- Registered owner
- Flying Bull Aviation LLC
- Location
- Santee, CA
- Owner type
- LLC
- Serial number
- CE-1300
- Year built
- 1988
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- December 5, 1988
- Certificate issued
- May 23, 2019
- Expires
- May 31, 2029
- Mode S code
- A0E41A
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 N1569PMatched 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 VJ3R2015FA0000623Circuit Breaker · failedPILOT REPORTED THAT THE ALTERNATOR WAS INOPERATIVE. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE ALTERNATOR CIRCUIT BREAKER SWITCH FAILED. THE TECH REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME.SDR 2014FA0000476Circuit Breaker · failedPILOT REPORTED THAT THE BEACON LIGHT WAS INOPERATIVE. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE BEACON LIGHT FAILED. THE TECHNICIAN REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME.SDR 2013FA0000676Circuit Breaker · failedRESISTANCE READING OUT OF LIMITS IN "ON" AND "OFF" POSITION.SDR VJ3R20130507001Relay · wornSMOKE IN CABIN AFTER GEAR RETRACTION FOR LANDING. PULLED LANDING GEAR CIRCUIT BREAKER, SMOKE ODOR LESSENED, LANDED ACFT AS PLANNED. JACKED ACFT, OPERATED GEAR AND IT OVERTRAVELED AGAINST HARD STOP ON GEARBOX. REPLACED MOTOR, SWUNG GEAR AGAIN AND IT OVERTRAVSDR VJ3R201301230001Cushion · intermittentUP CUSHION INCONSISTENT DURING LANDING GEAR OPERATIONAL CHECK.SDR 2012FA0000432Circuit Breaker · failedPILOT REPORTED THAT THE LANDING LIGHT WAS NOT WORKING. DURING TROUBLESHOOTING FOUND THAT THE LANDING LIGHT CIRCUIT BREAKER WAS TO BE AT FAULT. INSTALLED NEW LANDING LIGHT CIRCUIT BREAKER AND OPS CHECKED GOOD.SDR 2011FA0000445Pump · failedPILOT REPORTED GYRO WARNING LIGHT CAME ON IN FLIGHT. TROUBLESHOOTING, THE MECHANIC NOTICED ON INITIAL RUN UP PRESSURES WERE WITHIN LIMITS, AFTER ENGINE STARTED TO WARM UP THE PRESSURE STARTED TO DROP BELOW LIMITS. INSTALLED NEW AIR PUMP SYS WORKED NORMAL. NO SDR 2011FA0000041Circuit Breaker · failedPILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT. CIRCUIT BREAKER/SWITCH HAD BEEN REPLACED 500 FLIGHT HOURS PRIOR AND ESTIMATED 2000 CYCLES.SDR 2011FA0000035Circuit Breaker · odorPILOT REPORTED A BURNED ELECTRICAL ODOR. ODOR WENT AWAY WHEN LIGHTS WERE TURNED OFF. TECH DISCOVERED THE LANDING LIGHT/ CIRCUIT BREAKER TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1345 FLIGHT HOURS PRIOR AND ESTIMATED 21520 CYCLES.SDR 2010FA0000293Circuit Breaker · failed(VJ3R) PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 859 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 3436. NOTICED NEW CIRCUIT BREAKER. NO PROBABLE CAUSE OR RECOMMENDATIONS ATSDR 2005FA0001090Pump · vibratesPILOT REPORTED WHINING NOISE COMING FROM ENGINE AND FELT A VIBRATION COMING THROUGH THE MIXTURE CONTROL CABLE. TROUBLESHOOTING, THE MECHANIC FOUND THE AIR PUMP WAS VIBRATING. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)SDR 2001FA0000569Distributor Blk · inoperativeMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.SDR 2001FA0000567Distributor Blk · inoperativeMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.(K)SDR 20001019SH001Pump · defectiveUNABLE TO ADJUST FUEL FLOW TOP END AND IDLE MIXTURE. (X)
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 · 1
This aircraft carried N1569P before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.