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 = 'CF348C5' 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 = 'CF348C5' 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 REXA2014121801220Structure · wornNR 1 ENGINE AFT CORE COWL SHOWS WEAR AT PYLON INTERFACE AREA. MECH REMOVED DAMAGE AT PYLON INTERFACE AREA, FABRICATED RUB STRIPS PERFORMED NDT AND INSTALLED RUB STRIPS IAW SRM 54-13-00-201-006-A01 AND NDTM PART 1 51-20-006-250-A01 AND SRM 51-42-06-001-001-A01SDR REXA2014121801221Skin · damagedNR 2 ENGINE AFT CORE COWL SHOWS WEAR DAMAGE AT PYLON INTERFACE AREA. MECH REMOVED DAMAGE AT PYLON INTERFACE AREA, FABRICATED RUB STRIPS. PERFORMED NDT AND INSTALLED RUB STRIPS IAW SRM 54-13-00-201-006-A01 AND NDTM PART 1 51-20-006-25-A01, SRM 51-42-06-001-00SDR REXA2014121701216Skin · damagedNR 1 ENGINE AFT CORE COWL STAND OF BLOCK AT 3 O'CLOCK POSITION HAS DAMAGE ALIGNMENT TAB. MECH R & R STANDOFF BLOCK AND INSULATION PAD AT NR 1 ENGINE AFT CORE COWL AT 3 O'CLOCK POSITION IAW SRM 54-13-00-201-002-A01.SDR REXA2014121701217Pan · damagedNR 2 ENGINE AFT CORE COWL INSULATING PAD CRACKED AND STANDOFF BLOCK ALIGNMENT TAB DAMAGED AT 9 O'CLOCK POSITION. MECH R & R STAND OFF BLOCK AND INSULATING PAD AT NR 2 ENG AFT CORE COWL AT 9 O'CLOCK POSITION IAW SRM 54-13-00-201-002-A01.SDR CA141217007Acm · failed(CAN) PILOTS REPORTED SMOKE IN THE CABIN DURING ACFT TAXI. ACFT RETURNED TO GATE. FOUND ACM FAILED.SDR REXA2014121601211Structure · wornTASK CARD 900-71-440-100 RT ENG FWD UPPER CORE COWL BLOW OFF DOOR LATCH REST WORN. R & R RT ENG FWD UPPER CORE COWL BLOW OFF DOOR LATCH REST IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.SDR REXA2014121601212Structure · wornTASK CARD 900-71-440-100 RT ENG FWD LOWER CORE COWL BLOW OFF DOOR LATCH REST WORN. R & R RT ENG FWD LOWER CORE COWL BLOW OFF DOOR LATCH REST SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.SDR CA141216002Crossmember · cracked(CAN) WHILE CARRYING OUT INSPECTION IAW SBA670BA-32-020 A CRACK WAS IDENTIFIED ON MLG DOOR . THE SPECIFIC AREA OF THE CRACK WAS ON CROSSMEMBER. MLG DOOR HAS BEEN REPLACED IAW AMM WITH SERVICEABLE PART.SDR REXA2014121401207Hinge Bracket · wornTASK CARD 900-71-440-100 RT ENG FWD LOWER CORE COWL BLOW OFF DOOR HINGE BRACKET WORN. R & R RT ENG BLOW OFF DOOR HINGE BRACKET & HINGE LEVER IAW SRM 51-42-20-001-001-A01, AMM 71-12-05-05-400-801-A01 & SRM 51-41-02-001-001-A01.SDR CA141215001Bolt · sheared(CAN) DURING THE ACCOMPLISHMENT OF TASK RJ9-52-830-500 - DETAILED INSPECTION OF THE PASSENGER DOOR INTERNAL STRUCTURE - IT WAS REPORTED THAT ON THE UPPER LATCH AFT FITTING, THE ATTACHMENT BOLT HEAD WAS FOUND SHEARED FROM CORROSION.SDR SWIA201440169Pin · unserviceableRT ENGINE VIBRATION REACHED 5.2 AT FL 360. REPLACED FAN BLADE PINS WITH SERVICEABLE UNITS. LUBED FAN BLADE TANGS AND REINSTALLED ORIGINAL SET OF FAN BLADES IAW ENGINE MANUAL.SDR CA141126004Windscreen · failed(CAN) WHILE IN CRUISE THE LEFT HAND WINDSHIELD SHATTERED (OUTER LAYER). THE CREW CARRIED OUT THE QRH AND DESCENDED TO FL100. FLIGHT LANDED AT DESTINATION WITHOUT FURTHER ISSUE.SDR CA141126005Roller · missing(CAN) IN THE CLIMB AT 4000 FEET THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE FLAPS INDICATED ZERO HOWEVER VISUAL INSPECTION SHOWED THEM SLIGHTLY EXTENDED. CREW CONTINUED TO DESTINATION AT A LOWER ALTITUDE AND SLOWER AIRSPEED. MAINTENANCE INVESTIGATION FOSDR REXA2014111101135Tab · damagedTASK CARD 900-26-440-100 NR 2 ENG AFT CORE COWL STANDOFF BLOCK AT 9 O'CLOCK POSITION SHOWS DAMAGE TO ALIGNMENT TAB. R & R IAW SRM 54-13-00-201-002-A01 & SRM 51-42-06-001-001-A01.SDR REXA2014111001131Tab · damagedTASK CARD 900-26-430-100 NR 1 ENG AFT CORE COWL SHOWS DAMAGE TO STANDOFF BLOCK ALIGNMENT TAB AT 3 O'CLOCK POSITION. R & R IAW SRM 54-13-00-201-002-A01.SDR MASA2014110202715Fadec · warning messageRT FADEC CAUTION IN FLIGHT, RETURNED TO DEPARTURE AND A EMERGENCY WAS DECLARED. REPLACED RT FADEC.SDR CA141030009Actuator · failed(CAN) SLATS DID NOT EXTEND WHEN SELECTED FOR LANDING. MDC INDICATED "SLAT ACTUATOR SYSTEM FAILED MECHANICAL JAM." DURING SUBSEQUENT MAINTENANCE ACTION, SERVICE LETTER 27-074 REV. A WAS CARRIED OUT. THIS ACTUATOR FAILED TORQUE TEST AND WAS REPLACED.SDR CA141028008Bleed Valve · malfunctioned(CAN) RT BLEED CAUTION, RT VALVE WILL NOT CLOSE WHEN SELECTED FOR DEICING. RIGHT BLEED VALVE REPLACED IAW AMM 36-12-01. ENGINE RUN UP COMPLETED BLEED VALVES OPERATE NORMALLY.SDR CA141027003Windshield · fractured(CAN) IN CRUISE, FLIGHT CREW REPORTED A SHATTERED RT WINDSHIELD. DECISION WAS TAKEN TO DESCEND TO A LOWER FLIGHT LEVEL AND CONTINUE TO DESTINATION. UPON ARRIVAL, ACFT WAS REMOVED FROM SERVICE AND MAINTENANCE CONFIRMED THE OUTER PLY WAS FRACTURED. THE RT WINSDR CA141204017Shroud · failed(CAN) HP DUCTS HAVE BEEN INSPECTED FOR THE FIRST TIME (10 000 FH) BY AIR NOSTRUM IN OCTOBER AND ROUGHLY 80% OF THE DUCTS ARE FAILING THE AMM CHECK BECAUSE OF EXCESSIVE LEAKAGE OF THE EXTERNAL SHROUD. SSP EVALUATION CONFIRMED THAT THE DUCTS ARE LEAKING EXCESSIVSDR REXA2014102301098Plate · chafedTASK CARD 900-71-430-100 1 ENG LOWER & UPPER FWD CORE COWL SHOWS CHAFE DAMAGE TO LOWER & UPPER DOUBLER PLATE WHERE THE BLOW OFF DOORS LATCH CATCHES. DOOR MUST BE OPEN TO SEE. REPAIRED NR 1 ENG LOWER & UPPER FWD CORE COWL BLOW OFF DOOR CATCH REINFORCING PADS SDR REXA2014101101049Fireshield · peelingTASK CARD 900-54-440-301 RIGHT ENG LOWER FWD CORE COWL FIRE SHIELD PEELING UP, TYPICAL LOCATION. REPAIRED RT ENG LOWER FWD CORE COWL IAW EO R54090.SDR CA141015004Clamp · torn(CAN) AFTER DEPARTURE AND GEAR UP THE NO 2A HYD PUMP CAUTION LIGHT CAME ON AND SYSTEM QTY WENT TO 0% MAINTENANCE FOUND LEAK AT FLEXIBLE LINE (REF IPC 29-17-06, FIG. 1C, ITEM 128) FROM IB AFT NR 2 PYLON DOWN TO THE HYDRAULIC DAMPENER. THE SADDLE CLAMP P/N BBDRESDR REXA2014100801043Block · wornTASK CARD CRJ900 C1 NR 1 ENG AFT CORE COWL ALIGNMENT