# Service difficulty reports: N8268T A list on [N8268T](https://openairdocs.org/aircraft/N8268T.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 2018FA0000413](https://openairdocs.org/sdr/2018FA0000413.md): Display · failed · Oct 9, 2018 · N8268T · Beech F33A · Central Display > THE REMOTE AUXILIARY DISPLAY WENT INOPERATIVE DURING TAKE-OFF. - [SDR 2017FA0000653](https://openairdocs.org/sdr/2017FA0000653.md): Circuit Breaker · failed · Dec 18, 2017 · N8268T · Beech F33A · Light System Wiring > PILOT REPORTED LANDING LIGHT INOP. TROUBLESHOOTING DISCOVERED CIRCUIT BREAKER HAD FAILED. - [SDR VJ3S2016FA0000043](https://openairdocs.org/sdr/VJ3S2016FA0000043.md): Circuit Breaker · failed · Jan 29, 2016 · N8268T · Beech F33A · Light System Wiring > PILOT REPORTED THAT THE ANTI-COLLISION LIGHT WAS INOPERATIVE. THE TECH TROUBLESHOT THE SYS AND DISCOVERED THE ANTI-COLLISION LIGHT FAILED. THE TECH REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME. - [SDR 2011FA0000419](https://openairdocs.org/sdr/2011FA0000419.md): Pneumatic System · failed · Jun 25, 2011 · N8268T · Beech F33A · Pneumatic Distribution System > PILOT REPORTED INSTRUMENT AIR PRESSURE WAS LOW. UP ON 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 PUMP, SYSTEM WORKED NORMAL. NO - [SDR 2011FA0000392](https://openairdocs.org/sdr/2011FA0000392.md): Circuit Breaker · failed · Jun 23, 2011 · N8268T · Beech F33A · Exterior Lighting > PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CB/ SWITCH TO BE AT FAULT. SWITCH WAS PREVIOUSLY REPLACED 756.0 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 3024. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. - [SDR 2010FA0001144](https://openairdocs.org/sdr/2010FA0001144.md): Circuit Breaker · failed · Oct 31, 2010 · N8268T · Beech F33A · Light System Wiring > PILOT REPORTED LANDING LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1770 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 7080. NOTICED NEW CIRCUIT BREAKER MFG. NO PROBABLE CAUSE OR RECOMMENDATIONS - [SDR 2010FA0000523](https://openairdocs.org/sdr/2010FA0000523.md): Circuit Breaker · inoperative · Jun 4, 2010 · N8268T · Beech F33A · Exterior Lighting > PILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1516 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 6064. NOTICED NEW CIRCUIT BREAKER, NO PROBABLE CAUSE OR RECOMMENDATIONS AT THI - [SDR 2009FA0000094](https://openairdocs.org/sdr/2009FA0000094.md): Fuel Control · faulty · Feb 8, 2009 · N8268T · Beech F33A · Fuel Control/Turbine Engines > PILOT REPORTED ENGINE QUIT WHEN EXITING RUNWAY. UPON TROUBLESHOOTING, MECHANIC FOUND FCU HAD A ROUGH SPOT WHEN MOVING FUEL CONTROL ARM. FCU WAS REPLACED AND RUN-UP WAS PERFORMED AND OPS CHECK GOOD. NO RECOMMENDATIONS AT THIS TIME. (K) - [SDR 2005FA0001265](https://openairdocs.org/sdr/2005FA0001265.md): Nozzle · broken · Aug 23, 2005 · N8268T · Beech F33A · Fuel Injector Nozzle > ON ROUTINE PHASE INSPECTION THE FUEL INJECTOR NOZZLES WERE REMOVED FOR CLEANING, AT THIS TIME THE MECHANIC DIDN’T NOTICE ANY DEFECTS. THE NOZZLES WERE THEN PLACED IN A CLEANING TANK AND AFTER REMOVING THEM FROM THE TANK THE MECHANIC NOTICED THE RING THAT THE - [SDR 2005FA0000628](https://openairdocs.org/sdr/2005FA0000628.md): Relay · intermittent · Apr 25, 2005 · N8268T · Beech F33A · Landing Gear System Wiring > PILOT SELECTED GEARDOWN AND NOTHING HAPPENED, PILOT THEN CYCLED GEAR SELECTOR TWICE THEN GEAR WENT DOWN, AC RETURNED TO BASE. ON TROUBLESHOOTING, MECHANIC CYCLED GEAR 4 TIMES THEN RELAY FAILED, PROBABLE