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GENERAL SPECIFICATIONS
Engine: Textron Lycoming IO-540-AB1A5 230 BHP at 2.400 RPM
Maximum Takeoff Weight: 3.100 lbs (1.406 kg)
Baggage Allowance: 200 lbs (91 kg)
Fuel Total Capacity: 92 gal (348.2 ltrs)
Fuel Total Usable: 87 gal (329.3 ltrs)
Oil Capacity: 9 qts (8.5 ltrs)
Seating: 4
PERFORMANCE
Speed:
Maximum at sea level: 149 kts CAS
Cruise, 80% power at 6,000 ft: 144 kts CAS
Rate of Climb at Sea Level: 924 fpm (282 mpm)
Service Ceiling: 18.100 ft (5.517 m)
Takeoff Performance:
Ground Roll: 795 ft (242 m)
Total distance over 50ft obstacle: 1.514 ft (461 m)
Landing Performance:
Ground roll: 590 ft (180 m)
Total distance over 50ft obstacle: 1.350 ft (411 m)
Range:
80% power at 6,000 ft 87 gallons usable fuel: 825 nm (1.528 km) / 4:45 hrs
55% power at 10,000 ft 87 gallons usable fuel: 968 nm (1.793 km) / 8:05 hrs
AVIonICS
KX 155A Nav/Comm with Glideslope
KI 209 VOR/LOC/GS Indicator
KMA 28 Audio Panel/Marker Beacon/Four-position, Voice-activated Intercom
KT 76C Mode C Transponder
KAP 140 Two-axis Autopilot with Altitude Preselec
Avionics Cooling Fan
Emergency Locator Transmitter
KLN 94 Colour Moving-map GPS-IFR
MD 41-231 GPS-Nav Selector/Annunciator
2nd KX 155A Nav/Comm with Glideslope
KMD 550 Multifunction Display
KI 209A VOR/LOC/GS Indicator with GPS Interface
KCS Bendix-King 55A HSI
WX500 Stormscope Processor
MD 41-233 GPS-Nav (HSI)