NSN 9540-00-145-4524

Part Details | STRUCTURAL ANGLE


9540-00-145-4524 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.

Alternate Parts: AND101341201, AND10134-1201, 1238984, 1238984, S78, QQA2003, QQ-A-200/3, LS1013412011, LS10134-1201-1, 9540-00-145-4524, 00-145-4524, 9540001454524, 001454524

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JAN 01, 196300-145-452437017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS


Cross Reference | NSN 9540-00-145-4524
Part Number Cage Code Manufacturer
AND10134-120199237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
123898488277BOEING COMPANY, THEDBA BOEING
123898418355BOEING COMPANY, THEDBA BOEING
S7871379CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION
QQ-A-200/381348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
LS10134-1201-198897LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS

Technical Data | NSN 9540-00-145-4524
Characteristic Specifications
MATERIAL ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-4 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT0.750 INCHES NOMINAL
OVERALL WIDTH1.250 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.063 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.125 INCHES NOMINAL
BASE FLANGE THICKNESS0.063 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.063 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.063 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.150 POUNDS PER LINEAR FOOT
NONDEFINITIVE SPEC/STD DATAT4 TEMPER