速報APP / 教育 / PA 235C

PA 235C

價格:免費

更新日期:2017-02-13

檔案大小:34.5 MB

目前版本:1.4

版本需求:需要 iOS 9.1 或以上版本。與 iPad 相容。

支援語言:英語

PA 235C(圖1)-速報App

Gyronimo, Piper 235C, Performance Pad, PA-235C

(aka Cherokee Pathfinder)

Piper PA 28-235 C: Serial Numbers 28-11040 through 28-11255

with Lycoming O-540-B engine and CONSTANT SPEED PROPELLER

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 2, iPad Retina and iPad Mini.

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 Arrow IV has seven main pages:

1. The Mass & Balance (or Weight & Balance) Page

PA 235C(圖2)-速報App

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

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)

PA 235C(圖3)-速報App

- 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

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.

PA 235C(圖4)-速報App

Stall Speed will be computed as KIAS and KCAS using the actual values from the POH.

7. Setup

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.

PA 235C(圖5)-速報App

支援平台:iPad