N209LF
Service difficulty reports · 16
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 = 'N209LF' 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 = 'N209LF' 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 2A6D20220504004Bulkhead · damagedSHORT ED AND SHORT PD HOLES WERE DISCOVERED ON THE 7 DEGREE BULKHEAD ADJACENT TO THE RECESSED MEDICAL WALL INSTALLATION.SDR 2A6D20220503003Xmsn Deck · chafedR/H SIDE FWD. TRANSMISSION DECK WEB (P/N: 350A21-4418) IS DAMAGED IN THE FORM OF A CHAFING. THE DAMAGE IN THE FWD IS APPROXIMATELY 0.3” IN LENGTH, 0.3” IN WIDTH AND 0.019” IN DEPTH AND DAMAGE AT AFT IS APPROXIMATELY 0.3” IN LENGTH, 0.25” IN WIDTH AND 0.010” INSDR 2A6D20220429002Xmsn Deck · chafedCHAFING DAMAGE WAS DISCOVERED ON THE RH SIDE OF THE TRANSMISSION DECK. THE DEEPEST DEPTH IS 0.015" WITH A LENGTH OF 2.1" AND WIDTH OF 0.1.SDR 2A6D20220418001Frame · chafedDAMAGE TO BOTH X1790 FRAME (P/N: 350A214099) AND SUPPORT (P/N: 350A214107) IN THE
FORM OF A DENT AND CHAFE NEAR A LOWER FAIRING MOUNTING POINT. THE DAMAGE AREA WAS MEASURED TO BE 0.2” IN LENGTH,
0.2” IN WIDTH AND 0.03” IN DEPTH.SDR 2A6R2019012251001Reinforcement · crackedCRACK DAMAGE WAS NOTED ON THE RIGHT SIDE OF THE CABIN FLOOR NEAR THE DOOR POST WITHIN THE AREA OF THE DOOR STRUT FITTING.SDR 2A6R2018120551003Structure · corrodedCORROSION AND DELAMINATION OF THE ALUMINUM GROUND PLANE OF THE CABIN ROOF (CANOPY)IN SEVERAL SPOTSSDR 2A6R201812025102Door · crackedHINGED RIGHT HAND CABIN DOOR HAS A 9 INCH VERTICAL CRACK IN THE DOOR.SDR 2A6R201812055101Frame · crackedTAIL BOOM 3035 RING FRAME CRACKED AT 11:00 POSITION AT SKIN LAP.SDR QMLA2018100818109Blower · odorWHILE ON APPROACH TO HOSPITAL LANDING PAD, THE GENERATOR DISENGAGED. IT WAS RESET, AND THE SUBSEQUENT APPROACH AND LANDING WERE COMPLETED NORMALLY. THE CREW REPORTED AN ELECTRICAL ODOR AFTER LANDING. UPON INSPECTION, NO PROBLEMS WERE FOUND WITH ELECTRICAL SYSSDR QMLA2016022316008Unknown · odorSMELL OF AN UNIDENTIFIED BURNING ODOR IN COCKPIT.SDR QMLA2014102914128Unknown · smokeDURING CRUISE FLIGHT A CREW MEMBER REPORTED SEEING SMOKE IN THE CABIN FWD OF THE STRETCHER WITH A STRANGE SMELL IN THE CABIN. THE PILOT DID NOT WITNESS THIS SMOKE, BUT RETURNED TO BASE FOLLOWING A DISCUSSION WITH THE MEDICAL CREW. ONCE ON THE GND, THE PILOT SDR QMLA2014072914093Connector · contaminatedFLIGHT ABORTED DUE TO NOISE COMING FROM OIL COOLER FAN. DETERMINED WATER WAS PRESENT IN THE CONNECTOR.SDR QMLA2014051814057Attach Fitting · crackedON A POST FLIGHT INSPECTION, FOUND THE UPPER LT HORIZONTAL STABILIZER ATTACH FITTING CRACKED. REMOVED THE HORIZONTAL STABILIZER & FOUND THAT THE FITTING HAD COMPLETELY CRACKED INTO TWO SEPARATE PIECES. THE CRACK APPEARED TO PROPAGATE FROM THE TWO BOLTS THAT SDR QMLA2014041114035Attach Fitting · crackedCRACK FOUND ON RT SIDE CANOPY FRAME ATTACHMENT WEB PANEL FWD ON BELLY OF ACFT DURING AN EC130 AAIP A0560 100HOUR, 12MONTH AIRFRAME INSPECTIONSDR QMLA2013050213062Audio Panel · failedPILOT WAS GOING INTO A HOVER DETECTED SOMETHING BURNING, AT THE SAME TIME LOST ALL RADIO AND ICS COMMUNICATIONS. PILOT PUT THE ACFT BACK DOWN AND NOTICED HIS PILOT ICS CIRCUIT BREAKER POPPED. AFTER EXTENSIVE TROUBLESHOOTING, MX AOG ORDERED A 2 AMP CIRCUIT BRESDR UNFR20120100003Attach Fitting · brokenDURING AN INSPECTION, HORIZONTAL STAB WAS REQUIRED TO BE REMOVED. UPON REMOVAL, THE UPPER LT MOUNT FITTING WAS FOUND BROKEN COMPLETELY IN HALF. AN EDDY CURRENT INSPECTION OF THE AREA RESULTED IN THE DISCOVERY OF THE UPPER RT FITTING BEING CRACKED ALSO.
Back to N209LF