Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number AMS-QQ-A-200 11-T73511, a Society Of Automotive Engineers Inc item that is listed alongside the description “Beam Structural” and the NSN 9540014699501. To guarantee a swift procurement process for NSN part number AMS-QQ-A-200 11-T73511, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.
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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number AMS-QQ-A-200 11-T73511 is manufactured by Society Of Automotive Engineers Inc, it is specifically done so under CAGE Code 81343, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 9540-01-469-9501, one can also determine that this part falls under FSC 9540 Structural Shapes Nonferrous Base Metal. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-469-9501 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014699501 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | U | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS10140-1404 | 5 | 1 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | ACFT CEN SEC |
| AJJB | FIRST TIP RADIUS | 0.010 INCHES NOMINAL |
| BMPR | LEFT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BPXF | LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXH | RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXK | FILLET RADIUS WHERE BOTTOM LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.500 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | LEFT QUARTER RADIUS |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CTBR | LEFT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FEAT | SPECIAL FEATURES | WEAPONS SYSTEM IS AIRCRAFT, B-2 BOMBER (ATB) |
| ZZZK | SPECIFICATION/STANDARD DATA | 81348-QQ-A-200/11E/CANCELED/ GOVERNMENT SPECIFICATION AND 99237-AND10140 GOVERNMENT STANDARD |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 32.900 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | I SHAPE |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 2.500 INCHES NOMINAL |
| CMZZ | SECOND TIP RADIUS | 0.010 INCHES NOMINAL |
| CNQK | SECOND TIP STYLE | RIGHT QUARTER RADIUS |
| CNQN | FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/SECOND TIP |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11 |
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