Cirrus SR20 for sale
Used Cirrus SR20 from dealers in Europe. Depending on build 200 hp (TCM IO-360-ES) or 215 hp (Lycoming IO-390-C3B6), up to 1,429 kg take-off weight from S/N 2339. All data from the official type certificate (EASA IM.A.007 Iss. 19). Calculate ferry flight and engine reserve right on this page.
Cirrus SR20 for sale
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Variants
| Variant | Engine | Power | Max. take-off weight | Seats | Fuel | Source |
|---|---|---|---|---|---|---|
| SR20 | TCM IO-360-ES / Lycoming IO-390-C3B6 | 200 hp @ 2700 rpm (IO-360-ES) / 215 hp @ 2700 rpm (IO-390-C3B6) | 1.315 kg (2.900 lb) S/N 1005–1147 ohne SB 20-01-00 · 1.361 kg (3.000 lb) S/N 1148–1877, 1879–1885 bzw. 1005–1147 mit SB · 1.383 kg (3.050 lb) S/N 1878, 1886 ff. mit IO-360-ES (Note 6) · 1.429 kg (3.150 lb) S/N 2339 ff. mit IO-390-C3B6 (Note 7) | „Maximum Passenger Seating Capacity“: 3 (S/N 1005–2126); 3+1 (S/N 2127 ff., Note 5: Belegungsgrenze 4+1 nach AFM 11934-004E); Mindestbesatzung 1 Pilot | 229,0 l (60,5 US gal) / 212,0 l nutzbar (S/N 1005–1877, 1879–1885); 221,4 l (58,5 US gal) / 212,0 l nutzbar (S/N 1878, 1886 ff.) | EASA TCDS IM.A.007 Iss. 19 (22.04.2026), A.III |
- Engine
- TCM IO-360-ES / Lycoming IO-390-C3B6
- Power
- 200 hp @ 2700 rpm (IO-360-ES) / 215 hp @ 2700 rpm (IO-390-C3B6)
- Max. take-off weight
- 1.315 kg (2.900 lb) S/N 1005–1147 ohne SB 20-01-00 · 1.361 kg (3.000 lb) S/N 1148–1877, 1879–1885 bzw. 1005–1147 mit SB · 1.383 kg (3.050 lb) S/N 1878, 1886 ff. mit IO-360-ES (Note 6) · 1.429 kg (3.150 lb) S/N 2339 ff. mit IO-390-C3B6 (Note 7)
- Seats
- „Maximum Passenger Seating Capacity“: 3 (S/N 1005–2126); 3+1 (S/N 2127 ff., Note 5: Belegungsgrenze 4+1 nach AFM 11934-004E); Mindestbesatzung 1 Pilot
- Fuel
- 229,0 l (60,5 US gal) / 212,0 l nutzbar (S/N 1005–1877, 1879–1885); 221,4 l (58,5 US gal) / 212,0 l nutzbar (S/N 1878, 1886 ff.)
Values from the official type certificate only. Seat figures quoted verbatim; where several weights are certified, we show them all.
Frequently asked questions
Which engines does the Cirrus SR20 have?
Depending on build the TCM IO-360-ES with 200 hp or the Lycoming IO-390-C3B6 with 215 hp (EASA TCDS IM.A.007 Iss. 19, A.III).
What is the maximum take-off weight of the SR20?
Per serial number: 1,315 kg (S/N 1005–1147 without SB 20-01-00), 1,361 kg (S/N 1148–1885 or with SB), 1,383 kg (S/N 1878, 1886 ff. with IO-360-ES), 1,429 kg (S/N 2339 ff. with IO-390-C3B6) — the certificate lists several certified weights, we show them all (EASA TCDS IM.A.007 Iss. 19).