WEIGHT AND BALANCE FORM
Cirrus SR22T G6 · Weight And Balance
Overview
This document provides the weight and balance information for the Cirrus SR22, specifically for aircraft N986CD. It includes details on basic empty weight, passenger weights, baggage limits, and fuel calculations. Pilots are advised to consult the Aircraft Pilot Operating Handbook (POH) for specific operational limits and guidelines. The document is crucial for ensuring that the aircraft is loaded within its weight and balance limits for safe operation.
- Basic empty weight: 2305.0 lbs
- Maximum gross weight: 3400 lbs
- Maximum usable fuel: 81 gallons (486 lbs)
- Pilot weight: 143.5 lbs
- Front passenger weight: 143.5 lbs
- Rear passenger weight: 180 lbs each
- Maximum baggage weight: 130 lbs
Document
Source
Originally published by centuryair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Year
- 2009
- Pages
- 1
- File size
- 88 KB
- Publisher
- centuryair.com
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In this document
Weight Calculations
The document outlines the basic empty weight of the aircraft as 2305.0 lbs, which includes unusable fuel and full oil. It lists the weights for the pilot (143.5 lbs), front passenger (143.5 lbs), and two rear passengers (180 lbs each). The maximum baggage weight is noted as 130 lbs.
Fuel Information
The document specifies a maximum usable fuel capacity of 81 gallons, which equates to a weight of 486 lbs (81 gallons x 6 lbs/gallon). It provides a formula for estimating fuel burn based on gallons per hour and flight duration.
Weight Limits
The maximum gross weight (GW) for the aircraft is stated as 3400 lbs. The document emphasizes the importance of calculating total weight without fuel and total landing weight to ensure compliance with safety regulations.
Center of Gravity Limitations
The document includes placeholders for the center of gravity (CG) at takeoff and landing, indicating that pilots must calculate these values based on the loaded configuration of the aircraft.
Safety notes
- Pilots must consult the Aircraft POH for specific operational limits and guidelines.
Full document text
ITEM WEIGHT ARM (IN) MOMENT (IN-LB) BASIC EMPTY WEIGHT 2305.0 (Includes un- useable fuel and full oil) 138.2 318564 PILOT 143.5 FRONT PASSENGER 143.5 REAR PASSENGER 1 180 REAR PASSENGER 2 180 BAGGAGE (130 lb Max) 208 Total Weight Without Fuel USEABLE FUEL(81G. MAX) _____Gallons x 6 = ______# 154.9 TOTAL WEIGHT (MAX GW: 3400 lbs.) Estimated Fuel Burn (GPH x Hours x 6) 153.8 TOTAL LANDING WEIGHT CENTER OF GRAVITY LIMITATIONS CG TAKE- OFF=_____ _ CG LAND- ING=______ WEIGHT AND BALANCE FORM WEIGHT AND BALANCE FORM For Reference Only, Pilots must consult Aircraft POH For Reference Only, Pilots must consult Aircraft POH N986CD Cirrus SR22 N986CD Cirrus SR22 Current as of: 5/22/09 Current as of: 5/22/09