6625-00-727-8532 POWER SUPPLY Index 5310-00-727-8550 NUT,SELF-LOCKING,HEXAGON

National Stock Number:
9540-00-727-8537

Federal Supply Class:
9540

National Item Identification Number:
007278537

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:
1575127610INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
2238501634ALUMINUM CO OF AMERICA
409101484REYNOLDS METALS CO
2288501634ALUMINUM CO OF AMERICA
60-13829321TRANSTAR METALS CORP
409177783ALCOA/REYNOLDS METALS COMPANY
E1211080WLU1GENERAL DYNAMICS CORP CONVAIR DIV LINDBERGH FIELD FACILITY
E12110814170HUGHES MISSILE SYSTEMS CO SAN DIEGO
BAC1503-151181205THE BOEING COMPANY
AMS-QQ-A-200/281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/2 ALL0Y 2014 TMPR T81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/2 ALLOY 2014 TMPR T81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-STD-18481343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
PA406406012TRANSTAR METALS CORP
PA406506012TRANSTAR METALS CORP
S10771379CESSNA AIRCRAFT COMPANY
S17971379CESSNA AIRCRAFT COMPANY
E1211087B709TRACOR FLIGHT SYSTEMS INC SUB OF TRACOR INC
QQA200-281348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
FS10101-1008-189446HILLER AIRCRAFT CORPORATION


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.062 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.062 INCHES NOMINAL
FIRST TIP RADIUS0.031 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-4 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.062 INCHES NOMINAL
LENGTH12.000 FEET NOMINAL
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH1.000 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/2 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2014
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T4 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.031 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.130 POUNDS PER LINEAR FOOT


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