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 engine_model_key = 'CF348E5' 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 engine_model_key = 'CF348E5' 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 CA160224002Brake Assy · disintegrated(CAN) DURING APPROACH BRAKE RT FAULT EICAS MESSAGE DISPLAYED AND AFTER LANDING EMERGENCY BRAKE FAULT MESSAGE ALSO DISPLAYED ON EICAS. DURING CREW POST FLIGHT WALK AROUND, FOUND NR 4 BRAKE ASSY DISINTEGRATED AND HYDRAULIC FLUID LEAKING. DISPATCH WAS ADVISED TO SDR CA160208014Line · misaligned(CAN) WHILE COMPLETING AN A CHECK AND DOING LEAK CHECKS ON THE NR 1 ENGINE, AN OIL LEAK WAS DISCOVERED ON THE NR 1 ENGINE AT THE 6 O`CLOCK POSITION. THE LEAK WAS FROM THE SAME SCAVENGE LINE THAT HAD FAILED ON ANOTHER ENGINE IN THE FLEET THE DAY BEFORE. THE AIRSDR R61A201601110060Engine · failedF/A REPORTED SMOKE IN THE CABIN. CREW DECLARED AN EMERGENCY, RETURNED TO DEPARTURE AND WITH EMERGENCY VEHICLES ROLLING, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND OIL ALL OVER THE COMPRESSOR CASE. MAINTENANCE R & R ENGINE NR 2 IAW AMM AND OPS SDR MASA2015111612554Flashlight · inoperativeF/O FLASHLIGHT INOPERATIVE.SDR CA151024001Fan · failed(CAN) AIRCRAFT DECLARED MAYDAY REPORTED A SMELL OF SMOKE IN THE CABIN. CAPT ADVISED THAT HE DIDNÏ¿½T SMELL IT BUT BOTH F/ASÏ¿½S DID. DESCRIBED IT AS AN ELECTRICAL BURNING SMELL. FIRE SERVICES INSPECTED THE AIRCRAFT WITH THERMAL IMAGING CAMERAS, NOTHING ABNORMASDR R61A201510180729Fmu · malfunctionedCREW REPORTED THAT THE NR 2 ENGINE ROLLED BACK TO 27 PERCENT N1. AT 1000 FT, THE AUTOTHROTTLE TURNED OFF AND A MASTER CAUTION WARNING APPEARED. CREW DECLARED AN EMERGENCY AND ELECTED TO DIVERT. WITH EMERGENCY VEHICLES ROLLING, CREW LANDED WITHOUT INCIDENT. SDR R61A201510170727Engine · power lossCREW NOTED THAT THE NR 2 ENGINE WAS NOT PRODUCING FULL POWER. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES IAW AMM WITH NO DEFECTS NOTED. ACFT IS GOOD FOR SERVICE.SDR R61A201509140635Engine · power lossCREW REPORTED A LOUD BANG FOLLOWED BY LOSS OF ALL POWER FROM THE NR 1 ENGINE. CREW DECLARED AN EMERGENCY, RAN QRH AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT.SDR R61A201509110628Bleed Valve · failedCREW RECEIVED A BLEED NR 2 OVER PRESSURE MESSAGE. FOLLOWED QRH, REDUCED THRUST TO IDLE AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R ENGINE 2 NAPRSOV IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.SDR CA150909003Brake Disc · disintegrated(CAN) AFTER LANDING AND PARKING AT THE GATE THE CAPTAIN ADVISED THE LOCAL MAINTENANCE THERE THAT THE BRAKES ON THE RT SIDE DID NOT FEEL NORMAL AND THE NR 4 BRAKE WEAR PIN WAS MISSING. UPON VISUAL INSPECTION OF THE BRAKE THEY FOUND THE NR 4 BRAKE DISINTEGRATED SDR R61A201508140526Fmu · failedABOUT 3 MILES FROM LANDING, CREW REPORTED THE NR 1 ENGINE FAILED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AFTER BEING CHECKED OUT BY THE FIRE DEPARMENT, CREW TAXIED TO GATE UNDER OWN POWER. MAINTENANCE TROUBLESHOT, R & R FMU IAW AMM AND OPS SDR R61A201507150446Unknown · odorCREW REPORTED A STRONG VAPORIZED OIL ODOR SHORTLY AFTER TAKEOFF. