NSN 9540-01-071-6528
Part Details | STRUCTURAL ANGLE
9540-01-071-6528 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: AND101330602, AND10133-0602, QQA2003, QQ-A-200/3, K10A550, MS14284E023, 10565A, 10565-A, 9540-01-071-6528, 01-071-6528, 9540010716528, 010716528
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | FEB 13, 1979 | 01-071-6528 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-071-6528
Part Number | Cage Code | Manufacturer |
---|---|---|
AND10133-0602 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
K10A550 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
MS14284E023 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
10565-A | 55088 | PIMALCO INC.DIV ALCOA INC GLOBAL HARD ALLOY |
Technical Data | NSN 9540-01-071-6528
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 | O-ANNEALED |
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 | 0.094 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.094 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.094 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.094 INCHES NOMINAL |
NONDEFINITIVE SPEC/STD DATA | O TEMPER |