- Registered owner
- Wisconsin Aviation Four Lakes Inc
- Location
- Madison, WI
- Owner type
- Corporation
- Serial number
- 2843207
- Year built
- 1999
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- January 19, 1999
- Certificate issued
- November 22, 2016
- Expires
- November 30, 2029
- Mode S code
- A4E5A9
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 30
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1977 | 2 |
|---|---|
| 1979 | 3 |
| 1980 | 3 |
| 1986 | 2 |
| 1989 | 1 |
| 1996 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 2 |
| 2008 | 2 |
| 2009 | 1 |
| 2010 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 2024 | 2 |
Airframe · Piper PA-28-181
AD 2024-14-03Autopilot SystemAD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 17
Advisory, not mandatory.
See all 18 bulletins
NTSB investigations
No NTSB investigations matched to N4142QMatched 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 Piper PA-28-181 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2003FA0000953Oil Cooler · crackedDURING PREFLIGHT INSPECTION PILOT FOUND SIGNS OF AN OIL LEAK. THE MAINTENANCE TECHNICIAN FOUND OIL LEAK ON OIL COOLER. PERFORMED PRESSURE CHECK ON OIL COOLER AND FOUND BOTTOM FLANGE CRACKED. THIS IS A WEAK ARA ON THE OIL COOLER. RECOMMEND FINDING A REPLACESDR 2003FA0000955Oil Cooler · crackedDURING A MAINTENANCE INSPECTION OF THIS AIRCRAFT, THE OIL COOLER WAS FOUND TO BE CRACKED AROUND THE MOUNTING BOLT HOLES AND LEAKING FROM THE SEAM IN THAT AREA. PROBABLE CAUSE IS VIBRATION. RECOMMEND USING A SOLID PIECE OIL COOLER.SDR 2003FA0000766Oil Cooler · crackedFOUND OIL LEAK DURING 50 HOUR INSPECTION. FOUND COOLER TO BE CRACKED. RECOMMEND CHANGING TO A SOLID CAN COOLER.SDR 2003FA0000729Oil Cooler · crackedFOUND OIL LEAK DURING PREFLIGHT BY STUDENT PILOT. PRESSURE CHECKED OIL COOLER AND FOUND OIL LEAK AT TOP SEAM. THIS IS A WEAK AREA ON THE COOLER. MAY BE CAUSED BY VIBRATION OR IMPROPER INSTALLATION METHODS. REPLACEMENT WITH BETTER COOLER.SDR 20010227CW003Control Cable · frayedAILERON BALANCE CABLE FRAYED ABOUT 8 INCHES FROM TURN BUCKLE, NEW CABLE INSTALLED.SDR 20010227CW002Control Cable · frayedSTABILIZER CABLE FRAYED.SDR 20000925SH038Control Cable · frayedAILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)
STCs that may be installed · 333
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-28-181
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