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN ENGINE IAW MM 72-00-00 AND AMM AND NO DEFECTS WERE NOTED. ACFT IS GOOD FOR SERVICE.SDR R61A201505310355Seat Track · corrodedDURING HEAVY CHECK WAS REPORTED THAT LT SEAT TRACK BEAM EXTENSION IS CORRODED, FRAME 85-86. MAINTENANCE R & R ALL SOLID RIVETS INTOP OF BEAM IAW SRM 51-41-01, PERFORMED EWIS PROTECTION, IAW SWPM 20-67-00. RESTORED TOP COAT IAW SRM 175 51-23-04,05,06. ACFT RESDR UHLA201505290417Engine · shutdownCLIMBING THROUGH 11,000 FT, A LOUD BANG CAME FROM ENGINE 2 FOLLOWED BY YAW AND AN IMMEDIATE LOSS OF POWER. EMERGENCY WAS DECLARED AND RETURNED FOR LANDING. THE ENGINE STILL HAD N1 ROTATION AND ALL PARAMETERS WERE NORMAL. R & R E2.SDR C77A20150409014Override Switch · brokenRIGHT ENG FAILED IGNITION STATIC CHECK. IGNITERS DIDN’T FIRE WITH THE RT ENG IGNITION SWITCH ON. FOUND RT ENG OVERRIDE SWITCH WITH BROKEN TERMINAL. R & R ENG START PANEL IAW AMM 71-00-02 ON WO 15502334B4. OPERATIONS CHECKED GOOD. START PANEL ASSEMBLY PN 1SDR R61A201503190177Blade · bird ingestionCREW HEARD LOUD NOISE AFTER BRINGING THE GEAR UP. NR 2 ENGINE WENT AMBER, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NUMEROUS DAMAGED FAN BLADES DUE TO BIRD STRIKE. ACFT REMAINS OUT OF SERVICE. REPLASDR R61A201412291264Engine · malfunctionedAT ABOUT 1000 FT, CREW REPORTED A LOUD NOISE COMING FROM THE NR 2 ENGINE. RECEIVED A NR 2 ENGINE CONTROL FAULT MESSAGE, RAN QRH AND PLACED THE NR 2 ENGINE IN IDLE, AT THAT POINT NOISE SUBSIDED. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOSDR R61A201411281211Bearing · leakingCREW HEARD FORWARD LAVATORY FIRE DETECTOR GOING OFF AND A FEW SECONDS LATER RECEIVED A LAV SMOKE MESSAGE. F/A CALLED AND STATED THEY COULD SEE AND SMELL SMOKE IN THE CABIN. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTESDR R61A201411221199Skin · damagedDAMAGE ON LT SIDE OF CENTER FUSELAGE BELOW L3 PAX WINDOW BETWEEN FRAMES 24-25 STRINGER S18-19L. REPAIRED THE DAMAGE IAW SRM 53-21-01.SDR SWIA201439904Blade · vibrationDURING FLIGHT, THE NR 1 ENGINE LOW PRESSURE VIBRATION REACHED 4.0 CAUTION AND FLUCTUATED BETWEEN 3.7 AND 4.0 ENTIRE FLIGHT. DIVERTED, REMOVED NR 1, 25, 26 FAN BLADES PINS OF LT ENGINE AND CLEANED AND INSPECTED AND LUBRICATED IAW AMM. PERFORMED VIBRATION CHECSDR UHLA2014101700695Bleed Valve · malfunctionedDURING CLIMB AT AROUND 4000 FT, NR 1 BLEED OVERPRESSURE ILLUMINATED ON ECAS. RAN QRH, BLEED 1 VALVE HAS AN AMBER CROSS. DIVERTED, NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. AFTER TOUCHDOWN, BLEED 1 FAIL. R & R NR 1 ENGINE HIGH STAGE BLEED VALVE IAW AMM SDR UHLA2014101200683Engine · damagedWHILE CLIMBING 7000-8000 FT OUT, HEARD A LOUD BANG, SHORTLY AFTER CAUTION NR 1 ENGINE MESSAGES. REDUCED POWER, THE ITT PEAKED VERY HIGH AND SHUT DOWN ENGINE. DECLARED EMERGENCY, DIVERTED, LANDED WITHOUT INCIDENT. R & R NR 1 ENGINE RUNS OPS CHECKED GOOD.SDR UHLA2014092100673Wire Harness · damagedL2 DOOR, SERVICE DOOR, NOT INDICATING CLOSED OR OPEN. R & R L2 DOOR ELECTRICAL WIRE HARNESS IAW AMM 52-72-21. OPS CHECKED GOOD.SDR R61A201409131060Fcu · leakingCREW REPORTED THAT THEY HAD A 600 POUND FUEL IMBALANCE AND SELECTED THE CROSS FEED TO REBALANCE. THEY REPORTED THAT THEY SAW THE FUEL QUANTITY RAPIDLY DROP, FOLLOWED THE QRH AND SHUTDOWN THE NR 2 ENGINE. CREW DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUTSDR UHLA2014091100672Engine · odorNR 1 PACK HAD A STRONG ODOR ON CLIMBOUT, AND ODOR WENT AWAY WITH PACK 1 SELECTED OFF. R & R NR 1 ENGINE IAW CR72-10-400-0001. OPS CHECKED GOOD.SDR UHLA2014090800624Blade · damagedENCOUNTERED MULTIPLE BIRD STRIKES SHORTLY AFTER TAKEOFF. