- Registered owner
- Artisan Aviation Inc
- Location
- Rochester, NY
- Owner type
- Corporation
- Serial number
- 28R-7918117
- Year built
- 1979
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 20, 1979
- Certificate issued
- February 18, 1993
- Expires
- October 31, 2029
- Mode S code
- A1E840
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 22
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1979 | 2 |
|---|---|
| 1980 | 3 |
| 1981 | 1 |
| 1982 | 1 |
| 1986 | 2 |
| 1989 | 1 |
| 1994 | 1 |
| 1996 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2010 | 1 |
| 2013 | 1 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 2024 | 1 |
Airframe · Piper PA-28RT-201
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2020-26-16Wing SparInformation bulletins that may apply · 15
Advisory, not mandatory.
See all 16 bulletins
NTSB investigations
No NTSB investigations matched to N2218ZMatched 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-28RT-201 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2003FA0000428Alternator · overheatedA POOR CONNECTION BETWEEN THE OUTPUT STUD AND THE POSITIVE DIODE MOUNTING ASSEMBLY RESULTED IN EXTREME HEATING OF THE STUD AND MOUNTING ASSEMBLY. THIS HEAT ALSO MELTED THE TEFLON OUTPUT STUD INSULATOR AND VAPORIZED THE DIODE LEADS. THE DIODE MOUNTING ASSEMBLSDR B2E2003F00000Brush Block · damagedREMOVED SLICK MAGNETO IAW INSPECTION. FOUND DISTRIBUTOR GEAR MISSING CARBON BRUSH AND SPRING IN VERY POOR CONDITION. ALSO DISTRIBUTOR BEARING BAR WAS BURNED AND MELTED.
STCs that may be installed · 290
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-28RT-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