N118DL
Service difficulty reports not matched to an aircraft · 17
They name N118DL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N118DL' AND registry_match IS NULL 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 = 'N118DL' AND registry_match IS NULL 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 DL76S050470Pump · leakingFUEL IMBALANCE OF 3500LBS, DIVERTED TO OMA, FOUND BOLT AT LT ENGINE FUEL PUMP MISSING AND LEAKING. REPLACED GASKET AND 4 BOLTS.SDR DL76S050277Idg · malfunctionedDURING CLIMB-OUT AT 8000 FT, THE LEFT GENERATOR WENT OFF LINE, TRIED TO RESET ONCE BUT DID NOT COME BACK. DIVERT INTO JFK DUE TO SINGLE GENERATOR OPERATION. REPLACED LEFT IDG AND APU EXCITER.SDR DL76S040496Skin · delaminatedRIGHT OUTBOARD AILERON OUTBOARD END LOWER AND UPPER SKIN AND SPAR DELAMINATED APPROXIMATELY 14 INCHES LONG AT END OF PART. REPAIRED PER ER/A 090481-14.SDR DL76S030633Battery · dischargedON TRANSIT CHECK SQUIB TEST RIGHT EMERGENCY ESCAPE LIGHT DID NOT ILLUMINATE DURING TEST ONE. REMOVED AND REPLACED RT OFF WING ESCAPE SYSTEM BATTERY AND POWER PACK PER M/M. SQUIB TEST CKS NML.SDR DL76S030048Duct · crackedPILOT REPORTED NR 1 ENGINE HAD OVERHEAT LOOP 1 EICAS MSG AMD ALSO HAD OVERHEAT LOGHT ON PEDESTAL FLICKERING, CLOSED BLEED VALVE, LIGHT STILL FLICKERS, WENT OUT AFTER RETARDING THROTTLE. ON ENGINE INSPECTION FOUND TURBINE CASE COOLING DUCT CRACKED, REPLACED SDR DL76S021263Battery · inoperativeDURING S/C FOUND AFT RIGHT OVERHEAD EMERGENCY LIGHTS INOPERATIVE BY ROW 44E. R & R BATTERY ASSY, OPS CHECK NORMAL.SDR DL76S011832Check Valve · failedTHE CHECK VALVE ON THE RAT MODULE IN THE RT WHEEL WELL BLEW OUT CAUSING A LOSS OF HYD QTY AND PRESSURE IN THE CENTER SYSTEM. REPLACED MODULE.SDR DL76S011707Power Supply · dischargedON L/O, FOUND LEFT WING OVERWING EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK, CHECKS GOOD.SDR DL76S972022Fseu · failedRECEIVED LEADING EDGE SLAT ASSYM MSG AFTER SELECTING FLAPS FROM FLAPS ONE TO UP. REPLACED FSEU AND NR 10 SLAT INBOARD SENSOR, BITE CHECKS GOOD.SDR DL76S972039Floorbeam Web · crackedTHE FS 246 FLOORBEAM WEB WAS FOUND WITH A VERTICAL CRACK APPROX 3 LONG AT RBL 20. ADDITIONALLY, THE ATTACHING VERTICAL STIFFENER WAS FOUND CRACKED. REPAIRED PER ERA 330789-14.SDR DL76S972038Seat Track · crackedTHE FUSELAGE SEAT TRACKS LOCATED AT RBL 33, LBL 54 AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT APPROX FS 786. REPAIRED PER ERA 330781-14.SDR DL76S972029Skin · damagedUNIDENTIFIED SKIN REPAIR FOUND AT FS 640 JUST ABOVE S31R. FINAL CUTOUT IN SKIN IS 3.25 BY 2.75. REPAIRED PER PER ERA 361621-14.SDR DL76S972027Skin · dentedGROUND DAMAGE FOUND AT APPROX FS 510 BETWEEN STRINGERS 33L AND 35L. DAMAGE CUTOUT AND REPAIRED PER ERA 330797-14.SDR DL76S971018Actuator · wornRT I/B AILERON POSITION VARIES BETWEEN 30 TO 50 DEGREES GREATER THAN LEFT I/B AILERON. OCCASIONALLY GREATER THAN 50 DEGREES DEFLECTION OBSERVED, THIS OCCURED DURING ALL PHASES OF FLT. MADE INFLT CK FOR POSSIBLE SPOILER FLOAT NEGATIVE RESULTS. REPLACED RT INSDR DL76S962358Duct · crackedLT BLEED DUCT LIGHT ON AT FL 390. FOUND BLEED DUCT CRACKED IN WING JUST INBOARD OF LT ENGINE PYLON. REPLACED DUCT.SDR DL76S954006Bulb · failedEMERGENCY LIGHT AT SEAT 13B IS INOP. REPLACED BULB, CKS GOOD.SDR DL76S953358Cable Quadrant · crackedON TAXI OUT FOR TAKEOFF, WITH FLAPS AT 15 DEGREES, DURING FLT CONTROL CHECK THE AILERONS WERE BINDING, THEN STUCK FULL DEFLECTION RIGH WING DOWN. AC RETURNED TO BLOCK AND FOUND LEFT LATERAL CENTRAL CONTROL ACTUATOR WITH CABLE QUADRANT BROKEN. REPLACED QUADRA
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