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 aircraft_model_key = 'AW139' 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 aircraft_model_key = 'AW139' 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 CA190731019Control Module · cracked(CAN) NO. 2 HYDRAULIC PRESSURE CONTROL MODULE (PCM) DISCOVERED WITH A CRACK ON THE NUMBER 4 HYDRAULIC PUMP SUCTION BOX OF THE MODULE. #2 HYDRAULIC PCM REPLACED WITH SERVICEABLE UNIT. DETAILS FROM SAFETY REPORT: DURING A SERVICEABILITY CHECK, IT WAS NOTICED THSDR ALGA201908090001Tail Boom · corrodedDURING CORROSION INSP CORROSION DAMAGE NOTED TO TAIL BOOM ASSY. OEM REPAIR IAW RS139-5352 ISSUE A.SDR CA190711011Windshield · cracked(CAN) RIGHT HAND WINDSHIELD WAS HEARD TO CRACK AS PILOTS AWAITED RETURN OF PARAMEDICS AIRPORT. AIRCRAFT WAS PARKED ON THE CONCRETE PAD AREA OF THE APRON, SUBSEQUENT TO RUNWAY LANDING AND TAXI-IN. (TC# 20190711011)SDR ALGA201908090002Panel · corrodedDURING 10YR INSP LOWER PANEL ASSY WAS FOUND TO HAVE CORROSION DAMAGE TO FOUR (4) AREAS. OEM REPAIR: RS139-5336-0241 ISSUE A.SDR ALGA2019080920199Tab · debondedDURING 50HR INSP OUTBOARD TRIM TAB WAS FOUND TO BE DE-BONDED.SDR CA190704005Gearbox · making metal(CAN) MAIN GEARBOX SUMP CHIP, ACTIVATED CHIP BURNER 3X. WITH NO SUCCESS. HAD CHIP ON START UP. (TC# 20190704005)SDR AC2R2019062813901Structure · crackedCRACKS FOUND AT STA3120 OVERHEAD AFT AND FORWARD SIDE AT BOTH CB PANEL ANGLE LOWER ENDS.SDR AC2R2019F00231Structure · crackedCRACKS FOUND AT STA3120 OVERHEAD AFT AND FORWARD SIDE AT BOTH CB PANEL ANGLE LOWER ENDS.SDR 2019FA0000204Display · inoperativeDISPLAY UNIT WOULD NOT POWER UP WHEN ELECTRICAL POWER WAS APPLIED.SDR ALGA2019080900005Floor Panel · debondedBAGGAGE FLOOR PANEL WAS FOUND TO HAVE CORROSION & DE-BONDING DAMAGE.SDR ALGA201908090004Deck Plate · corrodedDURING 1200HR INSPUPPER DECK ASSY WAS FOUND TO BE CORRODED & DE-BONDEDSDR AC2A201906163901Skin · corrodedCORROSION FOUND BETWEEN PREVIOUS REPAIR AND SKIN ON LEFT AFT TAILCONE AREASDR CA190611010Blade · delaminated(CAN) WHILE IN CRUISE, IN IMC ON AN IFR FLIGHT FROM AIRPORT TO CANADA, WITH THE INTENT TO BREAK-OFF ON THE APPROACH AND PROCEED HOSPITAL TO DROP OFF OUR PATIENT, THE FLIGHT CREW EXPERIENCED A NOISE THEY BELIEVED WAS LIKELY EMITTING FROM THE MAIN ROTOR. OVER THSDR HEER20190605999Control Panel · odorON SHORT FINAL, A WAFT OF SMOKE ENTERED THE COCKPIT ACCOMPANIED BY ELECTRICAL BURNING SMELL. LIGHT CONTROL PANEL HAS SMOKE SMELL. CONTROL PANEL WILL BE REPLACED.SDR 2019FA0000197Display · inoperativeDISPLAY FAILED TO TURN ON UPON APPLYING ELECTRICAL POWER TO AIRCRAFT.SDR 2019FA0000191Display · inoperativeDISPLAY FAILED TO TURN ON UPON APPLYING ELECTRICAL POWER TO AIRCRAFT.SDR ALGA201908090003Stabilizer · crackedDURING 1200HR INSP CRACKS WERE FOUND ON TAILPLANE ASSY. OEM REPAIR: RS139-5511-0365 REV A.SDR CA190524013Servo · damaged(CAN) ON TWO SEPARATE OCCASIONS WE HAVE RECEIVED A HYDRAULIC COMPONENT WITH ALUMINUM SHIPPING CAPS THAT HAVE A RUBBER SEAL INSIDE WHICH BECOMES DISLODGED ON CAP REMOVAL AND THE RUBBER SEAL STAYS INSIDE THE PORT ON THE NEWLY INSTALLED COMPONENT. LUCKILY, IT HASSDR CA190524022Windshield · cracked(CAN) LH WINDSHIELD DEVELOPED CRACKES AFTER LANDING WHILE TAXIING BACK TO THE HANGAR. (TC# 20190524022)SDR CA190524023Capsule · stuck(CAN) DEFECT: NO AUDIO WARNING ON SHUTDOWN. RECTIFICATION: 1. FUSE F506 DISCOVERED BLOWN. AURAL WARNING GENERATOR IN MAU2 NO LONGER POWERED. FLIGHT CREW WILL BE THOROUGHLY BRIEFED AND INSTRUCTED TO CLOSELY MONITOR CAS AND MASTER CAUTION WINDOWS THROUGHOUT DURASDR AC2A2019051513901Support Fitting · corrodedCORROSION DAMAGE ON RIGHT OUTBOARD ENGINE MOUNT AIRFRAME SUPPORT FITTING REQUIRING REPLACEMENT OF FITTING.SDR AC2R2019050201Pressure Switch · leakingWHILE ENTERING A LEFT DOWNWIND FOR RWY 18 INTO KGAO ABOUT 3 MILES SOUTH OF THE AIRFIELD, THE HYDRAULIC UTIL PRESS CAS ILLUMINATED. WENT TO THE HYDRAULIC SYNOPTIC PAGE AND THE #2 HYDRAULIC RESERVOIR WAS INDICATING 50% HYDRAULIC FLUID. IMMEDIATELY LOWERED THE LASDR AC2A2020050113920Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113913Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113912Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113921Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR 2019FA0000190Warning Light · false activationDU DEGRADED CAS LIGHT ILLUMINATED 3 MINUTES PRIOR TO LANDING. NO DEGRADATION WAS NOTED ON DISPLAY, REVERSION MODES WORKED AS EXPECTED.SDR CA190411008Drain Valve · inoperative(CAN) DEFECT: RH FUEL DRAIN DRIPPING FUEL WHEN SAMPLED. RECTIFICATION: FOUND DRAIN VALVE MISSING FROM ASSEMBLY. DRAIN ASSEMBLY REPLACED REF 39-A-28-11-05-00A-720-A-A. SAFETY REPORT SUBMITTED BY MAINTENANCE PERSONNEL: C-XXXX HAD FUEL LEAK FROM RH FUEL TANK DRAISDR CA190328005Windshield · cracked(CAN) DEFECT: RH (PILOT) WINDSHIELD CRACKED. RECTIFICATION: 1. REPLACED R/H WINDSHIELD IAW 39-A-30-63-02-00A-520A-K. 2. INSTALLED WIPER PER AMP 39A-30-41-05-00A-720A-A. SAFETY REPORT FROM FLIGHT CREW ATTACHED.SDR AC2R2019032213901Deck Plate · delaminatedSEVERAL DELAMINATION'S OCCURRED THROUGHOUT DECK.SDR CA190318009Gearbox · making metal(CAN) DEFECT: METAL FLAKES FOUND ON #2 SUMP CHIP PLUG. RECTIFICATION: 1. CHIP PLUGS REMOVED AND CLEANED FROM METAL FLAKES. DUMMY ACTUATOR REMOVED FOR FURTHER INVESTIGATION. 2. LEONARDO PSE DETERMINED METAL FOUND WARRANTED MGB REPLACEMENT. MGB REMOVED AND UNDRESDR AC2A2020050113911Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113910Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR CA190306009Control Cable · seized(CAN) DEFECT: #1 ENGINE POWER CONTROL CABLE SEIZED. CORRECTIVE ACTION: #1 ENGINE POWER CONTROL CABLE REMOVED IAW 39-A-76-11-02-00A-720A-A NUMBER 1 POWER CONTROL CABLE-INSTALL PROCEDURE. ADJUSTMENT CARRIED OUT SATISFACTORY IAW 39-A-76-11-00-00A-271A-A POWER CONSDR AC2R2018112901Handle · vibrationCOCKPIT DOOR OPENED IN FLIGHT. LANDED AT GC205 (NEAREST CHEVRON PLATFORM. AFTER LANDING, CREW INSPECTED AND SECURED DOOR. DETERMINED CAUSE OF DOOR OPENING WAS VIBRATION OF THE DOOR HANDLE.SDR AC2A2020050113909Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113907Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113908Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113906Filter · crackedIBF MAINTENANCE INDICATOR FOUND TO BE CRACKED.SDR AC2A2020050113905Filter · crackedIBF MAINTENANCE INDICATOR FOUND TO BE CRACKED.SDR AC2A2020050113904Indicator · crackedIBF MAINTENANCE INDICATOR FOUND CRACKED. *SUPPLEMENTAL INFORMATION* PART NUMBER ENTERED ON ORIGINAL SDR IN SECTION 5 WAS IN ERROR. PART NUMBER WAS SUBMITTED AS 104440-201 AND SHOULD HAVE BEEN 104441-201.SDR HEER2018008021106Chip Detector · contaminatedNR 2 ENGINE CHIP LIGHT IN FLIGHT. FOUND SMALL SLIVER ON PLUG. REMOVED AND CHECKED FILTERS. NO OTHER PARTICLES FOUND. GROUND RUN AND LEAK CHECKED.SDR AC2A2020050113903Filter · crackedIBF MAINTENANCE INDICATOR FOUND TO BE CRACKED.SDR AC2A2020050113902Indicator · crackedIBF MAINTENANCE INDICATOR FOUND TO BE CRACKED.SDR AC2A2018072513901Fitting · corrodedCORROSION FORMING AT STA3300 RIGHT SIDE CABIN OVERHEAD AT BULKHEAD FITTING PENETRATION AREA. CORROSION WAS REMOVED AND FITTING REPLACED.SDR AC2A2018062913902Longeron · crackedRIGHT SIDE INTERNAL LONGERON CRACKED AS BS 6034 FROM LIGHTNING HOLE WEBBINGSDR AC2A2018062913901Attach Fitting · crackedRIGHT UPPER TAIL STRUCTURE ATTACH FITTING HAD A CRACK ABOVE THE LOCK FASTENER.SDR AC2A2020032313906Pressure Switch · leakingHYDRAULIC FLUID LEAKING FROM VENT HOLE.SDR ULXR201804050001Skin · delaminatedMAJOR DELAMINATION ON THE TAILBOOM SKIN.SDR AC2R2018040201Fan · overheatedPRIOR TO CRUISE CLEARANCE, PILOTS NOTICED A STRONG ELECTRICAL OVERHEAT ODOR WITH A SIMULTANEOUS FWD FAN CAS MESSAGE. NO SMOKE OR FLAMES WERE NOTED. CREW COMPLIED WITH QRH. REPLACED THE PILOT'S COCKPIT FAN.
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