NSN 9540-00-151-5114
Part Details | STRUCTURAL ANGLE
9540-00-151-5114 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, ASTM B221, 12440842400, 1244084-2400, 1244084, 1MA100D0610010, 1MA100D06-10010, S1244084, AND101330601QQA20011T6511, AND10133-0601/QQ-A-200/11-T6511, QQA20011, QQ-A-200/11, LS101330601, LS10133-0601, AMS101330601, AMS10133-0601, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-151-5114, 00-151-5114, 9540001515114, 001515114
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | MAR 31, 1971 | 00-151-5114 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-151-5114
Part Number | Cage Code | Manufacturer |
---|---|---|
AND10133-0601 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
1244084-2400 | 88277 | BOEING COMPANY, THEDBA BOEING |
1244084 | 88277 | BOEING COMPANY, THEDBA BOEING |
1MA100D06-10010 | 76301 | BOEING COMPANY, THEDBA BOEING |
S1244084 | 88277 | BOEING COMPANY, THEDBA BOEING |
AND10133-0601/QQ-A-200/11-T6511 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
LS10133-0601 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
AMS10133-0601 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-151-5114
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
LENGTH | 12.000 FEET NOMINAL |
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 | 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 |
WEIGHT PER UNIT MEASURE | 0.110 POUNDS PER LINEAR FOOT |