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 = 'CF343B1' 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 = 'CF343B1' 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 A6WA201401104527Acoustic Panel · damagedRIGHT LOWER TRANS COWL ACOUSTIC PANEL HAS FIVE EACH DENTS WITH GOUGING & CRACKED SKIN. REPLACED FIVE DENTS IAW CRJ 200 SRM 51-12-00. REPAIRED WITHIN STRUCTURAL LIMITS, NO CRACKS NOTED IN SKIN.SDR ASOA2014011609766Engine · overtempCLIMBING OUT OF 10,000 FEET, LT ENGINE ITT WENT INTO RED RANGE. N2 GAGE AT IDLE "VIBRATION" REMAINED. DECLARED AN EMERGENCY, ACFT RETURNED TO DEPARTURE. PERFORMED BORESCOPE INSPECTION ON LT ENGINE. DETERMINED UNSERVICABLE. ENGINE CHANGED IAW AMM 71-00-00SDR ASOA2014011609764O-Ring · failedAFTER TAKEOFF, RECEIVED RT OIL PRESSURE WARNING MESSAGE ACCOMPANIED WITH FLUCTUATIONS OF 25-36 PSI C/W QRH RETURNED TO DEPARTURE. ACFT RETURNED TO DEPARTURE AFTER TAKE OFF, EMERGENCY DECLARED. R & R RT ENGINE OIL PRESSURE SWITCH O-RING IAW AMM-79-31-03, LEASDR SWIA201435941Control Cable · brokenLT THRUST LEVER UNRESPONSIVE, PERFORMED QRH PROCEDURE & SHUTDOWN LT ENG. FLT 2901 REPLACED BROKEN LT ENG THROTTLE CONTROL CABLE IAW AMM.SDR VNAA2014010200002Carbon Seal · failedCREW REPORTED RT ENGINE LOW OIL PRESSURE UPON THRUST ADDITION FOR TAKEOFF. OIL PRESSURE DROPPED TO 22 PSI WITH RED MASTER WARNING ALERT. CREW REJECTED TAKEOFF BELOW 80 KTS. AND RETURNED TO GATE. MAINTENANCE INSPECTED, R & R RT ENGINE IDG CARBON SEAL AND PERFSDR CA131230002Landing Gear · failed(CAN) DURING CLIMB, AFTER SELECTING LANDING GEAR UP, FLIGHT CREW RECEIVED A NOSE GEAR UNSAFE INDICATION AND A LANDING GEAR DISAGREE INDICATION. FLIGHT CREW WERE ABLE TO CONFIRM GEAR DOWN AND LOCKED, HOWEVER COULD NOT CONFIRM NOSE GEAR UP. ACFT COMPLETED FLIGHSDR REXA2013121502407Display · false indicationRT THRUST REVERSER UNLOCK MESSAGE IN FLIGHT. EMERGENCY DECLARED. R & R RT PDU IAW AMM 78-32-03. OPS CHECKED GOOD. NO MESSAGES NOTED. LEAK CHECKED GOOD IAW AMM 78-32-03.SDR CA131211007Window · cracked(CAN) F/O SIDE WINDOW CRACKED. WINDOW REMOVED AND REPLACED IAW 56-12-01-00-801 AND 56-12-01-400-801.SDR CA131209007Engine · power loss(CAN) DURING CLIMB AT FL250, NR 1 ENGINE THRUST LOST, ACCOMPANIED WITH CLAPPING SOUND. DECIDED TO RETURN TO AIRPORT OF DEPARTURE. ACFT MADE SUCCESSFUL LANDING.SDR VNAA2013120600003Anti-Ice Valve · failedCREW REPORTED LT COWL ANTI-ICE MESSAGE IN FLIGHT WITH COWL ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, & R & R LT DUCT VALVE, R & R LT COWL ANTI-ICE RELIEF VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FSDR VNAA2013120600004Idg · failedCREW REPORTED NR 2 GENERATOR OFF MESSAGE WITH ACCOMPANYING INTEGRATED DRIVE, NR 2 GENERATOR DISCONNECT MESSAGE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED & R & R RT IDG AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR CA131209004Actuator · failed(CAN) CREW ADVISE THAT THERE WAS A FLAP FAIL ON FINAL APPROACH. ON LONG FINAL, FLAPS 8 SELECTED AND HAD THE FLAPS