- Registered owner
- Cooper Andrew P
- Location
- Glastonbury, CT
- Owner type
- Individual
- Serial number
- 25-2020
- Year built
- 1998
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- February 6, 1998
- Certificate issued
- October 9, 2024
- Expires
- October 31, 2031
- Mode S code
- ADF0C2
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-360 model are included below.
On this page
Airworthiness directives that may apply · 45
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1971 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 1 |
| 1980 | 2 |
| 1981 | 2 |
| 1986 | 3 |
| 1988 | 1 |
| 1989 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1995 | 4 |
| 1998 | 6 |
| 2000 | 2 |
| 2001 | 1 |
| 2002 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 4 |
| 2013 | 1 |
| 2022 | 2 |
| 2023 | 4 |
| 2024 | 1 |
See all 56 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
Airframe · Mooney M20K
SAIB 2023-02Landing Gear SystemSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-14-12Landing Gear SystemSAIB NE-13-32Propeller Spinner SectionSAIB CE-09-38Wings: Installation of Supplemental Type Certificate (STC) Wing Tip FairingsEngine · Continental TSIO-360 series
SAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-04Fuel Control/Reciprocating EnginesNTSB investigations
No NTSB investigations matched to N998ECMatched 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 Mooney M20K aircraft
FAA incident reports
No FAA accident or incident reports matched to N998ECMatched 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 Mooney M20K aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 98ZZZX3469Airbox · chafedTHE INDUCTION SYSTEM AIRBOX P/N 600406-501 COMES IN CONTACT WITH THE ADJACENT ENGINE MOUNT WHICH IN TURN CHAFES ENGINE MOUNT. RECOMMEND ADDING CHAFE PROECTION MATERIAL TO ENGINE MOUNT.SDR 98ZZZX3468Induction Tube · chafedCYLINDER NR 6 INDUCTION TUBE SETTLES ONTO THE UPPER CRANKCASE AND IF LEFT UNCORRECTED WILL CHAFE A HOLE INTO THE INDUCTION TUBE (P/N 649266-2. RECOMMEND ADDING ANTI-CHAFE MATERIAL TO THE INDUCTION TUBE.SDR 98ZZZX3467Breather · chafedTHE CRANKCASE BREATHER TUBE P/N 620062007 CHAFES AGAINST CYLINDER NR 6 INDUCTION TUBE P/N 649266-1 AND IF LEFT UNCORRECTED WILL CHAFE A HOLE INTO THE TUBES. RECOMMEND ADDING ANTI-CHAFE MATERIAL TO BOTH TUBES.SDR 98ZZZX3425Induction Tube · crackedFOUND CLYINDERS NR 3 (PN 649263) AND NR 4 (PN 649264) INDUCTION TUBES CRACKED UNDER THE INDUCTION TUBE FLANGES (PN 646933).
STCs that may be installed · 357
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Mooney M20K
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