AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
If you are in the market for NSN 9540-00-390-0745 supplies that are routinely offered with affordable pricing and prompt delivery, turn to AI NSN Parts. On this page, you will find popular part numbers like 60-3903, 56429, AMS-QQ-A-200 11, AMS QQ A 200 11, LS34769-1, and others that are available for procurement at any time. Be sure to browse our NSN 9540-00-390-0745 inventory as you see fit, and if you come across any item that grabs your attention, click on the “RFQ” button situated alongside it to access our online quote request service. Within 15 minutes of receiving your RFQ submission, one of our experts will supply you with a customized response that matches your specifications.
While other channels may ask you to sacrifice quality, pricing, or quick fulfillment, we consistently aim for an optimal balance that allows you to meet budgets and deadlines without ever foregoing dependability. Moreover, if you are seeking a hard-to-find NSN 9540-00-390-0745 part, our knowledgeable representatives can unearth product solutions when avenues come up short. With this in mind, start the procurement process today to see why customers steadily choose us for their operational needs.
| 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) | 00-390-0745 (003900745) |
| NCB Code | USA (00) |
| Manufacturer | Transtar Metals Corp, International Light Metals Corp, Society Of Automotive Engineers Inc, Sae International, Lockheed Martin Corporation, Federal Specifications |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 60-3903 | transtar metals corp | beam structural | RFQ |
| 56429 | international light metals corp | beam structural | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | RFQ |
| AMS QQ A 200 11 | sae international | beam structural | RFQ |
| LS34769-1 | lockheed martin corporation | beam structural | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | RFQ |
| PA27150 | transtar metals corp | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABMK | OVERALL WIDTH | 1.521 INCHES MINIMUM AND 1.537 INCHES MAXIMUM |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXJ | LEFT SIDE FLANGE HEIGHT | 2.626 INCHES MINIMUM AND 2.674 INCHES MAXIMUM |
| ADXK | RIGHT SIDE FLANGE HEIGHT | 2.626 INCHES MINIMUM AND 2.674 INCHES MAXIMUM |
| ADXL | LEFT SIDE FLANGE THICKNESS | 0.064 INCHES MINIMUM AND 0.076 INCHES MAXIMUM |
| ADXM | RIGHT SIDE FLANGE THICKNESS | 0.064 INCHES MINIMUM AND 0.076 INCHES MAXIMUM |
| AGTA | BASIC SHAPE STYLE | H SHAPE |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.313 INCHES MINIMUM AND 1.337 INCHES MAXIMUM |
| BPXF | LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.313 INCHES MINIMUM AND 1.337 INCHES MAXIMUM |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.313 INCHES MINIMUM AND 1.337 INCHES MAXIMUM |
| BPXH | RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.313 INCHES MINIMUM AND 1.337 INCHES MAXIMUM |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.044 INCHES MINIMUM AND 0.076 INCHES MAXIMUM |
| BPXK | FILLET RADIUS WHERE BOTTOM LEFT FLANGE JOINS WEB FLANGE/LEG | 0.044 INCHES MINIMUM AND 0.076 INCHES MAXIMUM |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.044 INCHES MINIMUM AND 0.076 INCHES MAXIMUM |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.044 INCHES MINIMUM AND 0.076 INCHES MAXIMUM |
| BPXN | WEB FLANGE THICKNESS | 0.064 INCHES MINIMUM AND 0.076 INCHES MAXIMUM |
| BRFD | WEIGHT PER UNIT MEASURE | 0.565 POUNDS PER SQUARE 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 |
| CNQN | FOURTH 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 |
| CTBR | LEFT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6 TEMPER |
| Relevant Components for NSN - 9540-00-390-0745, 9540003900745 | ||||
| 9510-00-224-1673 (9510002241673) | 9505-00-541-9654 (9505005419654) | 9540-01-353-5127 (9540013535127) | 9515-66-151-1706 (9515661511706) | |
| 9515-00-153-3357 (9515001533357) | 9535-01-012-2441 (9535010122441) | 9520-01-694-5689 (9520016945689) | 9510-01-484-4625 (9510014844625) | |
| 9530-00-993-4137 (9530009934137) | 9515-00-153-3227 (9515001533227) | 9515-01-555-3938 (9515015553938) | 9530-00-060-5594 (9530000605594) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote