| BASE FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| BASIC SHAPE STYLE | CHANNEL |
| DISTANCE BETWEEN FLANGES | 1.000 INCHES NOMINAL |
| FABRICATION METHOD | EXTRUDED |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.120 INCHES NOMINAL |
| FILLET RADIUS WHERE RIGHT FLANGE JOINS BASE FLANGE | 0.120 INCHES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| LEFT SIDE BOTTOM FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| LEFT SIDE DISTANCE TO CENTER OF BOTH FLANGES | 2.170 INCHES NOMINAL |
| LEFT SIDE FLANGE HEIGHT | 2.560 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.120 INCHES NOMINAL |
| OUTER RADIUS WHERE RIGHT FLANGE JOINS BASE FLANGE | 0.120 INCHES NOMINAL |
| OVERALL WIDTH | 4.340 INCHES NOMINAL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3511 TEMPER |
| RIGHT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| RIGHT SIDE DISTANCE TO CENTER OF BOTH FLANGES | 2.170 INCHES NOMINAL |
| RIGHT SIDE FLANGE HEIGHT | 2.560 INCHES NOMINAL |
| RIGHT SIDE FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| USAGE DESIGN | AIRCRAFT |
| WEIGHT PER UNIT MEASURE | 2.064 POUNDS PER LINEAR FOOT |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |