NSN 9540-01-468-0130
Part Details | STRUCTURAL ANGLE
9540-01-468-0130 A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet.
Alternate Parts: QQA20015, QQ-A-200/15, AMSQQA20015, AMS-QQ-A-200/15, CVC10001331CJ, CVC10001-331CJ, 9540-01-468-0130, 01-468-0130, 9540014680130, 014680130
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | SEP 24, 1999 | 01-468-0130 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-468-0130
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| QQ-A-200/15 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/15 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| CVC10001-331CJ | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-01-468-0130
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| LENGTH | 12.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 2.000 INCHES NOMINAL |
| OVERALL WIDTH | 2.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.320 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.320 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.032 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.032 INCHES NOMINAL |
| END ITEM IDENTIFICATION | B-2 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE, UNEQUAL LEGS AND THICKNESSES |