- Registered owner
- Claus Jay G
- Location
- Palmer, AK
- Owner type
- Individual
- Serial number
- 18-1972
- Year built
- 1952
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- February 2, 1976
- Certificate issued
- December 28, 2021
- Expires
- December 31, 2028
- Mode S code
- A25E3D
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming 0-290 model are included below.
On this page
Airworthiness directives that may apply · 26
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1956 | 3 |
|---|---|
| 1959 | 1 |
| 1960 | 1 |
| 1962 | 1 |
| 1968 | 1 |
| 1969 | 1 |
| 1972 | 1 |
| 1977 | 1 |
| 1978 | 1 |
| 1982 | 1 |
| 1985 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1996 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2001 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2015 | 1 |
| 2022 | 1 |
| 2025 | 1 |
| 2026 | 1 |
Airframe · Piper PA-18
AD 2025-02-11Rudder StructureAD 2022-03-15Fuel Quantity IndicatorAD 2015-08-04WingsInformation bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Piper PA-18
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-13-30IGNITION SYSTEM Toggle Style Magneto Switches on the Left Side Cabin Adjacent to the Pilot SeatSAIB CE-13-14Fuselage Cracking at Aft Tail Post Weld Joint on Piper Model PA-18 (L-21) AirplanesSAIB CE-03-02R1SAIB CE-04-91SAIB CE-01-27SAIB ACE-99-01Engine · Lycoming 0-290 series
SAIB NE-01-22NTSB investigations · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ANC91LA152Accident · Serious injuriesLimited investigationFinal reportAnaktuvuk Pass, AKThat the pilot inadvertently stall/spun the airplane to the ground. Contributing to the accident was the pilot's failure to adequately remove the ice/frost from the wings before starting the takeoff.NTSB ANC90LA073Accident · No injuriesLimited investigationFinal reportTalkeetna, AKCollapse of the left main landing gear due to an overload failure induced by previous damage which occurred during an improper level-off by the pilot.NTSB DEN80FTE65Accident · No injuriesClosedAurora, CONTSB MKC79DTG14Accident · No injuriesClosedLeeds, ND
FAA incident reports · 5
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20050617014789IRoll-Out (Fixed Wing) · Nome, AK(-23) Landed on gravel bar behind his house. Due to gusting crosswinds (19G25) and excessive use of brakes the aircraft nosed over striking the prop on the gravel bar, damaging approx. 2" at the prop end. Consulted with his CFI and expressed my concerns of…Accident 19910912042829ATo Init Climb(1st Pwr Reduct) · Anatuvuk Pass, AKWing stalled on initial climbout from remote strip. Crash landed. Pilot believes snow and ice not removed from wingAccident 19900521018969ARoll-Out (Fixed Wing) · Talkeetna, AKLeft main gear collapsed on landing. Aircraft then nosed over. Had damaged gear trying to land on a gravel bar.Accident 19800722029939ARoll-Out (Fixed Wing) · Aurora, COOvershot Private strip on landing. Started go-around, then aborted. Ran off runway into a ditch.Accident 19790822022209ALow Level Operations · Leeds, NDStudent pilot attempted to herd cows with his airplane. Hit cattle and crashed.
Service difficulty reports
No reports matched to N2515AGeneral 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 aircraft
STCs that may be installed · 445
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
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.