- Registered owner
- Third Step 5 LLC
- Location
- Gilbert, AZ
- Owner type
- LLC
- Serial number
- 28-22849
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- March 10, 1967
- Certificate issued
- February 4, 2023
- Expires
- February 28, 2030
- Mode S code
- A179BD
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
No NTSB investigations matched to N1942ZMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Piper PA-28-140 aircraft
FAA incident reports
No FAA accident or incident reports matched to N1942ZMatched 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 95ZZZX6157Spar Plate · corrodedFOUND DISSIMILAR METAL CORROSION BETWEEN AFT WING SPAR AND SPAR ATTACH PLATE. SUBMTTER SUGGESTED TO REMOVE PLATE AND PUT INSULATOR COMPOUND BETWEEN PLATE AND SPAR. ALSO, FOUND DISSIMILAR METAL CORROSION BETWEEN STABILATOR ATTACH FITTING STEEL CHANNELS AND RESDR 95ZZZX6156Spar Plate · corrodedFOUND DISSIMILAR METAL CORROSION BETWEEN AFT WING SPAR AND SPAR ATTACH PLATE. SUBMTTER SUGGESTED TO REMOVE PLATE AND PUT INSULATOR COMPOUND BETWEEN PLATE AND SPAR. ALSO, FOUND DISSIMILAR METAL CORROSION BETWEEN STABILATOR ATTACH FITTING STEEL CHANNELS AND RE
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