Alternative NSN: 9540-01-238-4731 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 012384731 |
NCB Code: USA (01) |
Manufacturers: Boeing Company The, Federal Specifications, Sae International, Society Of Automotive Engineers Inc |
Browse NSN parts of NSN 9540-01-238-4731 and get lowest price for your requested parts in 15 minutes. Just ordered part of NSN 9540-01-238-4731 like 1MA10500D01, AMS QQ A 200 11, AMS QQ A 200 11, QQ A 200 11 described as Beam Structural from industry leading manufactures such as Boeing Company The, Society Of Automotive Engineers Inc, Sae International, Federal Specifications. We are proud to offer an inventory of over 2 billion ready-to-ship parts, 24/7 availability, and key locations in the U.S./abroad. These attributes allow us to meet all aircraft on ground (AOG) requirements with ease.
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
1MA10500D01 | Boeing Company The | beam structural | Avl | RFQ |
AMS QQ A 200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
AMS QQ A 200 11 | Sae International | beam structural | Avl | RFQ |
QQ A 200 11 | Federal Specifications | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 0.850 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.040 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.040 INCHES NOMINAL |
AJJB | FIRST TIP RADIUS | 0.020 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.040 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.700 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.740 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 1.400 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | FULL RADIUS |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
FEAT | SPECIAL FEATURES | TOP FLANGE OUTER FACE CONCAVE |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATT | MATERIAL | ALUMINUM ALLOY 7075 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |
9505-00-056-1762 (9505000561762) |
9505-00-056-1763 (9505000561763) |
9505-00-057-2157 (9505000572157) |
9505-00-057-9449 (9505000579449) |
9505-00-059-6171 (9505000596171) |
9505-00-059-6172 (9505000596172) |
9505-00-059-6174 (9505000596174) |
9505-00-059-6175 (9505000596175) |
9505-00-059-6176 (9505000596176) |
9505-00-061-1592 (9505000611592) |
9505-00-061-1593 (9505000611593) |
9505-00-061-1594 (9505000611594) |
Before You Go, Why Don’t You Take a Look at Our Aviation Parts Catalog.
Request for Quote