Cessna 206H Stationair (1998-present) vs Piper Cherokee Six 300 (1966-1979)

Head-to-head — specs, at a glance.

Cessna 206H Stationair (1998-present)
Cessna 206H Stationair (1998-present)
Piper Cherokee Six 300 (1966-1979)
Seats
6 · 6
Engine
piston single · piston single
Gear
Fixed · Fixed
Cessna 206H Stationair (1998-present)Piper Cherokee Six 300 (1966-1979)
Cruise speedKTAS
142
146
Stall speed (Vs0)lower is betterKIAS
54
47
Rangenm
720
830
Useful loadlbs
1,360
1,607
Full-fuel payloadlbs
808
1,103
Service ceilingft
15.7k
16.3k
Fuel burnlower is bettergph
14.5
16
Cruise MPGmpg
11.3
10.5
Typical pricelower is betterUSD
$450k
$160k

Cessna 206H Stationair (1998-present)

The 1998 Cessna 206H marked the **return of the Stationair to production** after the 1986-1997 litigation gap. The 206H carried forward the U206G airframe (3,600 lb gross, double cargo door, fixed gear, 6 seats) but swapped the Continental IO-520 for a **Lycoming IO-540-AC1A5** -- the same 300 HP fuel-injected Lycoming used in the 182S Skylane.

  • +Still in active production with 2,000+ delivered; strong factory support
  • +Lycoming IO-540 engine more reliable than predecessor Continental IO-520
  • +G1000 NXi models (2014+) offer modern WAAS/VNAV/ADS-B capability
  • !Useful load reduced 240 lbs vs U206G due to heavier engine and avionics
  • !Early steam-gauge models (1998–2004) lack glass cockpit and modern autopilot integration
  • !G1000 and GFC 700 systems require specialized repair support
See the full 206H profile →

Piper Cherokee Six 300 (1966-1979)

The PA-32-300 Cherokee Six is a six-seat, fixed-gear, low-wing single built from 1966 to 1979 — a stretched, widened Cherokee with a 300 hp fuel-injected Lycoming IO-540 on the nose and a 3,400 lb gross weight. It is the airplane that earned the Cherokee Six its reputation as the "poor man's Bonanza": a genuinely large cabin, an optional double cargo door, and a useful load over 1,600 lb, at a fraction of a Beechcraft A36's price.

  • +Six-seat cabin with 1,600+ lb useful load
  • +Proven, widely-supported Lycoming IO-540 engine
  • +Fixed gear and simple construction mean lower maintenance complexity
  • !Wing spar life limits and inspection requirements dominate valuation
  • !16 GPH fuel burn limits economics for frequent flying
  • !Low-wing design restricts backcountry visibility and ground clearance
See the full PA-32-300 profile →

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