N779LF
Service difficulty reports · 19
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 = 'N779LF' 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 = 'N779LF' 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 2A6R2025013072203Deck Plate · chafedCHAFE DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK LH BEAM CAP (PN: B533K3202-201) BY A MEDICAL INTERIOR PANEL SCREW. AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-BK117-53-2024-3189, ISSUE A DATED 16 OCT 2024, SDR 2A6R2025013072202Deck Plate · dentedDENT DAMAGE WAS DISCOVERED ON THE RH ENGINE DECK PANEL (PN: B533K3339-213) THROUGH TO THE RH ENGINE MOUNT INBOARD SUPPORT BEAM (PN: B533K3316-207). AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-BK117-53-2024-3426SDR 2A6R2025013072201Floor Panel · chafedCHAFE DAMAGE WAS DISCOVERED ON THE COCKPIT FLOOR (PN: B531M8002101) WHERE THE SLANT CONSOLE MEETS THE COCKPIT FLOOR. AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-BK117-53-2024-3227, ISSUE A DATED 17 OCT 2024, WHISDR QMLA2024091120111Unknown · fumesSHORTLY AFTER TAKEOFF STARTED TO SMELL FUMES IN THE CABIN.SDR QMLA2019042549041Skin · crackedDURING A SCHEDULED MAINTENANCE EVENT, A CRACK WAS DISCOVERED ON TOP OF THE TAIL BOOM. THIS AIRCRAFT REMAINS OOS AT THE TIME OF THIS SUBMISSION AWAITING THE APPROVED REPAIR.SDR QMLA2017120717137Stiffener · corrodedWHILE REMOVING THE VIBRATION DAMPER UNDER PILOTS SEAT FOUND STIFFENER ASSEMBLY CORRODED THAT THE VIBRATION DAMPER ATTACHES TO.SDR QMLA2017092117098Drain · cloggedDURING ZONE INSPECTIONS, PULLED OFF THE VENT LINE GOING FROM RIGHT SIDE OF THE NR 1 ENGINE TO THE ENGINE DECK. FOUND THAT THE DRAIN COLLECTOR WAS CLOGGED WITH DEBRIS ON THE RIGHT SIDE OF THE Y-FITTING.SDR QMLA2012111212182Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA. TSDR QMLA2012111212181Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA.SDR QMLA2012111212180Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA.SDR QMLA2012083012143Starter Gen · malfunctionedGENERATOR DISCONNECT LIGHT CAME ON FOR THE NR 1 GENERATOR. LANDED WITHOUT INCIDENT UNDER POWER FROM BOTH ENGINES. SWAPED STARTER/GENERATOR FROM SIDE TO SIDE. FOUND ISSUED FOLLOWED GENERATOR.SDR QMLA2012081112132Engine · making metal20 MINUTES INTO FLIGHT, THE NR 2 ENGINE CHIP LIGHT ILLUMINATED. ACTIVATED THE FUZZ BURNER FOR APPROX 1 SECOND AND THE LIGHT EXTINGUISHED. APPROX 1 SECOND LATER THE CHIP LIGHT ILLUMINATED AGAIN. ACTIVATED THE FUZZ BURNER AGAIN AND LIGHT EXTINGUISHED. APPROSDR QMLA2011112611113Gearbox · making metalUPON SEVERAL ATTEMPTS TO BALANCE THE TAIL BLADE ASSY, THE MECHANIC HAD NUMEROUS CHIP LIGHT EVENTS. THE LAST INSPECTION OF THE CHIP PLUG FOUND NUMEROUS FLAKES TO DEEM THE TAIL ROTOR GEARBOX AS UNAIRWORTHY. TAIL ROTOR GEARBOX WAS REPLACED AND THE ACFT WAS RETUSDR QMLA2011060711066Transmission · making metalTRANSMISSION CHIP LIGHT ILLUMINATED IN FLIGHT, THIS WAS THE 4TH CHIP LIGHT EVENT WITHIN THE PREVIOUS SEVERAL MONTHS. PREVIOUS CHIP EVENTS WERE FUZZ REQUIRING NO FURTHER ACTION, CHIP EVENT ON 6/07/11 REQUIRED TRANSMISSION CHANGE IAW AMM 63-41-00 6-2. TRANSMISSSDR QMLA2011050611054Blade · damagedDURING THE PILOTS PRE FLIGHT, FOUND THAT THE TRIMMING SURFACE ON THE YELLOW BLADE WAS MISSING. UPON INSPECTION FOUND THE TWO RIVET HOLES, WHERE THE RIVETS HELP HOLD THE TRIMMING SURFACE TO THE BLADE, WAS IN ALMOST PERFECT CONDITION. SENT MAIN ROTOR BLADE TO AMSDR QMLA2010090910058Wire Harness · chafedFIRE EXT WARNING LIGHT ILLUMINATED ON CAD DISPLAY. AFTER INSP OF A/C FOUND, CHAFED WIRES. THE WIRE'S WERE LOCATED JUST AFT OF THE CO-PILOT'S SEAT. IN THE CABIN OVERHEAD, JUST INSIDE OF CABIN DOOR AREA. THEY WERE CHAFING AGAINST AN AIR CONDITIONING LINE. THE SDR QMLA2010071810038Unknown · odorENROUTE, CREW NOTICED A STRONG ELECTRICAL BURNING ODOR. A FEW MOMENTS LATER, COULD SMELL THE FUMES. ASKED IF THERE WAS ANY SMOKE OR FIRE. NONE DETECTED. DIVERTED, OPENED PILOT SIDE SLIDING WINDOW FOR FRESH AIR AND WITHIN 10 SECONDS, A STRONG ODOR OF JET FUEL ESDR QMLA2010071110033Attach Bracket · crackedUPON FINAL APPROACH INTO LANDING, CREW NOTICED ONE OF THE LANDING LIGHTS WOBBLEING UNDERNEATH THE ACFT. UPON SHUTDOWN, RT REAR LANDING LIGHT HAD BROKEN FREE FROM ITS MOUNT AND WAS HANGING BY A SINGLE WIRE. MECHANIC CALLED IN TO REPAIR. VISUAL INSP REVEALED RT SDR QMLA2010060510020Torque Box · malfunctionedNR 2 ENGINE TORQUE SYS FAILURE.
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