Piper PA-28 Archer II — Weight And Balance
1 weight and balance reference for the Piper PA-28 Archer II.
Overview
Weight & Balance for the Piper PA-28 Archer II
This document provides essential weight and balance information for the Piper PA-28 Archer II. It is intended for pilots and aviation personnel who need to ensure that the aircraft is loaded within its weight limits for safe operation. The document outlines the maximum weight capacities, loading configurations, and methods for calculating weight and balance before flight. Understanding these parameters is crucial for maintaining aircraft performance and safety during flight operations.
- Maximum Takeoff Weight: 2,550 lbs (1,157 kg)
- Forward CG Limit: 35 inches from datum
- Aft CG Limit: 47 inches from datum
- Weight of fuel: approximately 6 lbs per gallon
- Ensure proper weight distribution to maintain balance.
1 document