Comparison of Cessna 414 Chancellor and Piper PA-31 Navajo

Attribute	Cessna 414 Chancellor ×	Piper PA-31 Navajo ×
General
Manufacturer	Cessna	Piper Aircraft
Model	Cessna 414 Chancellor	Piper PA-31 Navajo
Country	United States	United States
Manufactured from (year)	1968	1967
Manufactured to (year)	1985	1984
Type	Twin Turboprops	Twin Turboprops
Icao	C414	PA31
Performance
Engine	2x Continental TSIO-520-NB	2x Lycoming TIO-540-A
Power, hp (hp)	310	310
Avionics	-	Garmin GNS 530W, Garmin 696 with XM weather, S-tek 55X autopilot w/GPSS
Max cruise speed (km/h)	435	420
Approach speed (km/h)	126	117
Travel range (km)	2,459	1,874
Service ceiling (m)	9,388	8,016
Rate of climb (m/sec)	7.72	7.32
Take off distance (m)	665	400
Landing distance (m)	718	575
Weights
Max take off weight (kg)	3,061	2,948
Max landing weight (kg)	2,697	2,948
Max payload (kg)	802	1,100
Fuel tank capacity (l)	806	719
Baggage volume (m³)	2.4	1.7
Dimensions
Seats	1	7
Cabin height (m)	1.3	1.3
Cabin width (m)	1.4	1.27
Cabin length (m)	3.5	3.27
Exterior length (m)	11.1	9.9
Tail height (m)	3.5	3.96
Fuselage diameter (m)	1.5	1.35
Wing span (m)	13.46	12.4
Wing tips	No Winglets	No Winglets