The NSN 9540-01-437-2658 part numbers CVC10010-116CJ, AMS-QQ-A-200 11, QQ A 200 11 manufactured by Triumph Actuation Systems, Triumph Aerostructures Llc, Society Of Automotive Engineers Inc, Federal Specifications Promulgat, Sae International 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 9540-01-437-2658 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 9540-01-437-2658 parts of Beam Structural, and one of our account managers will respond to it within fifteen minutes or less.
Alternative NSN: 9540-01-437-2658 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 014372658 |
NCB Code: USA (01) |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
CVC10010-116CJ | triumph actuation systems | beam structural | Avl | RFQ |
CVC10010-116CJ | triumph aerostructures llc | 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 |
AMS-QQ-A-200 11 | sae international | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
MATT | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
CNBD | FIRST TIP INNER RADIUS | 0.020 INCHES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.580 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 0.880 INCHES NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.580 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.063 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBJ | FIRST TIP OUTER RADIUS | 0.020 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
ABRY | LENGTH | 12.000 FEET NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.063 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.160 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
HEAT | HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER T76511 |
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