NSN 9540-01-437-7296
Part Details | STRUCTURAL ANGLE
9540-01-437-7296 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: QQA20011, QQ-A-200/11, AMSQQA20011, AMS-QQ-A-200/11, CVC10001330CA, CVC10001-330CA, 9540-01-437-7296, 01-437-7296, 9540014377296, 014377296
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | OCT 23, 1996 | 01-437-7296 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE W/ INNER AND OUTER CORNER RADII
SQUARE W/ INNER AND OUTER CORNER RADII
Cross Reference | NSN 9540-01-437-7296
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| CVC10001-330CA | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-01-437-7296
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | O-ANNEALED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 3.100 INCHES NOMINAL |
| OVERALL WIDTH | 5.100 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.420 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.190 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.210 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| FIRST TIP INNER RADIUS | 0.032 INCHES NOMINAL |
| FIRST TIP OUTER RADIUS | 0.032 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |