N764EA
Service difficulty reports · 20
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 = 'N764EA' AND registry_match = 'registration' 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.
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 = 'N764EA' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HYIA20200226001Heater · odorPILOT REPORTED SMELL OF EXHAUST IN CABIN, UPON INSPECTION MAINTENANCE DID NOT NOTE RESIDUAL SMELL. BELIEVED TO BE ISSUE WITH HEATER COMBUSTION CHAMBER. REMOVED AND REPLACED HEATER WITH NO FURTHER DEFECTS NOTED.SDR HYIA20191007001Spar Cap · crackedDURING A ROUTINE INSPECTION, A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND FORWARD UPPER SPAR CAP. THERE ARE NO OTHER DEFECTS NOTED IN THIS AREA, THIS INCLUDES NO LOOSE OR MISSING FASTENERS. THE CRACK IN THE SPAR CAP WAS CONFIRMED BY SURFACE EDDY CURRENSDR HYIA2019040320001Spar Cap · crackedA CRACK WAS IDENTIFIED AT THE RT SIDE OF LWR FWD CARRYTHROUGH SPAR CAP AFT MOST IB FASTENER LOCATION WHILE PERFORMING NDT PROCEDURE AS AMOC FOR AD2018-03-03R1. THE CRACK WAS CONFIRMED WITH BOLT HOLE EDDY CURRENT AFTER THE FASTENER WAS REMOVED. CRACK DIRECTIOSDR HYIA20180525001Axle · crackedDURING TAXI FOR DEPARTURE, THE CREW REPORTED THE AIRCRAFT PULLED TO THE RIGHT AS IF THE TIRE HAD GONE FLAT. THE AIRCRAFT BECAME DISABLED ON THE TAXIWAY. THE RT AXLE ASSEMBLY HAD FAILED CAUSING THE WHEEL ASSEMBLY TO RUB AGAINST THE RT LANDING GEAR STRUT. UPSDR HYIA20161121001Display · failedPILOT REPORTED A BURNING SMELL IN CABIN, AND RADAR WENT OFF. THE CABIN CIRCUIT BREAKER WAS THEN PULLED. MAINTENANCE INSPECTED AND REPLACED THE WEATHER RADAR DISPLAY WITH NO FURTHER DEFECTS NOTED.SDR HYIA20160912125Piston Ring · brokenCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. INSPECTION FOUND A BROKEN PISTON RING.SDR HYIA20160912124Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160912123Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE, VALVE SEAT SHOWS SIGNS OF DAMAGE.SDR HYIA20160912122Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE, VALVE SEAT SHOWS SIGNS OF DAMAGE.SDR HYIA20160912121Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE, VALVE SEAT SHOWS SIGNS OF DAMAGE.SDR HYIA20160803052Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE CRACKED AND DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160803043Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA03272015001Beam · crackedTHE LT NACELLE OTBD 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 SURROUNDISDR HYIA20131216002Dimmer · malfunctionedSHUT DOWN ENGS & EVACUATED ACFT AFTER DETECTING SMOKE COMING FROM THROTTLE QUADRANT AREA DURING TAXI TO RUNWAY 08. VISUAL INSPECTION OF INSTRUMENT PANEL LIGHT DIMMER ASSEMBLY & FOUND A FAILED RESISTOR INTEGRAL TO ASSEMBLY. REMOVED AFFECTED ASSEMBLY & INSTALLSDR HYIA20130213001Wire · chafedPILOT REPORTED THAT DURING CRUISE, SMOKE WAS NOTICED IN THE COCKPIT. AS A PRECAUTION THE PILOT ELECTED TO DEACTIVATE ELECTRICAL SYSTEMS AFTER DECLARING AN EMERGENCY. SAFELY LANDED AT DESTINATION. UPON MX INSPECTION, A WIRE WAS FOUND TO HAVE BEEN CHAFED BETWSDR HYIA20140415019Drag 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 OSDR HYIA764EA52010Control Cable · brokenON FINAL DECENT, CREW REPORTED FLAP MALFUNCTION ( SPLIT FLAPS ). PILOT DECLARED AN EMERGENCY, LANDING WAS UNEVENTFUL. MX FOUND (1) OF (2) FLAP EXTEND CABLES BROKEN. MX R & R BOTH EXTEND AND RETRACT CABLES.SDR HYIA764EASwitch · unserviceableCREW REPORTED AVIONICS MASTER SWITCH INOP. MAINTENANCE REMOVED AND REPLACED SWITCH.SDR HYI2005F00005Connecting Rod · unserviceableAT 3000 FT, ON APPROACH, LT ENGINE BEGAN TO RUN ROUGH, PILOT PERFORMED FLOW CHECK, ALL ENGINE INSTRUMENTS APPEARED NORMAL, BOOST PUMPS TO LOW AS A PRECAUTIONARY. LT ENGINE CONTINUED TO RUN ROUGHER THEN SHUTDOWN, PILOT FEATHERED LT PROPELLER, LANDED WITHOUT INCSDR HYI2003F00001Distributor Gear · failedON CLIMB OUT HYDRAULIC PRESSURE LITE REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR WAS EXTENDED FOR LANDING AND WHEN POWER WAS REDUCED THE RIGHT ENGINE LOST POWER. ENGINE WAS SHUTDOWN AND FEATHER, CREW LANDED WITHOUT INCIDENT. MECHANIC FOUND RIGHT ENGINE
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