Beech 35-C33

Service difficulty reports · 23

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Query with SQL
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 = '35C33'
  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 2019FA0000248Stop Pin · backed outTHE FULL RICH STOP PIN ON FUEL INJECTION CONTROL ASSEMBLY (PN 629904-2A11) BACKED COMPLETELY OUT AFFECTING THE MIXTURE WHEN THE MIXTURE CONTROL WAS IN THE FULL RICH POSITION. THE RESULT WAS REDUCED POWER AT FULL THROTTLE THAT WAS RECOVERED BY ADJUSTING THE MIXAug 12, 2019 · N9402S · Beech 35C33 · Engine Fuel and ControlSDR 2016FA0000036Pickup · failedELECTRIC MAGNETO FAILED. TROUBLESHOOT FOUND MAGNETIC PIC-UP CIRCUIT OPEN. REPLACED WITH NEW AND RUN CHECK SATISFACTORY. REMOVED PART APPEARS TO HAVE DEBONDED FROM CYLINDER AND THERE IS EVEDENCE THAT IT CONTACTED THE CRANK TRIGGER. OAT TEMPERATURE WAS JUST Jan 11, 2016 · N944CP · Beech 35C33 · Magneto/DistributorSDR 2015FA0000059Piston · brokenDURING AN ANNUAL INSPECTION, THE QUICK DRAIN OIL DRAIN VALVE WOULD NOT LOCK OPEN. A BLOCK OF WOOD WAS USED TO WEDGE UNDER THE DRAIN VALVE TO HOLD IT OPEN. AFTER THE OIL WAS DRAINED, THE VALVE WAS REMOVED AND THE VALVE LOCKED OPEN NORMALLY. LOOKED UP INTO THOct 27, 2014 · N5878S · Beech 35C33 · Reciprocating Engine Power SectionSDR 2010FA0000060Hub · mismanufacturedPROPELLER FACTORY NEW IN 12/10/99. PROPELLER HUB FOUND AT O/H TO BE UNAIRWORTHY DUE TO CYLINDER HOLES DEPTH DRILLED BY FACTORY TOO DEEP. 3 SMALL DIMPLES NOTED ON UNDERSIDE OF HUB ON INSPECTION. MFG HAS REJECTED HUB. FACTORY HAD TO HAVE IMPROPERLY DRILLED HUJan 19, 2010 · N1310A · Beech 35C33 · Propeller Hub SectionSDR 2008FA0000907Cylinder · crackedANNUAL INSP REVEALED A LARGE QUANITY OF VERY BLACK OIL RUNNING DOWN THE ENGINE MOUNT LEG AND AIRFRAME STRUCTURE. FURTHER INVESTIGATION FOUND THE LEAK TO ORIGINATE AT THE HEAD TO BARREL CONNECTIONS OF CYLINDERS NR 1, AND NR 3. COMPRESSION CHECK USING AN INPUTDec 8, 2008 · N653P · Beech 35C33 · Reciprocating Engine Cylinder SectionSDR 2008FA0000714V-Belt · departedPILOT REPORTED LOSS OF ELECTRICAL POWER IN CRUISE FLIGHT DURING NIGHT VFR. V-BELT OBSERVED MISSING FROM ACCESSORY CASE ABSENT FROM ALTERNATOR PULLEY. V-BELT APPARENTLY LOST IN FLIGHT THROUGH OPENING IN LOWER COWLING. OWNER REPORTS THAT ONLY 25-30 HOURS WAS PUTOct 9, 2004 · N55FL · Beech 35C33 · AC Generation SystemSDR 2003FA0001005Adapter · wornENGINE DEVELOPED OIL LEAK, FOUND THIS ADAPTER LEAKING AT THREADS, LOCKING NUT SAFETY WAS INTACT, TORQUE DOPE WAS INTACT. ALL REQUIREMENTS OF AD 96-12-22 WERE MET AS PREVIOUSLY INSPECTED 18 HOURS BEFORE FAILURE.Sep 5, 2003 · N866P · Beech 35C33 · Reciprocating Engine Oil SystemSDR AUS20030676Spar · corroded(AUS) WING SPARS PN 35110061-1 (LT) AND PN 351100612 (RT) CONTAINED EXFOLIATION CORROSION IN THE UPPER AND LOWER SPAR CAPS.Mar 28, 2003 · Beech 35C33 · Wing SparSDR 2001FA0000367Antenna · crackedA/C ARRIVED WITH AN ANTENNA 'FLUTTERS' SQUAK. UPON INSPECTION OF VHF COMM ANTENNA, IT WAS NOTED THAT THE ANTENNA WAS INSTALLED WITH NO SUPPORTING DOUBLER. UPON ANTENNA REMOVE, A 5.5 INCH RADIAL CRACK WAS DISCOVERED AROUND THE ANTENNA BASE. THE ADJOINING STRAug 16, 2001 · N6124V · Beech 35C33 · VHF Communications SystemSDR 2001F00363Antenna · crackedAIRCRAFT ARRIVED WITH AN ANTENNA 'FLUTTERS' SQUAWK. UPON INSPECTION OF VHF COMM