FAIL AND DID THE LANDING AT FLAPS ZERO. LANDING UNEVENTFUL. FLAP FAIL EVENT, OPERATING UNDER CREW RESET, RESOLVED ON W/O: 411581 TASKCARD: NR-00SDR CA131209006Oil System · leaking(CAN) NR 1 ENGINE OIL LEAK FOUND DURING FLIGHT, CREW PERFORMED NR 1 ENGINE INFLIGHT SHUTDOWN. DUE TO FOG AT DESTINATION AIRPORT CREW PERFORMED EMERGENCY LANDING AT AN ALTERNATE AIRPORT.SDR A6WA201311244438Mount Bracket · crackedLEFT ENG JET PIPE INBD & OTBD MOUNT NUTPLATE BRACKETS ARE CRACKED. R & R CRACKED NUTPLATE BRACKETS IAW CRJ 200 SRM 51-42-06.SDR A6WA201311234401Channel · gougedLEFT LOWER CORE COWL HANT CHANNEL CRACKED & GOUGED AT END CAP. REMOVED DAMAGED BY EDGE BLENDING, FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 54-00-00 FIG 102.SDR CA131126006Actuator · failed(CAN) FLAP FAIL AT 0 DEG POSITION ON APPROACH. ALL INBD AND OTBD ACTUATORS REPLACED. SYSTEM OPS CHECKED OK.SDR CA131125001Windshield · failed(CAN) DURING CLIMB, FLIGHT CREW DECLARED AN EMERGENCY AFTER THE LT WINDSHIELD SHATTERED. THE ACFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. A MAINTENANCE TEAM TRAVELLED ON SITE, REPLACED/TESTED THE WINDSHIELD AND RELEASED THE ACFT BACK INTO SERVICE.SDR A6WA201311204402Nut Plate · crackedRIGHT EXHAUST NOZZLE FAIRING ATTACH POINT NUTPLATE CLIP AT 6 O`CLOCK POSITION IS CRACKED. REMOVED UNSERVICEABLE NUTPLATE CLIP & REPLACED WITH A NEW SERVICEABLE ONE.SDR CA131119006Throttle Cable · failed(CAN) AT TOP OF DESCENT FROM FL250, THRUST LEVERS REDUCED TO IDLE AND LT ENGINE N1 REMAINED AT 94 PERCENT. LT ENGINE WAS NOT RESPONSIVE TO ANY THRUST LEVER MOVEMENT FORWARD OR AFT. THRUST LEVER MOVEMENT FELT NORMAL. THERE WERE NO OTHER MESSAGES NOR ABNORMAL SDR A6WA201311124359Retainer · crackedRIGHT PYLON PANEL 422AT HAS CRACKED SEAL RETAINER. REMOVED, FABRICATED & INSTALLED NEW SEAL RETAINER.SDR A6WA201311074358Stiffener · gougedRIGHT EXHAUST FAIRING FWD UPPER STIFFENER IS GOUGED. R & R DAMAGED STIFFENER.SDR A6WA201310314030Blades · damagedREQ BIRD STRIKE INSP LH ENG GEAR AND FLAPS WERE UP. LT ENG VIBE AT 1.5. N1 REDUCED 10 PERCENT COMPARED TO RT ENG APPROX 2 MINUTES ENG INDICATIONS RETURNED TO NORMAL. KEEP LT ENG AT REDUCED POWER SETTING AUDIBLE CHANGE WHEN TRYING TO INCREASE POWER. CW BS INSDR A6WA201310314360Trunnion · damagedDURING INCORPORATION OF THE MLG TRUNNION LOWER FLANGE, COLD WORKING FOUND TWO EACH OVERSIZED HOLES IN THE STRAP, PLANK & LOWER FLANGE. ONE ON THE LT SIDE & ONE ON THE RT SIDE. COMPLIED WITH REO 601R-57-21-2020 REV FOR COLD WORKING TWO EACH OVERSIZED FASTENERSDR CA131101009Panel · detached(CAN) FOUND MISSING ACCESS PANEL OF THE EXHAUST NOZZLE, PN 228 & 8722, 50181 & 8722, 911 ACCESS PANEL FOUND IN ANOTHER TOWN ON THE RUNWAY.SDR A6WA201311014028Check Valve · failedRECEIVED LT ENGINE OIL WARNING WITH ASSOCIATED DROP IN ENGINE OIL PRESSURE, ENGINE TO IDLE WITHIN 5 SECONDS. SHUTDOWN LT ENGINE IAW QRH. SERVICED LT ENGINE WITH 8 PTS. FOUND OIL TANK CHECK VALVE FAILED & LEAKING EXTERNALLY. R & R CHECK VALVE IAW AMM 79-12-13SDR