The NSN 9540-01-341-6983 part numbers such as QQ A 200 3, AMS-QQ-A-200 3, AMS-QQ-A-200 3, 60-7544, 1MA160B04-10340 manufactured by Federal Specifications, Society Of Automotive Engineers Inc, Sae International, Transtar Metals Corp, Boeing Company The are available in RFQ Experts’ inventory. An ASAP Semiconductor owned and operated website, RFQ Experts has over six billion parts in its inventory for NSN 9540-01-341-6983. ASAP is committed to streamlining the parts procurement process for our customers, making it easy for them to search through billions of parts to find exactly what they are looking for. We have dedicated account managers ready to solve procurement issues our clients face, whether it’s a need for obsolete parts, or an aircraft on ground situation. As an AS9120B, ISO 9001:2015, and FAA AC 0056B certified company, each and every part that we ship goes through numerous quality checks and inspections, to ensure that we sell only the highest-quality parts.
Alternative NSN: 9540-01-341-6983 |
Item Name: Beam Structural |
Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
NIIN: 013416983 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications, Society Of Automotive Engineers Inc, Sae International, Transtar Metals Corp, Boeing Company The |
Federal Specifications | Society Of Automotive Engineer.. | Sae International |
Transtar Metals Corp | Boeing Company The |
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
QQ A 200 3 | 9540-01-341-6983 | beam structural | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-341-6983 | beam structural | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-341-6983 | beam structural | Avl | RFQ |
60-7544 | 9540-01-341-6983 | beam structural | Avl | RFQ |
1MA160B04-10340 | 9540-01-341-6983 | beam structural | 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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