Part Details | STRUCTURAL ANGLE
9540-00-231-9920 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: AND101340501, AND10134-0501, ASTM B221, 1240624, 1240624, 1240624, 124-0624, AND101340501QQA2003T4, AND10134-0501/QQ-A-200/3-T4, QQA2003, QQ-A-200/3, HA383, 21334, 2-1334, RY30250, 10164, AMSQQA2003, AMS-QQ-A-200/3, 9540-00-231-9920, 00-231-9920, 9540002319920, 002319920
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-231-9920 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-231-9920
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10134-0501 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1240624 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1240624 | 18355 | BOEING COMPANY, THEDBA BOEING |
| 124-0624 | 11083 | CATERPILLAR INC.DBA CATERPILLAR |
| AND10134-0501/QQ-A-200/3-T4 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| HA383 | 10383 | KAISER ALUMINUM AND CHEMICAL CORPTRENTWOOD WORKS-MARKETING DEPT |
| 2-1334 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| RY30250 | 78022 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 10164 | 01484 | REYNOLDS METALS CO |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-231-9920
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-4 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 0.500 INCHES NOMINAL |
| OVERALL WIDTH | 0.625 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.063 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.050 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.050 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.060 POUNDS PER LINEAR FOOT |