Specifications
Aircraft Details
- Engine: PT6A-28 turboprop engines
- Maximum Cruise Speed: 300 knots
- Range: 1,800 nautical miles
- Seating Capacity: 6-8 passengers
- Avionics: Equipped with advanced avionics suite
- Cabin: Spacious cabin with comfortable seating
- Performance: Excellent climb rate and short takeoff distance
- Maintenance: Well-maintained with complete logs available
- Features: Air conditioning, pressurization, and a fully equipped galley
- Safety: Equipped with modern safety features and systems
About this Model
Overview
The Piper Cheyenne II is a pressurized, twin-engine turboprop positioned between entry-level turboprops and larger cabin-class types. It is commonly operated in owner-flown or corporate/utility roles where runway flexibility, turbine reliability, and higher cruise speed than piston twins are priorities. Typical aircraft in the fleet vary significantly by avionics suite, interior refit level, and engine/propeller program status, so the specific configuration matters as much as the base model.
Mission Fit
Mission fit tends to be strongest for 300–800 nm regional legs where turbine climb performance and pressurization reduce exposure to lower-altitude weather, while still retaining access to many community airports. It can also serve well for mixed-use operators who value payload and baggage practicality over cabin size. It is less aligned with missions that prioritize large-cabin comfort, extensive onboard amenities, or minimal pilot workload.
Cabin
The Cheyenne II cabin is pressurized and typically arranged for a small group with club-style seating in many configurations, plus an aft seating area depending on the interior. Cabin ambiance is functional rather than spacious, with comfort highly dependent on refurbishment quality, soundproofing, and environmental system condition. Boarding is typically via an airstair/door arrangement; baggage capacity is generally practical for the category but varies with interior and installed equipment.