NSN 9540-01-259-9617
Part Details | STRUCTURAL ANGLE
9540-01-259-9617 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: AND101330601, AND10133-0601, AND101330601QQA2008T4, AND10133-0601/QQ-A-200/8-T4, QQA2008, QQ-A-200/8, K10B18T4, 10531A, 10531-A, AMSQQA2008, AMS-QQ-A-200/8, 9540-01-259-9617, 01-259-9617, 9540012599617, 012599617
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JUL 23, 1987 | 01-259-9617 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-259-9617
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10133-0601 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| AND10133-0601/QQ-A-200/8-T4 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
| QQ-A-200/8 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| K10B18T4 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 10531-A | 55088 | PIMALCO INC.DIV ALCOA INC GLOBAL HARD ALLOY |
| AMS-QQ-A-200/8 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-259-9617
| Characteristic | Specifications |
|---|---|
| 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 | 0.750 INCHES NOMINAL |
| OVERALL WIDTH | 0.750 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.094 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| NONDEFINITIVE SPEC/STD DATA | T4 TEMPER |
