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 ASOA201701161065Engine · vibrationON T/O LEFT ENGINE VIBE AT 2.1 - RETURN TO ATL. REMOVED BLADES, PINS AND BUMPERS. PERFORMED GENERAL VISUAL INSPECTION OF FAN BLADES. RE-MAPPED FAN BLADES, LUBRICATED RETAINING PINS, INSTALLED FAN BLADES, PERFORMED CHECK OF THE ENGINE N1 VIBRATION LEVEL IAW TASSDR MASA2017011412809Engine · unknownNR 1 ENGINE VIBRATION AT 2.5, RETARDED THROTTLE TO IDLE, DECLARED AN EMERGENCY & LANDED WITH THE NR 1 ENGINE AT IDLE. PERFORMED BLADE SHAKE & APPLIED R.O., PERFORMED ENGINE RUNS WITH CREW, VIBRATION NEVER WENT ABOVE .8, WITHIN LIMITS.SDR VNAA2016121500030Warning Message · illuminatedRIGHT FADEC CAUTION MESSAGE. CYCLED SYSTEM CIRCUIT BREAKERS.SDR REXA2016121002471Engine · failedLEFT ENGINE FAILED IN FLIGHT, N1 DROPPED, ITT RED LINE, N2 DROPPED, VIBRATION REDLINE, PHYSICAL VIBRATION OF AIRFRAME PRECEDED BY A BANG. R & R THE LEFT ENGINE IAW JC 900-72-430-902. OPS CHECKED GOOD IAW JC 900-72-430-906
"SDR VNAA20162400029Engine · bird ingestionBIRD STRIKE DAMAGE TO LEFT ENGINE.SDR VNAA2016102400029Blade · damagedBIRD STRIKE DAMAGE TO LEFT ENGINE. REMOVED AND REPLACED FAN BLADES NUMBERS 6 AND 20. OPS CHECK GOOD IAW AMM. RELEASED FOR SERVICE.SDR VNAA2016060400003Sensor · inoperativeRIGHT ENGINE OIL PRESSURE INTERMITTENT IN FLIGHT. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RT OIL LEVEL, OIL TEMP SENSOR, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOSDR MASA2016052612710Engine · flamed outLEFT ENGINE FLAMEOUT CAUTION. MAINTENANCE TROUBLESHOOTING.SDR REXA2016031600412Carbon Seal · damagedEN-ROUTE, LT OIL PRESS WENT FROM GREEN TO AMBER TO RED. LT ENG OIL PRESS EICAS WARNING MSG CAME ON. FOLLOWED NON-NORMAL PROCEDURES, SHUTDOWN ENG & LANDED.
REMOVED STARTER FOUND AXIS D CARBON SEAL TO BE BAD. R & R AXIS D CARBON SEAL IAW AMM 72-64-01. LEASDR VNAA2016030800013Pressure Sensor · dirtyCREW REPORTED RECEIVING A LT MAIN EJECTOR CAUTION MESSAGE, ALONG WITH THE FUEL BOOST PUMPS CYCLING DURING CRUISE AT FL220. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, CLEANED THE LT PRIMARY EJECTOR’S PRESSURE SENSOR CONNESDR ASOA2016030314549Engine · shutdownRIGHT ENGINE AUTO SHUTDOWN DUE TO LIGHTNING STRIKE. R & R RT ENGINE ACFT RETURN TO SERVICE.SDR CA160224005Duct · ruptured(CAN) FLIGHT CREW REPORTED, LEFT HAND BLEED DUCT WARNING, THEN CHANGED TO LT BLEED DUCT CAUTION MESSAGE, LEFT PACK OFF. QRH ACTIONED. LT BLEED SELECTED OFF, LT BLEED DUCT WARNING RETURNED AGAIN WHEN POWER APPLIED TO CLIMB, RT BLEED SHUTDOWN & STARTED LOSING PRSDR MASA2016021612772Fadec · warning lightRT FADEC CAUTION, RETURNED TO FIELD, EMERGENCY DECLARED. OPENSDR VNAA2016010400006Idg · failedCREW REPORTED GENERATOR 2 FAIL. