- Registered owner
- Embry-Riddle Aeronautical University Inc
- Location
- Prescott, AZ
- Owner type
- Corporation
- Serial number
- 172S13308
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Certificate issued
- April 8, 2025
- Expires
- April 30, 2032
- Mode S code
- A6D860
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 36
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1971 | 2 |
| 1973 | 2 |
| 1974 | 2 |
| 1977 | 1 |
| 1979 | 1 |
| 1988 | 1 |
| 1991 | 1 |
| 1996 | 1 |
| 1998 | 2 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 4 |
| 2009 | 1 |
| 2011 | 1 |
| 2012 | 2 |
| 2013 | 2 |
| 2018 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 40 ADs
Information bulletins that may apply · 17
Advisory, not mandatory.
See all 21 bulletins
NTSB investigations
No NTSB investigations matched to N540ERMatched 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 Textron 172S aircraft
FAA incident reports
No FAA accident or incident reports matched to N540ERMatched 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 Textron 172S 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 2010FA0000988Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESSDR 2010FA0000987Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESSDR 2010FA0000986Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESSDR 201001094Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES
STCs that may be installed · 314
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Textron 172S
STC SA01233SEFabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assemblySTC 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.