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R & R ENGINE 2 BLADES 2, 3, 16, AND 17. DID RII AND HIGH POWER RUNS. HIGHEST VIBE WAS 1.4 FOR LP AT MAX THROTTLE.SDR UHLA2014090100636Seal Rest · gougedL1 DOOR SEAL REST, ON CUTOUT, GOUGED, LOWER AFT. R & R AFT SEAL REST, IAW SRM 51-41-01, & 51-43-01.SDR C77A20140818001Engine · failedNUMBER 1 ENG FAIL ON CLIMB OUT. APPROACHING 3500 FEET CREW HEARD A LOUD BANG ORIGINATING FROM THE CAPTAIN'S SIDE OF ACFT. ENG NR 1 CEASED PROVIDING POWER & THE CORRESPONDING ENG TEMP EXCEEDED TOLERANCES. R & R NR 1 ENG.SDR R61A201408030985Bracket · crackedDURING HEAVY CHECK, FOUND NLG STEERING MANIFOLD BRACKET IS CRACKED. MX R & R NLG STEERING MANIFOLD BRACKET IAW SRM 51-41-02, 51-43-03, PN 170-10788-401, BRACKET.SDR C77A20140717001Window Frame · gougedDURING BASIC 2 CHECK, MAINTENANCE FOUND GOUGE DAMAGE TO THE WINDOW FRAMES AT 6L PN 170-67477-403 BETWEEN FRAME 31 - 32, 7L PN 170-67477-403 BETWEEN FRAME 33 - 34, 15R PN 190-27007-401 BETWEEN FRAME 60 - 73 & 16R PN 170-66790-403 BETWEEN FRAME 74 - 75. THE DAMSDR UHLA2014063000473Blades · damagedBIRDSTRIKE ON NR 1 ENGINE AFTER ROTATION. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. INSPECTED AND FOUND DAMAGE TO THREE FAN BLADES, DID NOT GO THROUGH THE CORE. R & R SIX BLADES, THREE PAIRS, PERFORMED VIBRATION RUN, OPS CHECKED GOOD.SDR C77A20140622001Doubler · corrodedDURING BASIC CHECK IN SAT, INSPECTION DISCOVERED THE AFT CARGO, AFT LOWER CUT OUT INTERNAL DOUBLER PN 170-85307-001 TO HAVE CORROSION DAMAGE. THE DAMAGE IS LOCATED BETWEEN FRAME 80 & 81, STRINGER 27R - 28R. THE DAMAGE CONSISTS OF THE FOLLOWING APPROXIMATE DISDR UHLA2014061600485Unknown · odorVERY STRONG MUSTY/BURNING OIL ODOR DURING TAKEOFF AND DESCENT. ODOR WAS NAUSEATING AND NOTICED IN CABIN AND COCKPIT. PERFORMED ENGINE RUNS REF AMM 71-00-01. COULD NOT DUPLICATE ODOR IN COCKPIT OR CABIN.SDR C77A20140613002Slide · low pressureR2 DOOR SLIDE SHOWING LO PRESS AT 2550 PSI. REPLACED R2 DOOR SLIDE IAW TASK CARD. OK FOR SERVICE.SDR UHLA2014050900353Engine · vibrationINFLIGHT, NR 1 ENGINE HIGH LP VIBRATION UP TO 5.0, HP VIBRATION 1.7. VIBRATION CAN BE HEARD AND FELT. DIVERTED, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R NR 1 ENGINE.SDR C77A20140313027Plate · wornLT ENG OTBD THRUST REVERSER PN 15G0002-013, SN HRD00487, LT ENG OTBD THRUST REVERSER TRANS COWL INTERNAL UPPER & LOWER BONDING PLATES ARE WORN. IAW THE EFFECTIVITY OF THESE THRUST REVERSERS, THE BONDING PLATES THAT ARE REQUIRED ARE NO LONGER MANUFACTURED, PN SDR C77A201401240033Seal · wornRIGHT ENG OTBD THRUST REVERSER, PN 15G0003-014, SN HRD00343, THRUST REVERSER FRONT 12 O'CLOCK PLATFORM SEAL IS TORN. IAW THE AFFECTIVITY OF THESE THRUST REVERSERS, THE SEALS REQUIRED ARE NO LONGER MANUFACTURED, PN 14G0410-204. REPLACED UPPER SEALS ON WORK ORSDR