Specifications
CIRRUS SR22-G3 TURBO · Specifications
Overview
This document provides detailed specifications for the Cirrus SR22T and its variants, including the G3 and GTS models. It is intended for pilots and aviation enthusiasts seeking comprehensive data on the aircraft's performance, dimensions, and operational capabilities. Key information includes powerplant specifications, weight limits, fuel capacities, and performance metrics such as takeoff and landing distances. The document serves as a reference for understanding the aircraft's design and operational parameters, ensuring pilots can make informed decisions during flight planning and operations.
- Engine: Tornado Alley turbonormalized TCM IO-550-N, 310 hp @ 2,700 RPM
- Max Gross Weight: 3,400 lb
- Fuel Capacity: 92 gal usable, 552 lb usable
- Takeoff Distance (Ground Roll): 1,028 ft
- Max Level Speed: 219 kt at 25,000 ft
- Rate of Climb: 1,400 fpm at sea level
- V Y (Best Rate of Climb): 100 KIAS
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at airmart.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Specifications
- Pages ·
- 2
- File size ·
- 183 KB
- Copy found at ·
- airmart.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm) ·
- 716
- Engine (hp) ·
- 310
- Height (ft) ·
- 8
- Length (ft) ·
- 26
- Propeller ·
- Hartzell ASC
- Wingspan (ft) ·
- 38
- Engine model ·
- TCM IO-550-N
- Max speed (kt) ·
- 219
- Cruise speed (kt) ·
- 176
- Empty weight (lb) ·
- 2,330
- Fuel capacity (gal) ·
- 92
- Rate of climb (fpm) ·
- 1,400
- Service ceiling (ft) ·
- 25,000
- Max takeoff weight (lb) ·
- 3,400
Performance
- Fuel burn (gph) ·
- 17.5
- Landing over 50ft ·
- 2,344
- Max crosswind (kt) ·
- 24
- Takeoff over 50ft ·
- 1,594
- Landing distance (ft) ·
- 1,141
- Takeoff distance (ft) ·
- 1,028
- Stall speed clean (kt) ·
- 66
- Stall speed landing (kt) ·
- 61
V-speeds
- VA ·
- 133
- VR ·
- 73
- VX ·
- 80
- VY ·
- 100
- VFE ·
- 104
- VNE ·
- 204
- VNO ·
- 178
- VS1 ·
- 66
- VSO ·
- 61
Weight & balance
- Useful load (lb) ·
- 1,070
- Baggage allowance (lb) ·
- 130
- Max takeoff weight (lb) ·
- 3,400
What is the Specifications?
The Specifications is a specifications for the CIRRUS SR22-G3 TURBO.
How many pages is the Specifications?
The copy of the Specifications on file runs 2 pages.
Most owners only have the POH. Here's the essential set for the CIRRUS SR22-G3 TURBO.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
Related documents
- Cirrus SR22 G2 GTS Specifications and PerformanceCirrus SR22T · Specifications
- CIRRUS SR22 SPECS and PERFORMANCECirrus SR22T G6 · Performance Data
- Cirrus SR20 G3Cirrus SR20 G3 · Specifications
- Summary Aircraft Data 2009 Cirrus (SR20) N511RTCirrus SR20 G3 · Systems Description
- AAFC SR22T Quick Reference SheetCirrus SR22T G7 · V Speeds Reference
In this document
Powerplant
The Cirrus SR22T is equipped with a Tornado Alley turbonormalized TCM IO-550-N engine, delivering 310 horsepower at 2,700 RPM. The recommended time between overhauls (TBO) for the engine is 2,000 hours.
Dimensions and Capacities
The aircraft has a length of 26 feet, a height of 8 feet 9 inches, and a wingspan of 38 feet 4 inches. The cabin dimensions are 10 feet 10 inches in length, 4 feet 1 inch in width, and 4 feet 2 inches in height. The empty weight is 2,330 pounds, with a useful load of 1,070 pounds and a maximum gross weight of 3,400 pounds.
Performance
The SR22T has a takeoff distance of 1,028 feet for ground roll and 1,594 feet over a 50-foot obstacle. The maximum demonstrated crosswind component is 24 knots, with a rate of climb at sea level of 1,400 feet per minute. The maximum level speed at 25,000 feet is 219 knots.
Airspeeds
Key airspeeds include V X (best angle of climb) at 80 KIAS, V Y (best rate of climb) at 100 KIAS, and V A (design maneuvering) at 133 KIAS. The maximum flap extended speed (V FE) is 104 KIAS, and the never exceed speed (V NE) is 204 KIAS.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- All specifications are based on manufacturer’s calculations. Performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
Cirrus SR22 G3 GTS Turbo Specifications Powerplant Tornado Alley turbonormalized TCM IO-550-N, 310 hp @ 2,700 rpm Recommended TBO 2,000 hr Propeller(s) Hartzell ASC propeller, 3-blade Length 26 ft Height 8 ft 9 in Wingspan 38 ft 4 in Wing area 144.9 sq ft Wing loading 23.46 lb/sq ft Power loading 10.96 lb/hp Seats 4 Cabin length 10 ft 10 in Cabin width 4 ft 1 in Cabin height 4 ft 2 in Empty weight 2,330 lb Useful load 1,070 lb Payload w/full fuel 518 lb Max Gross weight 3,400 lb Fuel capacity, std 92 gal usable, 552 lb usable Oil capacity 8 qt Baggage capacity 130 lb Performance Takeoff distance, ground roll 1,028 ft Takeoff distance over 50-ft obstacle 1,594 ft Max demonstrated crosswind component 24 kt Rate of climb, sea level 1,400 fpm Max level speed, 25,000 ft 219 kt Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption) @ 86% power, best power and 5,500 feet 176 KTAS/4 hr/716 nm (17.5 gph) @ 75% power and 25,000 feet 211 KTAS/3.9 hr/823 nm (17.5 gph) @ 55% power and 25,000 feet 180 KTAS/5.5 hr/1,000 nm (11.8 gph) Max operating altitude 25,000 ft Landing distance over 50-ft obstacle 2,344 ft Landing distance, ground roll 1,141 ft Limiting and Recommended Airspeeds V X (best angle of climb) 80 KIAS V Y (best rate of climb) 100 KIAS V A (design maneuvering) @ 3,400 lb 133 KIAS V FE (max flap extended) 104 KIAS V NO (max structural cruising) 178 KIAS V NE (never exceed) 204 KIAS V R (rotation) 73 KIAS V S1 (stall, clean) 66 KIAS V SO (stall, in landing configuration) 61 KIAS V PD (maximum parachute deployment speed) 133 KIAS All specifications are based on manufacturer’s calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.