Weight & Balance
Cirrus SR20 · Weight And 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.
Document
Source
Originally published by www.classicairaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight And Balance
- Pages ·
- 164
- File size ·
- 1.5 MB
- Publisher ·
- www.classicairaviation.com
What is the Weight & Balance?
The Weight & Balance is a weight and balance for the Cirrus SR20.
How many pages is the Weight & Balance?
The copy of the Weight & Balance on file runs 164 pages.
Where does the Weight & Balance come from?
This copy of the Weight & Balance was originally published by www.classicairaviation.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the Cirrus SR20.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More Cirrus SR20manuals & documents
See all 18 →- DFC Autopilot Series Installation ManualWiring Diagram
- Cirrus Owners and Pilots Quick Reference Guide for SR Series aircraftV Speeds Reference
- 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
- Dual Fuel Level – Cirrus Aircraft w/ CIES Inc. SendersWiring Diagram
- Pilot’s Operating HandbookPilot's Operating Handbook
- Service BulletinService Bulletins
- AIRWORTHINESS DIRECTIVEAirworthiness Directives
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.
Safety notes
- Exceeding weight limits can lead to reduced performance and safety risks.
- Improper CG can affect aircraft stability and control.
Full document text
Section 1 General
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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