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Specifications for the Cirrus SR20

Cirrus SR20 · Specifications

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Overview

This document provides detailed specifications for the Cirrus SR20, a popular single-engine aircraft known for its advanced safety features and performance capabilities. It is intended for pilots, aviation enthusiasts, and anyone interested in understanding the technical aspects of the SR20. The document covers various aspects including engine specifications, weight and loading information, performance metrics, safety features, interior features, and dimensions. Each section provides precise data that is crucial for operational planning and aircraft performance assessment.

  • Max Takeoff Weight: 3,050 lbs
  • Empty Weight: 2,161 lbs
  • Useful Load: 889 lbs
  • Max Speed: 155 ktas
  • Sea-Level Climb Rate: 828 fpm
  • Cabin Width: 49 in
  • Standard Airframe Parachute

Document

Source

Originally published by airmart.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

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Specifications
Pages
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1
File size
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54 KB
Publisher
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airmart.com
About this document
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The Specifications for the Cirrus SR20 is a specifications for the Cirrus SR20.

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The copy of the Specifications for the Cirrus SR20 on file runs 1 pages.

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This copy of the Specifications for the Cirrus SR20 was originally published by airmart.com and is hosted on Sprinkle as a free, searchable reference copy.

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In this document

Engine

The Cirrus SR20 is powered by a Continental engine with a maximum horsepower of 200. This engine specification is essential for understanding the aircraft's performance capabilities.

Weight & Loading

The maximum takeoff weight for the Cirrus SR20 is 3,050 lbs, with an empty weight of 2,161 lbs, resulting in a useful load of 889 lbs. The aircraft can carry 56 gallons of usable fuel, which weighs 336 lbs.

Performance

The claimed maximum speed of the Cirrus SR20 is 155 knots true airspeed (ktas). At 75% power, the cruise performance is 152 ktas with an efficiency of 13.1 nautical miles per gallon (nmpg) and a range of 620 nautical miles. The sea-level climb rate is 828 feet per minute (fpm), while the climb rate at 6,000 feet is 545 fpm.

Advanced Safety Features

The SR20 is equipped with several advanced safety features, including a standard airframe parachute, airbag seatbelts, and a robust electrical system with factory-installed dual alternators. These features enhance occupant protection and overall safety.

Interior Features

The interior of the Cirrus SR20 includes standard sun visors, adjustable front seat adjustments, a separate baggage door, and a rear daylight window. The aircraft is also equipped with a side yoke for control.

Dimensions

The cabin dimensions of the Cirrus SR20 are as follows: width of 49 inches, height of 50 inches, and length of 130 inches. The wingspan measures 38.3 feet.

Safety notes

  • Approved for Spins: No

Full document text

Cirrus SR20 ENGINE Manufacturer Continental Horsepower (max) 200 WEIGHT & LOADING Max Takeoff (lbs) 3,050 Empty Weight (lbs) 2,161 Useful Load (lbs) 889 Usable Fuel (gal/lbs) 56/336 PERFORMANCE* Claimed Max Speed (ktas) 155 75% Power Cruise Performance (ktas) 152 75% Power Cruise Efficiency (nmpg) 13.1 75% Power Range (nm) 620 Equal Cruise Speed at 6,000 ft (%power/TAS/gph) 58/137/8.6 Sea-Level Climb (fpm) 828 Climb at 6,000 ft. (fpm) 545 Approved for Spins No ADVANCED SAFETY FEATURES Airframe Parachute Standard Airbag Seatbelts Standard 26g Occupant Protection Standard 3g Roll Cage Standard Factory Installed Dual Alternators Standard Robust/Fault-tolerant Electrical System Standard INTERIOR FEATURES Sun Visors Standard Front Seat Adjustments Adjustable Separate Baggage Door Standard Rear Daylight Window Standard Yoke Side Yoke Factory Installed Air Conditioning Available DIMENSIONS Cabin Width (in) 49 Cabin Height (in) 50 Cabin Length (in) 130 Wingspan (ft) 38.3 *Performance numbers are calculated from manufacturer’s POH

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