- Registered owner
- Williamsen Wesley
- Location
- Benedict, NE
- Owner type
- Individual
- Serial number
- 24-219
- Year built
- 1958
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- June 27, 1958
- Certificate issued
- April 23, 2020
- Expires
- April 30, 2030
- Mode S code
- A685F3
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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N5195PMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 95ZZZX2651Bungee Arm · crackedEARLY THIN WALL BUNGEE ARM HAD BEEN REPLACED PREVIOUSLY. INSPECTION FOUND BOTH LT AND RT ARMS CRACKED. ACFT SHOWS SIGN OF PREVIOUS REPAIR FOR GEAR UP LANDING. ACFT TT 3764.SDR 95ZZZX2652Bungee Arm · crackedUPON DOING 1,000 GEAR AD PER 77-13-21, FOUND RT BUNGEE ARM CRACKED AT RADIUS FOR RETAINER PINS. THIS IS SEEN OFTEN AND HAVE REPORTS OF COMPLETE FAILURE IDENTIFIED BY SEVERE SHAKING AT TAXI. THIS WAS THE EARLY THIN-WALLED BUNGEE ARMS. (PN 20846-000 AND PN 20SDR 95ZZZX2650Swivel Stud · wrong partWHILE PERFORMING INSPECTION FOR AD 77-13-21, FOUND RT SWIVEL STUD BENT (POSSIBLY CRACKED TOO) AND RT SWIVEL STUD WAS THE INCORRECT PART (WAS LARGER STUD FOR LATER MODELS, EXPECT ORIGINAL PREVIOUSLY DAMAGED AND REPLACED WITH WHAT COULD BE FOUND). ADVISE IN RULSDR 95ZZZX2649Swivel Stud · bentWHILE PERFORMING INSPECTION FOR AD 77-13-21, FOUND RT SWIVEL STUD BENT (POSSIBLY CRACKED TOO) AND RT SWIVEL STUD WAS THE INCORRECT PART (WAS LARGER STUD FOR LATER MODELS, EXPECT ORIGINAL PREVIOUSLY DAMAGED AND REPLACED WITH WHAT COULD BE FOUND). ADVISE IN RUL
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