At NSN Unlimited, we maintain a large database of parts 14784, 1M558, 22899, 60 4493, 60-4493 with NSN 9540-00-540-6025 used in civil and defense applications for the aerospace, marine, and commercial manufactured by International Light Metals Corp, Tracor Flight Systems Inc, The Boeing Company, Federal Specifications, Boeing Company The. 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: 9540-00-540-6025 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 005406025 |
NCB Code: USA (00) |
Manufacturers: International Light Metals Corp , Tracor Flight Systems Inc , The Boeing Company , Federal Specifications , Boeing Company The , Aluminum Co Of America , Transtar Metals Corp , Society Of Automotive Engineers Inc , Sae International , General Dynamics Corporation |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
14784 | 9540-00-540-6025 | beam structural | international light metals corp | Avl | RFQ |
1M558 | 9540-00-540-6025 | beam structural | tracor flight systems inc | Avl | RFQ |
1M558 | 9540-00-540-6025 | beam structural | the boeing company | Avl | RFQ |
1M558 | 9540-00-540-6025 | beam structural | federal specifications | Avl | RFQ |
1M558 | 9540-00-540-6025 | beam structural | boeing company the | Avl | RFQ |
22899 | 9540-00-540-6025 | beam structural | aluminum co of america | Avl | RFQ |
60 4493 | 9540-00-540-6025 | beam structural | transtar metals corp | Avl | RFQ |
60-4493 | 9540-00-540-6025 | beam structural | the boeing company | Avl | RFQ |
60-4493 | 9540-00-540-6025 | beam structural | tracor flight systems inc | Avl | RFQ |
60-4493 | 9540-00-540-6025 | beam structural | federal specifications | Avl | RFQ |
AMS-QQA200-11 | 9540-00-540-6025 | beam structural | federal specifications | Avl | RFQ |
AMS-QQA200-11 | 9540-00-540-6025 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQA200-11 | 9540-00-540-6025 | beam structural | sae international | Avl | RFQ |
AMS-QQA200-11 | 9540-00-540-6025 | beam structural | tracor flight systems inc | Avl | RFQ |
AMS-QQA200-11 | 9540-00-540-6025 | beam structural | the boeing company | Avl | RFQ |
BAC1505 26360 | 9540-00-540-6025 | beam structural | the boeing company | Avl | RFQ |
E711111 | 9540-00-540-6025 | beam structural | general dynamics corporation | Avl | RFQ |
E711111 | 9540-00-540-6025 | beam structural | tracor flight systems inc | Avl | RFQ |
QQA200-11 | 9540-00-540-6025 | beam structural | tracor flight systems inc | Avl | RFQ |
QQA200-11 | 9540-00-540-6025 | beam structural | the boeing company | Avl | RFQ |
QQA200-11 | 9540-00-540-6025 | beam structural | federal specifications | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.000 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.050 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.050 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.050 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.937 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.938 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 | 1.875 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.170 POUNDS PER LINEAR 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 |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATT | MATERIAL | ALUMINUM ALLOY 7075 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |
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