SR22-G3-TN Weight and Balance
Cirrus SR22 G3 · Weight & Balance
Overview
This document provides the weight and balance information for the Cirrus SR22 G3 aircraft. It includes detailed data on various weight components such as fuel, passengers, and cargo, as well as their respective arms and moments. The document is essential for pilots to ensure that the aircraft is loaded within its weight limits and that the center of gravity (CG) is within acceptable parameters for safe operation. It outlines the maximum takeoff weight, landing weight, and the CG limits for both takeoff and landing phases. This information is crucial for flight planning and ensuring compliance with safety regulations.
- Maximum Takeoff Weight: 3,400 lbs
- Maximum Ramp Fuel: 92 gallons (535 lbs)
- Pilot Weight: 170 lbs
- Luggage Maximum: 130 lbs
- Excess Payload: 180 lbs
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at inventory.steelaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight & Balance
- Pages ·
- 1
- File size ·
- 36 KB
- Copy found at ·
- inventory.steelaviation.com
What is the SR22-G3-TN Weight and Balance?
The SR22-G3-TN Weight and Balance is a weight & balance for the Cirrus SR22 G3.
How many pages is the SR22-G3-TN Weight and Balance?
The copy of the SR22-G3-TN Weight and Balance on file runs 1 pages.
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In this document
Weight and Balance Summary
The document summarizes the total weight and balance of the Cirrus SR22 G3, indicating a maximum takeoff weight of 3,400 lbs. It provides a breakdown of various weight components including pilot, passengers, luggage, and fuel, along with their respective arms and moments.
Fuel Information
Details on fuel weight are provided, indicating a maximum ramp fuel capacity of 92 gallons, which weighs approximately 535 lbs. The document also includes calculations for fuel burn during different phases of flight.
Center of Gravity Limits
The document specifies the center of gravity limits for the SR22 G3, with CG limits for takeoff and landing phases. It provides a graphical representation of the CG envelope based on various weight configurations.
Weight Calculations
It includes calculations for various weights at different configurations, showing how the CG shifts with changes in weight. This is critical for pilots to understand how loading affects aircraft performance.
Excess Payload
The document notes an excess payload of 180 lbs, which is important for pilots to consider when loading the aircraft to ensure compliance with weight limits.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Ensure the total weight does not exceed 3,400 lbs for safe operation.
- Verify that the center of gravity is within limits for both takeoff and landing.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
Position Item Weight Arm Moment 2,481 139.3 345.6 TKS Fluid (9.3 ppg/3.5 gal max) 3.5 Gals 33 148.0 4.8 Pilot 170 143.5 24.4 Front R 143.5 0.0 Rear L 180.0 0.0 Rear R 180.0 0.0 Luggage (130lbs max) 10 208.0 2.1 Ramp Fuel (5.82 ppg / 92 gal max) 92.0 Gals 535 154.9 82.9 3,229 142.4 459.8 Start/Taxi/Runup Fuel Burn, "-minus" 9 lbs 9 154.9 1.4 Takeoff Weight (3400 Max) & CG 3,220 142.4 458.4 Excess Payload 180 Destination: Fuel burn (Gal) 40.0 Gals 233 154.9 36.1 Fuel Remaining at Dest. 52.0 Gals 2,987 141.4 422.4 weight cg 2200 138 2700 139.1 3210 141.4 3210 141.4 3400 143.8 3400 148.1 2200 148.1 2200 138 SR22-G3-TN Weight and Balance BEW (includes unusable fuel, full oil, full 02) Destination Landing Weight & CG TOTAL RAMP Weight And CG 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 Center of Gravity Limits Takeoff Landing Envelope