Ownership guide

Piper PA-32R-300

499 registered in the US, built from about 1975 to 1977, 7 seats, most with the Lycoming TIO-540. Its Airworthiness Directives, its engines', and what to check before buying one.

The fleet

Registered in the US
499
Built
1975 to 1977
Half built by
1976
Seats
7
Engine type
Piston
Most common engine
Lycoming TIO-540

Engines installed

From the FAA aircraft registry, rebuilt daily. Years are those recorded on each registration.

Airworthiness Directives

21 current ADs name the PA-32R-300 airframe, 3 with a repeat action. Its engines carry 65 more. 13 equipment ADs name the model.

Every AD for the Piper PA-32R-300

What gets reported

19 Service Difficulty Reports since 2016: a mechanic or operator files one when a part fails or is found defective.

Systems reported most

  1. Fuselage, Landing Gear Attach Fittings2
  2. Reciprocating Engine Power Section1
  3. Flight Control System1
  4. Tire Tube1
  5. Landing Gear Actuator1
  6. Fuselage Structure (General)1

Parts reported most

  1. Camshaft, galled1
  2. Control cable, cracked1
  3. Tube, failed1
  4. Casting, cracked1
  5. Landing gear, none1
  6. Trunnion, failed1

The latest reports

  • 2026-08-13 · Engine Fuel Distribution · Servo, faulted

    Pilot reported the fuel pressure pegged max pressure causing the gauge to become inop. it was replaced and again the gauge went to max & became inop, the fuel flow at full throttle now exceeds 30gph indicated where it used to be 28gph & all the cylinder head temperatures in climb are cold with the highest temperature being 320 degrees, leaned out in cruise, cht's would be around 280. after this fi

  • 2023-12-04 · Global Positioning System · Unknown, unknown

    During maintenance flight, after installation of garmin gi275's and gfc500, the owner smelled the distinct odor of hot wires but did not observe any smoke. he declared an emergency and returned to kbjc and to our ramp without incident. after two days of intense inspection i discovered that the instrument lighting wire that went to the now removed vacuum gauge had not been properly capped and sto

  • 2023-11-27 · Propeller Hub Section · Hub, leaking

    Propeller model b3d34c433-c , red dyed oil coming from blade hub, on cowling , wind screen and puddle on hanger floor. prop overhaul date 12/ 2018 t.t. 604 hrs, disassembled and resealed 3/2022 t.t. 900 hrs, leakage reappeared on 11/2023 t.t. 1150.0 hrs.

  • 2021-12-03 · Fuselage Structure (General) · Landing gear, none

    On 12/3/2021 on take-off roll, the nose landing gear suddenly retracted causing the aircraft to suffer a prop strike and other non-structural damage. the cause was believed to be a worn hydraulic actuator. repairs were undertaken and the aircraft returned to service. after only 5 hours on may 12, 2022, again while on take-off roll at approximately 65 knots ias the nose landing gear retracted once

From the FAA's Service Difficulty Reporting System, refreshed monthly. Counts of what was reported, not failure rates: most of general aviation reports voluntarily, and a busy training fleet reports more than a private one.

Accident record

51 accidents since 2008, 17 fatal (59 people killed in them, a midair counting both aircraft), 11 aircraft destroyed.

What happened

  1. Controlled flight into terrain or object (CFIT)7
  2. Loss of engine power (total)5
  3. Fuel starvation3
  4. Hard landing3
  5. Loss of control in flight3
  6. Powerplant sys/comp failure3

Phase of flight

  1. Enroute16
  2. Landing9
  3. Approach8
  4. Initial climb7
  5. Takeoff6

The latest

DateWhereWhat happenedInjuriesNTSB number
2026-08-21Thomaston, GALanding: Landing gear not configuredNoneERA26LA322
2026-05-22Comanche, TXInitial climb: Loss of engine power (total)NoneCEN26LA202
2025-09-23White plains, NYLanding: Landing area undershootNoneERA25LA363
2025-06-24Big lake, AKApproach: Fuel starvationSeriousANC25LA055
2024-06-12Selma, ALLanding: Hard landingNoneERA24LA259
2023-07-02North myrtle beach, SCInitial climb: Aerodynamic stall/spinFatalERA23FA280

From the NTSB's aviation accident database, refreshed monthly; accidents only, homebuilts left out. Counts, not rates: nobody publishes how many hours each model flies, and a training fleet flies far more than a private one. Look up any case by its number in the NTSB's CAROL.

What it costs to run

Per hour flown

Per year, flown or not

Fuel
$0/hr
Engine reserve
$0/hr
A year
$0
All in, per hour
$0/hr

Everything else is yours to fill in: insurance, hangar and overhaul prices vary too much by pilot, airport and shop for a default to mean anything. Nothing you type leaves this page.

Before you buy one

  1. Run its N-number through the AD check: every AD that names its airframe and engine, as a checklist to take to the logbooks.
  2. For each repeat-action AD (3 on the airframe), find the last compliance in the logbooks and when the next one is due.
  3. Compare the engine's time since overhaul with its maker's published overhaul time, and look for the reason behind any long gap in flying.
  4. Ask the mechanic doing the pre-buy to look hard at the fuselage, landing gear attach fittings and for galled camshafts: they are what gets reported most on this model.
  5. 13 equipment ADs name the PA-32R-300 (a muffler, a seat belt, a display): find out which of that equipment is installed.
  6. Check the registration, the airworthiness certificate and the date of the last annual inspection.
  7. Work out the sales or use tax your state will charge with the aircraft tax calculator.

The rest of the PA-32R family

Questions

How many Piper PA-32R-300s are registered in the US?
499, in the FAA aircraft registry.
When was the Piper PA-32R-300 built?
From about 1975 to 1977. Half of those registered today were built by 1976.
What engine does the Piper PA-32R-300 have?
Most have the Lycoming TIO-540 (62% of those registered); others have the Lycoming IO-540.
What are common problems with the Piper PA-32R-300?
In 19 Service Difficulty Reports filed with the FAA since 2016, the systems reported most were fuselage, landing gear attach fittings, reciprocating engine power section, flight control system, and the part most often reported was a galled camshaft.
How many accidents has the Piper PA-32R-300 had?
51 in the NTSB's database since 2008, 17 of them fatal. The most common defining event was controlled flight into terrain or object (cfit). These are counts, not rates: how many hours the fleet flew is not published.
How many Airworthiness Directives does the Piper PA-32R-300 have?
21 current ADs name the PA-32R-300 airframe, 3 of them with a repeat action, and 65 more name its engines. Whether each applies to one aircraft depends on its serial number and installed equipment.

Figures from the FAA aircraft registry and the FAA's Airworthiness Directives, rebuilt daily. An AD listed for a model is one to read; whether it applies to one aircraft depends on its serial number, equipment and records.

Piper PA-32R-300 Ownership Guide: Fleet, ADs and What to Check | AerScheduler