At NSN Unlimited, we maintain a large database of parts 1MA10208D01, AMS-QQA200-11, QQA200 11, QQA200-11 with NSN 9540-00-508-8871 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Society Of Automotive Engineers Inc, Federal Specifications, Boeing Company The, 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: 9540-00-508-8871 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 005088871 |
NCB Code: USA (00) |
Manufacturers: Society Of Automotive Engineers Inc , Federal Specifications , Boeing Company The , Sae International |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1MA10208D01 | 9540-00-508-8871 | beam structural | society of automotive engineers inc | Avl | RFQ |
1MA10208D01 | 9540-00-508-8871 | beam structural | federal specifications | Avl | RFQ |
1MA10208D01 | 9540-00-508-8871 | beam structural | boeing company the | Avl | RFQ |
AMS-QQA200-11 | 9540-00-508-8871 | beam structural | federal specifications | Avl | RFQ |
AMS-QQA200-11 | 9540-00-508-8871 | beam structural | boeing company the | Avl | RFQ |
AMS-QQA200-11 | 9540-00-508-8871 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQA200-11 | 9540-00-508-8871 | beam structural | sae international | Avl | RFQ |
QQA200 11 | 9540-00-508-8871 | beam structural | federal specifications | Avl | RFQ |
QQA200-11 | 9540-00-508-8871 | beam structural | society of automotive engineers inc | Avl | RFQ |
QQA200-11 | 9540-00-508-8871 | beam structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 4.000 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.140 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.140 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.140 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.260 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.320 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.580 INCHES NOMINAL |
BQKH | LEG TIP THICKNESS | 0.060 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 1.128 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 | 90.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATT | MATERIAL | ALUMINUM ALLOY 7075 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |
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