The NSN 9540-01-428-9526 part numbers AMS QQ A 200 11, AMS-QQ-A-200 11, QQ-A-200 11, CVC10012-207CA manufactured by Sae International, Society Of Automotive Engineers Inc, Federal Specifications Promulgat, Triumph Aerostructures Llc, Triumph Actuation Systems is available in our inventory. As an ASAP Semiconductor owned and operated website, ASAP Aviation Unlimited has access to over three billion parts, paired with easy-to-use search engines that enable our customers to browse through our NSN 9540-01-428-9526 inventory quickly and efficiently. Our focus on quality control has earned us our FAA AC 0056B accreditation and AS9120B, ISO 9001:2015 certification, and we are the only independent distributor with a No China Sourcing pledge. If you are ready to get started, you can send an Instant RFQ form from this page for NSN 9540-01-428-9526 parts of Beam Structural, and one of our account managers will respond to it within fifteen minutes or less.
Alternative NSN: 9540-01-428-9526 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 014289526 |
NCB Code: USA (01) |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
AMS QQ A 200 11 | sae international | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | Avl | RFQ |
QQ-A-200 11 | federal specifications promulgat | beam structural | Avl | RFQ |
CVC10012-207CA | triumph aerostructures llc | beam structural | Avl | RFQ |
CVC10012-207CA | triumph actuation systems | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 5.330 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 7.600 INCHES NOMINAL |
CNBD | FIRST TIP INNER RADIUS | 0.030 INCHES NOMINAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
ABKW | OVERALL HEIGHT | 3.000 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.270 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.174 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AARN | FABRICATION METHOD | EXTRUDED |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.174 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | B-2 BOMBER |
AJJP | LEG THICKNESS | 0.155 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBJ | FIRST TIP OUTER RADIUS | 0.030 INCHES NOMINAL |
CRZC | RIGHT TOP INSIDE ANGLE | 89.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 91.0 DEGREES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
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