STANDOFF BLOCK AT 3 O'CLOCK POSITION SHOWS WEAR DAMAGE TO ALIGNMENT TAB. R & R NR 1 ENG AFT COWL ALIGNMENT BLOCK IAW SRM 54-13-00-201-002-A01.SDR REXA2014100801044Block · wornTASK CARD NR 2 ENG AFT CORE COWL ALIGNMENT STANDOFF BLOCK AT 9 O'CLOCK POSITION SHOWS WEAR DAMAGE TO ALIGNMENT TAB. R & R STANDOFF BLOCK IAW SRM 54-13-00-201-0025-A01.SDR REXA2014100801045Cowling · wornTASK CARD CRJ900 C1 NR 1 ENG AFT CORE COWL SHOWS WEAR DAMAGE AT PYLON INTERFACE AREA. REPAIRED NR 1 ENG AFT CORE COWL AT PYLON INTERFACE IAW SRM 54-13-00-201-006-A01.SDR REXA2014100801046Cowling · wornTASK CARD CRJ900 C1 NR 2 ENG AFT CORE COWL SHOWS WEAR DAMAGE AT PYLON INTERFACE AREA. REPAIRED NR 2 ENG AFT CORE COWL AT PYLON INTERFACE IAW SRM 54-13-00-201-006-A01 BY INSTALLATION OF RUB STRIPS.SDR CA140919002Wire · failed(CAN) DURING TROUBLESHOOTING OF AN INOPERATIVE AUXILIARY POWER UNIT (APU) ASSOCIATED WITH AN APU FAULT CAUTION MESSAGE, SIGN OF OVERHEATING CONDITION WAS NOTICED AT THE APU STARTER POSITIVE ELECTRICAL LUG. AIRCRAFT DEFERRED IN ACCORDANCE WITH MEL 49-10-01-1.SDR REXA2014091300975Nozzle · gougedTASK CARD 900-26-440-100 NR 2 ENG EXHAUST NOZZLE PYLON INTERFACE GOUGED & NEEDS TYPICAL REPAIR. REPAIRED NR 2 ENG EXHAUST NOZZLE IAW SRM 54-13-00-201-006-A01.SDR CA140912010Wire Harness · damaged(CAN) DURING TAXI OUT, SMOKE IN THE CABIN WAS DETECTED. THE CREW DECIDED TO RETURN TO GATE FOR PROBLEM RESOLUTION. MAINTENANCE FOUND THE ORIGIN OF THE SMOKE WAS A PROBLEM WITH AN ELECTRICAL WIRE ASSEMBLY BEHIND THE NR 2 GALLEY. ROOT CAUSE UNDER INVESTIGATISDR CA140917010Pressure Switch · failed(CAN) DURING TAXI-OUT THE LH ENGINE EICAS MESSAGE "PRESS L ENG" REMAINED. THE FLIGHT CREW RETURNED TO GATE. MAINTENANCE REPLACED THE LOW OIL PRESSURE SWITCH WITH NO FURTHER ISSUES.SDR WVER2014090590601Skin · crackedTHE TRANSCOWL SKIN UNDER THE EXTRUSION NEAR LATCH IS CRACKED AROUND 2 FASTENER HOLES.SDR REXA2014082700869Fireshield · damagedLEFT ENG LOWER CORE COWL INNER SKIN FIRE SHIELD SHOWS WEAR & CHAFFING AROUND FWD CUT OUT APPROX 6 O'CLOCK POSITION TYPICAL. REPAIRED IAW EO R54090.SDR REXA2014082700870Fireshield · damagedLEFT ENG LOWER CORE COWL FIRE SHIELD HAS A PEELED & BENT CORNER MIDDLE OF COWLING. REPAIRED IAW EA CRJ954-02862.SDR CA140818007Gasket · failed(CAN) ENROUTE, CREW ADVISED DISPATCH THEY HAD HYDRAULIC ENGINE DRIVEN PUMP 2A CAUTION MESSAGE AND NEEDED TO DESCEND TO FL 260. HALF HOUR LATER THEY ADVISED THEY HAD LOST NUMBER TWO HYDRAULIC SYSTEM. CREW DECLARED AN EMERGENCY WITH ATC. FLIGHT SUCCESSFULLY LANDSDR REXA2014081200826Cowling · chafedLEFT ENG AFT CORE COWL HAS CHAFE DAMAGE BETWEEN COWL & PYLON INTERFACE. REPAIRED LT ENG AFT CORE COWL IAW SRM 54-13-00-201-006-A01. NO FURTHER DAMAGE.SDR REXA2014081200828Fireshield · chafedRIGHT ENG LOWER CORE COWL HAS CHAFE DAMAGE ON FIRE SHIELDS IN THE DRAIN STARTER ACCESS PANEL, WITHIN REPAIR LIMITS OF R54090. REPAIRED DAMAGE TO RT LOWER CORE COWL FIRE SHIELD