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Aircraft record

N75HM1975 Piper PA-25-260

DeregisteredUnclaimedSource: FAA, updated Oct 16, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 2, 2020.

Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Aug 2006)7 ADs may apply

Registration
Deregistered
Last based in
Tucson, AZ
owner city / state
Engine
O-540-G1A5 · 260 hp
Lycoming
Owners
1
on record
NTSB events
2
substantial, 2006
ADs may apply
7
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 16, 2026
Last registered owner
Individual owner
City, state
Tucson, AZ
Canceled
Aug 2, 2020
Airworthiness
Restricted · Other
Airworthiness date
Dec 11, 2007

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-25-260
Year
1975
Serial number
257556182
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
1
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AA186B

Engine

Make and model
Lycoming O-540-G1a5
Type
Reciprocating
Power
260 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. until 2020Individual ownerTucson, AZ

Individual owners are shown by city and state only.

Safety record

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

NTSB events (2)

Accident · substantial damage

Aug 19, 2006 · North Plains, OR

The glider pilot's misjudgment of distance/speed during approach, which resulted in excessive speed at touchdown, and his failure to maintain directional control during the landing roll. A contributing factor was the glider pilot's lack of experience in the make and model of glider being flown.

Damage
Substantial
Injuries
Minor
Report
SEA06LA163

From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA06LA163)

Accident · substantial damage

Jul 17, 1998 · Leland, IL

Control interference between the pilot-in-command and the student. An excessive descent rate and inadequate flare by the student during landing are contributing factors. The inadequate supervision by the pilot-in-command is an additional factor.

Damage
Substantial
Injuries
None
Report
CHI98LA310

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI98LA310)

Accident history for this model

ADs published since 1998 that may apply (7)

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
2026-17-10Reciprocating Engine Cylinder SectionSep 14, 2026Engine (O-540-G1A5)Serial numbers per Table 2 or Table 3 of Lycoming Mandatory Service Bulletin No. 667A, dated March 12, 2026. Only with: Installed piston pin P/N LW-13445 with an OEM FAA Form 8130-3 production dated between January 7, 2021 and December 15, 2025, or where the production date cannot be determined or the form is unavailable.
2006-10-21Engine Components Incorporated (ECi) Reciprocating Engine Connecting RodsJun 22, 2006Engine (O-540-G1A5)Only with: ECi connecting rods P/N AEL11750 (forging P/N AEL11488) installed, rod serial numbers 54/6 and below, produced between January 2002 and January 2004.
2005-19-11Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360…Oct 21, 2005Engine (O-540-G1A5)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999.
2004-05-24Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and…Mar 30, 2004Engine (O-540-G1A5)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos.
99-26-05The New Piper Aircraft, Inc. Models PA- 25, PA-25-235, PA-25-260, PA-28S-160…Jan 13, 2000Airframe (PA-25-260)Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2); PA-28-151/161 only when STC SA2946SO is incorporated.
Show all 7 ADs
ADSubjectEffectiveApplies to
99-04-04Textron Lycoming Reciprocating Engines IO-540 and O-540 Engines Equipped With Slick…Feb 25, 1999Engine (O-540-G1A5)Only with: Equipped with Slick Aircraft Products magneto model numbers 6251, 6252, 6255, 6351 or 6355.
95-12-01Piper Aircraft Corporation PA-25 Series AirplanesJul 7, 1995Airframe (PA-25-260)

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

Service Difficulty Reports (0)

No Service Difficulty Reports found for this airframe since 1995.

Related aircraft

Show all 8 related aircraft
All 47 registered Piper PA-25-260 aircraft

Sources

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

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