- Registered owner
- Anderson Stephen A
- Location
- Yuba City, CA
- Owner type
- Individual
- Serial number
- 18-8009031
- Year built
- 1979
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- October 30, 1979
- Certificate issued
- December 24, 2023
- Expires
- December 31, 2030
- Mode S code
- AB3AE0
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 · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1956 | 1 |
|---|---|
| 1960 | 1 |
| 1961 | 1 |
| 1962 | 1 |
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1968 | 2 |
| 1969 | 3 |
| 1977 | 2 |
| 1978 | 3 |
| 1979 | 2 |
| 1980 | 3 |
| 1981 | 2 |
| 1982 | 1 |
| 1985 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1996 | 3 |
| 1997 | 1 |
| 1998 | 3 |
| 1999 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 1 |
| 2010 | 2 |
| 2012 | 1 |
| 2014 | 1 |
| 2015 | 1 |
| 2017 | 1 |
| 2022 | 2 |
| 2024 | 1 |
| 2025 | 1 |
| 2026 | 1 |
Airframe · Piper PA-18-150
AD 2025-02-11Rudder StructureAD 2022-03-15Fuel Quantity IndicatorAD 2015-08-04WingsInformation bulletins that may apply · 11
Advisory, not mandatory.
Airframe · Piper PA-18-150
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB ACE-96-04Engine · Lycoming 0-320 series
SAIB NE-06-31R6Engine Lubricating OilsNTSB investigations · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB WPR12CA028Accident · No injuriesData collectionFinal reportGrangeville, IDThe pilot's failure to maintain directional control during the landing roll.NTSB WPR10CA049Accident · No injuriesData collectionFinal reportLewiston, IDThe pilot's delayed decision to execute a go-around in gusting winds and with up-sloping terrain.NTSB FTW84LA280Accident · No injuriesLimited investigationFinal reportBlue Ridge, TXPlt had power at idle during descent from 900 ft AGL to 200 ft AGL. During a low pass over a field, plt advanced throttle, engine sputtered and did not accelerate. Heavy braking was used during forced landing roll and acft nosed over. Plt did not recall using…
FAA incident reports · 4
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20111030026129ALanding: Rollout · Grangeville, IDAt the time of the accident [privacy data omitted] performed a 3 point landing on runway 7 at gic. He then raised the tail wheel and lowered the tail wheel to make a right turn on the first taxiway (approximately 1400 feet from runway 7 threshold). The winds…Accident 20091101021459ALanding · Grangeville, ID[privacy data omitted] Was landing at a private airstrip named Pinnacle airstrip (01D8) about 10 miles south of the Grangeville airport. He elected to go around because of a tailwind. He struck brush and vegetation on the side of the runway that caused the…Incident 19890408023149ILevel Off Touchdown · Dallas, TXStudent lost control on landing. Instructor told him to release controls. Veered off runway.Accident 19840618074769AFcd/Prec Ldg From Cruise · Blue Ridge, TXGlided low over prospective landing area. Engine failed to respond. Nosed over braking to miss cattle on landing.
Service difficulty reports
No reports matched to N82213General 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-18-150 aircraft
STCs that may be installed · 484
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-18-150
STC SA01233SEFabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assemblySTC 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.