NSN 9540-01-334-2882

Part Details | STRUCTURAL ANGLE

9540-01-334-2882 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: AND101332001, AND10133-2001, AND101332001QQA2008T6511, AND10133-2001/QQ-A-200/8-T6511, QQA2008, QQ-A-200/8, K10B82T6511, AMSQQA2008, AMS-QQ-A-200/8, 9540-01-334-2882, 01-334-2882, 9540013342882, 013342882

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95FEB 19, 199101-334-288237017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-01-334-2882
Part Number Cage Code Manufacturer
AND10133-200199237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
AND10133-2001/QQ-A-200/8-T651114153DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER
QQ-A-200/881348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
K10B82T651181755LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS
AMS-QQ-A-200/881343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 9540-01-334-2882
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-6511 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT2.000 INCHES NOMINAL
OVERALL WIDTH2.000 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.094 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.250 INCHES NOMINAL
BASE FLANGE THICKNESS0.094 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.094 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.094 INCHES NOMINAL
NONDEFINITIVE SPEC/STD DATAT6511 TEMPER
END ITEM IDENTIFICATIONF-16 AIRCRAFT