|
|
|
National Stock Number:
9540-01-438-7991
Federal Supply Class:
9540
National Item Identification Number:
014387991
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.
|
Manufacturer Information:
| CVC10001-335GA | 80378 | TRIUMPH AEROSTRUCTURES, LLC | | MIL-T-81556 | 81349 | MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M |
|
Techincal Specification:
| BASE FLANGE THICKNESS | 0.080 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.090 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | ANNEALED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.080 INCHES NOMINAL | | LENGTH | 12.000 FEET NOMINAL | | OVERALL HEIGHT | 0.810 INCHES NOMINAL | | OVERALL WIDTH | 2.280 INCHES 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 | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
|