CESSNA 550 Citation II — Performance Data

This installation manual provides detailed instructions for the Shadin Fuel/Air Data Computer (ADC 200), specifically designed for various aircraft models, including the Cessna 550 Citation II. It outlines the system configuration, specifications, installation procedures, and operational instructions necessary for integrating the ADC 200 into the aircraft's avionics. The manual is intended for avionics technicians and pilots who are responsible for the installation and maintenance of the ADC 200 system. Key information includes electrical specifications, data output parameters, and limitations of the system, ensuring that users can effectively utilize the ADC 200 for accurate fuel and air data management.

• Input data range: Pitot 18 to 350 knots, Static -1000 to 55,000 feet, OAT -60°C to +60°C.
• Output data range: IAS 20 to 350 knots, TAS 20 to 600 knots, Fuel Flow 1 to 450 GPH.
• Installation must comply with TSO standards and 14 CFR part 43 regulations.
• Warm-up time varies with ambient temperature: 5 minutes at 70°C, up to 20 minutes at -40°C.
• The ADC 200 is not intended to replace primary flight instruments.