Specifications:
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Performance:
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APOLLO SPECIFICATIONS
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Welded steel alloy tube fuselage covered with medium weight fabric & polyurethane paint
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80 hp Rotax 912UL, 100 hp 912ULS (optional)
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Ground Adjustable Prop
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Folding wings (takes one person less than 10 minutes)
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Wingspan 30' (9.2M) (width with wings folded 7.85')
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Length 19' (5.8M) (20.2' with wings folded)
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Height 5.58' (1.7M)
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Inside Cabin Width - 44.1"
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Tricycle Gear (Tailwheel is no cost option)
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Empty Weight (w/o options) 715 lbs
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Gross Weight 1265 lbs
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Fuel Capacity 21 gal
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MEASURED PERFORMANCE (80 HP / 100 HP)
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Vc - 98 KTS / 110 KTS
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Vs - 32 KTS (flaps), 39 KTS (clean)
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Max Climb (MTOW) - 1,000 FPM / 1,200 FPM
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Max Range - 530 NM
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Takeoff Roll (no wind) - 400' / 300'
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Takeoff over 50' obstacle - 750' / 600'
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Landing over 50' obstacle - 680'
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Max Endurance - 7 hours +
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Useful Load - 550 lbs
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Payload (full fuel) - 424 lbs
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Max baggage - 40 lbs
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Design Load +4 - 2g, Load test to +6 - 3g w/o damage
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