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Aircraft record

N838PC1981 Piper PA-44-180T

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:1 NTSB accident (minor damage, Jun 2000)4 ADs may apply3 service difficulty reports

Registration
Valid
expires Nov 30, 2027
Based in
Fresno, CA
owner city / state
Engine
T0-360 SER · 210 hp
Lycoming
Owners
1
since 2020
NTSB events
1
minor, 2000
ADs may apply
4
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Gadamic LLC
Owner type
LLC
City, state
Fresno, CA
Certificate issued
Nov 16, 2020
Expires
Nov 30, 2027
Airworthiness
Standard · Normal
Airworthiness date
Aug 4, 1995

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Piper
Model
PA-44-180T
Year
1981
Serial number
448107056
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
AB775A

Engine

Make and model
Lycoming T0-360 Ser
Type
Reciprocating
Power
210 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2020 – nowGadamic LLCFresno, CA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · minor damage

Jun 12, 2000 · Englewood, CO

Failure of the instructor pilot-in-command and the pilot receiving instruction to maintain directional control. Factors were the pilot receiving instruction allowing the airplane to approach low and slow, and failure of the instructor to maintain adequate supervision of the flight.

Damage
Minor
Injuries
None
Report
DEN00LA108

From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN00LA108)

Accident history for this model

ADs published since 1998 that may apply (4)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2015-26-08Rudder Control SystemJan 20, 2016Airframe (PA-44-180T)Certain serial numbers: PA-44-180 44-7995001–44-8195026; PA-44-180 4495001–4496377; PA-44-180 4496379; PA-44-180 4496380; PA-44-180 4496384–4496386; PA-44-180T 44-8107001–44-8207020
2013-02-13Stabilizer Control SystemMar 11, 2013Airframe (PA-44-180T)
2010-15-10Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series AirplanesAug 31, 2010Airframe (PA-44-180T)Certain serial numbers: PA-28-140 28-20001–28-26946; PA-28-140 28-7125001–28-7725290; PA-28-150 28-03; PA-28-150 28-1–28-4377; PA-28-150 28-1760A; PA-28-160 28-03; …
2005-15-10The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T…Aug 26, 2005Airframe (PA-44-180T)Certain serial numbers: PA-34-200T 34-7570002–34-8170092; PA-34-220T 34-8133002–3449278; PA-44-180 44-7995001–4496168; PA-44-180T 44-8107001–44-8207020; PA-34-220T 3449279–3449309; PA-44-180 4496169–4496190. Only with: Equipped with a model 91E92-1 or 91E93-1 aircraft heater fuel pump.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (3)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Landing gear · strut · brokenApr 22, 2006

    LT GEAR STRUT BROKE AT HOUSING.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · strut · brokenApr 22, 2006

    LH MLG STRUT BROKE ON TAXI

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · hub · corrodedOct 9, 1996

    AFTER CLEANING OF HUB AND NDT, HUB WAS CORRODED BADLY ON THE INSIDE OF THE HUB ONLY. THE CAUSE OF THIS IS THE USE OF NON-APPROVED AUTO GREASE. SUBMITTER STATED IF THIS WAS NOT FOUND, IT IS POSSIBLE A CRACK AND FAILURE OF THE HUB WOULD OCCUR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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