IAW EO R54090.SDR CA140812004Engine · shutdown(CAN) DURING TAXI THE RT ENGINE DID AN AUTO SHUTDOWN. THE ITT BRIEFLY REACHED 1049. NEITHER ENGINE WAS AT POWER (9 KNOTS AT THE TIME OF THE EVENT) THE ENGINE HAD BEEN INSTALLED THE NIGHT BEFORE ROOT CAUSE UNDER INVESTIGATION.SDR CA140805005Pulley · seized(CAN) THE FLIGHT CREW REPORTED THAT THE ROLL CONTROL WAS STIFF IN FLIGHT FOR BOTH LT AND RT TURNS. MAINTENANCE INVESTIGATION FOUND A SEIZED PULLEY IN THE AILERON CIRCUIT AT THE LT WING ROOT. THE PULLEY WAS REPLACED AND SYSTEM TESTED SERVICEABLE.SDR REXA2014071500719Fireshield · damagedTASK CARD 90-26-440-100 NR 2 ENG LOWER CORE COWL FIRE SHIELD BETWEEN DRAIN PAN & ACOC VENT. REPAIRED NR 2 ENG LOWER CORE COWL FIRE SHIELD CHAFE IAW EO R54090.SDR CA140729004Selector Valve · malfunctioned(CAN) GEAR DISAGREE ON GEAR DOWN SELECTION., WHITE LIGHTS ON INITIAL , RE-SELECT HAD NO LIGHTS , THEN ALTERNATE EXTENSION THEY GOT ALL GREEN. REPLACED GEAR SELECTOR VALVE IAW AMM 32-32-10 GEAR SWING C/O NFF. ACFT RETURNED TO SERVICE.SDR SWIA201438654Bushing · galledRIGHT ENGINE FWD YOKE MOUNT LINK AND CLAMP-UP BUSHING GALLED AND SCORED AND BUSHING IS MIGRATED. REMOVED RT ENGINE FWD YOKE MOUNT LINK AND CLAMP-UP BUSHING AND REPLACED WITH A SERVICEABLE LINK AND CLAMP-UP BUSHING IAW AMM.SDR CA140709003Windshield · arced(CAN) ARCING ON THE ELECTRICAL HEATING SYSTEM ON LT WINDSHIELD.SDR CA140710001Seal · failed(CAN) AFTER TAKEOFF, DURING THE CLIMB PHASE OF FLIGHT, THE MAIN CABIN DOOR BEGAN SQUEALING. THE FLIGHT CREW DECIDED TO RETURN TO THE POINT OF DEPARTURE. AFTER ARRIVING, MAINTENANCE ACTION FOUND THAT THE MCD SEAL WAS RIPPED AT THE LOWER, FORWARD CORNER OF THE DSDR REXA2014063000660Fireshield · gougedTASK CARD 900-54-430-301 LT ENG LOWER COWL HEAT AROUND VENT PANEL HAS MINOR GOUGES. REPAIRED LT ENG COWL FIRE SHIELD IAW EO R54090.SDR REXA2014063000661Fireseal · wornTASK CARD 900-54-440-301 RT ENG LOWER COWL METAL FIRE SEAL ABOVE DRAIN MAST IS WORN THROUGH. REPAIRED RT COWL FIRE SEAL IAW EO 54090.SDR REXA2014062800659Heat Shield · bentTASK CARD 900-54-430-301 LT ENG LOWER COWL HEAT SHIELD AFT OF BLOW OUT DOOR HAS A TAB THAT IS BENT UP. REPAIRED HEAT SHIELD ON AFT SECTION OF LOWER CORE COWL IAW EA CRJ954-02711.SDR REXA2014062700657Structure · wornTASK CARD 900-26-430-100 NR 1 ENG AFT CORE COWL HAS WEAR MARKS AT PYLON INTERFACE AREA. REPAIRED NR 1 ENG AFT CORE COWL PYLON INTERFACE AREA IAW SRMM 54-13-00-101-001-A01 & 54-13-00-201-006-A01.SDR REXA2014062700658Cowling · wornTASK CARD 900-26-440-100 NR 2 ENG AFT CORE COWL HAS WEAR MARKS AT PYLON INTERFACE AREA. REPAIRED NR 2 ENG AFT CORE COWL PYLON INTERFACE AREA IAW SRM 54-13-00-101-001-A01 & 54-13-00-201-006-A01.SDR REXA2014062600651Plate · damagedTASK CARD 900-71-430-100 LT ENG LOWER BLOW OFF DOOR LATCH DIGGING INTO METAL. REPAIRED LT ENG LOWER BLOW OFF DOOR STRIKE PLATE IAW EA CRJ954-02716.
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