Piper PA-32 Saratoga II TC — Weight And Balance
1 weight and balance reference for the Piper PA-32 Saratoga II TC.
This document provides detailed specifications and performance data for the Piper PA-32 Saratoga II TC, a six-seat aircraft powered by a Textron Lycoming TIO-540-AHIA engine with 300 horsepower. It outlines critical dimensions, weight limits, fuel capacities, and performance metrics essential for pilots and aviation enthusiasts. The information is based on manufacturer's calculations and standard conditions, making it a reliable reference for understanding the aircraft's capabilities and limitations.
- Max gross weight: 3,600 lb
- Empty weight: 2,478 lb
- Useful load: 1,137 lb
- Takeoff distance over 50-ft obstacle: 1,810 ft
- Max operating altitude: 20,000 ft
- Cruise speed at high-speed power: 176 kt at 10,000 ft
- Max demonstrated crosswind component: 17 kt
How many Weight And Balance documents does Sprinkle have for the Piper PA-32 Saratoga II TC?
Sprinkle has 1 Weight And Balance document on file for the Piper PA-32 Saratoga II TC.
How many pages is the Piper PA-32 Saratoga II TC Weight And Balance?
The Piper PA-32 Saratoga II TC Weight And Balance runs 1 pages.
Where does Sprinkle's Piper PA-32 Saratoga II TC Weight And Balance come from?
This Piper PA-32 Saratoga II TC Weight And Balance was originally published by airmart.com and is hosted on Sprinkle with full text and specs.