1560-00-146-7245 PANEL,FAIRING,WING TO FUSELAGE Index 1560-00-146-7254 PANEL,FAIRING,WING TO FUSELAGE

National Stock Number:
9540-00-146-7249

Federal Supply Class:
9540

National Item Identification Number:
001467249

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:
1E8443999THE BOEING COMPANY
2238101634ALUMINUM CO OF AMERICA
718801484REYNOLDS METALS CO
AMS-QQA200-110U583SAE INTERNATIONAL
AMS-QQA200-1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
QQA200-1181348FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC


Techincal Specification:
BASE FLANGE THICKNESS0.125 INCHES NOMINAL
BASIC SHAPE STYLEANGLE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.125 INCHES NOMINAL
FIRST TIP RADIUS0.047 INCHES NOMINAL
FIRST TIP STYLESQUARE END
HEAT TREATMENTT-6 SOLUTION HEAT TREATED AND ARTIFICALLY AGED
LEFT INSIDE ANGLE87.0 DEGREES NOMINAL
LEFT SIDE FLANGE THICKNESS0.125 INCHES NOMINAL
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
OVERALL HEIGHT1.313 INCHES NOMINAL
OVERALL WIDTH1.500 INCHES NOMINAL
MATERIALALUMINUM ALLOY
NONDEFINITIVE SPEC/STD DATAT6 TEMPER
SECOND TIP RELATIONSHIP TO FIRST TIPNOT IDENTICAL
SECOND TIP RADIUS0.047 INCHES NOMINAL
SECOND TIP STYLEUPPER RADIUS
WEIGHT PER UNIT MEASURE0.430 POUNDS PER LINEAR FOOT


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