We appreciate your interest in our selection of parts that fall under the NSN 9540-01-330-7308. Below, top-requested part numbers like AMS-QQ-A-200 11, 60-14340, AMS QQ A 200 11, QQ-A-200/11, 1MA160D05-10277, and others are presented alongside their manufacturer for your perusal. In order to receive pricing options on any featured NSN 9540-01-330-7308, simply click on the “RFQ” button next to it and complete the quote request form you are directed to. Be sure to include as many details as you can about your requirements and restrictions alike so our team can best formulate ideal fulfillment options for your consideration.
Owned and operated by the NSN parts supplier ASAP Semiconductor, National Stock Numbers Quotes is only stocked with items that meet strict regulatory and statutory guidelines for export compliance and quality assurance. Moreover, all NSN 9540-01-330-7308 items on this page are sourced from leading manufacturers that we trust and have vetted as necessary. Aside from this steadfast commitment, we also aim to address the unique constraints of customers wherever possible, even if other channels have failed to. If you have any further questions about the services we offer or wish to discuss your needs directly, our representatives are always just a call or email away from assisting you!
Item Name | Beam Structural |
Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Base Metal |
National Item Identification Number (NIIN) | 01-330-7308 (013307308) |
NCB Code | USA (01) |
Manufacturer | Society Of Automotive Engineers Inc, Transtar Metals Corp, Sae International, Federal Specifications, Boeing Company The |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | RFQ |
60-14340 | transtar metals corp | beam structural | RFQ |
AMS QQ A 200 11 | sae international | beam structural | RFQ |
QQ-A-200/11 | federal specifications | beam structural | RFQ |
1MA160D05-10277 | boeing company the | beam structural | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.085 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.085 INCHES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND 73511 TEMPER |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.170 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
ABKW | OVERALL HEIGHT | 2.120 INCHES NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
HEAT | HEAT TREATMENT | T-73511 SOLUTION HEAT TREATED |
Relevant Components for NSN - 9540-01-330-7308, 9540013307308 | ||||
9505-00-063-6562 (9505000636562) | 9540-01-354-5094 (9540013545094) | 9540-01-166-2658 (9540011662658) | 9535-01-692-5618 (9535016925618) | |
9505-00-722-1588 (9505007221588) | 9540-01-589-9104 (9540015899104) | 9510-01-553-9634 (9510015539634) | 9540-00-487-5731 (9540004875731) | |
9510-00-188-1699 (9510001881699) | 9535-01-541-1664 (9535015411664) | 9505-00-065-8363 (9505000658363) | 9510-00-596-6288 (9510005966288) | |
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