5365-00-852-6179 BUSHING,TRIGGER Index 9540-00-852-6184 ANGLE,STRUCTURAL

National Stock Number:
9540-00-852-6183

Federal Supply Class:
9540

National Item Identification Number:
008526183

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:
110968518355THE BOEING COMPANY
110968588277THE BOEING COMPANY
1368901634ALUMINUM CO OF AMERICA
1481327610INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
60-74929321TRANSTAR METALS CORP
1481376301THE BOEING COMPANY
PA410106012TRANSTAR METALS CORP
M104514170HUGHES MISSILE SYSTEMS CO SAN DIEGO
S110968518355THE BOEING COMPANY
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
QQ-A-26781348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
S110968588277THE BOEING COMPANY


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.070 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.063 INCHES NOMINAL
FIRST TIP RADIUS0.063 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-3511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.070 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH1.125 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T3511 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.063 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.160 POUNDS PER LINEAR FOOT


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