Weight & Balance for Cessna Citation 500
Cessna Citation 500 · Weight And Balance
Overview
This document provides essential information regarding the weight and balance specifications for the Cessna Citation 500. It is intended for pilots and aviation personnel who need to ensure that the aircraft is loaded within its weight limits for safe operation. The document outlines the maximum takeoff weight, empty weight, and the various loading configurations that can affect the aircraft's center of gravity. It serves as a critical reference to maintain compliance with safety regulations and operational guidelines.
- Maximum takeoff weight: 10,000 lbs
- Empty weight: approximately 6,500 lbs
- Forward CG limit: 30 inches
- Aft CG limit: 36 inches
- Weight and balance calculations are essential for safe operation.
Document
Source
Originally published by www.baaa-acro.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 51
- File size
- 20 MB
- Publisher
- www.baaa-acro.com
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna Citation 500.
- 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
Maximum Takeoff Weight
The maximum takeoff weight for the Cessna Citation 500 is specified as 10,000 pounds. This weight includes the aircraft, passengers, cargo, and fuel. Exceeding this limit can compromise safety and performance.
Empty Weight
The empty weight of the Cessna Citation 500 is approximately 6,500 pounds. This weight is crucial for calculating the useful load and ensuring that the aircraft remains within its weight limits during flight.
Center of Gravity Limits
The center of gravity (CG) limits for the Cessna Citation 500 are defined to ensure stability during flight. The forward CG limit is 30 inches, while the aft limit is 36 inches from the reference point. Proper loading is essential to maintain these limits.
Loading Configurations
Different loading configurations can significantly affect the aircraft's performance. The document details various configurations, including passenger and cargo arrangements, to help pilots make informed decisions about loading.
Weight and Balance Calculations
The document includes formulas and examples for calculating weight and balance. Pilots are guided on how to determine the total weight and CG based on the loading configuration.
Safety notes
- Exceeding maximum takeoff weight can compromise safety.
- Improper loading can lead to instability during flight.
What's in the Cessna Citation 500 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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