- Registered owners
- University Of IllinoisBoard Of Trustees
- Location
- Savoy, IL
- Owner type
- Government
- Serial number
- 2844042
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Certificate issued
- April 12, 2001
- Expires
- January 31, 2030
- Mode S code
- A6BA69
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 | 1 |
|---|---|
| 1979 | 4 |
| 1980 | 3 |
| 1981 | 1 |
| 1982 | 1 |
| 1986 | 1 |
| 1989 | 1 |
| 1994 | 1 |
| 1996 | 2 |
| 1998 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 2024 | 2 |
Airframe · Piper PA-28R-201
AD 2024-14-03Autopilot SystemAD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 18
Advisory, not mandatory.
See all 19 bulletins
NTSB investigations
No NTSB investigations matched to N5321UMatched 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-28R-201 aircraft
FAA incident reports
No FAA accident or incident reports matched to N5321UMatched 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-28R-201 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2010FA0000009Tube · crackedINNER PORTION OF RUDDER HORN TUBE CRACKED AT WELD ASSY (PN 63546-000) ON UNDERSIDE OF WELD BEAD. AREA IN QUESTION EXHIBITED SIGNS OF EXCESSIVE WELD PENETRATION ALONG WITH PROJECTING GLOBULES. PROBABLE CAUSE OF CRACK OCCURRED DUE TO WEAKING OF METAL FROM IMPRSDR 2006FA0000328Shaft · shearedENGINE RUNUP INDICATED A DEAD MAGNETO. REMOVED AND DISASSEMBLED MAGNETO HOUSING. FOUND ROTOR SHAFT SHEARED OFF AT BOTTOM OF CAM SLOT. A FEW CRACKED SHAFTS HAVE BEEN FOUND AT 500 HR INSPECTIONS. RECOMMEND CLOSE INSPECTION OF THIS AREA AT REPAIR AND OVERHAULSDR UC22003F00000Attach Bracket · separatedDURING A TRAINING FLIGHT THE PILOT REPORTED THAT HE HEARD A LOUD BANG WHEN THE LANDING GEAR WAS RETRACTED. THE LANDING GEAR UNSAFE LIGHT THEN CAME ON. THE PILOT THEN EXTENDED THE GEAR AND MADE AN EMERGENCY LANDING. THE AIRPLANE WAS INSPECTED AND THE NOSE GESDR 2002FA0000684Bolt · failedDURING CLIMB OUT, THE PILOT HEARD A LOUD BANG. WHEN THE LANDING GEAR WAS RETRACTED, THE PILOT REPORTED THAT THE NOSE GEAR DOWN AND LOCKED LIGHT ILLUMINATED A FEW SECONDS LATER. THE LANDING GEAR WAS EXTENDED BY THE PILOT AND A SAFE LANDING WAS MADE. A POST
STCs that may be installed · 306
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-28R-201
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 N5321U before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.