Piper Arrow vs Piper Turbo Arrow III / Turbo Arrow IV (1977-1989)

Head-to-head — specs, at a glance.

Seats
4 · 4
Engine
piston single · piston single
Gear
Retract · Retract
Piper ArrowPiper Turbo Arrow III / Turbo Arrow IV (1977-1989)
Cruise speedKTAS
138
165
Stall speed (Vs0)lower is betterKIAS
55
55
Rangenm
695
880
Useful loadlbs
1,113
1,145
Full-fuel payloadlbs
681
683
Service ceilingft
16.2k
20.0k
Fuel burnlower is bettergph
11.6
12
Cruise MPGmpg
13.7
15.8
Typical pricelower is betterUSD
$115k
$130k

Piper Arrow

The Piper PA-28R Arrow is the retractable-gear member of the PA-28 Cherokee family, in continuous production since 1967 -- one of the longest production runs in general aviation history. With nearly 7,000 Arrows built across all variants, it is the most widely produced retractable-gear single-engine airplane ever made. The Arrow's primary role in general aviation is unmistakable: it is THE complex endorsement trainer, alongside the Cessna 172RG Cutlass and Mooney M20 series.

  • +Industry-standard complex trainer with exceptional parts availability
  • +Proven Cherokee platform delivers predictable handling and docile flight characteristics
  • +Retractable gear adds 15-18 knots cruise speed over fixed-gear comparable aircraft
  • !Electro-hydraulic gear system is maintenance-intensive and defines ownership costs
  • !Automatic gear extension system prone to nuisance extensions; many owners disable it
  • !Modest climb performance (831 fpm) limits high-altitude and hot-weather operations
See the full PA-28R-201 profile →

Piper Turbo Arrow III / Turbo Arrow IV (1977-1989)

The 1977-1989 Piper Turbo Arrow is the **turbocharged variant of the Arrow III / Arrow IV** -- the same tapered-wing airframe with a Continental TSIO-360 (replacing the NA Arrow's Lycoming IO-360) producing 200 HP through 20,000 ft. The Turbo Arrow targeted Cessna T210, Bonanza A36TC, and Mooney M20K buyers seeking high-altitude cross-country capability at sub-$200K acquisition cost.

  • +165 KTAS cruise at FL180 rivals Bonanza A36TC at lower acquisition cost
  • +20,000 ft service ceiling enables high-altitude cross-country flights
  • +4-seat configuration with 1,145 lbs useful load for modest loads
  • !Continental TSIO-360 runs hot; cylinder life highly dependent on pilot technique and cool-down discipline
  • !T-tail Arrow IV (1979-1989) has reduced pitch authority and stall recovery concerns vs. conventional tail
  • !Turbo exhaust system prone to cracking; requires frequent inspection of welds and slip joints
See the full PA-28R/RT-201T profile →

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