- Registered owner
- Coco Aircraft Inc
- Location
- Merritt Island, FL
- Owner type
- Corporation
- Serial number
- 2843504
- Year built
- 2002
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- February 24, 2002
- Certificate issued
- August 31, 2021
- Expires
- August 31, 2028
- Mode S code
- A3059C
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR20170815079Angle · crackedDURING ROUTINE INSPECTION, AN ANGLE INSTALLED AGAINST RIGHT WING INBOARDMOST FLAP SUPPORT WAS FOUND CRACKED. CRACKING EXTENDED THROUGH RIVET HOLES TO MATERIAL EDGE.SDR FQAR20170815077Angle · crackedDURING ROUTINE INSPECTION, AN ANGLE INSTALLED AGAINST LEFT WING INBOARD MOST FLAP SUPPORT WAS FOUND CRACKED. CRACKING EXTENDED THROUGH RIVET HOLES TO MATERIAL EDGE.SDR FQAR20161027043Bracket · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO 2" CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET. THESE CRACKS CAN ONLY BE SEEN WHEN THE ELT TRAY IS REMOVED.SDR FQAR20151023102Bracket · crackedDURING A PROGRESSIVE INSPECTION, 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 ASSY. IT CONTAINS 2 NUT PLATES TO ALSDR FQAR20150610079Carburetor · stuckTHE PILOTS ATTEMPTED TO START THE ENGINE 4 TIMES WITH NO LUCK. AFTER THE 4TH START ATTEMPT, THEY NOTED A STRONG ODOR OF FUEL; THEY SHUTOFF THE BATTERY MASTER AND EXITED THE PLANE. AFTER EXITING, THEY NOTED FUEL GUSHING FROM UNDER THE LOWER COWLING. MAINTENANSDR FQAR20150606072Carburetor · bindingDURING TOUCH AND GOES, THE PILOTS NOTED THAT THE THROTTLE WOULD BIND 1/3RD OF THE WAY UP ITS TRAVEL FROM IDLE. THEY WERE ABLE TO GET FULL POWER BY EITHER FORCING THE THROTTLE OR WIGGLING IT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE CARBURETOR WAS THE SOURSDR FQAR20150528074Cylinder Head · crackedBOROSCOPE INSPECTION INDICATED CRACKING IN THE RT ENGINE NR 4 CYLINDER HEAD. AFTER THE CYLINDER WAS REMOVED, CRACKS WERE OBSERVED TO THE SIDE OF THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR C-1440.SDR FQAR20150514053Cylinder Head · separatedDURING FLIGHT, THE ENGINE BEGAN TO RUN ROUGH. THE PROBLEM BECAME WORSE OVER THE NEXT FEW MINUTES AND WAS ACCOMPANIED BY A GREAT DEAL OF BANGING/RATTLING NOISES. THE PILOTS WERE ABLE TO MAKE A SAFE, THOUGH UNPLANNED, LANDING AT A NEARBY AIRPORT. INSPECTION RSDR FQAR20140716041Bracket · crackedDURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND TO BE 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 ASSY. IT CONTAINS 2 NUT PLSDR FQAR20140129007Tube · failedTHE NOSE TIRE WAS FOUND FLAT BETWEEN FLIGHTS. 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 12/18/2013 AND HAD SINCE ACCRUED 35 HOURS TIME IN SERVICE. THIS REPAIR STATSDR FQAR20140129014Tube · failedWHILE THE AIRCRAFT WAS EITHER TAXIING OR BEING PARKED, THE NOSE 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 11/7/2013 AND HAD SINCE ACCRUED 128 HOURS TI
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