CESSNA 310Q — Systems Description
1 systems description reference for the CESSNA 310Q.
This document serves as a systems description for the Cessna 310, detailing the various systems and components that make up the aircraft. It is intended for pilots, maintenance personnel, and aviation enthusiasts who seek a deeper understanding of the aircraft's operational capabilities and technical specifications. The document covers essential systems such as the electrical, fuel, and hydraulic systems, providing insights into their functions, configurations, and maintenance requirements. It aims to enhance the user's knowledge of the Cessna 310, ensuring safe and efficient operation of the aircraft.
- The Cessna 310 features a 28-volt electrical system with dual 12-volt batteries and a 70-amp alternator.
- Total fuel capacity is 110 gallons, with two wing-mounted tanks and a comprehensive fuel management system.
- The hydraulic system controls landing gear, flaps, and brakes, powered by an engine-driven hydraulic pump.
- Each Continental IO-520-U engine produces 285 horsepower, equipped with fuel injection for improved efficiency.
- Regular maintenance is essential, with specific schedules for inspections and fluid changes outlined in the manual.
How many Systems Description documents does Sprinkle have for the CESSNA 310Q?
Sprinkle has 1 Systems Description document on file for the CESSNA 310Q.
How many pages is the CESSNA 310Q Systems Description?
The CESSNA 310Q Systems Description runs 10 pages.
Where does Sprinkle's CESSNA 310Q Systems Description come from?
This CESSNA 310Q Systems Description was originally published by www.joachimwalther.de and is hosted on Sprinkle with full text and specs.