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 REXA2014062600652Rub Strip · wornTASK CARD 900-54-430-301 NR 1 ENG FWD UPPER CORE COWL AFT RUB STRIP HAS WEAR DAMAGE. REPAIRED NR 1 ENG FWD UPPER COWL AFT RUB STRIP IAW SRM 54-23-00-201-007-A01.SDR REXA2014062600654Rub Strip · damagedTASK CARD 900-54-430-301 NR 2 ENG FWD UPPER CORE COWL AFT RUB STRIP HAS DAMAGE. REPAIRED FWD UPPER CORE COWL AFT RUB STRIP IAW SRM 54-23-00-201-007-A01.SDR REXA2014062600655Rub Strip · wornTASK CARD 900-54-430-301 NR 2 ENG FWD LWR CORE COWL AFT RUB STRIP HAS WEAR DAMAGE. REPAIRED NR 2 ENG FWD LWR CORE COWL AFT RUB STRIP IAW SRM 54-23-00-201-007-A01.SDR MASA2014062202184Engine · vibrationNR 1 FAN VIBRATION AT 4.8 ENGINE SHUTDOWN, DIVERSION, EMERGENCY DECLARED. MX PERFORMED FAN BLADE VISUAL INSPECTION, CHECKED BLADES FOR STICKING & PERFORMED POWER RUNS AT MULTIPLE POWER SETTINGS, NO DEFECTS WERE FOUND.SDR CA140612001Detector · failed(CAN) UPON LOWERING FLAPS, FLIGHT CREW RECEIVED A "FLAPS FAIL" CAUTION MESSAGE. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE AND MAINTENANCE FOUND THE LT WING OTBD SKEW DETECTOR GIVING 0.25 VOLT AT 0 ORSDR REXA2014060300565Cowling · chafedTASK CARD 900-26-430-100 LT ENG AFT CORE EXHAUST COWL HAS CHAFE SPOTS AT PYLON TO COWL. REPAIRED CHAFED AREAS ON LT CORE COWL IAW SRM 54-13-00-201-006-A01.SDR REXA2014060300566Cowling · chafedTASK CARD 900-26-440-100 RT ENG AFT CORE EXHAUST COWL HAS CHAFE MARKS AT THE PYLON TO COWL INTERFACE. REPAIRED CHAFED AREAS ON RT CORE COWL IAW SRM 54-13-00-201-006-A01.SDR REXA2014060200564Fireshield · chafedTASK CARD 900-71-430-100 LT ENG LOWER CORE COWLING HAS CHAFE DAMAGE TO FIRE SEALS. REPAIRED AREA IAW EO R54090.SDR SWIA201437942Oil Filter · failedDURING CLIMB OUT, AMBER VIBRATION IN N2. FOLLOWED QRH, PULLED BACK ON POWER VIBRATION MESSAGE DISAPPEARED. RETURNED TO DEPARTURE, REPLACED LT ENGINE OIL FILTER, AND RAN LT ENGINE IAW AMM. DID NOT RECEIVE N-2 VIBRATION INDICATION COULD NOT DUPLICATE FAULT. SDR REXA2014053000561Fireshield · chafedTASK CARD 900-71-440-100 RT ENG LOWER CORE COWLING HAS CHAFE DAMAGE ON FIRE SEAL. REPAIRED FIRE SHIELD IAW EO R54090.SDR CA140528001Dowel Pin · damaged(CAN) AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AND THE CREW RECEIVED A GEAR DISAGREE MESSAGE AS WELL AS A PROXIMITY SYS 1 MESSAGE. THE FLIGHT RETURNED TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE INVESTIGATION FOUND THAT THE DOWELSDR REXA2014052300522Light · degradedFLOOR TRACK LIGHT DEGRADED ON LT SIDE OF ROWS 3 - 4. REPLACED EMERGENCY FLOOR TRACK LIGHT PN PL-88-900LH00 IAW AMM 33-51-01.SDR REXA2014052200520Rub Strip · damagedFORWARD LOWER CORE COWL, INNER BAND, OTBD SIDE IS RUBBING ON AFT CORE COWL. METAL MISSING IN PLACES. JOB CARD 900-54-430-300 IS FVI OF LT ENG NACELLE SMS 701035 5-22-14. REPAIRED FWD CORE COWL AFT EDGE RUB STRIP IAW SRM 54-23-00-201-007-A01.SDR REXA2014052200521Rub Strip · damagedTASK CARD 900-54-430-300 FWD UPPER CORE COWL, INNER BAND, OTBD SIDE IS RUBBING ON AFT CORE COWL. METAL MISSING IN PLACES. JOB