Piper PA-28R Arrow IV — Weight And Balance
2 weight and balance references for the Piper PA-28R Arrow IV.
This document serves as a comprehensive guide for the Piper Arrow PA28R-201, focusing on single-engine aerodynamics, performance metrics, and aircraft systems. It is designed for pilots and aviation enthusiasts, providing essential information on flight characteristics, weight and balance, and operational procedures. The guide includes detailed sections on aerodynamics, speeds, weight limits, takeoff and landing distances, and the aircraft's systems, including the power plant and landing gear. It aims to enhance understanding and operational safety for users of the Piper Arrow.
- Stall speed in landing configuration (VSO) is 55 KIAS.
- Maximum ramp weight is 2,758 lbs; maximum takeoff weight is 2,750 lbs.
- Maximum weight in baggage compartments is 200 lbs.
- Best rate of climb speed (VY) is 90 KIAS with gear up and flaps up.
- The maximum demonstrated crosswind is 17 knots.
How many Weight And Balance documents does Sprinkle have for the Piper PA-28R Arrow IV?
Sprinkle has 2 Weight And Balance documents on file for the Piper PA-28R Arrow IV.
What year is the Piper PA-28R Arrow IV Weight And Balance?
The Piper PA-28R Arrow IV Weight And Balance on file is dated 2025.
How many pages is the Piper PA-28R Arrow IV Weight And Balance?
The Piper PA-28R Arrow IV Weight And Balance runs 36 pages.
Where does Sprinkle's Piper PA-28R Arrow IV Weight And Balance come from?
This Piper PA-28R Arrow IV Weight And Balance was originally published by www.mga.edu and is hosted on Sprinkle with full text and specs.