The NSN 9540-01-315-3612 part numbers such as QQ A 200 3, AMS QQ A 200 3, AMS QQ A 200 3, 60-20285, 40-010-25 manufactured by Federal Specifications, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp, Bell Helicopter Textron Inc 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 9540-01-315-3612. 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: 9540-01-315-3612 |
Item Name: Beam Structural |
Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
NIIN: 013153612 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp, Bell Helicopter Textron Inc |
Federal Specifications | Sae International | Society Of Automotive Engineer.. |
Transtar Metals Corp | Bell Helicopter Textron Inc |
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
QQ A 200 3 | 9540-01-315-3612 | beam structural | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-315-3612 | beam structural | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-315-3612 | beam structural | Avl | RFQ |
60-20285 | 9540-01-315-3612 | beam structural | Avl | RFQ |
40-010-25 | 9540-01-315-3612 | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 2.250 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
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 | 0.975 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.975 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 1.950 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.251 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 |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
AARN | FABRICATION METHOD | EXTRUDED |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.050 INCHES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED OR T-3510 SOLUTION HEAT TREATED OR T-3511 SOLUTION HEAT TREATED |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T4 TEMPER OR T3510 TEMPER OR T3511 TEMPER |
You Can Click Here to Get Quote For Your Required Aircraft Parts Within 15 Minutes.
Request for Quote