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)