- Registered owner
- Florida Institute Of Technology
- Location
- Melbourne, FL
- Owner type
- Corporation
- Serial number
- 2843706
- Year built
- 2013
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- April 26, 2013
- Certificate issued
- April 21, 2014
- Expires
- April 30, 2030
- Mode S code
- A87C14
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 53
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 |
|---|---|
| 1967 | 1 |
| 1969 | 1 |
| 1977 | 3 |
| 1979 | 3 |
| 1980 | 4 |
| 1981 | 1 |
| 1982 | 1 |
| 1986 | 2 |
| 1989 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 2 |
| 2012 | 2 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 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 · 22
Advisory, not mandatory.
See all 24 bulletins
NTSB investigations
No NTSB investigations matched to N646FTMatched 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 N646FTMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ECQS2014082200491Alternator · failedALTERNATOR FAILED WHEN THROTTLE WAS DECREASED TO APPROXIMATELY 1600 RPM, THE ALTERNATOR FAIL CAS ILLUMINATED AND ALTERNATOR OUTPUT WENT TO ZERO. THE PROCESS COULD BE DUPLICATED CONSISTENTLY.SDR ECQS2014FA0000227Seal · failedAIRCRAFT WAS WRITTEN UP FOR POWER LOSS. RIGHT MAGNETO WAS PULLED WITH TACH TIME AT 695.3, TT ON RT MAGNETO. DOT TO OIL SEAL FAILING AND OIL LEAKING PAST AND GETTING INTO MAGNETO RESULTING INTO OIL GETTING ONTO POINTS WITH POWER LOSS.
STCs that may be installed · 371
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