• Wide Body model  * *                    31 inches I.D.
• Standard Body                               26 inches I.D.
• Wingspan........................................31 ft. 6 in.
• Chord...............................................60"
• Length..............................................20 ft. 0 in.
• Height...............................................6 ft. 0 in.
• Wing area........................................185 sq.ft.
• Standard Engine:..........................Rotax 503 (52HP) air cooled
• Empty weight..................................450 lbs.
• Useful load......................................500 lbs.
• Ultimate load factor.......................+6 -4
• Build time........................................100-200 hours
• Field assembly time......................20 min.
• Airframe  Aluminum tube (6061-T6, 2024-T3)
• Steel, 4130 Chromoly, Stainless Steel pop rivets,
• AN/Mil Spec. hardware.
• Standard Covering: SUPERFLITE, FAA approved fabric.
• * *  no extra charge

PERFORMANCE:

• VNE..............................................100 mph
• Top level speed...........................90mph
• Cruise speed..........................50-80 mph
• Stall speed..............................30-35 mph
• Climb rate.................................1200 fpm solo, 700 ft. dual
• Take off roll..................................96 fpm.solo, 196 ft. dual
• Glide ratio.................................11:1 solo, 9:1 dual
• Service ceiling.........................14,000 solo, 12,500 dual
• Fuel used at cruise.................2.3 gph to 4 gph
• Fuel capacity...........................10 gal. (U.S.)
• All data is based on average weight pilots, 170 lbs, and average sea level condition