Aircraft

Specifications:

• First flight: 8 August 1982
• Maximum Takeoff Weight: 8,000 lb (3,629 kg)
• Maximum Landing Weight: 7,800 lb (3,538 kg)
• Maximum Operating Altitude: 25,000 ft

Design:

• High-wing monoplane design
• Fixed tricycle undercarriage

Fuel:

• Fuel Capacities: 332 US Gallons

Size:

• Wingspan: 52 ft 1 in
• Wing Area: 279 sq ft
• Length: 37 ft 7 in
• Height: 14 ft 11 in
• Cabin Length: 12 ft 9 in

Passengers:

• Number of Crew: 1-2
• Number of Passengers: 9

Speed:

• Maximum Cruise Speed: 186 ktas

Avionics:

• GDU 1040A Pilot and Copilot Primary Flight Displays (PFD)
• GDU 1040A Multifunction Display (MFD)
• GDC 74A Dual Air Data Computer (ADC)
• GEA 71 Engine/​Airframe Unit
• GRS 77 Dual Attitude and Heading Reference System (AHRS)
• GMA 1347 Single Audio System with Integrated Marker Beacon Receiver
• GTX 33 Mode S Transponder
• Garmin Relative Terrain/​Obstacles
• Garmin FliteCharts-capable
• Garmin SafeTaxi-capable
• KN-63 DME
• Artex ME-406 2-Frequency (Non-Nav Interfaced)
• ELT with Remote Switch and Monitor Light (Dorsal-fin Installation)
• Avionics Cooling, (2) Cowl Deck Fans and (3) Display Fans
• PA System with Aft-cabin Speakers