9540-00-138-6469, ANGLE,STRUCTURAL

National Stock Number:
9540-00-138-6469

Federal Supply Class:
9540

National Item Identification Number:
001386469

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:

AMS-QQ-A-200/8	0U583	SAE INTERNATIONAL
AMS-QQ-A-200/8	81343	SOCIETY OF AUTOMOTIVE ENGINEERS INC
AND10134-1204	99237	AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
AND10134-1204	K8768	DEFENCE AVIATION REPAIR AGENCY
AND10134-1204/QQ-A-200/8-T6	14153	DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA
ASTM B221	81346	AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/8	81348	FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
SAE-AMS-QQ-A-200/8	0U583	SAE INTERNATIONAL

Techincal Specification:

BASE FLANGE THICKNESS	0.063 INCHES NOMINAL
BASIC SHAPE STYLE	ANGLE
FABRICATION METHOD	EXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE	0.125 INCHES NOMINAL
FIRST TIP RADIUS	0.063 INCHES NOMINAL
FIRST TIP STYLE	RIGHT QUARTER RADIUS
HEAT TREATMENT	T-6 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE	90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS	0.063 INCHES NOMINAL
LENGTH	10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT	1.000 INCHES NOMINAL
OVERALL WIDTH	1.250 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATION	AMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE
MATERIAL	ALUMINUM ALLOY 6061
NONDEFINITIVE SPEC/STD DATA	6061 ALLOY AND T6 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIP	NOT IDENTICAL
SECOND TIP RADIUS	0.063 INCHES NOMINAL
SECOND TIP STYLE	UPPER RADIUS
WEIGHT PER UNIT MEASURE	0.170 POUNDS PER LINEAR FOOT

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