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M-9-235 Specifications

Enhanced Gross Weight Taildragger
Engine: Lycoming (2000hr. TBO) I0-540-W1A5, 235 HP Fuel Injected
Gross Weight: 2800 lbs. (1270 kg)
Empty Weight: 1700 lbs. (771 kg)
Useful Load: 1100 lbs. (499 kg)
Stall Speed (full flaps / power off / light weight) (IAS): 46 mph (40 kts)
Take Off, Ground Roll (@ 2800 lbs.): 406 ft (124 m)
Take Off (@ 2800 lbs.) over 50' obstacle: 791 ft (242 m)
Landing (@ 2800 lbs.) over 50' obstacle: 900 ft (274 m)
Service Ceiling: 20,000 ft (6096 m)
Fuel Consumption US Gals. @ 65% Power (avg.): 11 gph (42 lph)
Cruise (75% Power / Opt. Alt.) (TAS): 158 mph (137 kts)
Starting at $307,900
Performance Observations are from Certification Flight Test - Sea Level, Standard Day Conditions.
(Do Not Use for Flight Planning)

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