9540-00-288-1145, ANGLE,STRUCTURAL

National Stock Number:
9540-00-288-1145

Federal Supply Class:
9540

National Item Identification Number:
002881145

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:

1047972	18355	THE BOEING COMPANY
1047972	88277	THE BOEING COMPANY
1245442	18355	THE BOEING COMPANY
12551-1	27610	INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP
1245442	88277	THE BOEING COMPANY
110-503062	89446	HILLER AIRCRAFT CORPORATION
2-1327	38597	LOCKHEED MARTIN CORPORATION
1822	77783	ALCOA/REYNOLDS METALS COMPANY
CDS148	81025	CHASE AIRCRAFT CO INC
AMS-QQ-A-200/3	81343	SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/3-T3511-0.250X2X10	81343	SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B221	81346	AMERICAN SOCIETY FOR TESTING AND MATERIALS
QQ-A-200/3	81348	FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
AND10133-2004	99237	AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD

Techincal Specification:

BASE FLANGE THICKNESS	0.250 INCHES NOMINAL
BASIC SHAPE STYLE	ANGLE
FABRICATION METHOD	EXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE	0.250 INCHES NOMINAL
FIRST TIP RADIUS	0.250 INCHES NOMINAL
FIRST TIP STYLE	RIGHT QUARTER RADIUS
HEAT TREATMENT	T-3511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE	90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS	0.250 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATION	AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL WIDTH	2.000 INCHES NOMINAL
MATERIAL	ALUMINUM ALLOY 2024
NONDEFINITIVE SPEC/STD DATA	2024 ALLOY AND T3511 TEMPER
OVERALL HEIGHT	2.000 INCHES NOMINAL
SECOND TIP RADIUS	0.250 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP	NOT IDENTICAL
SECOND TIP STYLE	UPPER RADIUS
WEIGHT PER UNIT MEASURE	1.110 POUNDS PER LINEAR FOOT

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