Cessna T210N - AirMart
CESSNA 210N · Specifications
Overview
This document provides performance data for the Cessna T210N, detailing the aircraft's specifications, capabilities, and operational limits. It is intended for pilots and aviation enthusiasts who require precise information about the aircraft's performance metrics. The data includes engine specifications, fuel capacities, speed, range, and various takeoff and landing distances. Understanding these parameters is crucial for safe and efficient flight operations in the Cessna T210N.
- Engine: CONTINENTAL TSIO-520-R, 310 hp
- Max Cruise Speed: 222 mph (193 kts)
- Stall Speed: 66 mph (57 kts)
- Range: 715 miles (621 nmi)
- Service Ceiling: 27,000 ft (8229 m)
- Empty Weight: 2305 lbs (1045 kg)
- Max Gross Weight: 4000 lbs (1814 kg)
- Takeoff Distance (50 ft obstacle): 1300 ft (396 m)
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
- 56 KB
- Publisher
- airmart.com
Common. One of the most common aircraft types we track.
Most owners only have the POH. Here's the essential set for the CESSNA 210N.
- 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
Engine Specifications
The Cessna T210N is powered by a single CONTINENTAL TSIO-520-R engine, delivering 310 horsepower. The recommended time between overhauls (TBO) for this engine is 1600 hours.
Performance Metrics
The aircraft achieves a maximum cruise speed of 222 mph (193 knots) and has a stall speed of 66 mph (57 knots). It has a service ceiling of 27,000 feet and a rate of climb of 930 feet per minute.
Weight and Balance
The empty weight of the Cessna T210N is 2305 lbs (1045 kg), with a maximum gross weight of 4000 lbs (1814 kg). This weight range is important for calculating load and balance for flight.
Fuel Capacity
The standard and maximum fuel capacity for the Cessna T210N is 90 gallons (340 liters), which is essential for planning flight range and endurance.
Takeoff and Landing Distances
For normal takeoff, the Cessna T210N requires 1300 feet (396 meters) over a 50-foot obstacle, and 765 feet (233 meters) for landing. These distances are critical for runway selection and safety during operations.
Full document text
Cessna T210N The values portrayed here are from manufacturers' data and are not representative of any particular aircraft being advertised. No. of Engines: 1 Engine Make: CONTINENTAL Engine Model: TSIO-520-R Horsepower: 310 hp Rec'd TBO: 1600 Standard Fuel: 90.00 gal | 340.0 L Max Fuel: 90.00 gal | 340.0 L 75% Cruise: 222 mph | 193 kts | 357 km/h Stall Speed: 66 mph | 57 kts | 107 km/h Range: 715 miles | 621 nmi | 1150 km Service Ceiling: 27000 ft | 8229 m Rate of Climb: 930 ft/min | 4.72 m/s Wingspan: 36.80 ft | 11.16 m Length: 28.17 ft | 8.58 m Height: 9.70 ft | 2.920 m Empty Weight: 2305 lbs | 1045 kg Gross Weight: 4000 lbs | 1814 kg Normal Over 50 Foot Obstacle Takeoff: 1300 ft | 396.00 m 2160 ft | 658.00 m Landing: 765 ft | 233.00 m 1500 ft | 457.0 m
What's in the CESSNA 210N 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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