The NSN 9540-01-367-1248 part numbers such as QQ-A-200 11, ASTM B221, AMS QQ A 200 11, AMS QQ A 200 11, 60 21205 manufactured by Federal Specifications, American Society For Testing And, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp 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 9540-01-367-1248. 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: 9540-01-367-1248 |
Item Name: Beam Structural |
Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
NIIN: 013671248 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications, American Society For Testing And, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp, Boeing Company The |
Federal Specifications | American Society For Testing A.. | Sae International |
Society Of Automotive Engineer.. | Transtar Metals Corp | Boeing Company The |
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
QQ-A-200 11 | 9540-01-367-1248 | beam structural | Avl | RFQ |
ASTM B221 | 9540-01-367-1248 | beam structural | Avl | RFQ |
AMS QQ A 200 11 | 9540-01-367-1248 | beam structural | Avl | RFQ |
AMS QQ A 200 11 | 9540-01-367-1248 | beam structural | Avl | RFQ |
60 21205 | 9540-01-367-1248 | beam structural | Avl | RFQ |
1MA160D01-10323 | 9540-01-367-1248 | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.562 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.750 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.875 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.187 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.625 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.926 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBJ | FIRST TIP OUTER RADIUS | 0.031 INCHES NOMINAL |
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 |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND ANNEALED CONDITION |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.187 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
CNBD | FIRST TIP INNER RADIUS | 0.031 INCHES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
You Can Click Here to Get Quote For Your Required Aircraft Parts Within 15 Minutes.
Request for Quote