9535-00-151-5113 SHIM STOCK,LAMINATED Index 9535-00-151-5116 SHEET,METAL

National Stock Number:
9540-00-151-5114

Federal Supply Class:
9540

National Item Identification Number:
001515114

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:
124408488277THE BOEING COMPANY
1244084-240088277THE BOEING COMPANY
1MA100D06-1001076301THE BOEING COMPANY
AMS-QQ-A-200/110U583SAE INTERNATIONAL
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS10133-06010U583SAE INTERNATIONAL
AMS10133-060181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS41540U583SAE INTERNATIONAL
AND10133-060199237AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD
AND10133-0601/QQ-A-200/11-T651114153DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA
ASTM B22181346AMERICAN SOCIETY FOR TESTING AND MATERIALS
LS10133-060198897LOCKHEED MARTIN CORP
QQ-A-200/1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC
S124408488277THE BOEING COMPANY


Techincal Specification:
BASIC SHAPE STYLEANGLE
BASE FLANGE THICKNESS0.063 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.094 INCHES NOMINAL
FIRST TIP RADIUS0.063 INCHES NOMINAL
FIRST TIP STYLERIGHT QUARTER RADIUS
HEAT TREATMENTT-6511 SOLUTION HEAT TREATED
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.063 INCHES NOMINAL
LENGTH12.000 FEET NOMINAL
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH0.750 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
NONDEFINITIVE SPEC/STD DATA7075 ALLOY AND T6511 TEMPER
SECOND TIP RADIUS0.063 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.110 POUNDS PER LINEAR FOOT


Click here to Register for Free 30-day Trial