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29.92 in. Hg (1013.25 mbar) at sea level) except where noted. The performance data do not take into account the expertise of the pilot or the maintenance condition of the airplane. The performance described can be achieved if the indicated procedures are followed and the airplane is maintained in good condition. 5.2. USE OF PERFORMANCE TABLES AND DIAGRAMS The performance data is shown in the form of tables and diagrams to illustrate the influence of different variables. The tables contain sufficiently detailed information to plan flights with precision and safety. Where the performance differs due to the type of propeller that is installed, the table or graph is printed for each propeller and clearly identified. 5.3. PERFORMANCE TABLE AND DIAGRAMS 5.3.1. Airspeed System Calibration
5.3.2. Cruising Performance Example: OAT: 70o F Pressure Altitude: 5000 ft Desired Power setting: 60% Configuration: Idle, most forward center of gravity, max. weight (this is the most adverse configuration) NOTE: Stall speeds in kts 5.3.4. Wind Components 中国通航网 www.ga.cn 通航翻译 www.aviation.cn 本文链接地址:钻石20系列飞机维护手册 DA 20 SERIES AIRPLANE MAINTENANCE MANUAL(37) |