- Registered owner
- Michel David L
- Location
- Pickens, SC
- Owner type
- Individual
- Serial number
- 24-1297
- Year built
- 1959
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 17, 1959
- Certificate issued
- July 19, 2024
- Expires
- July 31, 2031
- Mode S code
- A724C6
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming 0-540 model are included below.
On this page
Airworthiness directives that may apply · 80
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1959 | 4 |
|---|---|
| 1960 | 1 |
| 1961 | 2 |
| 1962 | 2 |
| 1963 | 2 |
| 1964 | 4 |
| 1965 | 2 |
| 1966 | 2 |
| 1968 | 1 |
| 1969 | 3 |
| 1974 | 1 |
| 1975 | 2 |
| 1976 | 3 |
| 1977 | 4 |
| 1979 | 2 |
| 1981 | 1 |
| 1982 | 1 |
| 1983 | 2 |
| 1989 | 2 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 2 |
| 1999 | 3 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 3 |
| 2016 | 1 |
| 2017 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 2 |
| 2026 | 2 |
See all 88 ADs
Information bulletins that may apply · 13
Advisory, not mandatory.
Airframe · Piper PA-24-250
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-08-50Landing Gear Manual Extension System InspectionSAIB CE-05-67SAIB CE-04-88Engine · Lycoming 0-540 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-13-06Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series EnginesSAIB NE-08-26R3Magneto/DistributorSAIB NE-06-32R1Reciprocating Engine - CrankshaftSAIB NE-05-40SAIB NE-03-18SAIB NE-03-12Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N56CCMatched 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-24-250 aircraft
FAA incident reports
No FAA accident or incident reports matched to N56CCMatched 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-24-250 aircraft
Service difficulty reports
No reports matched to N56CCGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Piper PA-24-250 aircraft
Reports on N56CC not matched to an aircraft · 3
They name N56CC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 97ZZZX5119Panel · crackedTHE INBOARD AREA OF THE RIGHT OUTBOARD WING PANEL HAS A .3750 INCH CRACK FROM THE TOP OF THE RADIUS CUT-OUT ON THE LEADING EDGE FAIRING.SDR 97ZZZX5118Skin · crackedDURING INSPECTION, A .75 INCH CRACK WAS FOUND NEAR A RIVET WHICH ATTACHES THE ENGINE NACELLE TRAILING EDGE FAIRING TO THE INBOARD FLAP. THE CRACK WOULD NOT HAVE RESULTED IN ANY DAMAGE, BUT SINCE IT IS PART OF A CONTROL SURFACE, RESULTED IN BEING A MAJOR REPAISDR 97ZZZX5117Bracket · crackedDURING INSPECTION, A .50 INCH CRACK WAS NOTED WHERE THE BRACKET FOR THE FLAP INNER CONNECT ATTACHES ON THE RIGHT OUTBOARD FLAP. IT APPEARS THE ROD END FOR THE INNER CONNECT WAS LOOSE WHERE IT ATTACHED TO THE BRACKET AND ALLOWED ENOUGH PLAY FOR THE ROD END TO
STCs that may be installed · 420
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-24-250
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