Cessna P210R Pressurized Centurion
CESSNA P-210 Pressurized Centurion II · Specifications
Overview
This document provides specifications for the Cessna P210R Pressurized Centurion, a single-engine aircraft known for its pressurized cabin and performance capabilities. It is designed for pilots and aviation enthusiasts seeking detailed information about the aircraft's engine, fuel capacity, weights, and performance metrics. The specifications include critical data such as engine model, fuel requirements, weight limits, and performance characteristics, making it a valuable reference for operational planning and understanding the aircraft's capabilities.
- Engine Model: Continental TSIO-520-CE, 6 cylinders, 325 HP
- Fuel Capacity: 90 gallons (120 gallons with long-range tanks)
- Takeoff Weight: 4,100 lbs; Landing Weight: 3,900 lbs
- Max Structural Cruising Speed: 167 KIAS
- Stall Speed Clean: 65 knots; Stall Speed Landing Configuration: 55 knots
- Best Rate of Climb: 1,150 FPM; Service Ceiling: 25,000 ft
Document
Source
Originally published by airmart.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Pages
- 1
- File size
- 24 KB
- Publisher
- airmart.com
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
Engine Specifications
The Cessna P210R is equipped with a Continental TSIO-520-CE engine, featuring 6 cylinders and a displacement of 520 cubic inches. It delivers a power output of 325 horsepower and utilizes a fuel-injected system with a constant speed propeller.
Fuel Capacity and Requirements
The aircraft has a fuel capacity of 90 gallons, with an option for long-range tanks that increase capacity to 120 gallons. The minimum octane rating for fuel is 100, although the average fuel burn at 75% power in standard conditions is not specified.
Weights and Capacities
In the normal category, the takeoff weight is 4,100 lbs and the landing weight is 3,900 lbs. The standard empty weight is 2,471 lbs, allowing for a maximum useful load of 1,629 lbs. The baggage capacity is limited to 200 lbs, and the oil capacity is 10 quarts.
Performance Metrics
The aircraft has a maximum speed not to exceed 200 KIAS and a maximum structural cruising speed of 167 KIAS. Stall speeds are 65 knots in a clean configuration and 55 knots in landing configuration. The best rate of climb is 1,150 feet per minute, with a service ceiling of 25,000 feet.
Full document text
Cessna P210R Pressurized Centurion Engine: Model Cont. TSIO-520-CE No. Cylinders 6 Displacement 520 cu. in. HP 325 Carbureted Or Fuel Injected Fuel Injected Fixed Pitch/ Constant Speed Propeller Constant Speed Fuel: Fuel Capacity 90 gallons Long Range Tanks: 120 gallons Min. Octane Fuel 100 Avg. Fuel Burn at 75% power in standard conditions per hour Unknown Weights and Capacities: Takeoff/Landing Weight Normal Category 4,100/3,900 lbs. Takeoff/Landing Weight Utility Category N/A Standard Empty Weight 2,471 lbs. Max. Useful Load Normal Category 1,629 lbs. Max. Useful Load Utility Category N/A Baggage Capacity 200 lbs. Oil Capacity 10 quarts Performance Do Not Exceed Speed 200 KIAS Max. Structural Cruising Speed 167 KIAS Stall Speed Clean 65 Knots Stall Speed Landing Configuration 55 Knots Climb Best Rate 1150 FPM Wing Loading 22.1 lbs./sq. ft. Power Loading 12.6 lbs./hp Service Ceiling 25,000 ft. Source: https://www.aopa.org/go-fly/aircraft-and-ownership/aircraft-fact-sheets/cessna-p210