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CIRRUS SR22 SPECS and PERFORMANCE

Cirrus SR22T G6 · Performance Data

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Overview

This document provides specifications and performance data for the Cirrus SR22 aircraft. It includes detailed information on weight, engine specifications, dimensions, and various performance metrics. The data is essential for pilots and aviation enthusiasts to understand the capabilities and limitations of the aircraft. Key performance figures such as takeoff distance, climb rate, and cruise speed are highlighted, making it a valuable reference for flight planning and operational considerations.

  • Base Weight: 2260 lbs (1025 kg)
  • Useful Load: 1340 lbs (607 kg)
  • Max Cruise Speed: 183 KTAS
  • Takeoff Distance: 1082 ft (330 m)
  • Climb Rate: 1270 ft/min (6.45 m/sec)
  • Max Operating Altitude: 17,500 ft (5,334 m)
  • Stall Speed with Flaps: 60 KCAS

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

Type
Performance Data
Pages
1
File size
28 KB
Publisher
airmart.com
Documentation completeness
6/7

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In this document

Weight

The Cirrus SR22 has a base weight of 2260 lbs (1025 kg) and a useful load of 1340 lbs (607 kg). The payload for a typical 3-hour trip with a 45-minute reserve is 974 lbs (442 kg). This information is crucial for pilots to ensure they operate within weight limits.

Engine

The aircraft is powered by a Continental IO-550-N engine, which produces 310 horsepower. Understanding the engine specifications helps pilots assess performance capabilities and maintenance requirements.

Dimensions

The Cirrus SR22 has a wingspan of 38 ft 4 in (11.68 m), a length of 26 ft (7.92 m), and a height of 8 ft 11 in (2.7 m). The cabin width is 49 in (124 cm) and the cabin height is 50 in (127 cm), providing insights into space and comfort for occupants.

Performance

Key performance metrics include a takeoff distance of 1082 ft (330 m) and a takeoff distance over a 50 ft obstacle of 1868 ft (569 m). The climb rate is 1270 ft/min (6.45 m/sec), with a maximum operating altitude of 17,500 ft (5,334 m). Stall speed with flaps is 60 KCAS, and the maximum cruise speed is 183 KTAS.

Full document text

CIRRUS SR22 SPECS and PERFORMANCE WEIGHT • Base Weight: 2260 lbs (1025 kg) • Useful Load: 1340 lbs (607 kg) • Payload (3 hr trip and 45 min res): 974 lbs (442 kg) ENGINE • Manufacturer: Continental • Model: IO-550-N • Horsepower: 310 DIMENSIONS • Wingspan: 38 ft 4in (11.68 m) • Length: 26 ft (7.92 m) • Height: 8 ft 11 in (2.7 m) • Cabin Width: 49 in (124 cm) • Cabin Height: 50 in (127 cm) PERFORMANCE • Takeoff: 1082 ft (330 m) • Takeoff Over 50 ft Obstacle: 1868 ft (569 m) • Climb Rate: 1270 ft/min (6.45 m/sec) • Max operating Altitude: 17,500 ft (5,334 m) • Stall Speed with Flaps: 60 KCAS • Max Cruise Speed: 183 KTAS • Cruise Speed, 8000’ @ 75% Power: 180 KTAS, 17.8 GPH • Landing Ground Roll: 1178 ft (359 m)