Weight & Balance for Cirrus SR20 G7
Cirrus SR20 G7 · Weight And Balance
Overview
This document serves as a Weight & Balance reference for the Cirrus SR20 G7, specifically for the aircraft with registration N593PU. It provides essential data for pilots to calculate the aircraft's weight and center of gravity (CG) for safe flight operations. The document includes sections for recording weights of various components, such as fuel, passengers, and baggage, as well as guidelines for determining the aircraft's total weight and CG. It emphasizes the importance of verifying weight and balance before flight, ensuring that the aircraft remains within safe operational limits.
- Licensed Empty Weight: 2,187.72 lbs
- Maximum Fuel Capacity: 58.5 gallons (153.80 lbs)
- Baggage Area Maximum: 130 lbs
- Total Weight Calculations must include all occupants and baggage
- Verify weight and balance before flight
Document
Source
Originally published by www.lakeelmoaero.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Year
- 2025
- Pages
- 1
- File size
- 442 KB
- Publisher
- www.lakeelmoaero.com
Common. One of the most common aircraft types we track.
Most owners only have the POH. Here's the essential set for the Cirrus SR20 G7.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Weight and Balance Calculations
The document outlines the procedure for calculating the aircraft's weight and balance, including the licensed empty weight of 2,187.72 lbs and the maximum fuel capacity of 58.5 gallons, equating to 153.80 lbs. It provides a breakdown of weights for front and rear seats, as well as baggage, to assist in determining the total weight for departure and destination.
Performance Data
Included are performance data fields for pilots to fill out, such as field elevation, temperature, wind direction, and pressure altitude. This information is crucial for assessing takeoff and landing performance under varying conditions.
Seat Occupancy and Useful Load
The document contains a seat occupancy table and a section for calculating the remaining useful load, which is vital for ensuring that the aircraft is not overloaded and that the weight distribution is within safe limits.
Safety Notes
The document repeatedly emphasizes the necessity of verifying weight and balance before flight, highlighting that the provided data is for planning purposes only.
Safety notes
- FOR PLANNING PURPOSES ONLY, VERIFY WEIGHT AND BALANCE BEFORE FLIGHT
Full document text
Pilot: Copilot: Rear Left: Rear Right: Item Weight Arm Moment Aircraft Licensed Empty Weight 2,187.72 140.17 306,642.03 Fuel (58.5 Gallons Maximum) Gal 153.80 Front Seats 143.50 Rear Seats 180.00 Baggage Area (130lbs Max) 208.00 Departure Total Estimated Fuel Burn Gal 153.80 Destination Total Gal Weather Information: Departure Destination Performance: *Max Weight* Field Elevation: Takeoff Roll: Temperature C: Takeoff 50ft Roll: Dew Point C: Altimeter Setting: Landing Roll: Wind Direction: Landing 50ft Roll: Wind Speed: Runway Heading: Depart Head Wind: Soft Field? Y or N: Depart X-Wind: Relative Humidity: Pressure Altitude: Dest Head Wind: Density Altitude: Dest X-Wind: Loaded Moment Normal Category 137.8 2100 139.1 2700 140.7 3050 148.1 3050 148.1 2100 Seat Occupancy Table: Remaining Useful Load: *FOR PLANNING PURPOSES ONLY, VERIFY WEIGHT AND BALANCE BEFORE FLIGHT* *FOR PLANNING PURPOSES ONLY, VERIFY WEIGHT AND BALANCE BEFORE FLIGHT* *FOR PLANNING PURPOSES ONLY, VERIFY WEIGHT AND BALANCE BEFORE FLIGHT* Sunday, February 2, 2025 2010 Cirrus SR20 N593PU *FOR PLANNING PURPOSES ONLY, VERIFY WEIGHT AND BALANCE BEFORE FLIGHT* USAGE: Fill out the areas in Yellow 2100 2200 2300 2400 2500 2600 2700 2800 2900 3000 3100 3200 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 TOTAL WEIGHT (LBS) AIRCRAFT ARM (INCHES AFT OF DATUM) Normal Category Departure CG Destination CG
What's in the Cirrus SR20 G7 TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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