NSN 9540-01-071-6529
Part Details | STRUCTURAL ANGLE
9540-01-071-6529 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: AND101330602, AND10133-0602, ASTM B221, 1MA100B0210011, 1MA100B02-10011, QQA2003, QQ-A-200/3, HA357, K10A55T3511, MS14284E025, 10164579, 10565A, 10565-A, AMSQQA2003, AMS-QQ-A-200/3, 101330602, 10133-0602, 9540-01-071-6529, 01-071-6529, 9540010716529, 010716529
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | FEB 13, 1979 | 01-071-6529 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-071-6529
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10133-0602 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1MA100B02-10011 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| HA357 | 10383 | KAISER ALUMINUM AND CHEMICAL CORPTRENTWOOD WORKS-MARKETING DEPT |
| K10A55T3511 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| MS14284E025 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 10164579 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| 10565-A | 55088 | PIMALCO INC.DIV ALCOA INC GLOBAL HARD ALLOY |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 10133-0602 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-071-6529
| 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 | 0.750 INCHES NOMINAL |
| OVERALL WIDTH | 0.750 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.094 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.094 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.094 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.156 POUNDS PER LINEAR FOOT |