- Registered owner
- Lewis Justin S P
- Location
- Choctaw, OK
- Owner type
- Individual
- Serial number
- 15079361
- Year built
- 1977
- Type
- Fixed wing single engine
- Engine
- 4 cycle
- Airworthiness
- Standard, utility
- Airworthiness date
- March 22, 1977
- Certificate issued
- August 10, 2023
- Expires
- August 31, 2030
- Mode S code
- A98C5D
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental 0-200 model are included below.
On this page
Airworthiness directives that may apply · 37
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 1 |
|---|---|
| 1968 | 1 |
| 1969 | 1 |
| 1971 | 1 |
| 1973 | 1 |
| 1974 | 1 |
| 1977 | 1 |
| 1979 | 1 |
| 1980 | 3 |
| 1981 | 3 |
| 1987 | 2 |
| 1988 | 2 |
| 1990 | 1 |
| 1993 | 4 |
| 1995 | 1 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 2 |
| 2000 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 2 |
| 2022 | 1 |
| 2023 | 1 |
See all 42 ADs
Information bulletins that may apply · 16
Advisory, not mandatory.
See all 18 bulletins
NTSB investigations
No NTSB investigations matched to N714QXMatched 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 Cessna 150M aircraft
FAA incident reports
No FAA accident or incident reports matched to N714QXMatched 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 Cessna 150M 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 QXEA2012041800328Stringer Splice · corrodedSTRINGER 30P, STRINGER SPLICE BETWEEN STA X-39.00 AND X -18.250 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE AREA REF NTM 51-00-01-250-801. DAMAGE FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-4456. ALODINED, PRIMED AND PAINTED ISDR QXEA2012041400325Threshold · corrodedSTUB FRAME FLANGE ANGLE BELOW PAX DOOR THRESHOLD HAS CORROSION OTBD OF STRINGER 25P AT STA X9.00. REMOVED FLANGE ANGLE IAW SRM 51-42-05-02-01. MATCH DRILLED NEW ANGLE, ALODINED AND INSTALLED STUB FRAME FLANGE ANGLE IAW SRM 51-40-07-02-01, 51-21-10-02-01 AND
STCs that may be installed · 332
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 150M
STC SA01233SEFabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assemblySTC SA00709CHInstallation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both dtd 8/30/96, or later FAA app rev.STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).