ANTENNA, IT WAS NOTED THAT THE ANTENNA WAS INSTALLED WITH NO SUPPORTING DOUBLER. UPON ANTENNA REMOVAL, A 5.5 INCH RADIAL CRACK WAS DISCOVERED AROUND THE ANTENNA BASE. THE ADJOINAug 16, 2001 · N6124V · Beech 35C33 · VHF Communications SystemSDR SW15200110536Bulkhead · crackedDURING 100 HOUR INSPECTION FOUND CRACKS IN THE DOUBLER TAIL, A CRACK ON THE RIGHT HAND SKIN SECTION AND A CRACK ON THE AFT BULKHEAD APPROX 1 INCH AT THE BEGINNING OF THE RADIUSED AREA RADIATING OUTBOARD .7500 ON THE RIGHT SIDE AND .5000 ON THE LEFT SIDE. THEMar 28, 2001 · N1444M · Beech 35C33 · Fuselage Main, BulkheadSDR SW15200110535Bushing · improper partTHE INCORRECT BUSHING WAS IDENTIFIED DURING DEMINSIONAL INSPECTION OF THE COUNTER- WEIGHT PRIOR TO INSTALLATION.Mar 26, 2001 · N94SS · Beech 35C33 · Elevator StructureSDR SW15200110531Doubler · crackedDURING 100 HOUR INSPECTION FOUND CRACKS IN THE DOUBLER TALL PN 002440000143. THE DOUBLER IS CRACKED JUST FORWARD OF THE AFT BULKHEAD APPROX 1 INCH JUST BEFORE THE RADIUSED AREA EXTENDING OUTBOARD .2500.Mar 26, 2001 · N94SS · Beech 35C33 · Fuselage Main, Plate/SkinSDR 20000620SH031Bulkhead · crackedCRACKS FORMED AROUND 4 OF ATTACHING BOLTS IN BULKHEAD IN USE LESS THAN 100 HOURS. ATTACHING FLANGE APPEARS TO BE RUBBING AGAINST HUB. FLANGE IS MISFORMED. MANUFACTURING DEFECT. (X)Jun 7, 2000 · N6134V · Beech 35C33 · Propeller Spinner SectionSDR AU990714Spar · corroded(AUS) LEFT AND RIGHT WING UPPER SPARS CONTAINED SEVERE INTERGRANNULAR CORROSION. ON THE LT WING A SECTION OF THE REAR HINGE HAD BEEN REMOVED WITH NO MATERIAL REPLACED. ON THE RT WING A SUSPECT REPAIR HAD BEEN CARRIED OUT WITH A DOUBLER ADDED. SUBMITTER SUSPEJul 13, 1999 · Beech 35C33 · Wing SparSDR AU980599Bracket · corroded(AUS) LT MAIN LANDING GEAR UPLOCK BRACKET CORRODED IN THE AREA OF THE UPLOCK PIVOT POINT. PART 5,634.May 26, 1998 · Beech 35C33 · Landing Gear Retraction/Extension SystemSDR AU980158Valve · leaking(AUS) NO1 CYLINDER EXHAUST VALVE LEAKING AND VALVE GUIDE WORN (STILLWITHIN LIMITS). NO3 CYLINDER INLET VALVE LEAKING.Feb 16, 1998 · Beech 35C33 · Reciprocating Engine Cylinder SectionSDR AU971466Hose · faulty(AUS) ALL FLUID HOSES IN ENGINE COMPARTMENT NOT PROTECTED BY FIRE SLEEVES. PERSONNEL/MAINTENANCE ERROR.Nov 21, 1997 · Beech 35C33 · Powerplant SystemSDR 97ZZZX3154Hub · crackedPROPELLER RECEIVED FOR INSPECTION OF RED DYE OIL LEAK (SMALL). DISASSEMBLED PROPELLER, INSPECTED HUB WITH 10X POWER MICROSCOPE, FOUND CRACK IN NR 2 BLADE SOCKET, LAST THREAD IN 8 O'CLOCK POSITION, 1.50 INCHES TO 2 INCHES LONG. NOTE: THIS PROPELLER HAS TTSN Jul 2, 1997 · N5908S · Beech 35C33 · Propeller Hub SectionSDR 97ZZZX1200Shuttle Valve · failedCHECK VALVE FAILED ON ENGINE DRIVEN VACUUM PUMP. SIDE RIVET HEAD SEPARATED FROM VALVE ASSEMBLY. RENDERED VALVE INOP.Mar 5, 1997 · N4887J · Beech 35C33 · Vacuum Distribution SystemSDR 95ZZZX3611Spar · crackedPERFORMING AD 93-24-03 FOUND UPPER RUDDER SPAR CRACKED.Jul 17, 1995 · N6142V · Beech 35C33 · Rudder, Spar/RibSDR 96ZZZX960Spar · crackedPERFORMING AD 93-24-03 FOUND CRACKED RUDDER SPAR UNDER UPPER HINGE BRACKET.May 18, 1995 · N6142V · Beech 35C33 · Rudder, Spar/RibSDR 95ZZZX946Hub · crackedPROPELLER IN FOR 5 YEAR TBO FOUND DURING OHC. FOUND HUB CRACKED.Feb 14, 1995 · N5827S · Beech 35C33 · Propeller Hub Section
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