Cessna 310 R - Walther Joachim
CESSNA 310Q · Systems Description
Overview
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.
Document
Source
Originally published by www.joachimwalther.de. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Systems Description
- Pages
- 10
- File size
- 160 KB
- Publisher
- www.joachimwalther.de
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In this document
Electrical System
The Cessna 310 is equipped with a 28-volt electrical system powered by two 12-volt batteries. The system includes a 70-amp alternator that provides power to the aircraft's electrical loads. Circuit breakers are used to protect the system from overloads, and the electrical panel displays the status of the batteries and alternator.
Fuel System
The fuel system consists of two wing-mounted fuel tanks with a total capacity of 110 gallons. The system includes fuel pumps, filters, and selectors that ensure a reliable supply of fuel to the engines. The fuel flow is monitored through gauges in the cockpit, allowing pilots to manage fuel consumption effectively.
Hydraulic System
The hydraulic system operates the landing gear, flaps, and brakes. It utilizes a hydraulic pump driven by the engine, providing the necessary pressure for operation. The system includes hydraulic fluid reservoirs and lines that connect to various components, ensuring smooth and reliable functionality.
Engine Specifications
The Cessna 310 is powered by two Continental IO-520-U engines, each producing 285 horsepower. The engines are equipped with fuel injection systems that enhance performance and efficiency. The document provides detailed specifications on engine operation, maintenance, and troubleshooting.
Maintenance Procedures
Regular maintenance is crucial for the safe operation of the Cessna 310. The document outlines recommended maintenance schedules, including inspections, fluid changes, and component checks. It emphasizes the importance of adhering to these procedures to ensure the aircraft remains in optimal condition.
Safety notes
- Ensure all electrical systems are functioning correctly before flight.
- Regularly check hydraulic fluid levels to prevent system failures during operation.
- Monitor fuel levels and quality to avoid engine performance issues.
Full document text
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What's in the CESSNA 310Q TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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