Piper PA-30 Twin Comanche — Performance Data
1 performance data reference for the Piper PA-30 Twin Comanche.
This document provides performance data for the Piper PA-30 Twin Comanche, a twin-engine piston aircraft introduced in 1964. It includes essential specifications that are crucial for pilots and aviation enthusiasts, such as horsepower, speed, range, fuel consumption, and various weight parameters. The document serves as a reference for understanding the aircraft's capabilities, including its takeoff and landing distances, climb rates, and operational ceilings. This information is vital for flight planning and operational safety.
- Total horsepower: 320 HP (2 x 160 HP engines)
- Best cruise speed: 169 KIAS
- Maximum range: 770 NM
- Takeoff distance: 950 FT (1,570 FT over 50ft obstacle)
- Landing distance: 700 FT (1,875 FT over 50ft obstacle)
- Gross weight: 3,600 LBS
- Fuel capacity: 90 GAL
How many Performance Data documents does Sprinkle have for the Piper PA-30 Twin Comanche?
Sprinkle has 1 Performance Data document on file for the Piper PA-30 Twin Comanche.
What year is the Piper PA-30 Twin Comanche Performance Data?
The Piper PA-30 Twin Comanche Performance Data on file is dated 1964.
How many pages is the Piper PA-30 Twin Comanche Performance Data?
The Piper PA-30 Twin Comanche Performance Data runs 2 pages.
Where does Sprinkle's Piper PA-30 Twin Comanche Performance Data come from?
This Piper PA-30 Twin Comanche Performance Data was originally published by airmart.com and is hosted on Sprinkle with full text and specs.