8447 | angle structural | american society for testing and | Avl | RFQ |
| ASTM B221 | 9540-00-145-8447 | angle structural | federal specifications | Avl | RFQ |
| QQ A 200 2 | 9540-00-145-8447 | angle structural | federal specifications | Avl | RFQ |
| QQ-A-200 2 | 9540-00-145-8447 | angle structural | the boeing company | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDEDEXTRUDED |
| ABKW | OVERALL HEIGHT | 2.000 INCHES NOMINAL2.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL2.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM12.000 FEET MAXIMUM |
| ADXL | LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | ANGLEANGLE |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL0.250 INCHES NOMINAL |
| AJGP | BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL0.125 INCHES NOMINAL |
| AJJB | FIRST TIP RADIUS | 0.125 INCHES NOMINAL0.125 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.580 POUNDS PER LINEAR FOOT0.580 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | RIGHT QUARTER RADIUSRIGHT QUARTER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.125 INCHES NOMINAL0.125 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICALNOT IDENTICAL |
| CNQK | SECOND TIP STYLE | UPPER RADIUSUPPER RADIUS |
| CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED OR T-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATEDT-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/2, ALLOY 2014ALUMINUM ALLOY AMS-QQ-A-200/2, ALLOY 2014 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND 7075 ALLOY AND T6 TEMPER OR T6 TEMPER OR T6511 TEMPERT6511 TEMPER |
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