NSN 9540-00-261-5112
Part Details | STRUCTURAL ANGLE
9540-00-261-5112 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: AND101342003, AND10134-2003, 4086, 734P, 1391557, 1391557, 1199946, 1199946, BAC15034283, BAC1503-4283, QQA20011, QQ-A-200/11, 2139, 2-139, LS32063, LS3206-3, AMS101342003, AMS10134-2003, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-261-5112, 00-261-5112, 9540002615112, 002615112
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1961 | 00-261-5112 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-261-5112
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10134-2003 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| 4086 | 77783 | ALCOA/REYNOLDS METALS COMPANY |
| 734P | 01634 | ALUMINUM CO OF AMERICA |
| 1391557 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1391557 | 18355 | BOEING COMPANY, THEDBA BOEING |
| 1199946 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1199946 | 18355 | BOEING COMPANY, THEDBA BOEING |
| BAC1503-4283 | 82918 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| 2-139 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| LS3206-3 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| AMS10134-2003 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-261-5112
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| OVERALL WIDTH | 2.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.125 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.125 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.470 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |