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)
95JAN 01, 196300-596-297137017 ( 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
10135-1002-2T488044AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE
AND10135-100299237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
P4532A77783ALCOA/REYNOLDS METALS COMPANY
3130401634ALUMINUM CO OF AMERICA
ASTM B22181346AMERICAN SOCIETY FOR TESTING ANDMATERIALS
11118270898BEECHCRAFT CORPORATIONDBA TEXTRON AVIATION
124252888277BOEING COMPANY, THEDBA BOEING
104729988277BOEING COMPANY, THEDBA BOEING
104729918355BOEING COMPANY, THEDBA BOEING
S104729988277BOEING COMPANY, THEDBA BOEING
BAC1504-100282918BOEING COMPANY, THEDBA BOEING
BAC1504-100243999BOEING COMPANY, THEDBA BOEING
QQA267TEMPERT481348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
QQ-A-200/381348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
E1612010WLU1GENERAL DYNAMICS CORPCONVAIR DIV
E16120114170HUGHES MISSILE SYSTEMS COSAN DIEGO
HA44410383KAISER ALUMINUM AND CHEMICAL CORPTRENTWOOD WORKS-MARKETING DEPT
LS35498897LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS
10135-1002-2T401624MPM POLYMER SYSTEMS INC
5035608588NATIONAL DISTILLERS AND CHEMICALCORP BRIDGEPORT BRASS CO DIV
14906977294PIPER AIRCRAFT INC.
622601484REYNOLDS METALS CO
P4532A01484REYNOLDS METALS CO
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
E1612017B709TRACOR 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
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.063 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.095 INCHES NOMINAL
BASE FLANGE THICKNESS0.063 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.063 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE SQUARE END
SECOND TIP RADIUS0.095 INCHES NOMINAL
SECOND TIP DIAMETER0.190 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.150 POUNDS PER LINEAR FOOT