- Owner type
- LLC
- Serial number
- 32-8206037
- Year built
- 1982
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- April 28, 1982
- Certificate issued
- December 17, 2024
- Expires
- December 31, 2031
- Mode S code
- AB37CE
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming IO-540 model are included below.
On this page
Airworthiness directives that may apply · 66
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 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1973 | 1 |
| 1975 | 1 |
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 1 |
| 1980 | 2 |
| 1981 | 1 |
| 1982 | 1 |
| 1983 | 1 |
| 1986 | 2 |
| 1989 | 2 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 5 |
| 1997 | 2 |
| 1998 | 4 |
| 1999 | 2 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 6 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 1 |
| 2015 | 2 |
| 2017 | 2 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 2 |
| 2026 | 2 |
Airframe · Piper PA-32-301
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2017-14-04Engine OilInformation bulletins that may apply · 26
Advisory, not mandatory.
See all 29 bulletins
NTSB investigations
No NTSB investigations matched to N8216TMatched 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-32-301 aircraft
FAA incident reports
No FAA accident or incident reports matched to N8216TMatched 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-32-301 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR P9KA2015103005Elt · intermittentDURING A ROUTINE ELT INSPECTION IAW 14 CFR 91.207, THE ELT G SWITCH WAS FOUND TO BE INTERMITTENT. THIS IS A RECURRING PROBLEM WITH THESE UNITS.SDR P9KA2014122201Intake Valve · leakingDURING A ROUTINE 100 HOUR INSPECTION, THE NR 2 CYLINDER WAS FOUND TO HAVE COMPRESSION OF 30/80 WITH LEAKAGE OUT THE INTAKE VLV. THIS IS THE THIRD OCCURRENCE OF THE SAME PROBLEM ON THIS FACTORY OVERHAULED ENG IN LESS THAN 500 HOURS SINCE OVERHAUL. THE FIRST TSDR 2012F00133Crankcase · crackedCRACK WAS DISCOVERED IN THE FORWARD LEFT CASE HALF PROPAGATING OUT FROM NR 2 CYLINDER BASE. DAMAGE FOUND DURING ROUTINE 100 HOUR INSPECTION. ENGINE GROUND RUN CONFIRMED CRACK WAS LEAKING OIL.SDR FYO2005F00000Bar · crackedNOTICED EXCESS PLAY BETWEEN RT AND LT PEDALS DUE TO ELONGATED THRU BOLTS IN ASSY. UPON DISASSEMBLY, FOUND TUBE TO HAVE EXTREME CRACK RADIATING FROM THRU BOLT HOLE AND RADIATING AROUND TO BACK SIDE OF TUBE AND GOING OUT TO EACH SIDE IN A SPIRAL FRACTURE. PARTSDR 99ZZZX3748Impulse Coupling · failedUPON ROUTINE INSPECTION OF IMPULSE COUPLING, FOUND ONE OF THE PAWL ANCHOR PINS LOOSE IN THE BODY OF THE IMPULSE. PART WAS IN SERVICE 202 HOURS. SUBMITTER HAS FOUND 4 OR 5 CASES OF EXCESSIVE WEAR OF LOW TIME IMPULSE COUPLERS (UNDER 300 HOURS).SDR 99ZZZX3171Impulse Coupling · wornUPON ROUTINE INSPECTION OF IMPULSE COUPLING, FOUND THAT ONE OF THE PAWL ANCHOR PINS WAS LOOSE IN THE BODY OF THE IMPULSE. PART WAS IN SERVICE 202 HOURS.SDR 99ZZZX2928Impulse Coupling · failedDURING 100-HOUR INPSECTION OF MAGNETO, IMPULSE WAS FOUND TO BE NEAR TOTAL FAILURE. BOTH PAWL PINS WERE LOOSE IN BODY OF IMPULSE WITH ONE NEARLY READY TO PULL FREE. THIS ASSY HAD BEEN INSPECTED 98 HOURS PRIOR AND FOUND TO HAVE NORMAL WEAR.SDR 98ZZZX3868Magneto · wornROUTINE CHECK OF IMPULSE COUPLING REVEALED BOTH PAWLS EXCEED NORMAL GAP BETWEEN PAWLS AND PLATE BY AN EXTREME AMOUNT. ALSO, ONE PAWL PIN WAS OBVIOUSLY BENT SO THE HEAD TIPPED OUTBOARD FROM CENTER. THIS PART HAD BEEN INSPECTED 100 HOURS PRIOR AND FOUND TO BE SDR 98ZZZX2671Point Set · failedUPON REPORT OF DEAD RIGHT MAGNETO, FOUND CONTACT POINT LOOSE IN POINT SET BODY. OTHERWISE, POINT SET IN EXCELLENT CONDITION.SDR 98ZZZX1081Impulse Coupling · failedMAG IMPULSE COUPLING FAILED. REMOVED FROM ENGINE AT 469.8 HOURS SINCE NEW.SDR 97ZZZX3811Line · crackedRUN-UP, ROUGH ENGINE, FUEL SMELL. FOUND INJECTOR LINE CRACKED. AIRCRAFT JUST OUT OF 100-HOUR INSPECTION, NO INDICATION OF CRACKS, ETC. HAVE SEEN ALERT ON THIS IN THE PAST, HAVE NEVER FOUND ONE CRACKED BEFORE.
STCs that may be installed · 352
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-32-301
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 N8216T before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.