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Aircraft record

N111KU1985 Cessna 425

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply6 service difficulty reports

Registration
Valid
expires May 31, 2030
Based in
Polson, MT
owner city / state
Engine
PT6A-112 · 500 hp
P&W Canada
Owners
1
since 2023
NTSB events
None
since 1982
ADs may apply
5
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Lot-A-Go Six LLC
Owner type
LLC
City, state
Polson, MT
Certificate issued
May 1, 2023
Expires
May 31, 2030
Airworthiness
Standard · Normal
Airworthiness date
Feb 11, 1985

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
Cessna
Model
425
Year
1985
Serial number
425-0226
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
12
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A030DE

Engine

Make and model
P&W Canada Pt6a-112
Type
Turbo-prop
Power
500 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. 2023 – nowLot-A-Go Six LLCPolson, MT · 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 (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (5)

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
2012-09-10Pratt & Whitney Canada Turboprop EnginesMay 23, 2012Engine (PT6A-112)Only with: Engines with power section maintenance involving first stage sun gear or planet gear replacement since December 22, 2008, and with TAATI PMA first stage sun gears P/N E3028456 or E3037304, or planet gear sets P/N E3101455-02 or E3101525-02 installed.
2005-20-25The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411…Nov 9, 2005Airframe (425)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; …. Only with: Equipped with an avionics bus circuit breaker switch P/N CM3589-50, 593-250-101, 593-250-102, W31-X2M5A-50, or W31-X1000-50.
2002-23-13Pratt & Whitney Canada PT6A Series Turboprop EnginesDec 31, 2002Engine (PT6A-112)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed.
98-04-28Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414…Mar 13, 1998Airframe (425)
97-25-04Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 AirplanesJan 21, 1998Airframe (425)

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

Service Difficulty Reports (6)

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.

  • Fuselage · skin · corrodedJun 9, 2010

    (UVVR) EXTERIOR SIDE OF FUSELAGE BOTTOM SKINS CORRODED FS 307.94 - FS 316.94, BL2L TO BL3R. FOUND UPON REMOVAL OF STORMSCOPE ANTENNA, MM, ZONE 311 &N 312.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedJun 9, 2010

    (UVVR) EXTERIOR SIDE OF OF FUESELAGE, TOP SKIN CORRODED FS 200.75 TO FS 212.87, BL6R TO BL9.5R. FOUND UPON REMOVAL OF VHF COMMUNICATIONS ANTENNA, MM, ZONE 252.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · fitting · crackedJun 7, 2010

    RT ENGINE INBD ENGINE MOUNT FITTING WAS FOUND CRACKED APPROX .30 INCHES IN LENGTH DURING INSPECTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Power plant · fitting · crackedJun 7, 2010

    RT ENGINE OTBD ENGINE MOUNT FITTING WAS FOUND CRACKED APPROX .20 INCHES IN LENGTH DURING INSPECTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · fork · crackedJun 7, 2010

    ((UVVR)) WHILE PERFORMING SUPPLEMENTARY INSPECTION DOCUMENT NR 32-20-02 A .25" CRACK WAS FOUND IN THE RT AXLE BORE OF THE NLG FORK ASSY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · corrodedJun 2, 2010

    ((UVVR)) RT OTBD WING L/E SKIN CORRODED UNDER AERODYNAMIC FILLER AT SKIN SPLICE SEAM JUST OTBD OF NACELLE STRUCTURE. CORROSION IS AT LEVEL 3. IT APPEARS THAT MOISTURE HAS SEEPED UNDER DEICE BOOT AT SKIN SPLICE SEAM WHERE THE 2 SECTIONS OF L/E ARE SPLICED TOGETHER.

    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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