The NSN 9540-01-103-0038 part numbers such as QQ A 200 15, AMS-QQ-A-200 15, AMS QQ A 200 15, 1MA160D06-10192, 10164584 manufactured by Federal Specifications, Society Of Automotive Engineers Inc, Sae International, Boeing Company The, Paaesikunta Logistiikkaosasto 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 9540-01-103-0038. 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: 9540-01-103-0038 |
Item Name: Beam Structural |
Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
NIIN: 011030038 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications, Society Of Automotive Engineers Inc, Sae International, Boeing Company The, Paaesikunta Logistiikkaosasto |
Federal Specifications | Society Of Automotive Engineer.. | Sae International |
Boeing Company The | Paaesikunta Logistiikkaosasto |
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
QQ A 200 15 | 9540-01-103-0038 | beam structural | Avl | RFQ |
AMS-QQ-A-200 15 | 9540-01-103-0038 | beam structural | Avl | RFQ |
AMS QQ A 200 15 | 9540-01-103-0038 | beam structural | Avl | RFQ |
1MA160D06-10192 | 9540-01-103-0038 | beam structural | Avl | RFQ |
10164584 | 9540-01-103-0038 | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.000 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 |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.622 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.628 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 | 3.250 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.396 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-76511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/15, ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T76511 TEMPER |
You Can Click Here to Get Quote For Your Required Aircraft Parts Within 15 Minutes.
Request for Quote