CAUSE AT THIS TIME UNKNOWN. INSTALLED NEW AND IMPROVED - [SDR 2003FA0000727](https://openairdocs.org/sdr/2003FA0000727.md): Pump · inoperative · Jun 18, 2003 · N8268T · Beech F33A · Pneumatic Distribution System > PUMP OUTPUT DECREASED AS ENGINE WARMED UP UNTIL IT BECAME UNACCEPTABLE AT LOWER RPM. AT 1000 RPM PRESSURE DROPPED BELOW 3 INCHES ON INDICATOR. TESTED AIR SYSTEM FOR LEAKS AND FOUND NONE. CHECKED REGULATOR AND MANIFOLD VALVE, REPLACED BOTH THE SYSTEM STILL F - [SDR 2003FA0000724](https://openairdocs.org/sdr/2003FA0000724.md): Power Supply · inoperative · Jun 17, 2003 · N8268T · Beech F33A · Exterior Lighting > TAIL STROBE WAS FOUND INOPERATIVE BY THE MECHANIC PERFORMING THE PHASE INSPECTION. ON FURTHER INVESTIGATION FOUND THE POWER SUPPLY INOPERATIVE. TIME SINCE REPAIRED 2295. - [SDR VJ32002F00076](https://openairdocs.org/sdr/VJ32002F00076.md): Pump · failed · Sep 20, 2002 · N8268T · Beech F33A · Pneumatic System > DURING 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 2002FA0000471](https://openairdocs.org/sdr/2002FA0000471.md): Brushes · worn · Apr 2, 2002 · N8268T · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. THE WEARER ON THIS BRUSH IS ABOVE NORMAL FOR 500 HO - [SDR 2002FA0000470](https://openairdocs.org/sdr/2002FA0000470.md): Brushes · worn · Apr 2, 2002 · N8268T · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. THE WEARER ON THIS BRUSH IS ABOVE NORMAL FOR 500 HRS - [SDR 2001FA0000509](https://openairdocs.org/sdr/2001FA0000509.md): Brushes · worn · Oct 29, 2001 · N8268T · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. - [SDR 2001FA0000506](https://openairdocs.org/sdr/2001FA0000506.md): Brushes · worn · Oct 29, 2001 · N8268T · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. - [SDR VJ32001F00008](https://openairdocs.org/sdr/VJ32001F00008.md): Brushes · worn · Oct 29, 2001 · N8268T · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP, WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. T - [SDR VJ32001F00003](https://openairdocs.org/sdr/VJ32001F00003.md): Brushes · worn · Oct 29, 2001 · N8268T · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISRUPTER BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. TH - [SDR 20010209CW002](https://openairdocs.org/sdr/20010209CW002.md): Pump · leaking · Dec 27, 2000 · N8268T · Beech F33A · Engine Fuel Pump > ENGINE DRIVEN FUEL PUMP LEAKING OIL FROM DRAIN. - [SDR 97ZZZX2082](https://openairdocs.org/sdr/97ZZZX2082.md): Bungee Spring · broken · Apr 9, 1997 · N8268T · Beech F33A · Aileron Control System > PILOT REPORTED A LOUD POPPING SOUND AND A BIND IN THE RUDDER PEDALS. A MECHANIC PERFORMED ROUTINE INSPECTION AND FOUND UPPER FORWARD RUDDER AILERON BUNGEE SPRING HAD BROKEN IN HALF ON THE CLIP END SIDE. SUBMITTER SUGGESTED DURING ROUTINE 100-HOUR ANNUAL PROG - [SDR 96ZZZX3778](https://openairdocs.org/sdr/96ZZZX3778.md): Carry-Through · cracked · Jul 11, 1996 · N8268T · Beech F33A · Wing Spar > INSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER. - [SDR 95ZZZX2709](https://openairdocs.org/sdr/95ZZZX2709.md): Bulkhead · cracked · May 10, 1995 · N8268T · Beech F33A · Fuselage Main, Bulkhead > FOUND DURING PROGRESSIVE INSPECTION AT ATCA. THE UPPER LEFT CORNER OF THE AFT BULKHEAD CRACKED APPROXIMATELY 1 INCH ALONG BULKHEAD BEND. ALSO, TWO CORNER CRACKS IN THE UPPER DOUBLER AT AFT BULKHEAD. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N8268T' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8268T/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.