Cessna 414 Chancellor
Explore the Cessna 414 Chancellor in side view and top view to compare its silhouette and proportions.
11.09 m36.4 ft
13.45 m44.1 ft
From Wikipedia
The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor.
Summary of “Cessna 414” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
Download
Free to use, with credit
Use these drawings for anything, commercial too, under Creative Commons Attribution 4.0 International. Credit us like this:
Drawing of the Cessna 414 Chancellor by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/C414/), CC BY 4.0Specifications
- Length
- 11.09 m36.4 ft
- Wingspan
- 13.45 m44.1 ft
- Max take-off weight
- 3.06 t6,700 lb
- Typical seats
- 8
- Cruise speed
- 339 km/h211 mph
- Max speed
- 435 km/h270 mph
- Range
- 2,458 km1,527 mi
- Ceiling
- 9,388 m30,800 ft
- Engines
- 2× Continental TSIO-520-NB (piston)
- Power
- 2× 310 hp
- First flight
- 1968
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.
