Performance Data for CESSNA P-210 Pressurized Centurion II
CESSNA P-210 Pressurized Centurion II · Performance Data
Overview
This document provides performance data specifically for the CESSNA P-210 Pressurized Centurion II. It is intended for pilots and aviation enthusiasts who require detailed information on the aircraft's operational capabilities. The manual includes critical performance metrics such as takeoff distances, climb rates, and fuel consumption, which are essential for flight planning and operational efficiency. The data is presented in a clear and concise manner, allowing users to quickly reference the information they need for safe and effective flight operations.
- Takeoff distance at max weight: 1,200 feet at sea level.
- Climb rate: 1,000 feet per minute at sea level.
- Cruise speed: 150 knots at 8,000 feet.
- Fuel consumption: 12 gallons per hour at cruise.
- Landing distance at max weight: 1,000 feet on dry runway.
Document
Source
Originally published by data.tmorris.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Performance Data
- Pages
- 10
- File size
- 268 KB
- Publisher
- data.tmorris.net
Most owners only have the POH. Here's the essential set for the CESSNA P-210 Pressurized Centurion II.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More CESSNA P-210 Pressurized Centurion IImanuals & documents
In this document
Takeoff Performance
The takeoff performance section outlines the required distances for takeoff under various weight conditions and environmental factors. For example, at sea level and standard temperature, the takeoff distance is approximately 1,200 feet for a maximum weight of 3,600 lbs.
Climb Performance
This section details the aircraft's climb rates at different weights and altitudes. The Cessna P-210 can achieve a rate of climb of approximately 1,000 feet per minute at sea level under optimal conditions.
Cruise Performance
Cruise performance metrics include fuel consumption rates and speeds at various altitudes. At a cruising altitude of 8,000 feet, the aircraft typically operates at a fuel flow of 12 gallons per hour while maintaining a speed of 150 knots.
Landing Performance
Landing performance data provides information on landing distances required under various conditions. The landing distance at maximum weight on a dry runway is approximately 1,000 feet.
Weight and Balance
This section explains the importance of weight and balance calculations for safe flight operations. It includes charts and tables to assist pilots in determining the aircraft's center of gravity based on load distribution.
Safety notes
- Ensure weight and balance calculations are performed before flight.
- Monitor fuel levels to avoid running out during flight.
Full document text
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