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Diamond DA40 for sale

Used Diamond DA40 from dealers in Europe: DA 40 with Lycoming IO-360, DA 40 D with TAE 125, DA 40 NG with Austro E4 (both Jet A-1) — each 1 pilot + 3 passengers. All data from the official type certificate (EASA IM.A.022 Iss. 24). Calculate ferry flight and engine reserve right on this page.

Diamond DA40 for sale

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Variants

VariantEnginePowerMax. take-off weightSeatsFuelSource
DA 40Lycoming IO-360 M1Anot yet verifiedUtility 980 kg; Normal 1.150 kg oder 1.200 kg (Note 11)1 Crew + 3 Passagiere156 l / 152,2 l nutzbar; Langstrecke 193 l / 189,2 lEASA TCDS IM.A.022 Iss. 24 (22.04.2021), A.III
DA 40 DTAE 125-01 / 125-02-99not yet verifiedUtility 980 kg; Normal 1.150 kg1 + 3113,6 l / 106,0 l nutzbar; Langstrecke 155,2 l / 147,6 lEASA TCDS IM.A.022 Iss. 24 (22.04.2021), B.III
DA 40 NGAustro Engine E4 (E4-A)not yet verified1.280 kg; mit MÄM 40-662: 1.310 kg1 + 3113,6 l / 106,0 l nutzbar; Langstrecke 155,2 l / 147,6 lEASA TCDS IM.A.022 Iss. 24 (22.04.2021), D.III
DA 40
Engine
Lycoming IO-360 M1A
Power
not yet verified
Max. take-off weight
Utility 980 kg; Normal 1.150 kg oder 1.200 kg (Note 11)
Seats
1 Crew + 3 Passagiere
Fuel
156 l / 152,2 l nutzbar; Langstrecke 193 l / 189,2 l
Source: EASA TCDS IM.A.022 Iss. 24 (22.04.2021), A.III
DA 40 D
Engine
TAE 125-01 / 125-02-99
Power
not yet verified
Max. take-off weight
Utility 980 kg; Normal 1.150 kg
Seats
1 + 3
Fuel
113,6 l / 106,0 l nutzbar; Langstrecke 155,2 l / 147,6 l
Source: EASA TCDS IM.A.022 Iss. 24 (22.04.2021), B.III
DA 40 NG
Engine
Austro Engine E4 (E4-A)
Power
not yet verified
Max. take-off weight
1.280 kg; mit MÄM 40-662: 1.310 kg
Seats
1 + 3
Fuel
113,6 l / 106,0 l nutzbar; Langstrecke 155,2 l / 147,6 l
Source: EASA TCDS IM.A.022 Iss. 24 (22.04.2021), D.III

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 IM.A.022 Iss. 24 (22.04.2021) · As of 2026-10-19
DA 40 — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
DA 40 D — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
DA 40 NG — 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 do the DA40 variants have?

DA 40: Lycoming IO-360 M1A (avgas), DA 40 D: TAE 125-01 or 125-02-99 (Jet A-1 piston), DA 40 NG: Austro Engine E4 (Jet A-1 piston) — EASA TCDS IM.A.022 Iss. 24. The TCDS does not state a power figure, so we do not show one.

What is the maximum take-off weight of the DA40 NG?

1,280 kg; with modification MÄM 40-662 1,310 kg (EASA TCDS IM.A.022 Iss. 24, D.III).

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