Beech Bonanza A36 vs Flight Risk Assessment (FRAT)使用状況と統計

Gyronimo Performance Beechcraft Bonanza 36 / Bonanza A36 The ultimate EFB computer for Mass & Balance and Performance for the Beechcraft Bonanza Model A36, Serials E-1 thru E-926, E-927 thru E-2110 and E-2111 thru E-3629, E-3631 thru E-3635 Performance computations for engine: Teledyne IO-520-B, IO-520-BA or IO-520-BB Max TOW 3600 or 3650lbs, Fuel Capacity 44 or 74 Gallons now includes: **** PROFESSIONAL LOAD MANIFEST ***** Sign the manifest on the iPad and send it via email or print via AirPrint. **** VARIABLE INTERIOR CONFIGURATIONS 2, 4, 6 Seats and variable baggage areas ***** (For Serials E-927 thru E-1370 and E-1371 and after. Calculate and interpolate performance data using the actual values from the Pilot's Operating Handbook (POH). Finish your complete fight planning in just a few seconds. Performance planning has never been easier and quicker. Results are updated immediately and displayed in high resolution graphics, enhanced for the iPad with retina displays. Change all important values using sliders. Experiment with the results and create "what if" scenarios in no time. Find your optimal cruise altitude, takeoff ground roll, landing distance, climb data and stall speeds. The Performance Pad has seven main pages: 1. The Mass & Balance (or Weight & Balance) Page Calculates Center of Gravity, Moments, Takeoff and Zero Fuel Mass. Set person and baggage weights in seconds using the convenient sliders. Check if the CG is within limits using three graphical displays - Moment Envelope - CG envelope - Aircraft axis 2. The Takeoff Page Using the actual data from the Operating Handbook the Performance Pad calculates and displays Ground Roll and Landing Distance based on: - Aircraft Mass - Takeoff Elevation in MSL (Pressure Altitude and Density Altitude will be computed) - Outside Air Temperature (OAT) - Altimeter Setting - Runway Conditions (i.e. paved dry to long grass or snow) - Runway Slope - Wind Conditions Wind Components Computer - Use the Wind Components page to determine your headwind or tailwind component. Rotate the wind dial to set wind direction, set windspeed and the results will be transferred to your takeoff computations automatically! 3. The Climb page Calculates time, fuel and distance based on - Difference between Takeoff Elevation and intended Flight Level - Altimeter Setting - Outside Air Temperature (OAT) - Altimeter Setting - Headwind or Tailwind Component Also the Rate of Climb and Climb Speed will be displayed. 4. The Cruise Page Using the actual data from the Pilot's Operating Handbook you can determine the optimal cruise altitude based on - Trip Distance - Flight Level - MAP / RPM - Temperature - Wind and Altimeter Setting 5. Landing Page Calculates Ground Roll and Landing Distance based on wind, elevation, altimeter setting etc. Like on the Takeoff Page you can use the Wind Components Computer to quickly determine head- or tailwind components 6. Stall Speed Page. Calculates The Stall Speed based on Bank Angle and Flap Settings. Stall Speed will be computed as KIAS and KCAS using the actual values from the POH. 7. Setup - Load and Save up to five Aircraft Settings and Scenarios. - Send a Mass & Balance Summary to your email address. Mode Switch: The Performance Pad can be used in two Modes: "Individual Mode" All calculations can be done independently from each other. "Plan Mode" Calculated values will be forwarded to the next page and an additional "Flight Summary Page" is available. Gyronimo LLC is not affiliated with Beechcraft/Textron Aviation. All Gyronimo Performance Pads for Beechcraft/Textron Aviation aircrafts are not sponsored or endorsed by Beechcraft/Textron Aviation. The author disclaims any liability for any direct, indirect, incidental, or consequential losses or damages in connection with your access to or use of this software. The information contained in this software is for general information purposes only.