- Registered owners
- Henegar Nathanie LHenegar Sam
- Location
- Owasso, OK
- Owner type
- Co-owned
- Serial number
- 15061086
- Year built
- 1964
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- December 28, 1964
- Certificate issued
- March 20, 2017
- Expires
- March 31, 2027
- Mode S code
- A27869
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 · 36
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 |
| 1975 | 1 |
| 1977 | 1 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 3 |
| 1983 | 1 |
| 1987 | 3 |
| 1988 | 2 |
| 1990 | 1 |
| 1993 | 4 |
| 1995 | 1 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 2 |
| 2004 | 1 |
| 2008 | 1 |
| 2011 | 1 |
| 2022 | 1 |
| 2023 | 1 |
See all 40 ADs
Information bulletins that may apply · 15
Advisory, not mandatory.
See all 17 bulletins
NTSB investigations
No NTSB investigations matched to N2586JMatched 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 150E aircraft
FAA incident reports
No FAA accident or incident reports matched to N2586JMatched 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 150E aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2007FA0000429Muffler · crackedPILOT REPORTED FATIGUE WHILE FLYING. NO OBVIOUS EXTERNAL SIGNS OF MUFFLER FAILURE WERE FOUND, SHROUD REMOVAL REVEALED A TIGHT CRACK FROM NR 2 RISER INTO BODY, 3 INCHES LONG THAT LEFT VERY LITTLE STAINING ON INSIDE OF SHROUD. MUFFLER BODY WAS DEFORMED WHERE RISSDR 2007FA0000434Muffler · crackedPILOT REPORTED FATIGUE WHILE FLYING. NO OBVIOUS EXTERNAL SIGNS OF MUFFLER FAILURE WERE FOUND, SHROUD REMOVAL REVEALED A TIGHT CRACK FROM NR 2 RISER INTO BODY, 3 INCHES LONG THAT LT VERY LITTLE STAINING ON INSIDE OF SHROUD. MUFFLER BODY WAS DEFORMED WHERE RISESDR 2007FA0000428Rib · crackedDURING LT LEADING EDGE SKIN REPLACEMENT OF HORIZONTAL STABILIZER DUE TO BIRDSTRIKE FOUND BOTH IB LEADING EDGE RIBS PN 0432001-46/ -6 CRACKED THROUGH UPPER AND LOWER MOUNTING TABS. WORKING RIVETS WERE FOUND AT THE TABS AND 2 RIVETS OB ON FORWARD SPAR. BIRDSTRIKSDR 2007FA0000427Rib · crackedDURING LT LEADING EDGE SKIN REPLACEMENT OF HORIZONTAL STABILIZER DUE TO BIRDSTRIKE FOUND BOTH IB LEADING EDGE RIBS PN 0432001-46/ -6 CRACKED THROUGH UPPER AND LOWER MOUNTING TABS. WORKING RIVETS WERE FOUND AT THE TABS AND 2 RIVETS OB ON FORWARD SPAR. BIRDSTRIKSDR 2007FA0000426Rib · crackedDURING LT LEADING EDGE SKIN REPLACEMENT OF HORIZONTAL STABILIZER DUE TO BIRD STRIKE FOUND BOTH IB LEADING EDGE RIBS PN 0432001-46/ -6 CRACKED THROUGH UPPER AND LOWER MOUNTING TABS. WORKING RIVETS WERE FOUND AT THE TABS AND 2 RIVETS OB ON FORWARD SPAR. BIRDSTRISDR 2007FA0000425Rib · crackedDURING LT LEADING EDGE SKIN REPLACEMENT OF HORIZONTAL STABILIZER DUE TO BIRD STRIKE FOUND BOTH IB LEADING EDGE RIBS PN 0432001-46/ -6 CRACKED THROUGH UPPER AND LOWER MOUNTING TABS. WORKING RIVETS WERE FOUND AT THE TABS AND 2 RIVETS OB ON FORWARD SPAR. BIRD STRSDR 2004FA0000369Main Bearing · separatedAFT THRUST FACES OF BOTH FRONT MAIN BEARING HALVES WERE SEPARATED FROM BEARING. THIS IS A ONE PIECE STYLE THRUST/MAIN BEARING. PROBLEM FOUND DURING OVERHAUL, NO INDICATIONS OF FAILURE NOTED BEFORE DISASSEMBLY. NO DAMAGE TO CASE OR CRANKSHAFT.
STCs that may be installed · 355
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 150E
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).