- Registered owner
- Florida Institute Of Technology
- Location
- Melbourne, FL
- Owner type
- Corporation
- Serial number
- 2842315
- Year built
- 2008
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- September 3, 2008
- Certificate issued
- August 28, 2023
- Expires
- August 31, 2030
- Mode S code
- A85C03
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 50
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 1 |
|---|---|
| 1969 | 1 |
| 1977 | 2 |
| 1979 | 4 |
| 1980 | 3 |
| 1981 | 1 |
| 1982 | 2 |
| 1986 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 3 |
| 2000 | 2 |
| 2001 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-28-161
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2020-26-16Wing SparInformation bulletins that may apply · 22
Advisory, not mandatory.
See all 24 bulletins
NTSB investigations
No NTSB investigations matched to N638FTMatched 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-28-161 aircraft
FAA incident reports
No FAA accident or incident reports matched to N638FTMatched 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-28-161 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 2017FA0000404Ignition Switch · wornPILOT REPORTED ENG ROUGHNESS. GROUND RUNS WERE MIXED, SOMETIMES IT WOULD RUN FINE. TROUBLESHOOTING LED TO INTERMITTENT GROUNDING AT KEY SWITCH. KEY SWITCH REPLACED. KEY SWITCH BACK WAS REMOVED. KEY SWITCH WAS INTERMITTENTLY GROUNDING INTERNALLY.SDR ECQS2015FA0000340Step · crackedCRACKED FOOTSTEP.SDR 2011F00154Shaft · brokenACFT WAS WRITTEN UP FOR POWER LOSS. LT AND RT MAGS WERE PULLED. TACH TIME ON BOTH MAGS, 933.5. INSP REVELED LT MAG CAM FOLLOWER SHAFT BROKEN. BOTH MAGS HAD OIL GETTING PAST OIL SEAL AS A RESULT, POINTS WERE PITTED, MAGS WERE REPLACED.SDR 2011F00153Shaft · failedACFT WAS WRITTEN UP FOR POWER LOSS. LT AND RT MAGS WERE PULLED. TACH TIME ON BOTH MAGS, 933.5. INSPECTION REVEALED LT MAG CAM FOLLOWER SHAFT BROKEN. BOTH MAGS HAD OIL GETTING PAST OIL SEAL AS A RESULT, POINTS WERE PITTED, MAG WERE REPLACED.
STCs that may be installed · 385
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-28-161
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