NSN 9540-01-412-1747
Part Details | STRUCTURAL ANGLE
9540-01-412-1747 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: MILT9046, MIL-T-9046, AMST9046, AMS-T-9046, CVC10001365GA, CVC10001-365GA, 9540-01-412-1747, 01-412-1747, 9540014121747, 014121747
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | APR 12, 1995 | 01-412-1747 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE

SQUARE END

SQUARE END

Cross Reference | NSN 9540-01-412-1747
Part Number | Cage Code | Manufacturer |
---|---|---|
MIL-T-9046 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
AMS-T-9046 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
CVC10001-365GA | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-01-412-1747
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | ANNEALED |
LENGTH | 12.000 FEET NOMINAL |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 1.170 INCHES NOMINAL |
OVERALL WIDTH | 1.600 INCHES NOMINAL |
LEFT SIDE FLANGE HEIGHT | 1.020 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.120 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.120 INCHES NOMINAL |
BASE FLANGE WIDTH | 1.450 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | SQUARE END |
SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |