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SR22 G3 Weight & Balance

Cirrus SR22 G3 · Weight And Balance

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Overview

This document provides the weight and balance information specifically for the Cirrus SR22 G3 aircraft. It includes detailed data on the weights of various components, including the pilot, passengers, fuel, and baggage, as well as the corresponding center of gravity (CG) calculations. This information is crucial for pilots to ensure that the aircraft is within safe operating limits for takeoff and landing. The document outlines the maximum allowable weights and CG limits, which are essential for flight safety and performance. It serves as a reference for pilots and aviation enthusiasts to understand the weight distribution and balance requirements of the SR22 G3.

  • Maximum fuel capacity: 92 gallons (552 lbs)
  • Total ramp weight: 2,959 lbs, CG: 142.21 inches
  • Takeoff weight: 2,950 lbs, CG: 142.17 inches
  • Landing weight: 2,650 lbs, CG: 140.73 inches
  • Baggage maximum weight: 130 lbs

Document

Source

Originally published by www.xuefeiji.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Weight And Balance
Pages
1
File size
136 KB
Publisher
www.xuefeiji.org
Documentation completeness
3/7

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In this document

Weight and Balance Data

The document lists various weight items including the pilot, fuel, passengers, and baggage, along with their respective arms and moments. For example, the maximum fuel capacity is 92 gallons, weighing 552 lbs, with a moment of 154.90. The total ramp weight is calculated at 2,959 lbs with a CG of 142.21 inches.

Weight Calculations

The document provides specific weight calculations for different phases of flight. The takeoff weight is noted as 2,950 lbs with a CG of 142.17 inches, while the landing weight is 2,650 lbs with a CG of 140.73 inches. These calculations are critical for ensuring the aircraft is balanced and within limits during flight.

Center of Gravity Limits

The document includes a graphical representation of the center of gravity limits for the SR22 G3, showing the envelope for both takeoff and landing. This information is vital for pilots to ensure that the aircraft remains within safe CG limits throughout the flight.

Safety notes

  • Ensure that the aircraft is within weight and CG limits before flight.
  • Improper weight distribution can affect aircraft performance and safety.

Full document text

Position Item Weight Arm Moment 2407 139.30 335.30 Pilot 143.50 0.00 Fuel (Gal- 92 Max) 92 552 154.90 85.50 Pax Names Front Pax 143.50 0.00 Rear Pax 180.00 0.00 Rear Pax 180.00 0.00 De-Ice 34.5 lbs full 148.40 0.00 O 2 (If Installed) 6.4 lbs full 265.30 0.00 Bags Max 130 lbs 208.00 0.00 Ramp Weight and CG 2,959.0 142.21 420.80 Fuel for Start, Taxi, & Runup -9.0 154.90 -1.39 Takeoff Weight and CG 2950.0 142.17 419.41 Fuel for Flight 50 -300 154.90 -46.47 Landing Weight and CG 2650.0 140.73 372.94 weight cg 2100 137.8 2700 139.1 3400 142.3 3400 148.1 2100 148.1 2100 137.8 SR22 G3 Weight & Balance BEW (Includes Unusable Fuel and Full Oil) 2000 2200 2400 2600 2800 3000 3200 3400 3600 136 138 140 142 144 146 148 150 Weight - Pounds C.G. - Inches Aft of Datum SR22 G3 Center of Gravity Limits Envelope Takeoff Landing