5340-01-339-1569 CLAMP,LOOP Index 4020-01-339-1571 ROPE,FIBROUS

National Stock Number:
9540-01-339-1570

Federal Supply Class:
9540

National Item Identification Number:
013391570

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:
10133-100329321TRANSTAR METALS CORP
1MA100C01-1003376301THE BOEING COMPANY
AMS-QQ-A-200/80U583SAE INTERNATIONAL
AMS-QQ-A-200/881343SOCIETY OF AUTOMOTIVE ENGINEERS INC
QQ-A-200/881348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
AND10133-100399237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
SAE-AMS-QQ-A-200/80U583SAE INTERNATIONAL


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.125 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.188 INCHES NOMINAL
FIRST TIP RADIUS0.125 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTO-ANNEALED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT1.000 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 6061
NONDEFINITIVE SPEC/STD DATAO TEMPER
SECOND TIP RADIUS0.125 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.281 POUNDS PER LINEAR FOOT


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