Part Details | STRUCTURAL ANGLE
9540-00-119-4897 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: 88287, CM2009, QQA2003, QQA200-3, AMSQQA2003, AMS-QQA200-3, 9540-00-119-4897, 00-119-4897, 9540001194897, 001194897
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | OCT 23, 1968 | 00-119-4897 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-119-4897
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 88287 | 01634 | ALUMINUM CO OF AMERICA |
| CM2009 | 71379 | CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION |
| QQA200-3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQA200-3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-119-4897
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE |
| 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 | 0.600 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.040 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.062 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.040 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| WEIGHT PER UNIT MEASURE | 0.076 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | -4 TEMPER |