Beech F33A

Service difficulty reports · 557

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duckdb -csv -c "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 aircraft_model_key = 'F33A'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2003FA0000493Pump · 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 NOT WORKING PROPERLY. BELIEVE DRY AIR PUMP VANEMay 5, 2003 · N1556A · Beech F33A · Pneumatic Distribution SystemSDR 2003FA0000490Throttle Cable · jammedPILOT REPORTED THROTTLE WAS HARD TO MOVE. ON FURTHER INVESTIGATION FOUND THROTTLE BUTTON WOULD JAM AND NOT RELEASE. THESE CABLES ARE PRETTY RELIABLE, AT THIS TIME, NO PROBLEM, CAUSE OR RECOMMENDATIONS TO PREVENT THIS FROM RECURRING.Apr 29, 2003 · N1570A · Beech F33A · Power LeverSDR XGN2003F00000Bearing · failedIN FLIGHT, AIRCRAFT LANDED WITHOUT INCIDENT. THE ALTERNATOR DRIVE END BEARING FAILED CAUSING THE ALTERNATOR ROTOR ASSEMBLY WITH THE DRIVEN GEAR TO EXTEND INTO THE ALTERNATOR DRIVE GEAR. THE MISALIGNMENT OF THESE TWO GEARS CAUSED THE ATTACH BOLTS ON THE ALTERMar 1, 2003 · N1096W · Beech F33A · AC Generator-AlternatorSDR VJ32003F00019Pump · 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 HIGHTER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANEJan 15, 2003 · N8173C · Beech F33A · Pneumatic Distribution SystemSDR VJ32003F00020Pump · 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 HIGHTER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANEJan 14, 2003 · N5540P · Beech F33A · Pneumatic Distribution SystemSDR VJ32003F00000Pump · 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 HIGHT RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERTY. BELIEVE DRY AIR PUMP VANEDec 31, 2002 · N5530A · Beech F33A · Pneumatic Distribution SystemSDR VJ32003F00013Pump · 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.Dec 12, 2002 · N5582X · Beech F33A · Pneumatic Distribution SystemSDR VJ32003F00017Pump · 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.Nov 27, 2002 · N1565A · Beech F33A · Pneumatic Distribution SystemSDR VJ32003F00015Pump · 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.Nov 25, 2002 · N8251C · Beech F33A · Pneumatic Distribution SystemSDR VJ32003F00016Pump · failedDURING GROUND RUN UP OUTPUT OF ENGNE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. DRY AIR PUMP SHAFT SHEARED.Oct 22, 2002 · N8101C · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00093Pump · 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. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Oct 14, 2002 · N1565A · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00087Bulkhead · crackedDURING A PROGRESSIVE INSPECTION OF THE EMPENNAGE SECTION OF THIS AIRCRAFT A MECHANIC FOUND A CRACK IN THE RADIUS BEND AREA UPPER LEFT CORNER OF THE BULKHEAD.Oct 4, 2002 · N6311Z · Beech F33A · Empennage StructureSDR VJ32002F00086Bulkhead · crackedDURING PROGRESSIVE INSPECTION OF THE EMPENNAGE SECTION OF THIS AIRCRAFT, A MECHANIC FOUND A CRACK IN THE RADIUS BEND AREA UPPER LEFT CORNER OF THE BULKHEAD.Oct 4, 2002 · N38071 · Beech F33A · Empennage StructureSDR