Single-engine piston

N555WM

1979 Piper Turbo Dakota

Registered 1 NTSB/FAA record
Built
1979
Serial
28-7921047
Class
Single-engine piston
Engines
Continental TSIO-360 series
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Raymore, MO
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Registration record

N555WM on the FAA register

Type
1979 Piper Turbo Dakota (FAA: Piper PA-28-201T)
Serial
28-7921047
Engines
Continental TSIO-360 series
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Raymore, MO
Certificate issued
2021-11-03
Airworthiness date
1979-09-19
Registration expires
2028-11-30
Airworthiness class
Standard · normal
Mode S (hex)
A713FE
Mode S (octal)
51611776
Seats (type)
4
Weight class
up to 12,499 lb
Range (type)
729 nm
Cruise (type)
156 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2028-11-30
    Registration expires (renewal due).
  • 2021-11-03
    Certificate of registration issued as N555WM to the current registrant.
  • 2017-12-19
    Accident at Versailles, MO; damage: substantial.
  • 1980-02-28
    N555WM previously assigned to a Cessna U206G Stationair / U206 Amphibian / 206 Turbine (s/n U20605309); cancelled.
  • 1979-09-19
    Airworthiness date on the current FAA record (standard category (normal)).
Overview

About N555WM

N555WM is a 1979 Piper Turbo Dakota (FAA model PA-28-201T), serial number 28-7921047. It is registered to an individual in Raymore, Missouri. The current certificate of registration was issued on November 3, 2021 and expires on November 30, 2028.

The FAA aircraft reference file describes the type as a single-engine piston, one Continental TSIO-360 series engine and 4 seats. Published figures for the type give a cruise speed of about 156 knots and a range of about 729 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (normal), dated September 19, 1979.

N555WM has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
156 kt
Range
729 nm
Power / thrust (each)
200
Takeoff over 50 ft
1,402 ft
Landing over 50 ft
1,697 ft
Fuel burn
12 gph

Published figures for the Piper Turbo Dakota type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2017-12-19 Accident · Versailles, MO Damage: Substantial NTSB · CEN18LA065
Reported aircraft: Piper PA-28-201T
Probable cause: The total loss of engine power due to fuel starvation when the cap fitting came off the inlet tee fitting on the throttle body/fuel metering unit.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Browse: Piper aircraft for sale· Aircraft registered in Missouri· Registry by state· FAA registry stats

Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.