At NSN Unlimited, we maintain a large database of parts 1MA160B04-10340, 60-7544, AMS-QQ-A-200 3, QQ-A-200 3 with NSN 9540-01-341-6983 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Society Of Automotive Engineers Inc, Boeing Company The, Transtar Metals Corp, Sae International, Federal Specifications. Utilize our interface to browse items by part number, part type, manufacturer, and more. Obtain insights on top MRO and FBO services, Manufacturer profiles, and part catalogs.
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Alternative NSN: 9540-01-341-6983 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013416983 |
NCB Code: USA (01) |
Manufacturers: Society Of Automotive Engineers Inc , Boeing Company The , Transtar Metals Corp , Sae International , Federal Specifications |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1MA160B04-10340 | 9540-01-341-6983 | beam structural | society of automotive engineers inc | Avl | RFQ |
1MA160B04-10340 | 9540-01-341-6983 | beam structural | boeing company the | Avl | RFQ |
1MA160B04-10340 | 9540-01-341-6983 | beam structural | transtar metals corp | Avl | RFQ |
60-7544 | 9540-01-341-6983 | beam structural | society of automotive engineers inc | Avl | RFQ |
60-7544 | 9540-01-341-6983 | beam structural | transtar metals corp | Avl | RFQ |
60-7544 | 9540-01-341-6983 | beam structural | boeing company the | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-341-6983 | beam structural | boeing company the | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-341-6983 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-341-6983 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-341-6983 | beam structural | transtar metals corp | Avl | RFQ |
QQ-A-200 3 | 9540-01-341-6983 | beam structural | transtar metals corp | Avl | RFQ |
QQ-A-200 3 | 9540-01-341-6983 | beam structural | society of automotive engineers inc | Avl | RFQ |
QQ-A-200 3 | 9540-01-341-6983 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 3 | 9540-01-341-6983 | beam structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.900 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | F-15 AIRCRAFT |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.219 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.450 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.329 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE END |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 98.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 82.0 DEGREES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T8511 TEMPER |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.231 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
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