NSN 9540-00-720-1326
Part Details | STRUCTURAL ANGLE
9540-00-720-1326 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: AND101331001, AND10133-1001, ASTM B221, 1210330, 1210330, S106, QQA2002, QQ-A-200/2, FS10101010, FS1010-1010, VS25215, VS252-15, 15889, HA362, 5738, AMSQQA2002, AMS-QQ-A-200/2, AMS 4153, 9540-00-720-1326, 00-720-1326, 9540007201326, 007201326
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-720-1326 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-720-1326
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10133-1001 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1210330 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1210330 | 18355 | BOEING COMPANY, THEDBA BOEING |
| S106 | 71379 | CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION |
| QQ-A-200/2 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| FS1010-1010 | 89446 | HILLER AIRCRAFT CORPORATION |
| VS252-15 | 14170 | HUGHES MISSILE SYSTEMS COSAN DIEGO |
| 15889 | 27610 | INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP |
| HA362 | 10383 | KAISER ALUMINUM AND CHEMICAL CORPTRENTWOOD WORKS-MARKETING DEPT |
| 5738 | 01484 | REYNOLDS METALS CO |
| AMS-QQ-A-200/2 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS 4153 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-720-1326
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| LENGTH | 12.000 FEET NOMINAL |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.063 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.063 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.155 POUNDS PER LINEAR FOOT |