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) | 00-148-4375 (001484375) |
NCB Code | USA (00) |
Manufacturer | General Dynamics Corporation, Hughes Missile Systems Co, Tracor Flight Systems Inc, Sae International, The Boeing Company, Lockheed Martin Corporation, Society Of Automotive Engineers Inc, Bae Systems Inc, Aluminum Co Of America, Federal Specifications |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
E712203 | general dynamics corporation | beam structural | RFQ |
E712203 | hughes missile systems co | beam structural | RFQ |
E712203 | tracor flight systems inc | beam structural | RFQ |
AMS QQ A 200 3 | sae international | beam structural | RFQ |
BAC1505-18884 | the boeing company | beam structural | RFQ |
2-2106 | lockheed martin corporation | beam structural | RFQ |
AMS QQ A 200 3 | society of automotive engineers inc | beam structural | RFQ |
E712203 | bae systems inc | beam structural | RFQ |
23160 | aluminum co of america | beam structural | RFQ |
QQ-A-200/3 | federal specifications | beam structural | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.064 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.064 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.064 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 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 |
BQJG | TOP FLANGE WIDTH | 1.500 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.230 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 | T-3511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3,ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3511 TEMPER |
Relevant Components for NSN - 9540-00-148-4375, 9540001484375 | ||||
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.
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