NSN 9540-01-443-7365 · NIIN 014437365 · FSC 9540
NO DASHES 9540014437365
In Stock
BEAM,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: B-1B AIRCRAFT
Technical characteristics
15 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABRY | LENGTH | INCHES MINIMUM 23.970 AND INCHES MAXIMUM 24.030 |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | INCHES MINIMUM 0.115 AND INCHES MAXIMUM 0.135 |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | INCHES MINIMUM 0.115 AND INCHES MAXIMUM 0.135 |
| AGAV | END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES MINIMUM 0.760 AND INCHES MAXIMUM 0.780 |
| BQJG | TOP FLANGE WIDTH | INCHES MINIMUM 1.670 AND INCHES MAXIMUM 1.690 |
| CMZY | FIRST TIP STYLE | |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | DEGREES MINIMUM 95.2167 AND DEGREES MAXIMUM 96.2167 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | FLANGE,RS |
| FEAT | SPECIAL FEATURES | USED IN THE HS PROJECT. THE /1RS IS USED TO MAKE P/N -003/005/007/009/0013/015/017/019/023/025/027 |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| ZZZV | FSC APPLICATION DATA | STRUCTURAL SHAPES |