VJ32002F00085Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT DURING A FLIGHT.Oct 4, 2002 · N5544A · Beech F33A · Main Landing GearSDR 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.Oct 4, 2002 · N5609S · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00078Magneto · failedDURING FLIGHT, CREW REPORTED ROUGH ENGINE. TROUBLESHOOTING BY MECHANIC BELIEVE RELATED TO MAGNETO NOT FIRING AT ATTITUDE. RETURNED TO MANUFACTURE FOR WARRANTY AND INSPECTION OF INTERNAL PARTS FOR POSSIBLE FAILURE.Sep 20, 2002 · N8252T · Beech F33A · Magneto/DistributorSDR VJ32002F00077Pump · 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.Sep 20, 2002 · N5544A · Beech F33A · Pneumatic SystemSDR VJ32002F00076Pump · 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.Sep 20, 2002 · N8268T · Beech F33A · Pneumatic SystemSDR VJ32002F00074Pump · 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.Sep 3, 2002 · N8112T · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00073Pump · 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. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Sep 3, 2002 · N5519A · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00072Pump · 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. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP. RECOMMENDATION FOR CORRECTIVE ASep 3, 2002 · N1569A · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00071Pump · 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.Sep 3, 2002 · N5599P · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00058Control Cable · frayedCABLE FRAYED WHERE IT PASSES THROUGH A PULLEY ASSEMBLY. CAUSE MAY BE DUE TO PULLEY NOT ROTATING WHEN CABLE IS EXERCISED. RECOMMEND TO INSTALL SEALED BEARING TYPE PULLEY IN THESE AREAS.Aug 6, 2002 · N8101C · Beech F33A · Aileron Control SystemSDR VJ32002F00054Relay · failedLANDING GEAR FAILED TO COME UP IN FLIGHT. JACKED AIRCRAFT AND OPS CHECKED LANDING GEAR SYSTEM AND RELAY FAILED. TAPPED ON UP SIDE OF RELAY AND POINTS RELEASE ALLOWING GEAR TO ROTATE UP. THIS RELAY HAD A MINIMUM OF 1031 GEAR CYCLES ON IT RECOMMENDATION FOR Jul 11, 2002 · N5540P · Beech F33A · Landing Gear Retraction/Extension SystemSDR VJ32002F00052Relay · failedLANDING GEAR FAILED TO COME UP IN FLIGHT. JACKED AIRCRAFT AND OPS CHECKED LANDING GEAR SYSTEM AND RELAY FAILED. TAPPED ON UP SIDE OF RELAY AND POINTS RELEASE ALLOWING GEAR TO ROTATE UP. THIS RELAY HAD A MINIMUM OF 1032 GEAR CYCLES ON IT. RECOMMENDATION FORJul 11, 2002 · N8112T · Beech F33A · Landing Gear Retraction/Extension SystemSDR VJ32002F00053Relay · failedDURING FLIGHT LANDING GEAR FAIL TO RETRACT. UP SIDE OF DYNAMIC RELAY POINTS FAIL TO RELEASE. PROBABLE CAUSE IS HEAT AND NUMBER OF GEAR RECYCLED. RECOMMENDATIONS FOR PREVENTIVE RECURRENCE DEVELOP BETTER RELAY.Jul 8, 2002 · N1565A · Beech F33A · Landing Gear Retraction/Extension SystemSDR VJ32002F00051Trim Switch · failedDURING GROUND RUN, TESTED RUDDER TRIM SWITCH. RUDDER TRIM MOVED TO THE LEFT BUT WOULD NOT MOVE TO THE RIGHT. PROBABLE CAUSE IS INTERNAL FAILURE OF THE SWITCH CIRCUITS.Jul 5, 2002 · N8112T · Beech F33A · Rudder Tab Control SystemSDR