CESSNA 414A — Specifications
2 specifications references for the CESSNA 414A.
This document provides specifications for the 1981 Cessna 414A RAM VII, detailing its airframe, engines, avionics, and additional features. It serves as a reference for potential buyers or aviation enthusiasts interested in the aircraft's capabilities and maintenance history. The document outlines critical information such as total time on airframe and engines, maintenance schedules, and equipment installed, making it a valuable resource for understanding the aircraft's performance and operational limits.
- Total airframe time: 4921 hours
- Engine SMOH: 1111 hours each
- Max takeoff weight: 7087 lbs
- Useful load: 2062 lbs
- Fuel capacity: 206 gallons
- Max range: 1328 nautical miles
- Annual maintenance due: April 2019
How many Specifications documents does Sprinkle have for the CESSNA 414A?
Sprinkle has 2 Specifications documents on file for the CESSNA 414A.
What year is the CESSNA 414A Specifications?
The CESSNA 414A Specifications on file is dated 1981.
How many pages is the CESSNA 414A Specifications?
The CESSNA 414A Specifications runs 4 pages.
Where does Sprinkle's CESSNA 414A Specifications come from?
This CESSNA 414A Specifications was originally published by macairgroup.com and is hosted on Sprinkle with full text and specs.