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Cessna 350 Corvalis — Normal Procedures

1 normal procedures reference for the Cessna 350 Corvalis.

Overview
FAA APPROVED AIRPLANE FLIGHT MANUAL Cessna 350 (LC42-550FG) with Garmin Integrated Flight Display · 2005

This document is the FAA Approved Airplane Flight Manual for the Cessna 350 (LC42-550FG), which includes essential information required by federal regulations and additional details provided by the manufacturer. It serves as a comprehensive guide for pilots operating this aircraft model, detailing normal procedures, limitations, performance specifications, weight and balance information, and emergency procedures. The manual is designed to ensure safe and efficient operation of the aircraft, incorporating revisions and updates to maintain compliance with aviation standards. The latest revision was issued on March 20, 2008, reflecting the most current operational guidelines and safety protocols.

  • The Cessna 350 (LC42-550FG) has a maximum takeoff weight of 3,600 lbs.
  • Normal cruise speed is approximately 160 knots.
  • The aircraft has a service ceiling of 25,000 feet.
  • Fuel capacity is 100 gallons, with 95 gallons usable.
  • The stall speed in landing configuration is 61 knots.
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