CARD 900-54-430-300 IS GVI FOR LT ENG NACELLE SMS 701035 5-22-14. REPAIRED FWD UPPER CORE COWL AFT RUB STRIP IAW SRM 54-23-00-201-SDR REXA2014052000517Cowling · chafedLEFT ENG CORE COWL HAS CHAFE DAMAGE TO THE PYLON INTERFACE. MECH REPAIRED CHAFE DAMAGE ON LT ENG CORE COWL IAW SRM 54-13-00-201-006-A01.SDR REXA2014052000518Liner · gougedLEFT ENG LOWER COWL INNER LINER GOUGED. REPAIRED LT ENG LOWER COWL INNER LINER IAW EA CRJ954-02572. NO FURTHER DAMAGE FOUND.SDR REXA2014052000528Panel · gougedTASK CARD 900-54-430-301 LT ENG LOWER COWL PANEL WITH 4 HOLES IN IT GOUGED. R & R INLET ASSEMBLY VENT IAW AMM 71-12-08-001-801-A01 & 71-12-08-400-801-A01.SDR REXA2014051900516Cowling · chafedRIGHT ENG CORE EXH COWL HAS CHAFE DAMAGE TO THE PYLON INTERFACE. REPAIRED CHAFE DAMAGE ON RT CORE COWL IAW SRM 54-13-00-201-000-A01.SDR CA140522001Skin · damaged(CAN) THE ACFT SUFFERED A LIGHTNING STRIKE AFTER DEPARTURE. SINCE THERE WAS NO LOSS OF SYSTEMS OR OTHER ABNORMAL INDICATIONS THE FLIGHT CONTINUED. AFTER ARRIVAL, MAINTENANCE INSPECTION OF THE ACFT FOUND EXTENSIVE DAMAGE. APPROXIMATELY 37 BURN MARKS OF VARYISDR CA140520005Elevator System · split(CAN) DURING CRUISE FLIGHT, THE CREW RECEIVED AN ELEVATOR SPLIT CAUTION MESSAGE. THE QRH ADVISES THEM TO LAND AT THE NEAREST SUITABLE AIRPORT, SO THE FLIGHT DIVERTED. MAINTENANCE TROUBLESHOOTING FOUND THE ELEVATOR PCU`S REQUIRED RIGGING. THERE IS NO RECENT HSDR REXA2014051600515Cowling · crackedPOSSIBLE CRACK ON NR 1 ENG INLET COWL FWD OF FADEC. THERE IS A ROUND PANEL WITH 4 BOLTS THE CRACK LOOKS LIKE IT STARTS HERE. REMOVED FADEC UNIT NR 1 ENG TO FOM IAW AMM 73-21-01-000-801-A01. REPAIRED CRACK ON #1 ENGINE INLET COWL AS PER EA CRJ954-02561 REV SDR SWIA201437609Engine · failedLEFT ENGINE OVERTEMP, CREW PULLED POWER BACK, THEN PUSHED UP. ENGINE OVERTEMPED AGAIN THEN FLAMED OUT. FOUND LT ENGINE COMPRESSOR DAMAGE, STAGE 4 AFT. REPLACED LEFT ENGINE OIL PRESSURE TRANSMITTER AND LT ENGINE.SDR SWIA201437564Clevis · galledLT ENGINE UPPER FORWARD MOUNT CLEVIS IS GALLED. REPLACED FWD MOUNT CLEVIS IAW MM.SDR CA140409007Hose · failed(CAN) AFTER LANDING AND DURING A 180 DEGREE TURN AT RUNWAY END FOR BACK TRACK TO EXITING TAXIWAY, FLIGHT CREW RECEIVED A NR 3 HYDRALIC SYS LOW PRESSURE CAUTION MESSAGE, NR 3 HYDRALIC FLUID QTY WAS OBSERVED AT 0 PERCENT. FLIGHT CREW SHUTDOWN NR 3 HYD SYS AND TSDR CA140407008Sensor · shorted(CAN) ON DEPARTURE, CREW RECEIVED A WING ANTI-ICE CAUTION INDICATION. FLIGHT RETURNED TO DEPARTURE POINT AND LANDED WITHOUT FURTHER INCIDENT. THIS CAUTION LIGHT HAD A REPEAT ILLUMINATION OVER THE LAST FEW DAYS. MAINTENANCE ACTION COMPLETED. A DEFINITIVE PRSDR CA140314014Flap System · failed(CAN) ON APPROACH, "FLAPS FAIL" C UPON SELECTION TO 8 DEGREES. ABORTED APPROACH. AFTER SELECTION BACK TO 0 DEGREES, "FLAPS FAIL", C, DISAPPEARED. SECOND APPROACH PERFORMED AND ACFT LANDED. NO MDC MESSAGES COULD BE RETRIEVED. FLAPS/SLATS SYSTEM OPS TEST PERSDR REXA2014030400270Fireshield · damagedTASK CARD 900-73-430-902, LT ENG LOWER CORE COWL HAS DAMAGE TO FIRE