- Registered owner
- Grand Michael
- Location
- Palacios, TX
- Owner type
- Individual
- Serial number
- 24-4256
- Year built
- 1965
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 8, 1965
- Certificate issued
- March 10, 2009
- Expires
- October 31, 2029
- Mode S code
- AAE6DC
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming TI0-540 model are included below.
On this page
Airworthiness directives that may apply · 75
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1965 | 1 |
|---|---|
| 1966 | 1 |
| 1969 | 1 |
| 1971 | 2 |
| 1973 | 1 |
| 1974 | 1 |
| 1975 | 3 |
| 1976 | 3 |
| 1977 | 4 |
| 1978 | 1 |
| 1979 | 3 |
| 1980 | 1 |
| 1981 | 1 |
| 1983 | 3 |
| 1984 | 1 |
| 1989 | 2 |
| 1991 | 3 |
| 1992 | 2 |
| 1993 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 3 |
| 1998 | 3 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 5 |
| 2008 | 4 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 6 |
| 2013 | 1 |
| 2015 | 2 |
| 2016 | 1 |
| 2017 | 2 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 2 |
| 2026 | 1 |
See all 94 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Piper PA-24-260
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-08-50Landing Gear Manual Extension System InspectionSAIB CE-04-88Engine · Lycoming TI0-540 series
SAIB NE-19-08Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve CylindersSAIB NE-08-32R1Propeller Governor Idler Gear Shaft Set ScrewSAIB NE-14-13Reciprocating Engine - Cylinder Mounting StudsSAIB NE-08-26R3Magneto/DistributorSAIB NE-09-04Fuel Control/Reciprocating EnginesSAIB NE-06-32R1Reciprocating Engine - CrankshaftSAIB NE-03-18SAIB NE-03-12SAIB NE-01-37Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N801PCMatched 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-24-260 aircraft
FAA incident reports
No FAA accident or incident reports matched to N801PCMatched 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-24-260 aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2004FA0000017Bracket · crackedDURING RUDDER REMOVAL FOR REQUIRED MAINTENANCE, A CRACK WAS FOUND IN MIDDLE RUDDER HINGE BRACKET MOUNTED ON THE VERTICAL FIN. THE CRACK IS AT THE HINGE BEARING HOLE. DUE TO THE LOCATION, THIS CRACK WOULD NOT HAVE BEEN VISIBLE WITHOUT REMOVING THE RUDDER FIRSSDR 2004FA0000016Bellcrank · crackedDURING ANNUAL INSPECTION, A CRACK WAS FOUND IN THE BELLCRANK BOLT HOLE. ON CLOSER INSPECTION IT WAS FOUND THAT ALL FOUR BOLT HOLES HAD CRACKS IN VARIOUS STAGES OF PROGRESSION. THE CRACKS BEGIN AT THE END OF THE PART AND PROCEED TOWARDS THE BOLT HOLE, ONLY ON
STCs that may be installed · 386
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-24-260
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