- Registered owner
- Coco Aircraft Inc
- Location
- Merritt Island, FL
- Owner type
- Corporation
- Serial number
- 2843512
- Year built
- 2002
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- May 4, 2002
- Certificate issued
- September 2, 2021
- Expires
- September 30, 2028
- Mode S code
- A39105
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O-360 model are included below.
On this page
Airworthiness directives that may apply · 70
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 |
| 1977 | 4 |
| 1979 | 4 |
| 1980 | 6 |
| 1981 | 1 |
| 1982 | 1 |
| 1986 | 2 |
| 1988 | 1 |
| 1989 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 7 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 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 · 26
Advisory, not mandatory.
See all 35 bulletins
NTSB investigations
No NTSB investigations matched to N329PAMatched 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
Investigations on N329PA not matched to an aircraft · 1
They name N329PA, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR2018060500031Muffler · damagedDURING INSPECTION FOR POWER LOSS, FOUND BOTH MUFFLERS TO HAVE DAMAGED FLAME TUBES, WITH PIECES OF THE FLAME TUBE OBSTRUCTING THE OUTLET OF THE FORWARD MUFFLER, CAUSING A RESTRICTION OF EXHAUST AND REDUCED POWER.SDR FQAR20171031094Frame · crackedDURING ROUTINE MAINTENANCE, A FUSELAGE FRAME THAT ACTS AS THE FORWARD WING ATTACH STRUCTURE WAS FOUND TO BE CRACKED/BROKEN AT THE UPPER RIGHT END. BROKEN AREA IS IN THE UPPERMOST RIVET TO EDGE OF MATERIAL. CRACK MAY ONLY BE SEEN BY REMOVING THE SIDE PANEL, DISSDR FQAR20171031093Door Frame · crackedDURING A ROUTINE INSPECTION, A COMPONENT THAT FORMS THE LOWER CABIN DOOR FRAME WAS FOUND TO BE CRACKED. CRACK WAS FROM LIGHTENING DIRECTLY ABOVE MAIN SPAR CARRY THOUGH AND EXTENDED TO EDGE OF MATERIAL. IT IS SPECULATED THAT THIS CRACKING IS CAUSED BY THE CABINSDR FQAR20170609035Bracket · crackedDURING A ROUTINE INSPECTION THE FWD ONE OF TWO Z-SHAPED BRACKETS IMMEDIATELY BEHIND THE FIREWALL, FOUND CRACKED. IT IS LIKELY CRACKING IS CAUSED BY THE MOVEMENT OF THE RUDDER PEDALS STRESSING THE SURROUNDING STRUCTURE.SDR FQAR20161016035Bracket · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED 2, 2 INCH CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET.SDR FQAR20150805085Universal Joint · separatedDURING FLIGHT, THE STUDENT PILOT SEATED AT THE LT CONTROLS NOTED THE YOKE & YOKE SHAFT HAD DISCONNECTED & NO LONGER WERE CONTROLLING THE PITCH OR ROLL. THE FLIGHT INSTRUCTOR TOOK CONTROL, HE NOTED THE AILERON TRAVEL WAS RESTRICTED BUT CONTROL COULD BE MAINTAISDR FQAR20150524046Cylinder Head · crackedBORESCOPE INSPECTION REVEALED THE NR 3 CYLINDER HEAD WAS CRACKED. AFTER REMOVAL, THE INSIDE OF THE HEAD WAS FOUND TO BE CRACKED TO EITHER SIDE OF THE LOWER SPARK PLUG HOLE. HEAD CASTING NR C-03224.SDR FQAR20150524045Cylinder Head · crackedBORESCOPE INSPECTION REVEALED THE NR 2 CYLINDER WAS CRACKED. AFTER REMOVAL, THE INSIDE OF THE HEAD WAS FOUND TO BE CRACKED AT THE EXHAUST VALVE SEAT. HEAD CASTING NR C-02084.SDR FQAR20150524044Cylinder Head · crackedBORESCOPE INSPECTION REVEALED THE NR 1 CYLINDER WAS CRACKED. AFTER REMOVAL, THE INSIDE OF THE HEAD WAS FOUND TO BE CRACKED TO EITHER SIDE OF THE LOWER SPARK PLUG HOLE. HEAD CASTING NR C-02282.SDR FQAR20150112004Bracket · crackedDURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND CRACKED BELOW WHERE THE FLAP HANDLE IS MOUNTED. THE BRACKET IN QUESTION IS LOCATED IN THE TUNNEL IN THE CENTER OF THE CABIN FLOOR AND IS USED TO MOUNT THE FLAP HANDLE ASSEMBLY. IT CONTAINS NUT PLATES TSDR FQAR20140129009Tube · failedBETWEEN FLIGHTS, THE LEFT MAIN TIRE WAS FOUND FLAT. THE WHEEL ASSY WAS REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSY. THE AFFECTED TUBE WAS INSTALLED AS PART OF A BUILT-UP WHEEL ASSY ON 11/14/2013 AND HAD SINCE ACCRUED 90 HOURS TIME IN SERVICE. THIS REPAIRSDR FQAR20140129015Tube · failedBETWEEN FLIGHTS, THE RT MAIN TIRE WENT FLAT. THE WHEEL ASSY WAS REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSY. THE AFFECTED TUBE WAS INSTALLED AS PART OF A BUILT-UP WHEEL ASSY ON 11/12/2013 AND HAD SINCE ACCRUED 66 HOURS TIME IN SERVICE. THIS REPAIR STATION SDR FQAR2013062404176Transmitter · out of tolerancePRIOR TO INSTALLATION OF FUEL QUANTITY SENDER IN THE FUEL TANK, THE SENDER WAS CHECKED IAW THE AIRCRAFT MM. THE UNIT FAILED THE TEST BY HAVING ONE DEAD SPOT AND BEING OUT OF TOLERANCE AT UPPER MECHANICAL LIMIT. UPPER MECHANICAL LIMIT REQUIRED 45 OHMS + OR -
STCs that may be installed · 383
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