NSN 9540-01-428-9035
Part Details | STRUCTURAL ANGLE
9540-01-428-9035 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, CVC10001375CA, CVC10001-375CA, 9540-01-428-9035, 01-428-9035, 9540014289035, 014289035
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | APR 02, 1996 | 01-428-9035 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE W/ INNER AND OUTER CORNER RADII
SQUARE W/ INNER AND OUTER CORNER RADII
Cross Reference | NSN 9540-01-428-9035
| 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 |
| CVC10001-375CA | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-01-428-9035
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | O-ANNEALED |
| LENGTH | 12.000 FEET NOMINAL |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| OVERALL WIDTH | 1.490 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.117 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.190 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.117 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| FIRST TIP INNER RADIUS | 0.030 INCHES NOMINAL |
| FIRST TIP OUTER RADIUS | 0.030 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| END ITEM IDENTIFICATION | B-2 BOMBER |