C77A201401240034Seal · wornRIGHT ENG OTBD THRUST REVERSER, PN 15G0003-014, SN HRD00343, THRUST REVERSER DRAIN MAST SEAL IS TORN. IAW THE AFFECTIVITY OF THIS THRUST REVERSER, THE SEAL REQUIRED IS NO LONGER MANUFACTURED, PN 14G0659-205. REPLACED LOWER SEALS ON WORK ORDER 738174-409 IAW SDR C77A201401240035Seal · wornRIGHT ENG OTBD T/R PN 15G0003-014, SN HRD00343, T/R LOWER REAR SEAL CORNER IS TORN. IAW THE AFFECTIVITY OF THIS T/R, THE SEAL REQUIRED IS NO LONGER MANUFACTURED, PN 14G0324-209. REPLACED LOWER SEALS ON WORK ORDER 738174-411 SERVICE BULLETIN 78-0050 R01 IAW ESDR UHLA2014011300005Engine · failedDURING CLIMB OUT, A LOUD BANG WAS HEARD, FOLLOWED BY ABNORMAL VIBRATION. NR 1 ENGINE FAIL MESSAGE. SHUTDOWN NR 1 ENGINE IN FLIGHT. RETURNED TO FIELD, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R NR 1 ENGINE AND REPLACED C SUMP SEALS, OPS CHECKED GOOD.SDR C77A20131223005Seal · tornLT ENG INBD THRUST REVERSER PN 15G0003-013, SN HRD00410, FRONT 12 O'CLOCK PLATFORM SEAL, PN 14G0410-204 IS TORN. IAW THE AFFECTIVITY OF THE THRUST REVERSER THE SEAL REQUIRED IS NO LONGER MANUFACTURED. REPLACED UPPER SEALS ON WO 739450-424 GE CF 34-8E SERVICESDR C77A20131223006Seal · tornLEFT ENG INBD THRUST REVERSER PN 15G0003-013, SN HRD00410, FRONT 12 O'CLOCK CORE COWL SEAL PN 14G0058-206 IS TORN. IAW THE AFFECTIVITY OF THE THRUST REVERSER THE SEAL REQUIRED IS NO LONGER MANUFACTURED. REPLACED UPPER SEALS ON WO 739450-435 GE CF 34-8E SERVISDR R61A201311221234Engine · malfunctionedHOLDING AT 14000 FEET, CREW HEARD A LOUD BANG AND FELT AIRCRAFT SHIMMY. NOTED THAT THE N1 ON NR 2 ENGINE WAS IN THE 49'S AND SPOOLING BACK UP. CREW RECEIVED MASTER CAUTION LIGHT AND RAN QRH. REPORTED THAT THE ENGINE WAS RUNNING NORMALLY AND OIL AND HYD LEVESDR UHLA2013102500537Engine · smokeLAVATORY SMOKE EICAS INDICATION DURING CLIMB THOUGH 1,000 FEET. CABIN FILLED WITH SMOKE. R & R NR 2 ENGINE IAW 72-10-400-0001. OPS CHECKED GOOD.SDR UHLA2013101900522Valve · leakingCREW REPORTED ODOR IN CABIN DURING ALL PHASES OF FLIGHT. CREW DEPLOYED OXYGEN MASKS. MX R & R E2 PRV.SDR UHLA2013100300478Engine · vibrationDURING CLIMB, NOTICED VIBRATION FROM RT ENGINE, VIBRATION REDUCED WITH POWER REDUCED. RECEIVED ENG 2 T2 HEAT FAIL MESSAGE, RAN QRH. ATC REPORTED AFTER TAKE OFF, TIRE RUBBER ON RUNWAY. DIVERTED, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MX R & R ENGINE ASDR R61A201310030980Support Bracket · crackedDURING HEAVY CHECK, LT PACK DUCT SUPPORT BRACKET IS CRACKED. MX R & R BRACKETS IAW SRM 51-41-01, 51-43-01.SDR R61A201310020950Transducer · failedFL 270, RECEIVED AN NR 2 ENG LOW OIL PRESSURE WARNING LIGHT. OIL PRESSURE READ ZERO. CREW FOLLOWED INSTRUCTIONS ON QRH AND SHUTDOWN NR 2 ENGINE, DECLARED AN EMERGENCY AND DIVERTED, WHERE THEY LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MX INSPECTED AND FOUNSDR C77A20130929016Seal · wornRT ENGINE INBD THRUST REVERSER FRONT12 O'CLOCK CORE COWL SEAL IS TORN. REPLACED UPPER SEALS IAW EO E17X-7800-001.3, REV 1.SDR C77A2013090300001Inlet · crackedLEFT ENGINE INLET COWL, CRACKED ON INNER BARREL AT FAN AIR INLET TEMP SENSOR, ACOUSTIC LINNER, AND T2 PROBE DOUBLER.
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