Weight & Balance
Cirrus SR20 · Weight & Balance
Overview
This document provides essential information regarding the weight and balance specifications for the Cirrus SR20 aircraft. It is designed for pilots and aviation enthusiasts to ensure safe operation by understanding the weight limits and balance parameters critical for flight safety. The manual includes detailed tables and guidelines for calculating weight and balance, as well as instructions for loading the aircraft correctly. Proper weight and balance management is crucial for maintaining aircraft performance and safety during flight operations.
- Maximum takeoff weight: 3,100 lbs (1,406 kg)
- Maximum landing weight: 3,000 lbs (1,361 kg)
- Forward CG limit: 35.0 inches
- Aft CG limit: 43.0 inches
- Proper loading is critical for maintaining CG within 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.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at www.classicairaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight & Balance
- Pages ·
- 164
- File size ·
- 1.5 MB
- Copy found at ·
- www.classicairaviation.com
What is the Weight & Balance?
The Weight & Balance is a weight & balance for the Cirrus SR20.
How many pages is the Weight & Balance?
The copy of the Weight & Balance on file runs 164 pages.
Common. More common than 98% of the aircraft models we track.
Full essential library on file for the Cirrus SR20.
Cirrus SR20 for sale now
Free — save the SR20 to your watchlist and track it in one place.
More Cirrus SR20manuals & documents
See all 25 →- Cirrus SR20 Model GuideModel Guide
- DFC Autopilot Series Installation ManualWiring Diagrams
- Service Bulletin SB2X-76-05Service Bulletins
- Cirrus Owners and Pilots Quick Reference Guide for SR Series aircraftV Speeds Reference
- FAA APPROVED AIRPLANE FLIGHT MANUALChecklist
- Validation ReportOther Documents
- PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for the CIRRUS DESIGN SR20Pilot's Operating Handbook
- Standard Practice Maintenance ManualMaintenance Manual
- Aviation Maintenance Alert - Cirrus SR20 and SR22 AircraftMaintenance Manual
- PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for the CIRRUS SR20Training Manual
- CIRRUS SR20 NORMAL CHECKLISTEmergency Procedures
- PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for the CIRRUS DESIGN SR20Pilot's Operating Handbook
Related documents
- SCHWEIZER RSG SPARE PARTS LISTSCHWEIZER 269C-1 · Parts Catalog
- ASC-AOR-15-04-001Beechcraft Beechjet 400A · Training Manual
- Variable Stiffness Spar Wind-Tunnel Model Development and TestingNASA · Technical Report
- 2000 CITATION EXCEL | SN 5089 | N135SPCessna Citation Excel · Systems Description
- A Fully Non-metallic Gas Turbine Engine Enabled by Additive ManufacturingNASA · Technical Report
If you fly the Cirrus SR20, you may also be researching these.
—In this document
General Information
This section outlines the importance of weight and balance in aviation, emphasizing how it affects aircraft performance, stability, and safety. It introduces the key concepts and terms related to weight and balance, such as maximum takeoff weight, useful load, and center of gravity (CG).
Weight Limits
The Cirrus SR20 has a maximum takeoff weight of 3,100 lbs (1,406 kg). The maximum landing weight is 3,000 lbs (1,361 kg). Pilots must ensure that the total weight of the aircraft, including passengers, cargo, and fuel, does not exceed these limits to maintain safe flight operations.
Center of Gravity (CG) Limits
The CG limits for the Cirrus SR20 are critical for ensuring stability during flight. The forward CG limit is 35.0 inches, and the aft CG limit is 43.0 inches from the datum. Proper loading and weight distribution are necessary to keep the CG within these limits for safe operation.
Loading Instructions
This section provides detailed instructions on how to load the aircraft correctly. It includes guidelines on distributing weight among passengers and cargo to maintain the CG within limits. It also emphasizes the importance of securing all items to prevent shifting during flight.
Weight and Balance Calculations
Pilots are provided with formulas and examples for calculating the weight and balance of the aircraft. This includes how to determine the total weight, moment, and CG location based on the loading configuration. Accurate calculations are essential for flight safety.
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
- Exceeding weight limits can lead to reduced performance and safety risks.
- Improper CG can affect aircraft stability and control.
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
Section 1 General
Show full textShow less
Hartzell Section 2 Limitations Hartzell - - 1 1 - - 1 1 - - 1 1 1 1 1 1 - - 1 1 1 1 1 1 - - 1 1 When the PFD is coupled with Autopilot System, the following Limitations apply: Section 3 Emergency Procedures Maintain Aircraft Control Analyze the Situation Take Appropriate Action Land as soon as Conditions Permit Propeller RPM will not increase: Propeller overspeeds or will not decrease: -- 60 of 164









