NSN 9540-01-004-7675
Part Details | STRUCTURAL ANGLE
9540-01-004-7675 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: AND101342001, AND10134-2001, 1MA100A0310114, 1MA100A03-10114, QQA2002, QQA200-2, AMSQQA2002, AMS-QQA200-2, 9540-01-004-7675, 01-004-7675, 9540010047675, 010047675
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JUN 10, 1975 | 01-004-7675 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE W/ INNER AND OUTER CORNER RADII
SQUARE W/ INNER AND OUTER CORNER RADII
Cross Reference | NSN 9540-01-004-7675
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10134-2001 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| 1MA100A03-10114 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQA200-2 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQA200-2 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-004-7675
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED AND STRESS RELIEVED BY STRETCHING |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| OVERALL WIDTH | 2.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| FIRST TIP INNER RADIUS | 0.010 INCHES NOMINAL |
| FIRST TIP OUTER RADIUS | 0.010 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| WEIGHT PER UNIT MEASURE | 0.358 POUNDS PER SQUARE FOOT |
| NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER |