- Registered owner
- Wdf Montana LLC
- Location
- Kalispell, MT
- Owner type
- LLC
- Serial number
- 41772
- Year built
- 2007
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- July 28, 2007
- Certificate issued
- April 18, 2023
- Expires
- April 30, 2030
- Mode S code
- A0F94F
Columbia Aircraft Mfg LC41-550FGTCDS A00003SEAirframe · Columbia Aircraft Mfg LC41-550FGTCDS E5SOEngine · Continental TSIO-550-C
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 24
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1993 | 1 |
|---|---|
| 1996 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 4 |
| 2009 | 2 |
| 2010 | 1 |
| 2011 | 2 |
| 2012 | 1 |
| 2013 | 1 |
| 2016 | 2 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 5 |
Airframe · Columbia Aircraft Mfg LC41-550FG
AD 2023-09-09Exhaust Turbine System (Recip)AD 2023-10-02Indicating/Recording System, NavigationAD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 11
Advisory, not mandatory.
Airframe · Columbia Aircraft Mfg LC41-550FG
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-09-12Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 InstallationsEngine · Continental TSIO-550-C
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-18-16POWERPLANT Alternator Drive CouplingSAIB NE-17-11POWERPLANT Engine damage as a result of kickbackSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-08Reciprocating Engine Cylinder SectionSAIB NE-02-41NTSB investigations
No NTSB investigations matched to N162CAMatched 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 Columbia Aircraft Mfg LC41-550FG aircraft
FAA incident reports
No FAA accident or incident reports matched to N162CAMatched 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 Columbia Aircraft Mfg LC41-550FG aircraft
Service difficulty reports
No reports matched to N162CAGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Columbia Aircraft Mfg LC41-550FG aircraft
Reports on N162CA not matched to an aircraft · 43
They name N162CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR SWIA200110068Switch · failedON TAXI, FLAPS SELECTED 15 DEGREES. FLAP INDICATOR GOES FROM 15 DEGREES TO 0 DEGREES EVERY MINUTE. GREEN BARS DISAPPEAR WHEN FLAPS ARE AT 0 DEGREES. THEY REAPPEAR AT FLAP 15. NO MAP INDICATION, JUST ONE CHIME ALERT. AS WE TAXIED BACK, ADVANCED SWS/FLAP ONSDR SWIA200110067Warning System · activatedABORTED TAKEOFF - TRIPLE CHIME - AURAL WARNING - BRAKES, FLAPS, AUTO FEATHER OCCURRED DURING TAKEOFF ROLL. REPLACED AND SECURED AURAL WARNING UNIT. PERFORMED OPS CHECK OF AUTO FEATHER SYSTEM. OPS CHECK GOOD. SN ON 0419 SN OFF 0224.SDR SWIA200110066Control Unit · failedDURING CRUISE, ASWS & FLAP LIGHTS ON MAP & ASYMMETRY DISSAGREEMENT, CONTROL FAULT LIGHTS ON OVERHEAD. PANEL FLAP INDICATOR FLUCTUATING 0 DEGREES - 45 DEGREES SEVERAL TIMES INTERMITTENTLY. INSTALLED SERVICEABLE FCU. OPS CHECK GOOD.
See all 43 unmatched reportsSTCs that may be installed · 88
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Columbia Aircraft Mfg LC41-550FG
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