NSN 9540-00-720-1320
Part Details | STRUCTURAL ANGLE
9540-00-720-1320 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: AND101341006, AND10134-1006, AND101341006, AND10134-1006, ASTM B221, 1294834, 1294834, 1240703, 1240703, AND101341006, AND10134-1006, 40557, 40371, AND101341006QQA2002T6, AND10134-1006/QQ-A-200/2-T6, QQA2002, QQ-A-200/2, FS10121009, FS1012-1009, AND101341006, AND10134-1006, 15501, 14628, HA19, 21314, 2-1314, AND101341006, AND10134-1006, 7303, AMSQQA2002, AMS-QQ-A-200/2, AND101341006, AND10134-1006, 9540-00-720-1320, 00-720-1320, 9540007201320, 007201320
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-720-1320 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-720-1320
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10134-1006 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| AND10134-1006 | 01634 | ALUMINUM CO OF AMERICA |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1294834 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1294834 | 18355 | BOEING COMPANY, THEDBA BOEING |
| 1240703 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1240703 | 18355 | BOEING COMPANY, THEDBA BOEING |
| AND10134-1006 | 43999 | BOEING COMPANY, THEDBA BOEING |
| 40557 | 99267 | BOHN ALUMINUM AND BRASS CODIV OF GULF AND WESTERN MFG CO |
| 40371 | 99267 | BOHN ALUMINUM AND BRASS CODIV OF GULF AND WESTERN MFG CO |
| AND10134-1006/QQ-A-200/2-T6 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
| QQ-A-200/2 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| FS1012-1009 | 89446 | HILLER AIRCRAFT CORPORATION |
| AND10134-1006 | 14170 | HUGHES MISSILE SYSTEMS COSAN DIEGO |
| 15501 | 27610 | INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP |
| 14628 | 27610 | INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP |
| HA19 | 10383 | KAISER ALUMINUM AND CHEMICAL CORPTRENTWOOD WORKS-MARKETING DEPT |
| 2-1314 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| AND10134-1006 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| 7303 | 01484 | REYNOLDS METALS CO |
| AMS-QQ-A-200/2 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AND10134-1006 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 9540-00-720-1320
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| LENGTH | 12.000 FEET NOMINAL |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 0.875 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 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 | 0.202 POUNDS PER LINEAR FOOT |