Diamond DA42 Twin Star vs Piper PA-34-220T Seneca V

Head-to-head — specs, at a glance.

Diamond DA42 Twin Star
Diamond DA42 Twin Star
Piper PA-34-220T Seneca V
Seats
4 · 6
Engine
piston twin · piston twin
Gear
Retract · Retract
Diamond DA42 Twin StarPiper PA-34-220T Seneca V
Cruise speedKTAS
180
197
Stall speed (Vs0)lower is betterKIAS
59
61
Rangenm
1,100
700
Useful loadlbs
1,069
1,380
Full-fuel payloadlbs
729
642
Service ceilingft
18.0k
25.0k
Fuel burnlower is bettergph
10
26.4
Cruise MPGmpg
20.7
8.6
Typical pricelower is betterUSD
$420k
$280k

Diamond DA42 Twin Star

The Diamond DA42 Twin Star, introduced in 2004, is a revolutionary aircraft — the first certified twin to use diesel/jet fuel engines. Powered by two Austro Engine AE 300 turbodiesel engines (170HP each), the DA42 burns approximately 10 GPH total — less than many single-engine aircraft and roughly one-third of what a conventional piston twin like the Baron consumes.

  • +Exceptional fuel efficiency: 10 GPH total vs 30 GPH for comparable piston twins
  • +Twin-engine safety with positive single-engine climb performance
  • +Global multi-engine training standard with proven design
  • !Austro engine parts availability: 4-6 week lead times for common components
  • !Requires Austro-authorized service centers; not all A&P shops support diesel engines
  • !High engine overhaul cost ($70,000 total for both engines) despite low hourly operating cost
See the full DA42 profile →

Piper PA-34-220T Seneca V

The Piper PA-34 Seneca is a six-seat, twin-engine light aircraft that has been in production, in various forms, since 1971. Developed as a twin-engine derivative of the Piper Cherokee Six, the PA-34 was first certified on 7 May 1971 and introduced as a 1972 model year aircraft. With over 5,000 airframes built through 2019 and licensed production in Brazil (Embraer EMB-810) and Poland (PZL M-20 Mewa), the Seneca is one of the most successful piston twins ever produced.

  • +Counter-rotating engines eliminate critical-engine handling; ideal multi-engine trainer
  • +Spacious six-seat cabin with aft cargo door; practical business transport
  • +Turbocharged variants cruise 188–195 knots at altitude with 700 nm IFR range
  • !Twin-engine operating costs ($35k–$45k annually at 100 hours); uneconomical for local flying
  • !Nose gear collapse risk from bolt fatigue and rigging neglect; repetitive AD inspection burden
  • !TSIO-360 top-end distress common if lean-of-peak operation poorly monitored; compression checks essential
See the full PA-34 profile →

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