Part Details | STRUCTURAL ANGLE
9540-00-145-5699 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: AND101351002, AND10135-1002, 30032, QQA20011, QQ-A-200/11, AMS101351002, AMS10135-1002, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-145-5699, 00-145-5699, 9540001455699, 001455699
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-145-5699 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
RIGHT QUARTER RADIUS
SQUARE END
RIGHT QUARTER RADIUS
Cross Reference | NSN 9540-00-145-5699
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10135-1002 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| 30032 | 01634 | ALUMINUM CO OF AMERICA |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS10135-1002 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-145-5699
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | K$DRL |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 0.750 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.095 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.063 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | SQUARE END |
| SECOND TIP RADIUS | 0.095 INCHES NOMINAL |
| SECOND TIP DIAMETER | 0.190 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.150 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T6$JT6511 TEMPER |