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R NR 2 INTEGRATED DRIVE GENERATOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR CA151231004Skin · corroded(CAN) FOUND 2 CORROSION AREAS AT LT WING T/E BETWEEN WS370.25-398.93. DUE TO EXTENSIVE CORROSION DAMAGE, THE PART, PN:CC690-15116-3 NEEDS TO BE REPLACED.SDR CA151223009Bleed Valve · failed(CAN) CREW REPORTED A RIGHT HAND BLEED CAUTION MESSAGE AFTER TAKE OFF. QRH FOLLOWED AIRCRAFT RETURNED TO DEPARTURE AIRPORT . MAINTENANCE TROUBLESHOOTING CARRIED OUT AND 10TH STAGE BLEED VALVE REPLACED. FUNCTION CHECKS CARRIED OUT WITH NO FURTHER FAULTS TO REPOSDR CA151119010Acm · failed(CAN) AFTER PUSHBACK THE COCKPIT FILLED WITH SMOKE AND ASH, LEFT PACK AUTO FAIL MSG CAME ON. THE PACK WAS SHUT OFF AND THE SMOKE CLEARED. THE A/C RETURNED TO GATE.SDR CA151111006Fitting · cracked(CAN) NLG ALTERNATE-RELEASE ACTUATOR FWD FITTING CRACKED.SDR CA151104003Frame · cracked(CAN) CRACK FOUND ON RT SIDE OF UPPER FRAME FS235, WL 110.SDR CA151028003Fadec · malfunctioned(CAN) LEFT ENGINE DEGRADED, MESSAGE FOLLOWED BY A FLAMEOUT. THEY WERE ON CONTINUOUS IGNITION DUE TO LIGHT TURBULENCE. AFTER FLAMEOUT THEY HAD LT ENGINE HIGH ITT MESSAGE AND THE MDC SHOWS A PEAK OF 968 DEGREES AND A DURATION OF 9.1 SECS. AFTER RECEIVING LT ESDR N6WA2015100101Fmu · malfunctionedRIGHT FADEC CAUTION ILLUMINATED INFLIGHT. B1 CODE 006794 FIM TASK 73-21-03-810-826, R & R NR 2 ENG FMU IAW AMM 73-21-03. OPERATIONS & LEAK CHECKED GOOD IAW 71-00-00.SDR CA151001008Ahrs · failed(CAN) AIRCRAFT TURNED BACK DUE TO FAILED NR 1 AHRS FAILED, RED MAG FLAG, ATC REPORTED NAVIGATION WAS INNACURATE, HEADING OFF.SDR CA150928004Link · broken(CAN) DURING REPLACEMENT OF RT INBD GROUND SPOILER ACTUATOR OUTPUT LINK (SCHED MAINTENANCE), FOUND THE CENTRAL FITTING WITH ONE BORE BROKEN.SDR N6WA2015092201Warning System · false activationRIGHT FADEC CAUTION MSG IN FLIGHT. RAN NR 2 ENG MULTIPLE TIMES IAW AMM 71-00-00, COULD NOT DUPLICATE FAULT AT THIS TIME.SDR CA150916013Skin Panel · corroded(CAN) CORROSION FOUND ON RT WINGLET LOWER SKIN PANEL.SDR CA150916010Skin · corroded(CAN) CORROSION ON BOTH LT AND RT LOWER WING SKIN PANELS CC690-15116-3/4.SDR CA150916011Drag Angle · cracked(CAN) WE HAVE CRACK ON OUR VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLE ON AFT LHS . THE CRACK IS .750 INCH LONG.SDR CA150909005Sensor · malfunctioned(CAN) LEFT HAND BRAKE OVERHEAD WARNING MESSAGE DURING CLIMB OUT FROM DEPARTURE POINT. BTMS TEMP INDICATORS INITIALLY INDICATED MAX TEMP BUT THEN DISPLAY WENT BLANK. AN EMERGENCY WAS DECLARED AND CREW ELECTED RETURNED TO DEPARTURE POINT. ON LANDING AND BRAKE TESDR CA150901011Ecu · burned(CAN) DURING REGULAR