New Turbochargers Vortex Generators New ADSB Out Known Ice Certified New Deice Boots All New Tires New Carpeting

Home Airport(s)

KPRX – Cox Field Airport (PRX), Paris, Texas

Serial Number

414-0816

Registration Number

N414JD

Engine Details (e.g. Total Engine Time; Suggested TBO; Hours Remaining)

CONTINENTAL TSIO 520 NB2B ENGINES Left Engine: 42.2 SFRM Right Engine: 37.4 SFRM New Turbochargers Left Propeller: 42.2 SPOH Right Propeller: 42.2 SPOH

Performance Specs

Max Take-Off Weight (P): ~6,750 lbs Engines: 2 × Continental TSIO-520 (310 hp each) Cruise Speed: ~215 kts Range: ~1,200 nm Service Ceiling: ~24,000 ft Take-Off Run: ~1,900 ft Take-Off Run (50 ft): ~3,400 ft Landing Roll: ~1,500 ft

Avionics

GPS​/​NAV COM #1: Northstar M3 GPS King KNS80, KY196 GPS​/​NAV COM #2: Northstar M3 GPS KX-155 Audio Panel: KMA24H MFD: Avidyne Flightmax Transponder #1: Stratus ESG Transponder #2: Garmin GJK-327 ADS-B Compliant: Y Auto Pilot: CESSNA​/​ARG 400B Radar Altimeter: Bonzer Fuel Flow Totalizer: Y Engine Monitor: NISIGHT GEM WX-500 Other: Eventide Argus, Davtron M903 CVOR, P2 Gear Advisory IN-404A RMI

Aircraft Model Overview (Reference only)

The Cessna 414 Chancellor is a refined, pressurized twin-engine aircraft designed to bridge the gap between light twins and larger executive-class piston aircraft. By 1975, the 414 Chancellor had matured into a capable and comfortable traveling platform, widely respected for its balance of performance, operating economics, and cabin comfort. The 414 is powered by twin Continental TSIO-520 engines, each producing approximately 310 horsepower. These turbocharged engines allow the aircraft to maintain strong performance at altitude, making it well suited for cruising in the mid-teens above weather and turbulence. The aircraft’s pressurized cabin reduces pilot fatigue and enhances passenger comfort on longer trips, giving it capabilities approaching those of larger piston twins while maintaining relatively manageable operating costs. Inside, the Cessna 414 Chancellor typically accommodates six to seven occupants in a comfortable cabin configuration. Club seating arrangements, generous baggage space, and large windows contribute to its appeal for business travel and family transportation. The cockpit layout, while traditional in 1975, provided solid IFR capability, and many aircraft have since been upgraded with modern avionics, enhancing their cross-country performance and safety. Within the general aviation market, the 414 has long been regarded as a practical “sweet spot” pressurized twin. It offers meaningful speed and altitude capability without stepping into turboprop acquisition and maintenance costs. Operators value its sturdy construction, predictable handling, and comfortable cabin environment. The 1975 Cessna 414 Chancellor remains a respected aircraft decades after production. Its combination of pressurization, turbocharged performance, and executive-level comfort continues to make it a compelling choice for pilots seeking serious cross-country capability in a piston twin.