- Registered owner
- Lot-A-Go Six LLC
- Location
- Polson, MT
- Owner type
- LLC
- Serial number
- 425-0226
- Year built
- 1985
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- February 11, 1985
- Certificate issued
- May 1, 2023
- Expires
- May 31, 2030
- Mode S code
- A030DE
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1980 | 1 |
|---|---|
| 1984 | 2 |
| 1986 | 1 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 3 |
| 2001 | 2 |
| 2002 | 1 |
| 2005 | 3 |
| 2012 | 1 |
| 2014 | 1 |
| 2018 | 2 |
| 2023 | 1 |
See all 22 ADs
Information bulletins that may apply · 9
Advisory, not mandatory.
Airframe · Cessna 425
SAIB CE-13-27R1Flight Controls Frayed Flap Extend CablesSAIB AIR-21-20TE FLAP CONTROL SYSTEM, Flight Controls –Flap Cable TensionSAIB CE-14-11R1Landing Gear; Nose Landing Gear TrunnionsSAIB CE-13-22Electrical Power System Circuit Breaker SwitchSAIB CE-13-09Doors: Cargo/Baggage DoorSAIB CE-10-01Fuel: Fuel Tank Selector Valve SystemsSAIB CE-06-46R1SAIB ACE-99-05Engine · Pratt & Whitney Canada PT6A-112
SAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N111KUMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 425 aircraft
FAA incident reports
No FAA accident or incident reports matched to N111KUMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 425 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UVVR2010060900013Skin · corroded(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.SDR UVVR2010060900012Skin · corroded(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.SDR UVVR2010060800011Fork · cracked((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.SDR UVVR2010060700010Fitting · crackedRT ENGINE OTBD ENGINE MOUNT FITTING WAS FOUND CRACKED APPROX .20 INCHES IN LENGTH DURING INSPECTION.SDR UVVR2010060700009Fitting · crackedRT ENGINE INBD ENGINE MOUNT FITTING WAS FOUND CRACKED APPROX .30 INCHES IN LENGTH DURING INSPECTION.SDR UVVR2010060200008Skin · corroded((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 TOG
STCs that may be installed · 171
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 425
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller