Part Details | STRUCTURAL ANGLE
9540-00-145-7542 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: AND101342002, AND10134-2002, 1244707, 1244707, QQA20011, QQ-A-200/11, 21355, 2-1355, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-145-7542, 00-145-7542, 9540001457542, 001457542
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JAN 01, 1963 | 00-145-7542 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-145-7542
Part Number | Cage Code | Manufacturer |
---|---|---|
AND10134-2002 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
1244707 | 88277 | BOEING COMPANY, THEDBA BOEING |
1244707 | 18355 | BOEING COMPANY, THEDBA BOEING |
QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
2-1355 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-145-7542
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 1.000 INCHES NOMINAL |
OVERALL WIDTH | 2.000 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.156 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.156 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.156 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.156 INCHES NOMINAL |
WEIGHT PER UNIT MEASURE | 0.530 POUNDS PER LINEAR FOOT |
NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6 TEMPER |