MAINTENANCE, SMELL OF SMOKE WAS NOTICED IN THE AVIONICS BAY AND SLAT CB ON ACPC FOUND TRIPPED. SFECU NR 1 FOUND TO BE BURNT.SDR CA150817017Probe · malfunctioned(CAN) REJECTED TAKEOFF DUE TO NR 3 BRAKE OVERHEAT INDICATION. MAINTENANCE DOCUMENTED THAT THE MDC CODE SHOWED B1-006938. THE FIM PROCEDURE WAS CARRIED OUT NO FAULT FOUND. NR 3 BRAKE TEMPERATURE PROBE WAS REPLACED IAW AMM. ALL FAULTS CLEARED FROM MDC AND AIRSDR REXA2015081200783Plate · chafedTASK CARD 900-71-430-100, LEFT ENG LOWER CORE COWL BLOW OUT DOOR HINGE & LATCH PLATE CHAFED. R & R LATCH PLATE IAW SRM 51-42-06 & SRM 51-42-13. BLENDED HINGE BODY IAW EA 954-03625. R & R HINGE LEVER IAW SRM 51-42-02 0.003 MATERIAL REMOVED.SDR REXA2015081200790Plate · chafedTASK CARD 900-71-430-100, LEFT ENG LOWER CORE COWL BLOW OUT DOOR HINGE & LATCH PLATE CHAFED. R & R LATCH PLATE IAW SRM 51-42-06 & SRM 51-42-13. BLENDED HINGE BODY IAW EA 954-03625. R & R HINGE LEVER IAW SRM 51-42-02 0.003 MATERIAL REMOVED.SDR REXA2015080800778Engine · malfunctionedAFTER TAKEOFF IN CLIMB, THRUST ACCELERATING FROM 200KTS - 250KTS 6000 FT, RT ENG LOUD NOISE, YAW RT, LOSS OF OIL PRESS, ITT SPIKED, ENG FLAMED OUT N1 & N2 DECELERATION. PERFORMED EAC ENG FIRE OR SEVERE ENG DAMAGE & ALL QRH PROCEDURES. REPLACED RT ENG PN ON &SDR CA150814002Engine · malfunctioned(CAN) NORMAL TAKE OFF, HDG 100, CLIMBING TO 7000 FT. DURING SECOND STAGE CLIMB, WITH CLIMB THRUST SET, PASSING 6000 FT, THE CAPTAIN REPORTED A LOUD BANG ACCOMPANIED BY A YAW TO THE RIGHT. THIS WAS FOLLOWED BY A TRIPLE CHIME, ENG OIL PRESSURE WARNING, AND ITT SSDR ASOA2015080713457Light · missingEMERGENCY LIGHTN MISSING IN FRONT OF FORWARD LAVATORY. REPLACED EMERGENCY LIGHT IAW AMM 33=51=01. ACFT OK FOR SERVICE.SDR CA150804002Brake Assy · seized(CAN) NR 2 BRAKE ASSY REPLACED DUE TO NORMAL WEAR. PERFORMED NORMAL SCHEDULED FLIGHTS, ON THE 4TH LANDING THE NR 2 BRAKE ASSY FAILED IN THE LOCKED POSITION CAUSING NR 2 TIRE TO NOT ROTATE. THE AIRCRAFT ROLLED OUT ONTO THE TAXIWAY AND THE TIRE DEFLATED. MAISDR CA150801001Motor · failed(CAN) DURING APU START SEQUENCE ON RAMP IN PREPARATION FOR SCHEDULED FLIGHT, THE APU ACCELERATED TO 9% AND HUNG WITH RAPIDLY INCREASING ITT. THE START ATTEMPT WAS INTERRUPTED PRIOR TO ITT EXCEEDANCE BY THE PILOT STARTING THE APU. TROUBLESHOOTING BY MAINTENANCESDR CA150727028Window · cracked(CAN) ON CLIMB AT FL 150, RT SIDE WINDOW CRACKED. ATB.SDR CA150721006Anti-Ice Valve · failed(CAN) FLIGHT CREW ADVISED ON CLIMBOUT OF DEPARTURE POINT, THE LT COWL ANTI-ICE VALVE FAILED TO OPEN. AFTER SEVERAL ATTEMPTS TO GET VALVE TO OPEN, FLIGHT RETURNED TO THE DEPARTURE POINT. MAINTENANCE ACTION HAD THE ANTI-ICE VALVE REPLACED AND THE ACFT RETURNEDSDR REXA2015071700725Engine · failedCLIMBING TO FL 220, RT ENGINE VIBRATION BEGAN TO CLIMB, SHORTLY AFTER THE RT ENGINE ITT ALSO BEGAN TO RISE. THE VIBRATION WAS PEAKING, REDUCED THE THRUST LEVER. AT THE SAME TIME RECEIVED A FWD LAV SMOKE WARNING, SHORTLY AFTER RECEIVED A AFT LAV SMOKE WARNINGSDR CA150720012Actuator · damaged(CAN) AS PER FLIGHT CREW, THE LHS ENGINE WAS STARTING HOT WITH ALL OTHER ENGINE INDICATIONS NORMAL. A RAPID INCREASE IN ITT WAS OBSERVED WITH ITT REACHING AS HIGH AS 940 DEGREES AT WHICH TIME THE FADEC WOULD ABORT THE START. HOT ICON WAS ON ON THE ASSOCIATED ISDR REXA2015071400685Cowling · chafedTASK CARD 900-54-440-301 RT ENG LOWER CORE COWL CHAFED NEAR DRAIN. REPAIRED DAMAGE TO RT ENG LOWER CORE COWL FIRE SHIELD IAW EO R54090 SEE RC 60012 FOR EO.SDR REXA2015071400689Guide · wornTASK CARD 900-54-430-300 LT CORE COWL ALIGNMENT GUIDE WORN. R & R LT AFT CORE COWL ALIGNMENT GUIDE IAW REO 690-54-13-097.SDR CA150707007Acm · failed(CAN) R PACK AUTOFAIL CAUTION MESSAGE POSTED ON THE EICAS AND CABIN CREW REPORTED SMOKE IN THE CABIN. FLIGHT CREW DECIDED TO RETURN TO GATE. T/S REVEALED RT ACM SEIZED (NOT ROTATING).SDR REXA2015062900645Rub Strip · chafedTASK CARD 900-54-430-301 LEFT ENG AFT CORE COWL RUB STRIP CHAFED. REMOVED DAMAGE ON LT ENG AFT CORE COWL RUB STRIP TO A REMAINING THICKNESS OF .083, MINIMUM ALLOWABLE THICKNESS. .100 OUT OF LIMITS IAW SRM 54-13-00-201-005-A01. RECEIVED NEW LT ENG AFT CORE CSDR REXA2015062900648Rub Strip · chafedTASK CARD 900-54-430-301 LT ENG UPPER & LOWER CORE COWLS RUB STRIP CHAFED. REPAIR DAMAGED SEGMENTS IAW SRM 54-23-00.SDR CA150626004Pump · leaking(CAN) DURING APPROACH A TOTAL LOSS OF FLUID FROM NR 3 HYD SYS WAS OBSERVED. AN EMER DECLARED. MX FOUND 3A HYD PUMP LEAKING FROM CASE DRAIN DURING PUMP OPERATION. REPLACED 3A PUMP IAW AMM 29-12-03. HYD SYS 3 BLED IAW AMM 29-10-00, GEAR SWINGS CARRIED OUT WISDR CA150622006Ballast · burned(CAN) ON GND, PRIOR TO FIRST FLIGHT OF THE DAY, STRONG ELEC SMELL IN THE FWD AREA OF CABIN WHEN ELEC POWER WAS APPLIED TO THE ACFT. REMOVED THE CEILING PANELS & SIDE WALL PANELS TO ACCESS OVERHEAD & SIDEWALL LIGHTING IN THE FWD AREA OF THE CABIN. SMELL FOUNDSDR CA150615004Regulator · failed(CAN) DURING TAKEOFF ROLL, FLIGHT ATTENDANT WITNESSED A LOUD SCREECHING & POPPING SOUND FROM THE GALLEY COFFEE MAKER & WATER SPILLING ONTO THE FLOOR. THE FLIGHT ATTENDANT PUSHED EMER CALL BUTTON & CREW REJECTED TAKEOFF. MX TROUBLESHOOTING DETERMINED THAT THESDR REXA2015061200580Plate · gougedTASK CARD 900-71-440-901 RT ENG LOWER THRUST REVERSER COWL OUTER LATCH COVER STRICKER PLATES GOUGED. R & R STRIKER PLATES ON RT LOWER TRANSCOWL IAW SRM 51-42-06.
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