NSN 9540-01-071-6542
Part Details | STRUCTURAL ANGLE
9540-01-071-6542 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: AND101330701, AND10133-0701, ASTMB221, QQA2003, QQ-A-200/3, K10A22T3511, MS14284E041, AMS101330701, AMS10133-0701, AMSQQA2003, AMS-QQ-A-200/3, 9540-01-071-6542, 01-071-6542, 9540010716542, 010716542
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | FEB 13, 1979 | 01-071-6542 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-071-6542
Part Number | Cage Code | Manufacturer |
---|---|---|
AND10133-0701 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
ASTMB221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
K10A22T3511 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
MS14284E041 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
AMS10133-0701 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-01-071-6542
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 0.875 INCHES NOMINAL |
OVERALL WIDTH | 0.875 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 | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.063 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.063 INCHES NOMINAL |