CESSNA CARAVAN 208 FLOATPLANE — Specifications
1 specifications reference for the CESSNA CARAVAN 208 FLOATPLANE.
Overview
Certification Specifications and Acceptable Means of Compliance for Normal, Utility, Aerobatic, and Commuter Category Aeroplanes CS-23 Amendment 4 · 2015
This document outlines the certification specifications and acceptable means of compliance for normal, utility, aerobatic, and commuter category aeroplanes, specifically focusing on the Cessna Caravan 208. It provides detailed regulations and guidelines that must be adhered to for airworthiness, flight performance, and operational limitations. The document is intended for aviation professionals, including aircraft manufacturers, operators, and regulatory authorities, ensuring that the aircraft meets safety and performance standards. The specifications cover various aspects such as weight limits, flight testing, and performance metrics necessary for certification.
- Maximum takeoff weight for Cessna Caravan 208 is 5,670 kg (12,500 lb).
- VSO must not exceed 113 km/h (61 knots) for single-engine aeroplanes at maximum weight.
- Take-off distance must be determined for each weight, altitude, and temperature.
- Climb performance must be shown out of ground effect and at speeds meeting cooling requirements.
- The document outlines compliance requirements for airworthiness and operational limitations.
1 document