VJ32002F00049Pump · failedDURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT 800 RPM. RAN AIRCRAFT UP TO 1600 RPM BEFORE PRESSURE READ 4.5. CHECKED PRESSURE SYSTEM FOR LEAKS AND CHECKED REGULATOR ALL CHECKED WELL.Jul 3, 2002 · N5585Y · Beech F33A · Pneumatic SystemSDR VJ32002F00050Flow Divider · failedAT NORMAL POWER SETTINGS THE ENGINE RAN ROUGH AT 6000 TO 7000 FEET. REMOVED FUEL FLOW MANIFOLD VALVE AND INSTALLED NEW FUEL FLOW MANIFOLD VALVE. GROUND OPERATION OF THE ENGINE CHECKED NORMAL. PART SENT IN FOR WARRANTY.Jun 28, 2002 · N5582X · Beech F33A · Fuel DividerSDR 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 NEJun 17, 2002 · N5609S · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2002FA0000771Flow Divider · fluctuatesFUEL FLOW FLUCTUATES IN-FLIGHT AND THE ENGINE WAS ROUGH RUNNING AT ALTITUDE, AT LOW ALTITUDE THE ENGINE WAS SMOOTH IN OPERATION. OPERATION CHECK OF ENGINE ON THE GROUND FOUND THE FUEL FLOW DIVIDER WOULD FLUCTUATE. REMOVED FLOW DIVIDER AND INSTALLED A NEW OVEJun 11, 2002 · N8240T · Beech F33A · Fuel DividerSDR 2002FA0000770Relay · sticksLANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED IAW MM. INSPECTION OF THE SYSTEM FOUND THAT THE DYNAMIC RELAY WOULD STICK IN THE DOWN POSITION. A NEW DYNAMIC RELAY WAS INSTALLED AND THE SYSTEM OPERATIOJun 11, 2002 · N1569A · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2002FA0000769Motor · noisyGEAR MOTOR MAKES GRINDING NOISE WHEN THE GEAR IS RETRACTED. MOTOR WAS REMOVED AND A NEW MOTOR INSTALLED OPERATION OF THE GEAR SYSTEM IAW MM, CHECKED NORMAL.Jun 11, 2002 · N8252T · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2002FA0000772Pump · failedUNABLE TO MAKE INSTRUMENT AIR PRESSURE AT LOW RPM, INSPECTED SYSTEM AND FOUND THAT THE PUMP WAS MAKING SMALL CHUNKS OF CARBON FOUNDED IN THE REGULATOR AND INLET FILTER. PURGED SYSTEM AND CLEANED LINES IN SYSTEM. NEW INLET AND INLINE FILTER INSTALLED. NEW PUJun 10, 2002 · N1568P · Beech F33A · Vacuum Distribution SystemSDR 2002FA0000715Fuel Control · inoperativeFLUCTUATION IN FUEL FLOW AND UNABLE TO ADJUST IDLE MIXTURE. THEY FOUND THAT THE MIXTURE CONTROL WAS STIFF WHEN MOVED, (POSSIBLE GALLING). FUEL CONTROL WAS REMOVED AND A NEW ONE INSTALLED, ENGINE WAS TRIMMED, TEST FLIGHT CHECKED NORMAL. FUEL CONTROL WAS SENTJun 6, 2002 · N8240T · Beech F33A · Fuel Control/Reciprocating EnginesSDR 2002FA0000716Pump · failedIN FLIGHT, THE ENGINE WAS ROUGH AND FUEL FLOW WAS BELOW NORMAL AND FLUCTUATING AT THAT POWER SETTING. A SAFE LANDING WAS MADE. A GROUND CHECK OF THE ENGINE OPERATION WAS PERFORMED. IT WAS FOUND THAT THE ENGINE DRIVEN FUEL PUMP WAS SUCKING AIR THRU THE CASE Jun 4, 2002 · N8240T · Beech F33A · Engine Fuel PumpSDR AUS20020560Muffler · distorted(AUS) RH MUFFLER BUCKLED AND DISTORTED IN AREA UNDER THE HEATER SHROUD. ONE HEAT TRANSFER STUD MISSING. EXHAUST GAS ESCAPING INTO CABIN HEATER SYSTEM.May 31, 2002 · Beech F33A · Engine Noise SuppressorSDR 2002FA0000657Indicator · inoperativeTHIS IS NEW FROM STOCK AND WAS JUST ORDER FROM MFG. WAS INSTALLED AND THE METER MOVEMENT WAS ONLY .5 OF THE TRAVEL. PART WAS REMOVED AND