DA20 C1

Gyronimo Performance Pad -Diamond DA20 C1-
The ultimate computer for Mass & Balance and Performance.

- Weight & Balance (with Aux Fuel Tank option)
- Takeoff distance
- Climb distance (for cruise and takeoff climb power)
- Cruise Range (based on Max Flight Duration Charts in POH)
- Landing Distance
- Stall Speed


Engine: Continental IO240, 125hp at 2800RPM and two-bladed fixed pitch propeller: W69EK7-63, 3G or K-63.
Max Ramp Wgt = 1770lbs, MTOW = 1764lbs
Based on Flight Manual Revision 28, Feb 2014.

Calculate and interpolate performance data using the actual values
from the Diamond DA20 C1 Pilot's Operating Handbook (POH).

**** now includes professional Load Manifest wit digital signature ****

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 Retina screens.


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,
and climb rate.

The Performance Pad has multiple pages:

1. The Mass & Balance (or Weight & Balance) Page
Calculates Center of Gravity, Moments, Takeoff and Zero Fuel Mass as well as Percent MAC (% MAC).

Set person and baggage weights in seconds using the convenient sliders.
Check if the CG is within limits using three graphical displays
- CG envelope
- Aircraft axis
or see a complete load manifest that you can send to your email address
to quickly prove that you have completed the Weight & Balance for you flight.

- Send a Mass & Balance Summary to your email address.


2. The Takeoff Page
- 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
- Engine RPM
- Temperature
- Wind and Altimeter Setting

and calculate Break Horse Power (% BHP), Fuel Flow and True Airspeed

The Max Range and Range including Reserve will be displayed graphically.

The Fuel Management allows to enter Reserve Time for Contingency, Alternate and Final Reserve.
The Fuel Usage is displayed graphically.

Fuel Efficiency is computed in Miles per Gallon and Liter per 100km to set set results in a perspective.

5. Landing Page
Calculates Ground Roll and Landing Distance based on various factore.
As on the Takeoff Page you can use the Wind Components Computer to quickly determine head- or tailwind components

6. Load / Save.
- Load and Save up to five Aircraft Settings and Scenarios.




DISCLAIMER:

Gyronimo LLC is not affiliated with Diamond Aircraft Industries.
This app is not sponsored or endorsed by Diamond Aircraft Industries.


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.

更新履歴
updated landing data table