NSN 9540-01-072-9576
Part Details | STRUCTURAL ANGLE
9540-01-072-9576 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: 26873, ASTM B221, QQA2003, QQ-A-200/3, K10A50T42, K10A50T3511, 60354, MS14285E017, AMSQQA2003, AMS-QQ-A-200/3, 607239, 60-7239, 9540-01-072-9576, 01-072-9576, 9540010729576, 010729576
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAR 07, 1979 | 01-072-9576 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE W/ INNER AND OUTER CORNER RADII
SQUARE W/ INNER AND OUTER CORNER RADII
Cross Reference | NSN 9540-01-072-9576
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 26873 | 77783 | ALCOA/REYNOLDS METALS COMPANY |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| K10A50T42 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| K10A50T3511 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 60354 | 26710 | MID-CENTRAL MFG. INC. |
| MS14285E017 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 60-7239 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-072-9576
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.200 INCHES NOMINAL |
| OVERALL WIDTH | 2.750 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.080 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.030 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.080 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 |
| WEIGHT PER UNIT MEASURE | 0.374 POUNDS PER LINEAR FOOT |
| SPECIFICATION/STANDARD DATA | 81755-K10 MANUFACTURERS STANDARD |
| END ITEM IDENTIFICATION | F-16 AIRCRAFT |