NSN 9540-01-072-1176
Part Details | STRUCTURAL ANGLE
9540-01-072-1176 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: 5566, 78B, ASTM B221, QQA2003, QQ-A-200/3, LS3826, K10A267T8511, MS14284E279, NAS34124, NAS341-24, 11362A, 11362-A, AMSQQA2003, AMS-QQ-A-200/3, 607919, 60-7919, PA3420, 9540-01-072-1176, 01-072-1176, 9540010721176, 010721176
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | FEB 23, 1979 | 01-072-1176 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-072-1176
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5566 | 77783 | ALCOA/REYNOLDS METALS COMPANY |
| 78B | 01634 | ALUMINUM CO OF AMERICA |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| LS3826 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| K10A267T8511 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| MS14284E279 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| NAS341-24 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| 11362-A | 55088 | PIMALCO INC.DIV ALCOA INC GLOBAL HARD ALLOY |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 60-7919 | 29321 | TRANSTAR METALS CORP |
| PA3420 | 06012 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-072-1176
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 2.500 INCHES NOMINAL |
| OVERALL WIDTH | 2.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.438 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.438 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.438 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.438 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 2.315 POUNDS PER LINEAR FOOT |