- Registered owner
- Fejes Guide Service Ltd
- Location
- Anchorage, AK
- Owner type
- Corporation
- Serial number
- 18-7909099
- Year built
- 1979
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- March 28, 1979
- Certificate issued
- June 10, 1988
- Expires
- July 31, 2027
- Mode S code
- AB42BC
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 ANC21LA099Accident · No injuriesClass 4 · LimitedFinal reportCordova, AKThe pilot’s failure to maintain control of the airplane after landing in gusty wind conditions.NTSB ANC15CA002Accident · No injuriesData collectionFinal reportCordova, AKThe pilots decision to land and failure to maintain control of the airplane during landing in gusty wind conditions.NTSB ANC11CA089Accident · No injuriesData collectionFinal reportCape Yakataga, AKThe pilot inadvertently switching off the engine magnetos during the initial climb, resulting in a loss of engine power. Contributing to the accident was the manufacturer's placement of the magneto switches.
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20210922012909ATaxi · Yakutat, AKPilot is a guide and was transporting a bear hunter to a hunting location along the beach. The pilot had spotted a dead whale that had washed onto the shore. The wind was gusting over 30 knots, a crosswind to landing direction. Pilot landed high on the shore.…Accident 20141008020179ALanding: Touchdown · Yakataga, AKDuring an off airport landing a strong gust of wind hit the right wing which lowered the left wing into brush which caused the the aircraft to spin around and the right wing then contacted trees and brush.Accident 20110829019049ATakeoff: Climb Out · Cordova, AKOn August 29, 2011 at approximately 1600 hrs. Local time a Piper model PA-18 aircraft sustained substantial damage following a complete loss of engine power during take-off initial climb. The commercial rated pilot and passenger were not injured in the…
Service difficulty reports
No reports matched to N82448General 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.