- Registered owner
- Villines Dustin
- Location
- Lincoln, AR
- Owner type
- Individual
- Serial number
- 1058
- Year built
- 2000
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 15, 2000
- Certificate issued
- February 22, 2023
- Expires
- February 28, 2030
- Mode S code
- A0DCF8
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming I0360 model are included below.
On this page
Airworthiness directives that may apply · 56
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1964 | 1 |
|---|---|
| 1966 | 1 |
| 1967 | 2 |
| 1969 | 1 |
| 1972 | 1 |
| 1973 | 2 |
| 1975 | 1 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 1 |
| 1982 | 1 |
| 1989 | 1 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 1 |
| 1998 | 3 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 3 |
| 2004 | 1 |
| 2005 | 3 |
| 2006 | 8 |
| 2007 | 2 |
| 2008 | 8 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 3 |
| 2015 | 1 |
| 2017 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Cirrus Design SR20
AD 2024-24-11Power LeverAD 2022-03-15Fuel Quantity IndicatorAD 2009-05-05Primary Flight DisplaysInformation bulletins that may apply · 26
Advisory, not mandatory.
See all 30 bulletins
NTSB investigations
No NTSB investigations matched to N155CDMatched 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 Cirrus Design SR20 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2007FA0000286Mount · brokenENGINE MOUNT RT FRONT CROSSOVER TUBE BETWEEN LT AND RT ENGINE SUPPORTS FOUND BROKEN AT THE WELD RT SIDE. ENGINE WAS CHANGED ABOUT 250 HRS AGO, NO MENTION OF ENGINE MOUNT DAMAGE. COULD HAVE BEEN A HARD LANDING, BUT NO OTHER SIGNS WERE NOTED. CONTACT WITH MFGSDR 2001FA0000610Bearing · brokenPROPELLER GOVERNOR CABLE EXTREMELY STIFF WITH POSSIBLE BROKEN WIRE INSIDE OUTER SHROUD. THIS CAUSED THE THROTTLE LEVER BEARING, WHERE THE ROD END FOR THE PROP GOVERNOR CABLE ATTACHES TO THE THROTTLE LEVER, TO BREAK APART. THE STRENGTH OF THE BEARING FOR THISSDR 2001FA0000609Bracket · brokenBOTH LEFT AND RIGHT MAIN LANDING GEAR INBOUARD FAIRING BRACKETS BROKEN, CAUSING FAIRING TO BE VERY LOOSE. GAUGE OF METAL IS TOO THIN FOR THIS HIGH VIBRATION APPLICATION.
STCs that may be installed · 172
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cirrus Design SR20
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