NSN 9540-00-596-2971
Part Details | STRUCTURAL ANGLE
9540-00-596-2971 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: 1013510022T4, 10135-1002-2T4, AND101351002, AND10135-1002, P4532A, 31304, ASTM B221, 111182, 1242528, 1047299, 1047299, S1047299, BAC15041002, BAC1504-1002, BAC15041002, BAC1504-1002, QQA267TEMPERT4, QQA2003, QQ-A-200/3, E161201, E161201, HA444, LS354, 1013510022T4, 10135-1002-2T4, 50356, 149069, 6226, P4532A, AMSQQA2003, AMS-QQ-A-200/3, E161201, 9540-00-596-2971, 00-596-2971, 9540005962971, 005962971
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JAN 01, 1963 | 00-596-2971 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
RIGHT QUARTER RADIUS
SQUARE END
RIGHT QUARTER RADIUS
Cross Reference | NSN 9540-00-596-2971
Part Number | Cage Code | Manufacturer |
---|---|---|
10135-1002-2T4 | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
AND10135-1002 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
P4532A | 77783 | ALCOA/REYNOLDS METALS COMPANY |
31304 | 01634 | ALUMINUM CO OF AMERICA |
ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
111182 | 70898 | BEECHCRAFT CORPORATIONDBA TEXTRON AVIATION |
1242528 | 88277 | BOEING COMPANY, THEDBA BOEING |
1047299 | 88277 | BOEING COMPANY, THEDBA BOEING |
1047299 | 18355 | BOEING COMPANY, THEDBA BOEING |
S1047299 | 88277 | BOEING COMPANY, THEDBA BOEING |
BAC1504-1002 | 82918 | BOEING COMPANY, THEDBA BOEING |
BAC1504-1002 | 43999 | BOEING COMPANY, THEDBA BOEING |
QQA267TEMPERT4 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
E161201 | 0WLU1 | GENERAL DYNAMICS CORPCONVAIR DIV |
E161201 | 14170 | HUGHES MISSILE SYSTEMS COSAN DIEGO |
HA444 | 10383 | KAISER ALUMINUM AND CHEMICAL CORPTRENTWOOD WORKS-MARKETING DEPT |
LS354 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
10135-1002-2T4 | 01624 | MPM POLYMER SYSTEMS INC |
50356 | 08588 | NATIONAL DISTILLERS AND CHEMICALCORP BRIDGEPORT BRASS CO DIV |
149069 | 77294 | PIPER AIRCRAFT INC. |
6226 | 01484 | REYNOLDS METALS CO |
P4532A | 01484 | REYNOLDS METALS CO |
AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
E161201 | 7B709 | TRACOR FLIGHT SYSTEMS INCSUB OF TRACOR INC |
Technical Data | NSN 9540-00-596-2971
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 0.750 INCHES NOMINAL |
OVERALL WIDTH | 1.000 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.095 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 | SQUARE END |
SECOND TIP RADIUS | 0.095 INCHES NOMINAL |
SECOND TIP DIAMETER | 0.190 INCHES NOMINAL |
WEIGHT PER UNIT MEASURE | 0.150 POUNDS PER LINEAR FOOT |