Alternative NSN: 9540-01-363-8555 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013638555 |
NCB Code: USA (01) |
Manufacturers: Boeing Company The, Federal Specifications, Sae International, Society Of Automotive Engineers Inc |
Browse NSN parts of NSN 9540-01-363-8555 and get lowest price for your requested parts in 15 minutes. Just ordered part of NSN 9540-01-363-8555 like 1MA160D05-10406, 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 |
---|---|---|---|---|
1MA160D05-10406 | 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 | 2.750 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.100 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.230 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.390 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 | 4.620 INCHES NOMINAL |
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-73511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 7075 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T73511 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