AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
Part Number 1MT360A01-10011 described as Beam Structural with NSN 9540-01-251-0815 with FSC 9540 Structural Shapes Nonferrous Base Metal by Manufacture Boeing Co The is available in stock. We provide comprehensive database of aerospace and aviation components, sub-assemblies, and completed assemblies allows us to respond to your RFQ within 15 minutes.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-251-0815 Item Description: Beam Structural | 9540 | 012510815 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1mt360a01-10011 | 5 | 1 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.300 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.350 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.350 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.250 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 | 2.125 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE-LEG | 0.250 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE-LEG | 0.250 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 3.100 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W- INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.090 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.090 INCHES NOMINAL |
| 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 |
| FEAT | SPECIAL FEATURES | MACHINED ALL OVER |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATT | MATERIAL | TITANIUM MIL-T-81556 TYPE 3 COMP A |
| ZZZT | NONDEFINITIVE SPEC-STD DATA | A COMPOSITION AND 3 TYPE |
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