BASIC SHAPE STYLE | Z SHAPE |
BOTTOM FLANGE WIDTH | 1.003 INCHES NOMINAL |
FABRICATION METHOD | EXTRUDED |
FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.032 INCHES NOMINAL |
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.032 INCHES NOMINAL |
FIRST TIP STYLE | SQUARE END |
HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
OVERALL HEIGHT | 0.229 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 BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.063 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
USAGE DESIGN | AIRCRAFT |
WEIGHT PER UNIT MEASURE | 0.145 POUNDS PER LINEAR FOOT |
WEB FLANGE THICKNESS | 0.063 INCHES NOMINAL |
TOP FLANGE WIDTH | 0.810 INCHES NOMINAL |