5945-00-119-9003 RELAY,THERMAL Index 9540-00-119-9008 ANGLE,STRUCTURAL

National Stock Number:
9540-00-119-9007

Federal Supply Class:
9540

National Item Identification Number:
001199007

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:
13090718355THE BOEING COMPANY
13090788277THE BOEING COMPANY
1M13676301THE BOEING COMPANY
269677783ALCOA/REYNOLDS METALS COMPANY
60-7829321TRANSTAR METALS CORP
77U01634ALUMINUM CO OF AMERICA
AMS-QQ-A-200/30U583SAE INTERNATIONAL
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
BAC1503739582918THE BOEING COMPANY
LS322798897LOCKHEED MARTIN CORP
PA331006012TRANSTAR METALS CORP
QQ-A-200/381348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
T323003462HOWMET CORPORATION


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.188 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 TREATMENTT-3511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.188 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT1.750 INCHES NOMINAL
OVERALL WIDTH1.750 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 RADIUS0.125 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.746 POUNDS PER LINEAR FOOT


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