NSN 9540-01-235-6000
Part Details | STRUCTURAL ANGLE
9540-01-235-6000 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: 1MA100D0110040, 1MA100D01-10040, QQA20011, QQ-A-200/11, NAS34211, NAS342-11, AMSQQA20011, AMS-QQ-A-200/11, 602403, 60-2403, 9540-01-235-6000, 01-235-6000, 9540012356000, 012356000
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JUL 03, 1986 | 01-235-6000 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-235-6000
Part Number | Cage Code | Manufacturer |
---|---|---|
1MA100D01-10040 | 76301 | BOEING COMPANY, THEDBA BOEING |
QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
NAS342-11 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
60-2403 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-235-6000
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | O-ANNEALED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 0.875 INCHES NOMINAL |
OVERALL WIDTH | 1.125 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.125 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.125 INCHES NOMINAL |
WEIGHT PER UNIT MEASURE | 0.652 POUNDS PER LINEAR FOOT |
SPECIFICATION/STANDARD DATA | 76301-1A100 MANUFACTURERS STANDARD |