- Registered owners
- Maus Christopher JMaus Kala L
- Location
- Anchorage, AK
- Owner type
- Co-owned
- Serial number
- 18-7417
- Year built
- 1960
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- July 12, 1960
- Certificate issued
- February 16, 2022
- Expires
- February 28, 2029
- Mode S code
- A42D23
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 ANC04CA116Accident · No injuriesData collectionFinal reportTalkeetna, AKThe pilot's selection of an unsuitable landing area, which resulted in a nose over. A factor associated with the accident was tundra.NTSB ANC01LA114Accident · No injuriesLimited investigationFinal reportAnchorage, AKThe pilot's inadvertent ground loop during the landing roll.NTSB ANC97TA095Accident · No injuriesFinal reportTok, AKThe second pilot/dual student's failure to maintain a proper glidepath, and the pilot-in-command/flight instructor's inadequate supervision. A factor associated with the accident was a downdraft.
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 20040927024159ARoll-Out (Fixed Wing) · Talkeetna, AK(-23) This flight was conducted under CFR 14 part 91. I interviewed the pilot and he stated that he was landing on muskeg and on rollout a soft area was encountered causing the 30" wheel to sink. The aircraft rolled up on end, bending a wing strut. The pilot…Accident 20010816039759ARoll-Out (Fixed Wing) · Anchorage, AK(-23) During landing, the aircraft veered right and the pilot was unable to correct and subsequently the right main gear collapsed forcing the aircraft off to the side of the runway. The right wing main spars were bent as were the prop tips. No injuries.…Accident 19970627017079ALevel Off Touchdown · Tok, AK(.4) The second pilot was a rated float plane pilot, but did not meet the criteria to act as pilot-in-command (PIC) by his employer, the U.S. Fish and wildlife service (usfws). The PIC, who was also employed by the usfws, was a certificated flight instructor,…
Service difficulty reports
No reports matched to N3685ZGeneral 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.