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National Stock Number:
9540-01-453-1853
Federal Supply Class:
9540
National Item Identification Number:
014531853
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:
| CVC10002-102GA | 80378 | TRIUMPH AEROSTRUCTURES, LLC | | 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:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.190 INCHES NOMINAL | | BASE FLANGE WIDTH | 5.404 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.375 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | ANNEALED | | LEFT INSIDE ANGLE | 95.0 DEGREES NOMINAL | | LEFT SIDE FLANGE HEIGHT | 1.940 INCHES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.270 INCHES NOMINAL | | OVERALL HEIGHT | 2.200 INCHES NOMINAL | | OVERALL WIDTH | 5.550 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-81556, COMP AB-1 MIL SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | TITANIUM ALLOY | | NONDEFINITIVE SPEC/STD DATA | 6AL-4V COMPOSITION AND ANNEALED CONDITION | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
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