The NSN 9540-01-353-6239 part numbers such as QQ-A-200 3, AMS-QQ-A-200 3, AMS QQ A 200 3, 60-2933, 4E-394 manufactured by Federal Specifications, Sae International, Society Of Automotive Engineers Inc, 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 9540-01-353-6239. 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: 9540-01-353-6239 |
Item Name: Beam Structural |
Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
NIIN: 013536239 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp, Boeing Company The |
Federal Specifications | Sae International | Society Of Automotive Engineer.. |
Transtar Metals Corp | Boeing Company The |
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
QQ-A-200 3 | 9540-01-353-6239 | beam structural | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-353-6239 | beam structural | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-353-6239 | beam structural | Avl | RFQ |
60-2933 | 9540-01-353-6239 | beam structural | Avl | RFQ |
4E-394 | 9540-01-353-6239 | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.093 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
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 |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T0 TEMPER |
ABKW | OVERALL HEIGHT | 1.750 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.344 POUNDS PER LINEAR FOOT |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
You Can Click Here to Get Quote For Your Required Aircraft Parts Within 15 Minutes.
Request for Quote