- Registered owners
- Board Of TrusteesUniversity Of Illinois
- Location
- Savoy, IL
- Owner type
- Government
- Serial number
- 2843145
- Year built
- 1998
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- September 23, 2004
- Certificate issued
- September 8, 1998
- Expires
- April 30, 2028
- Mode S code
- A4E5EA
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O-360 model are included below.
On this page
Airworthiness directives that may apply · 70
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 1 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1977 | 4 |
| 1979 | 4 |
| 1980 | 6 |
| 1981 | 1 |
| 1982 | 1 |
| 1986 | 2 |
| 1988 | 1 |
| 1989 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 7 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 2024 | 3 |
| 2026 | 1 |
Airframe · Piper PA-28-181
AD 2024-14-03Autopilot SystemAD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 26
Advisory, not mandatory.
See all 35 bulletins
NTSB investigations
No NTSB investigations matched to N4144KMatched 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
No FAA accident or incident reports matched to N4144KMatched 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 Piper PA-28-181 aircraft
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UC2R20030001AClip · mismanufacturedNAVIGATION CONTROL OF NAV/COMM TOGGLED FREQUECY UNCOMMANDED, WHICH CAUSED LOSS OF OPERATION OF VOR/LOC DURING FLT. OPERATOR COMPLAINED THAT THIS CONDITION MADE NAV UNRELIABLE FOR USE. TRACED PROBLEM TO KHZ NAV FREQUENCY CONTROL VERY SUSCEPTIBLE TO TRIGGERINGSDR UC22002F00004Cotter Pin · failedDURING TRAINING FLIGHT, THE PILOTS RIGHT RUDDER PEDAL WAS REPORTED TO BE UNRESPONSIVE DURING FLIGHT. THE PILOT LANDED THE AIRPLANE WITHOUT AN INCIDENT. UPON INSPECTION OF THE PILOTS RIGHT RUDDER PEDAL AND THE TOE BRAKE ASSEMBLY THE CLEVIS ASSY WAS FOUND DISCSDR 2002FA0000275Control Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMULAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS, FAIRLEADS OR SDR 2002FA0000274Control Cable · wornDURING A ROUTNE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS, FAIR LEADS OR SDR 2002FA0000273Control Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS, FAIR LEADS OSDR 99ZZZX4206Valve · leakingPILOT REPORTED FUEL SMELL FROM CABIN DURING FLIGHT. AIRCRAFT WAS LOOKED AT BY MAINTENANCE AND THE FUEL SELECTOR WAS FOUND LEAKING FUEL. UPON FURTHER INVESTIATION, THE SNAP RING ON THE FUEL SELECTOR HANDLE SIDE OF THE UNIT WAS FOUND MISSING. THIS ALLOWED THESDR 98ZZZX4652Bushing · wornDURING A SCHEDULED INSPECTION OF THE CARBURETOR AIRBOX VALVE BUSHING AND GROMMET WERE FOUND COMPLETELY WORN THROUGH. THIS IS A RECURRING PROBLEM ON FLEET OF ARCHER 111'S. THESE BUSHINGS AND GROMMETS HAVE TO BE REPLACED EVERY 50 TO 100 HOURS OF OPERATION. SUSDR 98ZZZX4651Grommet · wornDURING A SCHEDULED INSPECTION OF THE CARBURETOR AIRBOX VALVE BUSHING AND GROMMET WERE FOUND COMPLETELY WORN THROUGH. THIS IS A RECURRING PROBLEM ON FLEET OF ARCHER 111'S. THESE BUSHINGS AND GROMMETS HAVE TO BE REPLACED EVERY 50 TO 100 HOURS OF OPERATION. SUSDR 99ZZZX288Grommet · wornDURING A 100-HOUR INSPECTION, CARBURETOR AIR BOX GROMMET ON THE CONTROL VALVE SHAFT WAS FOUND COMPLETELY WORN THROUGH AND STARTED TO ELONGATE THE HOLE IN THE TOP OF THE CARBURETOR AIR BOX IN WHICH THE GROMMET IS INSTALLED. FOUND THIS PROBLEM ON SEVERAL OTHER
STCs that may be installed · 383
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
Earlier aircraft with this N-number · 1
This aircraft carried N4144K before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.