N108LN
Service difficulty reports · 18
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 = 'N108LN' 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 = 'N108LN' 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 QMLA2026030720015Unknown · odorSTRANGE BURNING ODOR AND SMELL IN CABIN OF AIRCRAFT.SDR QMLA2025020320012Unknown · odorDURING TAKE-OFF AND CLIMB THERE WAS A STRONG ODOR THROUGHOUT THE CABIN. THE BEST WAY TO DESCRIBE IT, IS THAT IT SMELLS LIKE PROPANE. THIS HAS BEEN AN ONGOING ISSUE WITH THE AIRCRAFT. THE CREW DID NOT FEEL COMFORTABLE FLYING IN THE AIRCRAFT UNTIL FIXED, SO THE SDR 2A6D20240828006Structure · gougedGOUGE AT THE OUTBOARD FLANGE RIVNUT LOCATION IN THE FORM OF SHEAR OUT. THE GOUGE WAS MEASURED TO BE APPROXIMATELY 0.1” X 0.1285”X 0.060”.SDR 2A6D20240828005Support · damagedDAMAGE TO THE RH BI-DIRECTIONAL SUPPORT FITTING (P/N: 350A211232.23) AND SUPPORT BEAM (P/N: 350A211293.20) IN THE FORM OF CHAFING CAUSED DUE TO CABLE. THE CHAFE DAMAGE AT SUPPORT BEAM MEASURED TO BE APPROXIMATELY 0.30” X 0.20” X 0.015”. THE CHAFE DAMAGE AT BI-SDR 2A6D20240828004Stiffener · wornDAMAGE TO THE LH STA2700 STIFFENER (LH PN: 350A21-1071.22; RH PN: 350A211071.23) IN THE FORM OF WEAR CAUSED BY A NEARBY BOLT HEAD.SDR 2A6D20240828003Bulkhead Web · chafedDAMAGE TO THE 15° BULKHEAD LH WEB (PN: 350A21-1032.86) IN THE FORM OF SEVERAL CHAFES. THE CHAFES WERE REPORTED TO BE 0.20” X 0.10” AND 0.004” DEEP, AS WELL AS 0.20” X 0.30” AND 0.010” DEEPSDR 2A6D20240828002Structure · gougedDAMAGE TO THE LH UPPER CARGO EDGING (P/N: 350A211041.22) IN THE FORM OF A GOUGE CAUSED WHILE INSTALLING BLIND FASTENER. THE GOUGE DAMAGE NEAR AFT SIDE OF THE LH EDGING AND WAS MEASURED TO BE APPROXIMATELY 0.40” X 0.15” X 0.02”.SDR 2A6D20240828001Floor Panel · corrodedTHERE IS CORROSION DAMAGE TO THE CABIN FLOOR EDGING (PN: 350A21-1359-20/21).SDR QMLA2023040920029Unknown · unserviceableFUMES AND SMOKE APPARENTLY COMING FROM GNS530 AFTER START UP. MECHANIC MEL'D GNS530 DISABLED AND COLLARED CIRCUIT BREAKER. SUSPECT MALFUNCTIONING GNS530 OR WIRING LEADING TO GNS 530.SDR 2A6D2021082603959Frame · chafedTHE LH X-FRAME HAS ONE CHAFED AREA LOCATED ON ITS OBD BEADED FACE AFT UPPER SIDE MEASURING 0.3” X 0.3” X 0.035” DEEP.SDR QMLA2019083091973Air Filter · overservicedA PRECAUTIONARY LANDING WAS MADE AFTER AN UNIDENTIFIED ODOR CAME INTO THE CABIN FROM THE ENGINE COMPARTMENT. IT WAS THEN DISCOVERED THAT THE AIR FILTER WAS OVERSERVICED AND THE OIL WAS DRIPPING ONTO THE HOT ENGINE. THE ENGINE WAS CLEANED AND THE EXCESS OIL WASSDR QMLA2016030916024Support Frame · chafedTHE TRANSMISSION SUPPORT FRAME, PN 350A21-1041-143, HAS CHAFING DAMAGE ON THE LOWER FLANGE, FROM AN UNSECURED CABLE, PN 704A34-1302-23. PN 350A38-1040-20 ATTACHES TO PN 350A21-1041-143.SDR QMLA2015050515035Door · delaminatedRIGHT LATERAL CARGO HOLD DOOR HAS DELAMINATION.SDR QMLA2014102014125Adapter · crackedFREQUENCY ADAPTER IS CRACKED ON THE RED BLADE.SDR QMLA2014081214100Unknown · odorSTRONG ODOR OF FUEL PROMPTED PRECAUTIONARY LANDING. POST FLIGHT INSPECTION DID NOT REVEAL ANY FUEL LEAKS.SDR QMLA2012080212125Connector · contaminatedDURING TAKEOFF, HAD A FLICKERING ENGINE FIRE LIGHT. REMOVED CONNECTOR ON ENGINE DECK, CLEANED WITH CONTACT CLEANER, SUSPECT MOISTURE, APPLIED STABILANT TO CONNECTOR REINSTALLED CONNECTOR. FIRE LIGHT FLICKED 2-3 TIMES AGAIN. APPLIED STABILANT TO CONNECTOR. SDR QMLA2012060612093Coil · failedAIR CONDITIONER COMPRESSOR FAILED IN-FLIGHT RESULTING IN SMOKE/FUMES IN THE COCKPIT. VISUAL INSPECTED AND FOUND AIR CONDITIONING BELT SLIGHTLY LOOSE, BELT TIGHTENED, BUT NO OTHER DEFECTS NOTED DURING INSPECTION OF SYS. GROUND RUN REVEALED AIR CONDITIONER COSDR QMLA2011061711070Drive Shaft · shearedTHE PILOT REPORTED A GENERATOR LIGHT DURING ENGINE START. HE ATTEMPTED TO RESET THE GENERATOR WITH NO SUCCESS. DURING SUBSEQUENT TROUBLESHOOTING THE MECHANIC FOUND THE STARTER/GENERATOR DRIVESHAFT SHEARED. THE STARTED/GENERATOR WAS REPLACED WITH A SERVICEAB
Back to N108LN