CESSNA 350 — Systems Description
1 systems description reference for the CESSNA 350.
Overview
CESSNA 350 Specification and Description · 2008
This document provides specifications and descriptions for the Cessna 350 aircraft, including its design, performance, and equipment. It serves as a comprehensive guide for evaluating the aircraft's capabilities and features, including details about its powerplant and avionics.
- Cessna 350 is a single-engine, low-wing aircraft.
- It seats four passengers and has a tricycle landing gear design.
- The aircraft is certified under U.S. FAA regulations.
- It features a Teledyne Continental IO-550-N engine.
- The document includes warranty information for various components.
- Cessna reserves the right to revise specifications due to improvements or regulations.
- The aircraft has a maximum ramp weight of 3,400 lbs.
- Fuel capacity is 106 gallons.
1 document
CESSNA 350 — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the CESSNA 350?
Sprinkle has 1 Systems Description document on file for the CESSNA 350.
What year is the CESSNA 350 Systems Description?
The CESSNA 350 Systems Description on file is dated 2008.
Where does Sprinkle's CESSNA 350 Systems Description come from?
This CESSNA 350 Systems Description was originally published by aircraftking.com and is hosted on Sprinkle with full text and specs.