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Extra 300 for sale

Used Extra 300 from dealers in Europe — the aerobatic type with Lycoming AEIO-540 or AEIO-580, 780 to 950 kg depending on variant and ACRO category. All data from the official type certificate (EASA A.362 Iss. 09). Calculate ferry flight and engine reserve right on this page.

Extra 300 for sale

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Variants

VariantEnginePowerMax. take-off weightSeatsFuelSource
EA 300Lycoming AEIO-540-L1B5 / -L1B5D224 kW / 300 BHPNormal 950 kg; ACRO I 820 kg; ACRO II 870 kg1 Pilot (hinten) + 1160 l / 158 l nutzbar; Langstrecke 194 l / 192 lEASA TCDS A.362 Iss. 09 (05.08.2026), A
EA 300/Swie EA 300: AEIO-540-L1B5 / -L1B5D224 kW / 300 BHPNormal 920 kg; Aerobatic 820 kg1 Pilot171 l / 169 l nutzbar; Langstrecke 205 l / 203 lEASA TCDS A.362 Iss. 09 (05.08.2026), B
EA 300/LAEIO-540-L1B5/-L1B5D oder AEIO-580-B1AAEIO-540: 224 kW / 300 BHP; AEIO-580: 235 kW / 315 BHP @ 2700 rpm, 226 kW / 303 BHP @ 2600 rpmNormal 950 kg; ACRO I 820 kg; II 870 kg; III 950 kg1 + 1171 l / 165,5 l; Langstrecke 205 l / 199,5 l; Raised 189 l / 187 lEASA TCDS A.362 Iss. 09 (05.08.2026), C
EA 300/LCLycoming AEIO-580-B1A235 kW / 315 BHP @ 2700 rpm; 226 kW / 303 BHP @ 2600 rpmwie /L: Normal 950 kg; ACRO I 820 kg; II 870 kg; III 950 kg1 + 1189 l / 187 l nutzbarEASA TCDS A.362 Iss. 09 (05.08.2026), G
EA 300/LTLycoming AEIO-580-B1A235 kW / 315 BHP @ 2700 rpm; 226 kW / 303 BHP @ 2600 rpmwie /L: Normal 950 kg; ACRO I 820 kg; II 870 kg; III 950 kg1 + 1221 l / 209 l nutzbarEASA TCDS A.362 Iss. 09 (05.08.2026), F
EA 300/SCLycoming AEIO-580-B1A235 kW / 315 BHP @ 2700 rpm; 226 kW / 303 BHP @ 2600 rpmNormal 870 kg; Aerobatic 780 kg1 Pilot224 l / 221 l nutzbarEASA TCDS A.362 Iss. 09 (05.08.2026), E
EA 300
Engine
Lycoming AEIO-540-L1B5 / -L1B5D
Power
224 kW / 300 BHP
Max. take-off weight
Normal 950 kg; ACRO I 820 kg; ACRO II 870 kg
Seats
1 Pilot (hinten) + 1
Fuel
160 l / 158 l nutzbar; Langstrecke 194 l / 192 l
Source: EASA TCDS A.362 Iss. 09 (05.08.2026), A
EA 300/S
Engine
wie EA 300: AEIO-540-L1B5 / -L1B5D
Power
224 kW / 300 BHP
Max. take-off weight
Normal 920 kg; Aerobatic 820 kg
Seats
1 Pilot
Fuel
171 l / 169 l nutzbar; Langstrecke 205 l / 203 l
Source: EASA TCDS A.362 Iss. 09 (05.08.2026), B
EA 300/L
Engine
AEIO-540-L1B5/-L1B5D oder AEIO-580-B1A
Power
AEIO-540: 224 kW / 300 BHP; AEIO-580: 235 kW / 315 BHP @ 2700 rpm, 226 kW / 303 BHP @ 2600 rpm
Max. take-off weight
Normal 950 kg; ACRO I 820 kg; II 870 kg; III 950 kg
Seats
1 + 1
Fuel
171 l / 165,5 l; Langstrecke 205 l / 199,5 l; Raised 189 l / 187 l
Source: EASA TCDS A.362 Iss. 09 (05.08.2026), C
EA 300/LC
Engine
Lycoming AEIO-580-B1A
Power
235 kW / 315 BHP @ 2700 rpm; 226 kW / 303 BHP @ 2600 rpm
Max. take-off weight
wie /L: Normal 950 kg; ACRO I 820 kg; II 870 kg; III 950 kg
Seats
1 + 1
Fuel
189 l / 187 l nutzbar
Source: EASA TCDS A.362 Iss. 09 (05.08.2026), G
EA 300/LT
Engine
Lycoming AEIO-580-B1A
Power
235 kW / 315 BHP @ 2700 rpm; 226 kW / 303 BHP @ 2600 rpm
Max. take-off weight
wie /L: Normal 950 kg; ACRO I 820 kg; II 870 kg; III 950 kg
Seats
1 + 1
Fuel
221 l / 209 l nutzbar
Source: EASA TCDS A.362 Iss. 09 (05.08.2026), F
EA 300/SC
Engine
Lycoming AEIO-580-B1A
Power
235 kW / 315 BHP @ 2700 rpm; 226 kW / 303 BHP @ 2600 rpm
Max. take-off weight
Normal 870 kg; Aerobatic 780 kg
Seats
1 Pilot
Fuel
224 l / 221 l nutzbar
Source: EASA TCDS A.362 Iss. 09 (05.08.2026), E

Values from the official type certificate only. Seat figures quoted verbatim; where several weights are certified, we show them all.

Type certificate data: EASA TCDS A.362 Iss. 09 (05.08.2026) · As of 2026-10-19
EA 300 — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
EA 300/S — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
EA 300/L — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
EA 300/LC — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
EA 300/LT — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
EA 300/SC — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)

Ferry flight

Distance
—
Flight time
—

Great circle between the two airfields. Not a substitute for flight planning. Airfield data: OurAirports (public domain), as of 2026-10-19

Engine reserve

TBO per the engine manufacturer's service document

Remaining to TBO
— h
Reserve per hour
— EUR

Calculation: overhaul cost ÷ TBO. Manufacturer calendar limits apply in addition.

Frequently asked questions

Which engines does the Extra 300 have?

EA 300 and /S: Lycoming AEIO-540-L1B5/-L1B5D (224 kW / 300 BHP); /L optionally also AEIO-580-B1A; /LC, /LT and /SC: AEIO-580-B1A (235 kW / 315 BHP @ 2700 rpm; 226 kW / 303 BHP @ 2600 rpm) — EASA TCDS A.362 Iss. 09.

Which take-off masses apply per aerobatic category?

EA 300 and /L e.g. normal 950 kg, ACRO I 820 kg, ACRO II 870 kg (plus ACRO III 950 kg on the /L); /S normal 920 kg / aerobatic 820 kg; /SC normal 870 kg / aerobatic 780 kg (EASA TCDS A.362 Iss. 09).

How many seats does the Extra 300 have?

EA 300, /L, /LC and /LT: two seats, pilot in the rear; /S and /SC are single-seat (EASA TCDS A.362 Iss. 09).

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