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Piper PA-28 for sale

Used Piper PA-28 from dealers in Europe — one page for the whole family: Cherokee, Warrior, Archer and Arrow, 150 to 200 hp. All data from the official type certificates (FAA 2A13, EASA IM.A.234). Calculate ferry flight and engine reserve right on this page.

Piper PA-28 for sale

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Variants

VariantEnginePowerMax. take-off weightSeatsFuelSource
PA-28-140Lycoming O-320-E2A / -E3D150 hpNormal 2.150 lb / Utility 1.950 lb4 / Utility 250 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. VIII
PA-28-161 Warrior IILycoming O-320-D3G / -D2A160 hpNormal 2.325 lb / Utility 2.020 lb4 / Utility 250 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XVI-A
PA-28-161 Warrior II/III (spätere S/N)Lycoming O-320-D3G160 hpTakeoff 2.440 lb, Ramp 2.447 lb / Utility 2.020 lb4 / Utility 250 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XVI-B/C
PA-28-180 CherokeeLycoming O-360-A3A / -A4A180 hpNormal 2.400 lb / Utility 1.950 lb4 / Utility 250 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. III
PA-28-180 ArcherLycoming O-360-A4A / -A4M180 hpNormal 2.450 lb / Utility 1.950 lb4 / Utility 250 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XII
PA-28-181 Archer IILycoming O-360-A4M / -A4AS/N 28-7690001–28-7990589: 180 hp; spätere S/N: Start 180 hp (5 min), Dauer 178 hpTakeoff 2.550 lb / Utility 2.130 lb4 / Utility 250 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XV-A
PA-28-181 Archer IIILycoming O-360-A4M / IO-360-B4A180 HPNormal 1.157 kg (2.550 lb) / Utility 967 kg (2.130 lb)„Max. Passenger Seating Capacity“: Normal 3; mit G3X-Avionik 2 (Notes 7/10); Utility 1189 l (50 gal) gesamt / 182 l (48 gal) nutzbarEASA TCDS IM.A.234 Iss. 8 (09.04.2026), Sec. A · EASA TCDS IM.A.234 Iss. 8, A.III
PA-28R-180 ArrowLycoming IO-360-B1E180 hp2.500 lb450 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. IX
PA-28R-200 ArrowLycoming IO-360-C1C200 hp2.600 lb450 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. X
PA-28R-200 Arrow IILycoming IO-360-C1C (NOTE 22) / IO-360-C1C6 (NOTE 23)200 hp @ 2700 rpm2.650 lb450 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XI, S. 15
PA-28R-201 Arrow IIILycoming IO-360-C1C6200 hp2.750 lb477 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XVII
PA-28R-201T Turbo Arrow IIIContinental TSIO-360-F / -FB200 hpTakeoff 2.900 lb, Ramp 2.912 lb477 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XVIII
PA-28RT-201 / -201T Arrow IVLycoming IO-360-C1C6 / Continental TSIO-360-FB200 hp; XX-B (spätere S/N): Start 200 hp (5 min), Dauer 196 hp2.750 lb / 2.900 lb477 galFAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XX/XXI
PA-28-140
Engine
Lycoming O-320-E2A / -E3D
Power
150 hp
Max. take-off weight
Normal 2.150 lb / Utility 1.950 lb
Seats
4 / Utility 2
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. VIII
PA-28-161 Warrior II
Engine
Lycoming O-320-D3G / -D2A
Power
160 hp
Max. take-off weight
Normal 2.325 lb / Utility 2.020 lb
Seats
4 / Utility 2
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XVI-A
PA-28-161 Warrior II/III (spätere S/N)
Engine
Lycoming O-320-D3G
Power
160 hp
Max. take-off weight
Takeoff 2.440 lb, Ramp 2.447 lb / Utility 2.020 lb
Seats
4 / Utility 2
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XVI-B/C
PA-28-180 Cherokee
Engine
Lycoming O-360-A3A / -A4A
Power
180 hp
Max. take-off weight
Normal 2.400 lb / Utility 1.950 lb
Seats
4 / Utility 2
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. III
PA-28-180 Archer
Engine
Lycoming O-360-A4A / -A4M
Power
180 hp
Max. take-off weight
Normal 2.450 lb / Utility 1.950 lb
Seats
4 / Utility 2
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XII
PA-28-181 Archer II
Engine
Lycoming O-360-A4M / -A4A
Power
S/N 28-7690001–28-7990589: 180 hp; spätere S/N: Start 180 hp (5 min), Dauer 178 hp
Max. take-off weight
Takeoff 2.550 lb / Utility 2.130 lb
Seats
4 / Utility 2
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XV-A
PA-28-181 Archer III
Engine
Lycoming O-360-A4M / IO-360-B4A
Power
180 HP
Max. take-off weight
Normal 1.157 kg (2.550 lb) / Utility 967 kg (2.130 lb)
Seats
„Max. Passenger Seating Capacity“: Normal 3; mit G3X-Avionik 2 (Notes 7/10); Utility 1
Fuel
189 l (50 gal) gesamt / 182 l (48 gal) nutzbar
Source: EASA TCDS IM.A.234 Iss. 8 (09.04.2026), Sec. A · EASA TCDS IM.A.234 Iss. 8, A.III
PA-28R-180 Arrow
Engine
Lycoming IO-360-B1E
Power
180 hp
Max. take-off weight
2.500 lb
Seats
4
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. IX
PA-28R-200 Arrow
Engine
Lycoming IO-360-C1C
Power
200 hp
Max. take-off weight
2.600 lb
Seats
4
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. X
PA-28R-200 Arrow II
Engine
Lycoming IO-360-C1C (NOTE 22) / IO-360-C1C6 (NOTE 23)
Power
200 hp @ 2700 rpm
Max. take-off weight
2.650 lb
Seats
4
Fuel
50 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XI, S. 15
PA-28R-201 Arrow III
Engine
Lycoming IO-360-C1C6
Power
200 hp
Max. take-off weight
2.750 lb
Seats
4
Fuel
77 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XVII
PA-28R-201T Turbo Arrow III
Engine
Continental TSIO-360-F / -FB
Power
200 hp
Max. take-off weight
Takeoff 2.900 lb, Ramp 2.912 lb
Seats
4
Fuel
77 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XVIII
PA-28RT-201 / -201T Arrow IV
Engine
Lycoming IO-360-C1C6 / Continental TSIO-360-FB
Power
200 hp; XX-B (spätere S/N): Start 200 hp (5 min), Dauer 196 hp
Max. take-off weight
2.750 lb / 2.900 lb
Seats
4
Fuel
77 gal
Source: FAA TCDS 2A13 Rev. 66 (10.10.2025), Abschn. XX/XXI

