- Registered owner
- 5b Aviation LLC
- Location
- Duncan, OK
- Owner type
- LLC
- Serial number
- 28-20757
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- April 16, 1965
- Certificate issued
- October 17, 2023
- Expires
- October 31, 2030
- Mode S code
- A8C9E8
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming 0-320 model are included below.
On this page
Airworthiness directives that may apply · 77
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 |
|---|---|
| 1965 | 1 |
| 1966 | 1 |
| 1967 | 3 |
| 1968 | 3 |
| 1969 | 2 |
| 1970 | 1 |
| 1971 | 3 |
| 1972 | 4 |
| 1974 | 3 |
| 1975 | 2 |
| 1977 | 4 |
| 1978 | 2 |
| 1979 | 4 |
| 1980 | 4 |
| 1981 | 1 |
| 1982 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 4 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 1 |
| 2010 | 3 |
| 2012 | 1 |
| 2013 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2020 | 1 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-28-140
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2020-24-05Wing SparInformation bulletins that may apply · 30
Advisory, not mandatory.
See all 40 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
No FAA accident or incident reports matched to N6655WMatched 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-28-140 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 2018FA0000462Cylinder · crackedCYLINDER HEAD IS CRACKED. THIS IS THE THIRD CYLINDER ON THIS ENGINE THAT THE HEAD HAS DEVELOPED HOLES IN THEM. THE FIRST WENT AT ABOUT 800 HOURS. WE OPERATE THIS ENGINE IN A FLIGHT SCHOOL. HAPPENED UNDER NORMAL FLIGHT OPERATIONS. PROBABLE CAUSE UNKNOWN. SDR 9LIS2016FA0000006Cylinder Head · crackedTHE CYLINDER HEAD CRACKED AT THE NINETH COOLING FIN. CRACK RUNS ALONG THE FIN. THE CRACK IS ABOUT .5" LONG. THE CYLINDER HAD LOW COMPRESSION. THE CRACK OCCURRED UNDER NORMAL OPERATING CONDITIONS OF A FLIGHT SCHOOL. PROBABLE CAUSE: METAL FATIGUE. THE FOLL
STCs that may be installed · 469
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-28-140
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