9540-00-720-1324 ANGLE,STRUCTURAL Index 9540-00-720-1328 ANGLE,STRUCTURAL

National Stock Number:
9540-00-720-1326

Federal Supply Class:
9540

National Item Identification Number:
007201326

Description:
ANGLE,STRUCTURAL

Detail:
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.


Manufacturer Information:
121033018355THE BOEING COMPANY
121033088277THE BOEING COMPANY
1588927610INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
573801484REYNOLDS METALS CO
AMS 41530U583SAE INTERNATIONAL
AMS 415381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10133-100199237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
FS1010-101089446HILLER AIRCRAFT CORPORATION
HA36210383KAISER ALUMINUM AND CHEMICAL CORP TRENTWOOD WORKS-MARKETING DEPT
QQ-A-200/281348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
S10671379CESSNA AIRCRAFT COMPANY
S1067EK50TEXTRON AVIATION INC
VS252-1514170HUGHES MISSILE SYSTEMS CO SAN DIEGO


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.063 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.188 INCHES NOMINAL
FIRST TIP RADIUS0.063 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-6 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.063 INCHES NOMINAL
LENGTH12.000 FEET NOMINAL
OVERALL HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
MATERIALALUMINUM ALLOY
NONDEFINITIVE SPEC/STD DATAAMS-4153 STANDARD AND 2014 ALLOY AND T6 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.063 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.155 POUNDS PER LINEAR FOOT


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