NSN 9540-01-369-9117
Part Details | STRUCTURAL ANGLE
9540-01-369-9117 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: AND101332401, AND10133-2401, 1MA100D0110164, 1MA100D01-10164, 1MA10010164, 1MA100-10164, QQA20011, QQ-A-200/11, AMS101332401, AMS10133-2401, AMSQQA20011, AMS-QQ-A-200/11, 9540-01-369-9117, 01-369-9117, 9540013699117, 013699117
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 08, 1993 | 01-369-9117 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-369-9117
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10133-2401 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| 1MA100D01-10164 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 1MA100-10164 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS10133-2401 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-369-9117
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | O-ANNEALED |
| LENGTH | 10.000 INCHES MINIMUM AND 12.000 INCHES MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 2.250 INCHES NOMINAL |
| OVERALL WIDTH | 2.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.250 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 |