Cirrus SR22T 2.4

Gyronimo Performance Pad -Cirrus SR22T-

An advanced analytical tool designed for performance and weight & balance computations specific to the Cirrus SR22T, particularly models with Teledyne Continental Motors Turbocharged Engines and a takeoff weight of 3600 pounds.

*** Now includes a professional load manifest ***

• Sign the manifest digitally on the iPad and export via email for streamlined documentation.
• Utilize actual values from the Pilot's Operating Handbook (POH) to accurately calculate and interpolate performance data.
• Achieve comprehensive flight planning rapidly, minimizing preparation time while ensuring accuracy.
• Results are updated in real-time with high-resolution graphics optimized for iPad 2/3 and iPad Mini displays.
• Adjust key parameters through intuitive sliders, enabling quick experimentation with various scenarios and "what if" analyses.
• Identify optimal cruise altitudes, ground roll for takeoff, landing distances, climb performance metrics, and stall speeds efficiently.

The Performance Pad conveniently organizes its functionalities across seven primary pages:

1. Mass & Balance (Weight & Balance) Page
Calculates center of gravity, moments, takeoff weight, and zero fuel weight based on user input. Quickly set passenger and baggage weights using sliders; verify CG limits through graphical representations including Moment Envelope, CG Envelope, and aircraft axis diagrams.
2. Takeoff Page
Employs POH data to compute ground roll and landing distances considering variables such as aircraft weight, pressure altitude, density altitude, outside air temperature (OAT), altimeter settings, runway surface conditions, slope, and wind conditions. Includes a Wind Components Calculator allowing pilots to determine headwind or tailwind components by adjusting wind direction and speed; results seamlessly integrate into performance calculations.
3. Climb Page
Calculates climb time, required fuel consumption, and distance based on altitude differences, pressure settings, OAT, and wind components. Presents climb rate and speed metrics for comprehensive assessment.
4. Cruise Page
Determines optimal cruise altitude utilizing trip distance, flight level preferences, MAP/RPM settings, temperature, wind conditions, and pressure altitude data derived from the POH.
5. Landing Page
Estimates ground roll and landing distance considering wind factors and environmental conditions. Features a Wind Components Calculator similar to the takeoff page for efficient wind component assessment during landing planning.
6. Stall Speed Page
Calculates stall speeds at various bank angles and flap configurations, providing values in both KIAS and KCAS based on POH data.
7. Setup
Saves up to five aircraft configurations or scenarios for quick recall. Sends mass & balance summaries via email directly from the app. Accesses instructional video tutorials and manuals through linked resources.

The software features mode toggles for enhanced usability:

• "Individual Mode": Performs independent calculations without inter-page data transfer.
• "Plan Mode": Transfers calculated data between pages and offers a comprehensive "Flight Summary" overview for integrated planning.

The developer disclaims liability for any damages or losses resulting from the use of this application. The information provided is intended solely for general reference purposes and should be verified against official sources before flight use.