SHIELD. REPAIR ACCOMPLISHED ON EA CRJ954-02330, PN OFF & ON CN624-3172-203.SDR SWIA201436677Engine · vibrationAT FL 380, ROUGHLY 30 SECONDS AFTER REDUCING TL TO CRUISE SETTING A SIGNIFICANT VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. REPLACED LT ENGINE ASSY IAW AMM.SDR REXA2014021900222Track · damagedTASK CARD 900-54-440-500 FT ENG UPPER TRANSLATING COWL UPPER TRACK SLIDER MOUNT POINT DAMAGED. REPAIRED UPPER TRANS COWL TRACK & INSTALLED NEW SLIDER INSERT IAW REO 690-78-30-163 & EO R78027.SDR CA140218003Windshield · cracked(CAN) DURING THE CLIMB THROUGH FL350, THE LT WINDSHIELD STARTED ARCING INTERNALLY IN THE HEAT ELEMENT NEAR THE UPPER RT CORNER OF THE WINDOW. SHORTLY AFTER THIS THE OUTER WINDOW PANE SHATTERED. THE QRH WAS FOLLOWED AND THE ACFT LANDED UNEVENTFULLY AT DESTINATSDR CA140212001Bushing · cracked(CAN) DURING REPLACEMENT OF THE LT AFT SPAR LINK, SB670BA-57-016, THE LOWER FITTING FORWARD BUSHING WAS FOUND TO BE CRACKED. BUSHING REPLACED IAW THE APPLICABLE AMM REFERENCE. ACFT HOURS: 26230, ACFT CYCLES: 13363.SDR CA140204004Light · overheated(CAN) MAINTENANCE DISCOVERED THE PILOTS FORWARD SIDE CONSOLE FLOOD LIGHT ASSY INOPERATIVE, BURNED AND MELTED CONDITION. REPLACED WITH NEW LAMP ASSY AND TESTED SERVICEABLE. AFH 27014.12, AFC 13726.SDR REXA2014012900172Fireshield · chafedRIGHT LOWER COWL ENG DRAINS FIRE SHIELD IS CHAFED AT THE FWD OTBD CORNER. REPAIR IAW EO R540490 USING ONE CORNER FROM A NEW FIRE SHIELD PN CN624-3170-203. RT LOWER TR IS PN CN 624-0104-003 & SN SB087. REPAIRED CHAFE ON RT LOWER COWL ENG DRAIN FIR SHIELD IAWSDR CA140122006Duct · leaking(CAN) THE FLIGHT CREW REPORTED A RT WING ANTI-ICE CAUTION MESSAGE. EXTENSIVE TROUBLESHOOTING OF THE SENSORS AND INDICATION SYSTEM WAS CARRIED OUT, A TEST FLIGHT WAS ALSO CARRIED OUT WITH NO RESOLUTION. THE PICCOLO TUBES WERE REMOVED FOR INSPECTION AND DEBRISSDR SWIA201436003Engine · malfunctionedENG FAILURE DURING TAKEOFF. LOUD NOISE, HIGH VIBES & ITT EXCEEDANCE. FLT 4803 REPLACED ENGINE IAW AMM.SDR CA140124008Blade · corroded(CAN) ACFT WAS CLIMBING OUT WHEN THE CREW REQUESTED TO STOP THE CLIMB AT 12000 FT, DECLARED EMERGENCY REPORTING AN ENGINE PROBLEM AND STATING THEY WANTED TO ENTER A HOLD TO WORK THE APPROPRIATE CHECKLISTS, RETURNED TO DEPARTURE. IT WAS A STAGE 2 HPT BLADE UNSDR CA131219012Lock · cracked(CAN) DURING SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED THAT THE LOCKWIRE ATTACHMENT TABS ON BOTH RT WING GROUND SPOILER ACTUATORS WHICH SECURE THE LENGTH ADJUSTMENT JAM NUT WERE BROKEN OFF. THE LOCKING DEVICES WERE REPLACED WITH SERVICEABLE PARTS IAW SDR CA131219005Handle · sheared(CAN) WHILE OPENING MAIN PASSENGER DOOR IN HANGAR, WHEN THE OUTER DOOR HANDLE WAS PULLED, THE HANDLE SHEARED OFF AT THE TOP OF THE HANDLE ASSY. REPLACEMENT HANDLE ON ORDER. ACFT TT 8724, CYCLES 4308. SUSPECT HANDLE HAS SAME TIME.SDR CA131216019Computer · unserviceable(CAN) AFTER DEPARTURE FLIGHT CREW REPORTED THAT THE CROSS FLOW PUMP CAME ON AND THEY GOT A FUEL IMBALANCE OF 600-700 LBS. THEY WERE UNABLE TO RECTIFY THE