N918FX
Service difficulty reports · 22
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 = 'N918FX' 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 = 'N918FX' 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 MTNA20250407002Oxygen Mask · no testDURING PREFLIGHT OF AIRCRAFT FOR FLIGHT 8120 BQN-AUA, THE CAPTAINS SIDE O2 MASK WOULD NOT TEST. BQN MAINTENANCE REPLACED THE CAPTAINS SIDE MASK AND FLIGHT 8120 DEPARTEDSDR MTNA20241218001Fan · failedODOR OF SMOKE FOLLOWED BY RECIRC FAN #2 FAULTED IN FLIGHT.SDR MTNA20220701001None · nonePRIOR TO THE INITIAL DESCENT, IN CRUISE FLIGHT, THE CREW NOTICED A TRANSIENT OVER-TORQUE ON ENGINE #2, FOLLOWED BY A DECREASE IN NP. THE CREW ASSESSED THE SITUATION, SHUT DOWN AND SECURED ENGINE #2, AND DECLARED AN EMERGENCY. THE FLIGHT CONTINUED TO MIA, WHERSDR MTNA20220419001None · nonePITCH TRIM ASYMMETRY IN FLIGHT. PITCH, ROLL, AND RUDDER TRIM INDICATOR INOP. TRIPPED CIRCUIT BREAKER. REMOVED AND RECONNECTED LEFT AND RIGHT ELECTRIC PITCH TRIM ACTUATOR CONNECTORS AFTER CLEANING WITH CONTACT CLEANING. REMOVED AND REPLACED CREW ALERTING COMPUTSDR MTNA20210209001Indicator · faultedPITCH TRIM ASYMMETRY MASTER CAUTION IN FLIGHT. FOUND TRIM INDICATOR CIRCUIT BREAKER POPPED. INSPECTED AND CLEANED CANNON PLUGS FOR RIGHT AND LEFT ELEVATOR TRIM ACTUATOR. INSPECTED ASSOCIATED WIRING AND VARISTORS IN TAIL CONE FOR
CORROSION. REPLACED TRIM INDICSDR MTNA20210128001Circuit Breaker · trippedPITCH TRIM ASYMMETRY IN CRUISE FLIGHT. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AT THE SCHEDULED ARRIVAL AIRPORT. MAINTENANCE FOUND TRIM INDICATOR CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AND SYSTEM OPERATIONALLY CHECKED GOOD. MAINTESDR MTNA202008210001O-Ring · leakingDURING CRUISE RT TORQUE UNCOMMENCED TORQUE INDICATED 120%, ACCOMPANIED AIRPLANE ASSEMETRY. MAINTENANCE FOUND PROPELLER CONTROL UNIT O-RING LEAKING AT REDUCTION GEAR BOX. REPLACED O-RING OPERATIONALLY CHECKS GOOD. PER PRATT & WHITNEY MM 05-50-00 OVERTORQUE WSDR MTNA202008172101O-Ring · leakingDURING CRUIS, RIGHT UNCOMMANDED TORQUE INDICATED 120%, ACCOMPANIED BY AIRPLANE ASYMMETRY. REPLACED #2 PROPELLER CONTROL UNIT O-RINGS, OPERATIONALLY CHECKS GOOD. UPON FOQA DOWNLOAD FOUND OVERTORQUE TO HAVE BEEN 146%. REPLACED RH PROPELLER ASSEMBLY FOR INSPECTIOSDR 2017FA0000273Floor Support · brokenLEFT FLOOR SUPPORT BROKEN BETWEEN FRAMES 31 AND 32.SDR MTNA20170621001Engine · shutdownDURING LEVEL-OFF AT 10,000 FEET FOR CRUISE FLIGHT, A POP SOUND WAS HEARD, FOLLOWED BY A LACK OF RESPONSE FROM THE NR 2 CONDITION LEVER AND COMPLETE SHUTDOWN OF THE NR 2 ENGINE. THE CREW DECLARED AN EMERGENCY, AND THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENTSDR MTNA2017030900039Smoke Warning · activatedDURING CLIMB AND PART OF CRUISE, THE AFT SMOKE INDICATION ON THE CREW ADVISORY PANEL CAME ON ALONG WITH A WARNING LIGHT AND REPETITIVE CHIME. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT.SDR MTNA20140827016Fitting · damagedMAIN CARGO DOOR FITTINGS ATTACHED TO FUSELAGE DISCOVERED TO HAVE OVERSIZED HOLES. APPLIED SERVICE BULLETIN 42-52-0076 & HOLES REMAINED OVERSIZE IAW ATR EMAIL IAW DT S-5011/14-22727 DATED 8/22/2014 & 8/25/2014. APPROVED DATA IS SRAS DT S-5011 14 8665 ISSUE A DSDR MTNA20131111044Pan · dentedAFT CARGO DOOR HAS THREE DENTS THAT ARE OUT OF LIMITS ON LOWER PAN. REPAIRED LOWER DOOR PAN IAW M-7 DWG NR 42R47000-09 REV. I/R.SDR MTNA20131008042Floor Panel · corrodedFOUND CORROSION ON FLOOR PANEL 214BF, OUT OF LIMITS. REPLACED FLOOR PANEL IAW SRM.SDR MTNA201112220001Computer · out of adjustDURING DESCENT, ACFT EXPERIENCED AN MC LIGHT AND SINGLE CHIME, IMMEDIATELY FOLLOWED BY THE AUTOPILOT DISCONNECT WARNING. FLT CONTROL CAUTION WAS ILLUMINATED ON CAP, AND A LOCAL PITCH TRIM ASYM LIGHT WAS NOTED ON THE INSTRUMENT PANEL. THE MC AND LOCAL ALERTSSDR MTNA2012F00033Warning System · multiple indDURING DESCENT, ACFT EXPERIENCED A MC LIGHT AND SINGLE CHIME, IMMEDIATELY FOLLOWED BY THE AUTOPILOT DISCONNECT WARNING. FLT CONTROL CAUTION WAS ILLUMINATED ON THE CAP, AND A LOCAL PITCH TRIM ASYM LIGHT WAS NOTED ON THE INSTRUMENT PANEL. THE MC AND LOCAL ALERSDR MTNA0906001Splice · corrodedDURING A 4 YEAR INSP FOUND A CORRODED SPLICE PLATE AT FRAME 42. REMOVED AND INSTALLED A NEW DOUBLER IAW THE SRM, CH. 51-25-01, 51-25-02 AND 51-21-27.SDR DHL2008F00013Attach Angle · corrodedDURING THE YEARLY INSPECTION FOUND EXFOLIATION CORROSIOIN LEVEL 2. THE CORROSION WAS ON LT LOWER WING SKIN ATTACH ANGLE THAT ATTCHES THE WING SKIN TO THE LT OUTBOARD NACELLE SKIN AT RIB 12. REPAIRED IAW ATR 42 SRM 51-21-42, 51-21-58, 51-22-02 AND ATR REPAIR SDR MAC070707Tee Fitting · corrodedDURING INSPECTION, LEVEL 2, CORROSION WAS FOUND ON THE (T-FITTINGS) ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTED ARE LOCATED AT RT IB, CENTER, AND OB HINGE FITTINGS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM ALLOYED FITTINGS)SDR MAC070706Fitting · corrodedDURING INSPECTION, LEVEL 2 CORROSION WAS FOUND ON THE (T- FITTINGS) ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTED ARE LOCATED AT THE IB, CENTER, AND OB HINGE FITTINGS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM ALLOYED FITTINGSSDR MAC050701Power Lever · lack of lubeIN CRUISE FLIGHT AT FL220 THE NR 2 POWER LEVER APPEARED TO BE FROZEN AT ITS POWER SETTING. AFTER DESCENT TO 12,000 FT THE NR 2 POWER LEVER BECAME FREE AND THE POWER COULD THEN BE CHANGED. SERVICE BULLETIN ATR42-76-0009 HAD PREVIOUSLY BEEN ACCOMPLISHED. PANESDR MAC080601Gcu · openNR 1 GENERATOR FAILED IN FLIGHT. ELECTRICAL SMOKE IN COCKPIT PRECEDED GENERATOR FAILURE. NO RESET WAS ATTEMPTED. THERE WAS NO EVIDENCE OF FIRE OR HEAT DAMAGE. THE PROBLEM WAS TRACED TO A GENERATOR CONTACTOR.
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