N781EA, cancelled Oct 5, 2019

Service difficulty reports · 17

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N781EA' AND deregistration_id = 'N781EA-2019-10-05'
  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 HYIA20150813001Balance Tube · defectivePILOT REPORTED FUEL SMELL IN FLIGHT. R & R THE LT ENG BALANCE TUBE & FWD DRAIN. LEAK CHECKED GOOD WITH NO DEFECT NOTED. ADDITIONALLY CAS ORDERED THAT ALL FUEL LINES & FUSELAGES BE INSPECTED, AS WELL AS RE-INSPECTING THE BALANCE TUBE & FUEL DRAIN FOR POSSIBLAug 10, 2015 · N781EA · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA20150729001O-Ring · leakingPILOT REPORTED FUEL ODOR IN COCKPIT. R & R THE RIGHT FUEL BOWL O-RING, NO FURTHER DEFECTS NOTED.Jul 26, 2015 · N781EA · Cessna 402C · Fuel Control/Reciprocating EnginesSDR HYIA20150720001Sealant · unknownPILOT REPORTED FUEL SMELL IN CABIN. ENCAPSULATED & FILLET SEALED RT WING TE AFT SPAR WEB RIVETS. LEAK CHECKED GOOD IAW AMM CH 28-10.Jul 17, 2015 · N781EA · Cessna 402C · Wing Miscellaneous StructureSDR HYIA20150723001Structure · leakingPILOT REPORTED FUEL SMELL IN CABIN. FOUND A LEAK IN THE LT OTBD FLAP RIB AREA. SEALED INSIDE FUEL TANK WITH PRC. LEAK CHECKED GOOD.Jul 10, 2015 · N781EA · Cessna 402C · Wing Miscellaneous StructureSDR HYIA20150706001Tube · leakingPILOT REPORTED FUEL SMELL IN COCKPIT. INSPECTED ALL FUEL LINES IN CABIN & ON BOTH WINGS. FOUND LT ENG BALANCE TUBE LEAKING. R & R LT ENG BALANCE TUBE, LEAK CHECKED GOOD.Jul 3, 2015 · N781EA · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA03272015003Beam · crackedTHE RT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY FROM NACELLE, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDIMar 27, 2015 · N781EA · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20140523003Indicator · separatedELEVATOR JAMMED ON TAKEOFF, COULD NOT PULL YOKE BACK TO ROTATE. VOR 2 INDICATOR CASE DROPPED ONTO THE CONTROL YOKE PREVENTING FULL REARWARD TRAVEL. TAKEOFF WAS ABORTED WITH NO FURTHER INCIDENT. FOUND VOR INDICATOR BACK CASE SEPARATED FROM FRONT OF INDICATORMay 21, 2014 · N781EA · Cessna 402C · Visual Omnirange (VOR) SystemSDR HYIA20121108001Attach Fitting · crackedDURING REPLACEMENT OF WING SPAR STRAP ON RT WING, OTBD ENGINE BEAM FITTING WAS DISCOVERED TO BE CRACKED IN TWO LOCATIONS. OPENNov 6, 2012 · N781EA · Cessna 402C · Wing, Attach FittingsSDR HYIA20120708001Brake · malfunctionedWHILE TAXIING, THE PILOT REPORTED A LOSS OF BRAKING PRESSURE THAT AFFECTED THE RT BRAKE. UPON INSPECTION BY MX, A CORRECTIVE ACTION OF SERVICING THE BRAKE MASTER CYLINDER. NO VISIBLE LEAKS WERE NOTED UPON INSPECTION.Jul 8, 2012 · N781EA · Cessna 402C · Landing Gear Brake SystemSDR HYIA20140415061Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE May 31, 2011 · N781EA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415028Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OFeb 11, 2011 · N781EA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA781RHENG1115Pump · faultyCREW REPORTED, AFTER LEVELING OFF IN CRUISE, RT ENGINE FUEL FLOW STARTED TO FLUCTUATE SLIGHTLY. AFTER ABOUT 30 SECONDS, FUEL FLOW FLUCTUATION INCREASED IN LARGER INCREMENTS, THEN WENT TO ZERO. AT THIS POINT THE ENGINE QUIT. AUXILIARY PUMP WAS TURNED ON HIGH ANov 14, 2010 · N781EA · Cessna 402C · Engine Fuel PumpSDR HYIA781EA LFTWGSpar Cap · corrodedPRIOR TO REPAINTING OF ACFT, STRIPPING PROCESS REVEALED SIGNIFICANT INTERGRANNULAR CORROSION ON THE LT WING OTBD AFT SPAR, LWR CAP. MX CURRENTLY EVALUATING POSSIBLE REPAIR OR REPLACEMENT OF LT AFT OTBD SPAR, LWR CAP.Nov 5, 2009 · N781EA · Cessna 402C · Wing SparSDR HYIA781EA AVMSTRMaster Switch · unserviceablePREFLIGHT, CREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE. MX R & R CIRCUIT BREAKER SWITCH. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE.Sep 29, 2009 · N781EA · Cessna 402C · DC Power Distribution SystemSDR HYIA781EAFitting · leakingON CLIMB-OUT PILOT NOTICE FUEL LEAKING FROM BELOW THE COCKPIT INSTRUMENT PANEL. MX INSPECTED ADJUSTED LINE ON FUEL BLEED FITTING UNDER INSTRUMENT PANEL. OPERATIONAL CHECKS AND LEAKS CHECKS WERE PERFORMED WITH NO DEFECTS NOTED.Mar 20, 2009 · N781EA · Cessna 402C · Aircraft Fuel Distribution SystemSDR 1350502N781EACircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER.Jul 13, 2006 · N781EA · Cessna 402C · Flight Control System WiringSDR HYI2002F00014Gyro · failedCREW LOST HEADING INFORMATION IN CRUISE AT 5000 FT. DECLARED EMERGENCY AND RECEIVED NON GYRO VECTORS TO ISL 15 HYA. ATTEMPTED TO RESET GYRO C/B- WOULD NOT RESET. LANDED WITHOUT INCIDENT. MECHANIC CHANGED REMOTE GYRO (UG102). AIRCRAFT RETURNED TO SERVICE.Aug 30, 2002 · N781EA · Cessna 402C · Attitude Gyro and Indicating System
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