CA131023001Display · failed(CAN) PILOT DECLARED EMERGENCY LANDING (PAN-PAN) DUE TO LOSS OF ALL SOURCE OF NAVIGATION EXCEPT FOR STANDBY INSTRUMENT. WAITING FOR FURTHER INFORMATION FROM PILOT REPORT AND MX CREW. LANDING WAS UNEVENTFUL. OPERATOR IS INVESTIGATING AND TROUBLESHOOTING. THEY SSDR CA131023010Fuel Control · malfunctioned(CAN) RT ENGINE IS LOOSING POWER. ENGINE GROUNDED. CARRIED OUT. NR 2 ENGINE WOULD NOT ACCEL ABOVE 54 PERCENT N1 AND 80 PERCENT N2. ITT 500 DEGREES AND FUEL FLOW 900 LBS, HR APR SYS CHECK CARRIED ON NR 1 ENGINE CHECKED SERVICEABLE. UNABLE TO TEST NR 2 DUE SDR VNAA2013101700007Pdu · failedCREW REPORTED LT THRUST REVERSER UNLOCK CAUTION MESSAGE IN DESCENT OUT OF FL200. CREW DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT, R & R LT THRUST REVERSER PDU AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR A6WA201310144257Tailpipe · crackedRIGHT ENGINE TAIL PIPE FROM FWD STIFFENER IS CRACKED AT INBD 4 O`CLOCK. REPAIRED RT ENGINE TAIL PIPE STIFFENER IAW CMM 78-11-00.SDR CA131011005Shroud · corroded(CAN) THE FUEL SHROUD ASSY IN THE CARGO BAY UNDERFLOOR, LOCATED FS574.0, WAS FOUND CORRODED AND WAS LEAKING INTO THE BELLY INSULATION REF IPC 28-20-00, FIG 5, ITEM 105. THE CORROSION AT THE O-RING LOCATION WAS DETERIORATED TO THE POINT WHERE THE O-RING WOULD NSDR CA131008007Panel · missing(CAN) DURING GROUND HANDLING THE RAMP CREW NOTICED A PANEL MISSING FROM THE LT ENGINE TAILCONE. IT IS NOT KNOWN WHEN OR WHERE THE PANEL DEPARTED THE ACFT HOWEVER THE DAMAGE INDICATES THAT IT DEPARTED IN FLIGHT. THE ENGINE TAILCONE ASSY WAS REPLACED. PANEL, PSDR CA131010005Computer · inoperative(CAN) REPLACED BOTH FLIGHT CONTROL COMPUTERS, FCC, FOR OPS PURPOSES WITH O/H UNITS. THE ACFT DID NOT HAVE ANY PROBLEMS BEFORE THIS WAS DONE. EXPERIENCED MULTIPLE AP DISCONNECTS BOTH INTERMITTENTENTLY AND 1 HARD FAILURE. HAD TO PROCURE 3 MORE UNITS IN ORDER TSDR CA131004001Compressor · fod(CAN) FLIGHT CREW REPORTED THAT THE LT ENGINE INDICATED TURBINE TEMPERATURE, ITT WAS RUNNING 60 ABOVE THE RT ENGINE AND WAS SLOW TO SPOOL. BOROSCOPE INSPECTION REVEALED ENGINE COMPRESSOR DAMAGES. OBSERVED DAMAGES ARE CONSISTENT WITH FOREIGN OBJECT DEBRIS, FOSDR VNAA2013092400011Oil System · low pressureCREW REPORTED LT ENGINE OIL PRESSURE AMBER DURING TAKEOFF ABOVE 80 KTS AND FOR FIRST 3 MINUTES AFTER TAKEOFF. MAXIMUM PSI OBSERVED WAS 150 PSI. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MX INSPECTED, R & R LT ENGINE AND PERFORMED CHECKS IAW AMM. SDR CA130916006Line · chafed(CAN) DURING THE ACCOMPLISHMENT OF TASK RJ2-57-900-320, INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION, THE STANDBY FUEL FEED SYS TUBE ASSEMBLY THAT JOINS THE 2 BOOST PUMPS IN THE CENTER WING TANKS WAS FOUND CHAFING ON THE CENTER FRAME AT APPROXIMATELY FSDR SWIA201334499Bolt · damagedLT ENGINE FWD YOKE PIN BOLTS UPPER & LOWER HAVE AREAS OF PITTING. C-CHECK REPLACED IAW AMM.SDR SWIA201334500Bearing · damagedLT ENGINE FWD YOKE MOUNT LOWER BEARING IS PITTED. C-CHECK REPLACED