PROBLEM WITH THE QRH AND ELECTED TO RETURN TO DEPARTURE. MAINTENANCE REPLACED THE FUEL QUANTITY COMPUTERSDR CA131216020Engine · vibration(CAN) THE OPERATOR REPORTED THAT DURING CLIMBOUT, THE CREW OBSERVED ENGINE VIBRATION INDICATIONS OF 1.7 MILS, PEAKING AT 2.0 MILS. THE VIBRATION WENT AWAY WHEN THE ACFT LEVELED OFF IN CRUISE. THE VIBRATION RETURNED WHEN THROTTLES WERE BROUGHT OUT OF IDLE. ISDR CA131216013Actuator · failed(CAN) ENGINE FLAMED OUT JUST AFTER LANDING. MX FOUND OTBD VG ACTUATOR SHEARED.SDR REXA2013120902224Shaft · shearedAFTER LANDING, RECEIVED A LT ENGINE BLEED CAUTION, THEN LT ENGINE DEGRADED. CAUTION FOLLOWED WITHIN 30 SECONDS BY LT ENGINE FLAMEOUT. DURING THIS WHOLE EVENT, ALL ENGINE GAUGES SHOWED NORMAL. INSPECTED LT ENGINE & FOUND OTBD VG SHAFT SHEARED. R & R VGV SSDR CA131216021Bleed Valve · failed(CAN) FUEL ODOR IN COCKPIT DURING ENGINE POWER UP. REPLACED BLEED VALVE AND PRESSURE SEAL REGULATOR. PERFORMED 2 LEGS AND PROBLEM WENT AWAY.SDR CA140204006Shaft · sheared(CAN) AFTER LANDING AND AS WE EXITED THE RUNWAY WE RECEIVED "LT ENG BLEED" CAUTION THEN "LT ENG DEGADED" CAUTION FOLLOWED WITHIN 30 SEC BY "LT ENG FLAMEOUT". DURING THIS WHOLE EVENT ALL ENGINE GAUGES SHOWED NORMAL. INSPECTED LT ENGINE AND FOUND OTBD VG SHAFTSDR CA131128010Resolver · failed(CAN) BASED ON THE MAINTENANCE DIAGNOSTIC COMPUTER, THE HORIZONTAL STABILIZER POSITION RESOLVER AND/OR ITS CONNECTOR IS AT FAULT. THE RESOLVER WAS REPLACED ON NOVEMBER 18TH AS PART OF AN ACTION PLAN. THE DISCREPANCY CHANGED TO PITCH FEEL FAULT AND STAB FAULTSDR CA131115003Starter · failed(CAN) ACFT AOG DUE TO A LT ENGINE START PROBLEM. MECHANICS WERE SENT THERE AND FOUND SUBSTANTIAL DAMAGE TO THE LT ENGINE ATS. THE ATS IS SEPARATED AT THE STATOR TURBINE LEVEL. LT ENGINE ATS WAS REPLACED AND LT ENGINE INSPECTED WITHOUT OTHER FINDINGS.SDR CA131112010Pulley · seized(CAN) THE FLIGHT CREW REPORTED THAT THE AILERON CONTROL FELT STIFF IN BOTH DIRECTIONS. MAINTENANCE INVESTIGATION FOUND THE AILERON PULLEY AT THE LH WING ROOT SEIZED. THE PULLEY WAS REPLACED AND THE ACFT RETURNED TO SERVICE. PULLEY, PN 600-90800-4, AIPC 27-11SDR CA131101008Duct · failed(CAN) DURING ROUTINE INSPECTION OF SLATS, ACUATORS AND ANTI-ICE DUCTS THE LT TELESCOPING DUCT WAS FOUND BENT, FURTHER INVESTIGATION SHOWED THAT THE MIDDLE TUBE WAS EXTENDED APPROX 8" MORE THAN THE RT. A NEW TELESCOPING DUCT WAS INSTALLED IAW AMM AND ACFT RELESDR CA131101002Drain Line · chafed(CAN) DURING REPLACEMENT OF THE NR 1 HYDRAULIC EDP, IT WAS NOTICED THAT THE ECS FUEL DRAIN LINE WAS CHAFED. LT ENGINE ECS FUEL DRAIN LINE, PN CN627-8035-001, AIPC 71-71-03, FIG 5-35, REPLACED. ENGINE, PN CF34-8C5, SN 194345, TSN 15594, CSN 8288, TSR 2303, CSSDR CA131031004Line · leaking(CAN) THE NR 2 HYDRAULIC SYS FLUID LEVEL WAS REPORTED AS LOW. MAINTENANCE FOUND THE FLEX LINES TO THE NR 2 EDP LEAKING. THE NR 2 EDP WAS REMOVED AND DEFERRED IAW THE MEL THE MEL PROCEDURE INCLUDES THE REMOVAL OF THE FLEX LINES. UPON REINSTALLATION OF THE ED
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