- Registered owner
- N8242t LLC
- Location
- Phoenix, AZ
- Owner type
- LLC
- Serial number
- CE-1610
- Year built
- 1991
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- September 10, 1991
- Certificate issued
- November 2, 2022
- Expires
- November 30, 2029
- Mode S code
- AB4267
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 N8242TMatched 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
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2016FA0000146Circuit Breaker · failedPILOT REPORTED THAT THE STROBE LIGHT WAS INOPERATIVE. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE STROBE LIGHT FAILED. THE TECH REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME.SDR 2012FA0000780Switch · failedPILOT REPORTED THAT THE BEACON LIGHT WAS INOPERATIVE. AFTER TROUBLESHOOTING THE TECH FOUND THE BEACON LIGHT TO BE AT FAULT. R & R THE BEACON LIGHT SWITCH AND OPS CHECK WAS NORMAL. THE EXISTING BEACON LIGHT SWITCH WAS INSTALLED 1/9/09 AT 17048 AC HRS WITH A SDR VJ3R2012FA0000027Circuit Breaker · brokenPILOT REPORTED NAVIGATION LIGHTS INOPERATIVE. ON TROUBLESHOOTING, FOUND THE CIRCUIT BREAKER AT FAULT. INSTALLED NEW CIRCUIT BREAKER. OPS CHECKED OK. SWITCH THAT FAILED WAS INSTALLED TO COMPLY WITH AD 2008-13-17. THIS ACFT HAS HAD 6 OF THE IMPROVED CIRCUIT BSDR 2011FA0000239Circuit Breaker · failedPILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT AD 2008-13-17 HAD BEEN COMPLETED 2163 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 8652. NOTICED NEW CIRCUIT BREAKER MFG. NO PROBABLE CAUSE OR RECOMMENDATIONS ATSDR 2010FA0000441Circuit Breaker · inoperative(VJ3R) NO POWER THROUGH THE SWITCH.SDR 2009FA0000026Pump · low pressurePILOT REPORTED INSTRUMENT AIR PRESSURE LOW AT IDLE ON RUN UP. ON TROUBLESHOOTING, THE MECHANIC DETERMINED THE AIR PUMP WAS NOT PRODUCING ENOUGH PRESSURE AT IDLE. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)SDR 2003FA0000767Pump · inoperativeFLIGHT CREW REPORTED THAT GYRO WOULD NOT ERECT AT LOW RPM. DISCOVERED LOW INSTRUMENT AIR PRESSURE. REPLACED AIR PUMP AND SYSTEM OPS CHECKED NORMAL. NO RECOMMENDATION AT THIS TIME.SDR 2003FA0000495Pump · 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 HIGHT RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANES SDR VJ32002F00015Relay · intermittentLANDING GEAR WOULD NOT COME DOWN, RELAY INTERMITTENT IN OPERATION. NEW RELAY INSTALLED AND FUNCTIONAL OPERATION ON THE LANDING GEAR WAS PERFORMED CYCLING THE GEAR MANY TIMES, LANDING GEAR OPERATION CHECKED, NORMAL.SDR 2002FA0000337Master Cylinder · inoperativeBRAKE MASTER CYLINDER WILL NOT HOLD PRESSURE, WHEN PRESSURE IS APPLIED TO THE BRAKE IT BLEEDS DOWN. REMOVED AND INSTALLED NEW MASTER CYLINDER, OPERATION CHECKED NORMAL.SDR VJ32002F00012Pump · inoperativeLOW OUTPUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.SDR VJ32002F00006Motor · inoperativeMOTOR SLOW TO RETRACT AND EXTEND GEAR. MOTOR VERY NOISEY. MOTOR SENT IN FOR WARRANTY.SDR VJ32002F00005Relay · failedLANDING 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 97ZZZX874Spar · crackedINSPECTION FOUND CRCKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER. SUBMITTER STATED THIS IS THE 17TH AIRCRAFT REPORTED.
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
Earlier aircraft with this N-number · 3
These aircraft carried N8242T before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.