NSN 9540-01-037-5567
Part Details | STRUCTURAL ANGLE
9540-01-037-5567 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: AND101331002, AND10133-1002, ASTM B221, 1MA10010032, 1MA100-10032, AND101331002ASTM B221T6511, AND10133-1002/ASTM B221-T6511, QQA20011, QQ-A-200/11, K10D58T6511, 10018B, 10018-B, AMS101331002, AMS10133-1002, AMSQQA20011, AMS-QQ-A-200/11, 9540-01-037-5567, 01-037-5567, 9540010375567, 010375567
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAR 21, 1977 | 01-037-5567 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-037-5567
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10133-1002 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1MA100-10032 | 76301 | BOEING COMPANY, THEDBA BOEING |
| AND10133-1002/ASTM B221-T6511 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| K10D58T6511 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 10018-B | 55088 | PIMALCO INC.DIV ALCOA INC GLOBAL HARD ALLOY |
| AMS10133-1002 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-037-5567
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 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 | 0.219 POUNDS PER LINEAR FOOT |