TESTED ON THE BENCH AND HAD A HIGH AMP DRAW.May 13, 2002 · Beech F33A · Trailing Flap Position Indicating SystemSDR VJ32002F00035Magneto · failedMAGNETO FAILED ON GROUND RUN UP. MAGNETO WAS REMOVED AND A REPAIRED MAGNETO INSTALLED. WHEN THE COVER WAS REMOVED THE DISTRIBUTOR BLOCK WAS FOUNDED TO HAVE A GRAY POWDER DUST ON IT. TOTAL TIME ON MAGNETO FROM NEW IS 95.0 HOURS. PART SENT IN FOR WARRANTY.May 13, 2002 · N5544A · Beech F33A · Magneto/DistributorSDR VJ32002F00037Pump · failedUNABLE TO ADJUST LOW-END FUEL PRESSURE ON TRIM RUN OF A NEW OVERHAULED ENGINE FROM RAM. PUMP WAS REMOVED AND NEW PUMP INSTALLED. COMPLETED TRIM RUNS OF ENGINE. OPERATIONAL CHECK OF ENGINE CHECKED NORMAL. PUMP SENT BACK TO RAM FOR WARRANTY.May 10, 2002 · N38071 · Beech F33A · Engine Fuel PumpSDR 2002FA0000687Filter · crackedDURING INSPECTION OF BRACKET ENGINE INDUCTION AIR FILTER FRAME ASSEMBLY FOUND THE (STEEL) SCREEN CRACKED AND SECTIONS MISSING NEAR THE RIVET RETAINING AREAS. SEE BRACKET AIR FILTER DOCUMENT.May 7, 2002 · N7RQ · Beech F33A · Engine Air Intake SystemSDR VJ32002F00030Magneto · failedMAGNETO FAILED IN FLIGHT AND A SAFE LANDING WAS MADE. GROUND CHECK OF THE MAGNETOS CONFIRMED THAT THE MAGNETO WAS DEAD. MAGNETO WAS REMOVED AND REPAIRED MAGNETO INSTALLED. GROUND OPERATION AND MAGNETO CHECKED NORMAL. PART SENT FOR WARRANTY.May 7, 2002 · N5519A · Beech F33A · Magneto/DistributorSDR VJ32002F00028Pump · inoperativeLOW OUT PUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.Apr 26, 2002 · N1565A · Beech F33A · Pneumatic SystemSDR VJ32002F00027Relay · stuckLANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED IAW MM. INSPECTION OF THE SYSTEM FOUND THAT THE DYNAMIC RELAY WOULD STICK IN THE DOWN POSITION. A NEW DYNAMIC RELAY WAS INSTALLED AND THE SYSTEM OPERATIApr 26, 2002 · N1569A · Beech F33A · Landing Gear Retraction/Extension SystemSDR VJ32002F00022Pump · inoperativeNO INSTRUMENT AIR PRESSURE AT 1000 RPM, SYSTEM CHECKED AND FOUND THE AIR PUMP HAD NO OUTPUT. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. GROUND RUN OF THE AIRCRAFT SYSTEM CHECKED NORMAL.Apr 18, 2002 · N5599P · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00021Relay · stuckLANDING 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 WOULD STICK THREE OUT OF FOUR TIMES WHEN THE GEAR WAS CYCLED. RELAY WAS REMOVApr 9, 2002 · N1556A · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2002FA0000476Brushes · wornMAGNETO 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 HOApr 2, 2002 · N6322A · Beech F33A · Magneto/DistributorSDR 2002FA0000475Brushes · wornMAGNETO 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 HOApr 2, 2002 · N6322A · Beech F33A · Magneto/DistributorSDR 2002FA0000473Pump · inoperativeLOW OUT PUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP, OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.Apr 2, 2002 · N5609S · Beech F33A · Pneumatic SystemSDR 2002FA0000471Brushes · wornMAGNETO 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 HOApr 2, 2002 · N8268T · Beech F33A · Magneto/Distributor
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