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National Stock Number: 9540-01-435-5250
Federal Supply Class: 9540
National Item Identification Number: 014355250
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.
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Manufacturer Information:
CVC10001-1019GA | 80378 | TRIUMPH AEROSTRUCTURES, LLC | CVC10001-1019GAX144 | 14153 | DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA | MIL-T-81556 | 81349 | MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M |
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Techincal Specification:
BASE FLANGE THICKNESS | 0.500 INCHES NOMINAL | BASIC SHAPE STYLE | ANGLE | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.380 INCHES NOMINAL | FIRST TIP OUTER RADIUS | 0.062 INCHES NOMINAL | FIRST TIP INNER RADIUS | 0.062 INCHES NOMINAL | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII | HEAT TREATMENT | ANNEALED | LEFT INSIDE ANGLE | 105.0 DEGREES NOMINAL | LEFT SIDE FLANGE THICKNESS | 0.450 INCHES NOMINAL | LENGTH | 12.000 FEET NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-81556, COMP AB-1 MIL SPEC SINGLE MATERIAL RESPONSE | MATERIAL | TITANIUM ALLOY | NONDEFINITIVE SPEC/STD DATA | AB-1 COMPOSITION AND ANNEALED CONDITION | OVERALL HEIGHT | 2.000 INCHES NOMINAL | OVERALL WIDTH | 2.100 INCHES NOMINAL | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
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