Piper Arrow vs Piper Turbo Arrow III (1977-1978)

Head-to-head — specs, at a glance.

Seats
4 · 4
Engine
piston single · piston single
Gear
Retract · Retract
Piper ArrowPiper Turbo Arrow III (1977-1978)
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 specifications on this page describe one airplane: the PA-28R-201 Arrow III, TCDS 2A13 Section XVII -- semi-tapered wing, conventional tail, normally aspirated Lycoming IO-360-C1C6, 2,750 lb.** The T-tail PA-28RT-201 Arrow IV is a different section of the same certificate with a different airspeed limit on every line, and the turbocharged PA-28R-201T is a different engine on its own page. Their figures are in the Variants table; do not read the frontmatter numbers onto them.

  • +THE complex endorsement trainer—proven, docile handling for gear/prop training
  • +Excellent parts availability and mechanic familiarity across the industry
  • +Strong cross-country platform: 695 nm range, 138 KTAS cruise, IFR capable
  • !Electro-hydraulic gear system is a chronic maintenance challenge and recurring expense
  • !Automatic gear extension (AGE) system prone to failures; many operators disable it
  • !Engine overhaul cost ($36k–$54k) is a major ownership consideration on high-time airframes
See the full PA-28R-201 profile →

Piper Turbo Arrow III (1977-1978)

**The specifications on this page describe one airplane: the PA-28R-201T Turbo Arrow III, TCDS 2A13 Section XVIII -- the conventional-tail turbocharged Arrow, S/N 28R-7703001 through 28R-7803373 and 2803001 through 2803012.** The T-tail PA-28RT-201T Turbo Arrow IV is Section XXI of the same certificate and carries a *different figure on every airspeed limit*; its numbers are in the Variants table below, and they are not the ones in this page's frontmatter.

  • +154 KTAS cruise at 75% power—compelling speed-for-cost against naturally aspirated Arrow III
  • +20,000 ft maximum operating altitude enables high-altitude cross-country flights
  • +Four-seat touring capability at turbocharged performance levels
  • !Continental TSIO-360 runs hot; cylinder life heavily dependent on pilot technique and cool-down discipline
  • !Shorter 1,800 hr TBO versus naturally aspirated Arrow's 2,000 hr
  • !Turbo exhausts crack more frequently than naturally aspirated; costlier system maintenance
See the full PA-28R-201T profile →

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