NSN 9540-01-339-1570
Part Details | STRUCTURAL ANGLE
9540-01-339-1570 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: AND101331003, AND10133-1003, 1MA100C0110033, 1MA100C01-10033, QQA2008, QQ-A-200/8, AMSQQA2008, AMS-QQ-A-200/8, 101331003, 10133-1003, 9540-01-339-1570, 01-339-1570, 9540013391570, 013391570
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | MAY 17, 1991 | 01-339-1570 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-339-1570
Part Number | Cage Code | Manufacturer |
---|---|---|
AND10133-1003 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
1MA100C01-10033 | 76301 | BOEING COMPANY, THEDBA BOEING |
QQ-A-200/8 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQ-A-200/8 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
10133-1003 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-339-1570
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | O-ANNEALED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 1.000 INCHES NOMINAL |
OVERALL WIDTH | 1.000 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.125 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.125 INCHES NOMINAL |
WEIGHT PER UNIT MEASURE | 0.281 POUNDS PER LINEAR FOOT |
NONDEFINITIVE SPEC/STD DATA | O TEMPER |
END ITEM IDENTIFICATION | F-15 AIRCRAFT |