BASE FLANGE THICKNESS | 0.040 INCHES NOMINAL |
BASIC SHAPE STYLE | CHANNEL |
FABRICATION METHOD | EXTRUDED |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.063 INCHES NOMINAL |
FILLET RADIUS WHERE RIGHT FLANGE JOINS BASE FLANGE | 0.063 INCHES NOMINAL |
FIRST TIP STYLE | SQUARE END |
HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
LEFT SIDE FLANGE HEIGHT | 0.750 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.040 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
OVERALL WIDTH | 1.000 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 FLANGE HEIGHT | 0.750 INCHES NOMINAL |
RIGHT SIDE FLANGE THICKNESS | 0.040 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
USAGE DESIGN | AIRCRAFT |
WEIGHT PER UNIT MEASURE | 0.118 POUNDS PER LINEAR FOOT |