Alternative NSN: 9540-01-459-6460 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 014596460 |
NCB Code: USA (01) |
Manufacturers: Boeing Company The, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp |
Browse NSN parts of NSN 9540-01-459-6460 and get lowest price for your requested parts in 15 minutes. Just ordered part of NSN 9540-01-459-6460 like 1MA160B04-10375, 60-11659, AMS-QQ-A-200 3, AMS-QQ-A-200 3 described as Beam Structural from industry leading manufactures such as Boeing Company The, Transtar Metals Corp, Society Of Automotive Engineers Inc, Sae International. 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 |
---|---|---|---|---|
1MA160B04-10375 | Boeing Company The | beam structural | Avl | RFQ |
60-11659 | Transtar Metals Corp | beam structural | Avl | RFQ |
AMS-QQ-A-200 3 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
AMS-QQ-A-200 3 | Sae International | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 3.250 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.190 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.190 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | F-15I ACFT |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.4375 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.4375 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 | 2.875 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 1.122 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-8511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALOY, AMS-QQ-A-200/3, ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 2024 AND TEMPER T8511 |
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