Weight & Balance for the Piper PA-28 Archer
Piper PA-28 Archer · Weight And Balance
Overview
This document provides essential weight and balance information for the Piper PA-28 Archer. It is designed for pilots and aviation enthusiasts who need to understand the loading limits and weight distribution for safe flight operations. The document outlines the maximum weight capacities, center of gravity limits, and procedures for calculating weight and balance before flight. It is crucial for ensuring that the aircraft is loaded within safe parameters to maintain performance and safety during flight.
- Maximum takeoff weight: 2,550 lbs (1,157 kg)
- CG limits: 34.0 inches to 40.0 inches from the datum
- Weight calculation procedures are essential for safe loading
- Example loading scenarios help illustrate weight distribution
- Proper weight and balance ensure optimal aircraft performance
Document
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Maximum Weight Limits
The maximum takeoff weight for the Piper PA-28 Archer is 2,550 lbs (1,157 kg). This section details the maximum weight for various configurations, including maximum baggage and passenger weights.
Center of Gravity Limits
The center of gravity (CG) limits for the Piper PA-28 Archer are specified as 34.0 inches to 40.0 inches from the datum. This section explains how to measure and calculate the CG based on the load distribution.
Weight Calculation Procedures
This section provides step-by-step procedures for calculating the total weight and CG of the aircraft. It includes examples of how to account for passengers, baggage, and fuel.
Loading Example
An example loading scenario is provided to illustrate how to apply the weight and balance calculations. This includes a sample calculation with specific weights for passengers and baggage.
Safety notes
- Always verify weight and balance before flight to ensure safety.
- Exceeding weight limits can affect aircraft performance and safety.