FWD YOKE ASSEMBLY IAW AMM.SDR SWIA201334501Bushing · damagedLT ENGINE AFT THRUST MOUNT BUSHING IS PITTED. C-CHECK REPLACED AFT THRUST MOUNT BUSHING IAW AMM.SDR CA130910006Window · cracked(CAN) RIGHT WINDSHIELD CRACKED DURING CLIMBOUT.SDR CA130912004Engine · fluctuates(CAN THE FLIGHT CREW RECEIVED ENGINE FLUCTUATION INDICATIONS. ATC WAS ADVISED AND AN EMERGENCY DECLARED. THE ACFT TAXIED WITHOUT FURTHER INCIDENT.SDR CA130828002Selector Valve · failed(CAN) FOLLOWING GEAR UP SELECTION, THE NLG DIDN`T RETRACT AND FLIGHT CREW RECEIVED A GEAR DISAGREE WARNING. THE NLG RETRACTED SHORTLY AFTER. DECISION WAS TAKEN TO RETURN AND LAND, UPON GEAR DOWN SELECTION THE NLG DIDN`T EXTEND. A SUCCESSFUL ALTERNATE EXTENSSDR CA130815003Indicator · failed(CAN) NR 2 PARKING BRAKE ACCUMULATOR LOW. RESOLVED ON W/O: 395796, TASKCARD: NR-00006, CHARGE ACCUMULATOR FOUND GAUGE NOT TO MATCH THE CHARGE PRESSURE. GAUGE STRUCTURALLY FAILED WHEN SYS CHARGED. NR 2 SYSTEM PARKING BRAKE ACCUMULATOR CHARGE GAUGE REPLACEDSDR VNAA2013081000006Track · lack of lubeCREW REPORTED LEFT THRUST REVERSER UNLOCKED AMBER CAS MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED, LUBED THRUST REVERSER TRACKS AND PDU. PLUNGER AND PERFORMED CHECKED IAW AMM. ACFT RELEASED FOR SERVICE.SDR REXA2013074501566Engine · power lossABORTED TAKE OFF AT 80 KNOTS DUE TO RT ENGINE N1 WOULD NOT GO ABOVE 60 PERCENT. POWER APPEARS LOW. RETURNED TO GATE. EMERGENCY NOT DECLARED. INSPECTED ENGINE, NO DEFECTS NOTED.SDR A6WA2013081641140Structure · crackedLEFT UPPER CORE COWL HAS CRACK ON INBD EDGE NEAR FWD HINGE. REPAIR CRACK IAW EA 15-2013-350, TASK 71-12-01-300-826, AOL SRS 118.SDR REXA2013080801571Warning Message · false activationDURING CRUISE AT FL200, RECIEVED A LEFT ENGINE N2 OVERSPEED INDICATION. N1, ITT, FF, OIL TEMP, OIL PRESSURE ALL REMAINED NORMAL. THRUST REDUCED TO 80 PERCENT AND N2 INDICATION RETURNED TO NORMAL. CONTINUED FLIGHT WITH PERFORMED OPS CHECK AND INSPECTED BLUE HASDR A6WA2013081641139Structure · debondedLEFT LOWER CORE COWL AT THE HINGE HAS PROTECTIVE METAL SHEET DISBONDED FROM INTERNAL COMPOSITE. FABRICATED AND INSTALLED RETAINING STRIP ON LT LOWER CORE COWL AT THE HINGE PROTECTIVE METAL SHEETING.SDR CA130731007Window · cracked(CAN) REF: DEFECT-1125817, F/O SIDE WINDOW SHATTERED. CREW SAW ELEMENT BURNING IN THE WINDOW THEN IT SHATTERED. RESOLVED ON W/O: 394307 TASKCARD: NR-00001, F/O SIDE WINDOW REPLACED IAW MM 56-12-01. PRESSURIZATION CHECK CARRIED OUT, FUNCTION CHECKED SERVICEASDR A6WA2013081641136Frame · crackedRIGHT JETPIPE FAIRING NR 1 FRAME CRACKED AT 3:00 POSITION AT TOOLING HOLE. REPAIRED IAW CMM 78-11-00, REPAIR SRS 043.SDR A6WA2013081641137Structure · chafedLEFT LOWER CORE COWL HAS 6 CHAFES ON INTERNAL COMPOSITE. MEASURED CHAFE MARKS ON LT LOWER CORE COWL INNER SKIN FOUND TO BE WITHIN SERVICEABLE LIMITS, 1 FOUND TO BE WITHIN REPAIREABLE LIMITS AND 1 FOUND TO HAVE PARTIAL PENETRATION AND REPAIRED IAW CMM 71-12-01
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