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Specifications
Airframe
- Total time
- 3,727 hr
- MSN
- 17700512
Performance (across variants)
- Range
- 600 nm
- Cruise
- 144 kt
- Service ceiling
- 17,000 ft
- MTOW
- 1,200 kg
- Passengers
- Up to 4
Description
This Cardinal is well-equipped and ready to travel. It features a low-time engine with 175 hours, a high useful load of 1046 pounds, and a Hartzell composite lightweight scimitar propeller. The panel includes a Garmin GTN-650 driving an Aspen Evolution with AOA. An STEC 30 autopilot with altitude hold assists with flying, while the JPI 900 monitors the engine. Safety features include voice stall/gear warning and a Monroy anti-collision system. Other extras include Gami injectors, SkyTec starter, LED lighting, photo windows, and CiES fuel senders.
Comparable sales
Type certification
The FAA paperwork
TCDS A20CE · Rev 19 · issued 2003-03-31
- Category
- Normal
- MTOW
- 1,270 kg
- Seats
- 1 crew · 3 passengers
- Fuel
- 227 L
Approved fuel100/130100LL100
Engine
Lycoming IO-360-A1B6 or IO-360-A1B6D, 200 hp, 2700 rpm
Certification basis
Part 23 of the Federal Aviation Regulations effective February 1, 1965, as amended by 23-1 through 23-6.