- Registered owner
- Simply Living LLC
- Location
- Fort Myers, FL
- Owner type
- LLC
- Serial number
- CE-1454
- Year built
- 1990
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- April 4, 1990
- Certificate issued
- October 15, 2019
- Expires
- October 31, 2029
- Mode S code
- A72A8E
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental IO-520 model are included below.
On this page
Airworthiness directives that may apply · 75
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 3 |
|---|---|
| 1973 | 2 |
| 1974 | 3 |
| 1975 | 1 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1981 | 2 |
| 1984 | 1 |
| 1986 | 1 |
| 1987 | 2 |
| 1988 | 6 |
| 1991 | 4 |
| 1993 | 4 |
| 1994 | 2 |
| 1995 | 3 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 3 |
| 1999 | 2 |
| 2000 | 3 |
| 2001 | 4 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2019 | 2 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
See all 89 ADs
Information bulletins that may apply · 16
Advisory, not mandatory.
See all 16 bulletins
NTSB investigations
No NTSB investigations matched to N5609SMatched 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 Beech F33A aircraft
Investigations on N5609S not matched to an aircraft · 2
They name N5609S, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20110901020189IGround/Ramp/Ma · Goodyear, AZStudent pilot started the aircraft and possibly left the throttle in the "forward" position causing the aircraft to accelerate out of control striking a fixed pole. Damage to the aircraft consisted of the engine, prop and spinner assembly, and some fairings.Incident 20011101028809ILevel Off Touchdown · Goodyear, AZ(-23) "During touch & go practice, the landing gear would not extend. The landing gear circuit breaker was tripped and manual gear extension attempted. Guidance was received to return to Goodyear where additional attempts were made to lower the gear. All…
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2013FA0000286Circuit Breaker · failedPILOT REPORTED THE NAV LIGHT AS BEING INOPERATIVE. DURING TROUBLESHOOTING, FOUND THE CIRCUIT BREAKER TO BE AT FAULT. NO PROBABLE CAUSE AT THIS TIME. REPLACED THE CIRCUIT BREAKER.SDR 2012FA0000365Switch · failedPILOT REPORTED THAT THE TAXI LIGHT WAS NOT WORKING. DURING TROUBLESHOOTING FOUND THAT THE TAXI LIGHT CURCUIT BREAKER SWITCH WAS FOUND TO BE AT FAULT. THE SWITCH WAS INSTALLED ON 09 AUG 2010 WITH A TSN OF 1128 WITH AN ESTEMATED 4512 CYCLES. INSTALLED A NEW TAXISDR 2012FA0000364Circuit Breaker · failedPILOT REPORTED THAT THE LANDING LIGHT WAS NOT WORKING. DURING TROUBLESHOOTING FOUND THAT THE LANDING LIGHT CIRCUIT BREAKER WAS FOUND TO BE AT FAULT. THE CIRCUIT BREAKER WAS INSTALLED ON 03 APRIL 2010 WITH A TSN OF 1507 WITH AN ESTEMATED 6028 CYCLES. INSTALLEDSDR 2011FA0000223Circuit Breaker · failedPILOT REPORTED NAV LIGHTS INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17, HAD BEEN COMPLETED 2423 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 9692. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.SDR 2010FA0001080Circuit Breaker · unserviceablePILOT REPORTED STROBE LIGHTS INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT, A.D. 2008-13-17 HAD BEEN COMPLETED 1997 HOURS PRIOR. NOTICED NEW CIRCUIT BREAKER/SWITCHES. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.SDR 2010FA0000814Circuit Breaker · inoperativePILOT REPORTED TAXI LIGHT INOPERATIVE. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/ TO BE AT FAULT AD 2008-13-17 HAD BEEN COMPLETED 1879 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 7516. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.SDR 2010FA0000294Circuit Breaker · failed(VJ3S) PILOT REPORTED LANDING LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1500 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 6000. NOTICED NEW CIRCUIT BREAKER. NO PROBABLE CAUSE OR RECOMMENDASDR 2003FA0001054Valve · failedDURING ROUTINE PHASE INSPECTION, THE MANIFOLD VALVE WAS FOUND TO BE LEAKING FUEL THROUGH THE AIR VENT. PROBABLE CAUSE IS INTERNAL FAILURE OF THE DIAPHRAGM. NO RECOMMENDATION AT THIS TIME.SDR 2003FA0000496Pump · wornDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANESSDR VJ32002F00083Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.SDR 2002FA0000765Relay · failedLANDING GEAR FAILED TO EXTEND IN FLIGHT, GEAR WAS HAND CRANKED DOWN AND A SAFE LANDING WAS MADE. AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED IAW MM. THE RELAY CONTROL STICK IN THE UP POSITION WHEN THE GEAR WAS CYCLED. RELAY WAS REMOVED AND A NESDR 2002FA0000473Pump · inoperativeLOW OUT PUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP, OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.SDR VJ32002F00010Relay · inoperativeLANDING GEAR WOULD NOT COME DOWN, A SMALL TAP TO THE TOP OF THE RELAY THE GEAR CYCLED DOWN NORMAL. RELAY WAS REMOVED AND A NEW RELAY WAS INSTALLED. LANDING GEAR OPERATIONAL CHECKED NORMAL. RELAY SENT IN FOR WARRANTY.SDR 20010613CW013Flow Divider · stuckENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN, THE FUEL FLOW DIVIDER WOULD STICK OPEN, LETTING FUEL TOO CONTINUAL TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL.SDR 20010607CW002Fuel Control · defectiveTHE PILOT REPORTED A ROUGH ENGINE IN FLIGHT AND RETURNED TO AIRPORT, A SAFE LANDING WAS MADE. MAINTENANCE GROUND RUN AIRCRAFT AND A FLUCTUATION IN FUEL FLOW WAS NOTED. THEY FOUND THAT THE MIXTURE CONTROL WAS STIFF WHEN MOVING. (POSSIBLE GALLING). FUEL CONT
STCs that may be installed · 531
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech F33A
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