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

Type certificate data: FAA TCDS 2A13 Rev. 66 (10.10.2025) · EASA TCDS IM.A.234 Iss. 8 (09.04.2026) · As of 2026-10-19
PA-28-140 — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28-161 Warrior II — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28-161 Warrior II/III (spätere S/N) — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28-180 Cherokee — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28-180 Archer — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28-181 Archer II — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28-181 Archer III — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28R-180 Arrow — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28R-200 Arrow — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28R-200 Arrow II — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28R-201 Arrow III — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28R-201T Turbo Arrow III — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
PA-28RT-201 / -201T Arrow IV — 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

What is the difference between Cherokee, Warrior, Archer and Arrow?

All belong to the PA-28 family. Cherokee (PA-28-140/-180): 150–180 hp. Warrior (PA-28-161): 160 hp. Archer (PA-28-180/-181): 180 hp. Arrow (PA-28R/RT): 180–200 hp; Turbo Arrow with Continental TSIO-360 (FAA TCDS 2A13 Rev. 66).

What is the maximum take-off weight across the PA-28 family?

From 2,150 lb (PA-28-140 normal) up to 2,900 lb (Turbo Arrow III/IV takeoff); Archer III per EASA normal 1,157 kg (2,550 lb) — see the table for each variant with its source.

How much fuel does a Piper Arrow carry?

Arrow and Arrow II: 50 gal; Arrow III, Turbo Arrow III and Arrow IV: 77 gal (FAA TCDS 2A13).

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