The NSN 9540-01-428-2774 part numbers CVC10012-154CA, ASTM B221, AMS-QQ-A-200 11, QQ A 200 11, 60-21307 manufactured by Triumph Aerostructures Llc, Triumph Actuation Systems, Astm International, Sae International, Federal Specifications Promulgat 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 9540-01-428-2774 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 9540-01-428-2774 parts of Beam Structural, and one of our account managers will respond to it within fifteen minutes or less.
Alternative NSN: 9540-01-428-2774 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 014282774 |
NCB Code: USA (01) |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
CVC10012-154CA | triumph aerostructures llc | beam structural | Avl | RFQ |
CVC10012-154CA | triumph actuation systems | beam structural | Avl | RFQ |
ASTM B221 | astm international | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | sae international | beam structural | Avl | RFQ |
QQ A 200 11 | federal specifications promulgat | beam structural | Avl | RFQ |
60-21307 | transtar metals corp | beam structural | Avl | RFQ |
AMS QQ A 200 11 | society of automotive engineers inc | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 2.478 INCHES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
AJJP | LEG THICKNESS | 0.120 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.689 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 5.250 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CSMZ | LEFT TOP INSIDE ANGLE | 110.0 DEGREES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.120 INCHES NOMINAL |
AARN | FABRICATION METHOD | EXTRUDED |
ABRY | LENGTH | 12.000 FEET NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.120 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | B-2 BOMBER |
AGTA | BASIC SHAPE STYLE | T SHAPE |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.561 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 1.108 POUNDS PER SQUARE FOOT |
CMZY | FIRST TIP STYLE | SQUARE END |
CRZC | RIGHT TOP INSIDE ANGLE | 70.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATL | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND CONDITION ANNEALED |
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