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 MALA100060Proximity Sensor · faultedAFTER THE GEAR WAS SELECTED UP, RECEIVED A GEAR DISAGREE - WARNING AND WOW INPUT - CAUTION. WHEN SELECTED DOWN RECEIVED NOSE STEERING INOP - CAUTION. COMPLETED NOSE STEERING FAULT AND NOSE STEERING CAUTION CLEARED. FOUND PROXIMITY SENSOR PX11 (RT NLG WOFFW)SDR ASOA201000533Glowstrip · brokenPHOTOLUMINESCENT STRIP IN FRONT OF SIDE GALLEY CARTS IS BROKEN IN 2 PLACES. REPLACED BROKEN PHOTO LUMINESCENTS STRIP IN FRONT OF GALLEY CARTS IAW AMM 33-51-01. (CLOSED)SDR MASA2010040500307Engine · noisyDIVERT TO SAV - DECLARED EMERGENCY. LT ENG LOUD NOISE AND INDICATION FLUX. R2 NR 1 ENG.SDR MALA100055Sensor · out of rigON TAKEOFF DURING GEAR RETRACTION, WE GOT A GEAR DISAGREE WARNING. LT AND RT MAIN GEAR INDICATIONS WERE CYCLING FROM DISAGREE TO DOWN AND NOSE GEAR WAS RED DURING THIS TIME. PERFORMED GEAR DISAGREE CHECKLIST FROM POM. PERFORMED ACTION PLAN NR1 ADR REFERENCESDR ASOA201000451Door · bindingFWD CARGO DOOR WILL NOT OPEN.SDR ASOA201000328Glowstrip · missingA PHOTOLUMINASCENT STRIP IS MISSING BY THE FWD LAV DOOR. REPLACED STRIP IAW AMM 33-51-01.SDR MALA100034Light · damagedDURING INSPECTION, NOTED LT SIDE GALLEY FLOOR TRACK LIGHT STRIP BROKEN/MISSING. INSTALLED NEW FLOOR TRACK LIGHT STRIP ON LT SIDE OF GALLEY.SDR MALA100026Light · inoperativeEMERGENCY FLOOR PATH LIGHTING DAMAGED ON RT SIDE OF GALLEY. R & R EMERGENCY FLOOR PATH LIGHTING ON RT SIDE OF GALLEY, PN ON/OFF PL88-900LH00, PL88-930LH05 IAW AMM CH 33-51-00 (CONFIG A210 LIGHTING CHECKS GOOD).SDR ASOA201000296Megaphone · inoperativeF/A REPORTED MEGAPHONE INOP.SDR MASA2010020700116Fan Blade · lack of lubeON CLIMBOUT IN MEMPHIS LEFT ENGINE VIBRATION WAS HIGH 1.6MILS BUT IN THE GREEN BAND AT CRUISE WHEN POWER REDUCED VIB WENT TO 1.8. CREW WAS ABLE TO KEEP THE VIB IN THE GREEN DURING THE FLIGHT. THE FLIGHT ATTENDANTS CALLED TO ASK ABOUT THE VIBRATION AND THE LOSDR CA100122002Hinge · worn(CAN) ON JANUARY 4TH/2010, A FLOATATION VALVE HINGE WAS FOUND LOOSE, FURTHER INSP REVEALED THAT 4 OF THE 6 PIANO HINGE TYPE LUGS WERE WORN OUT. THE DAMAGE WAS OBSERVED BY COINCIDENCE DURING A TRANSIT CHECK INSP. THE FLOATATION VALVE WAS REPLACED AND THE ACFT RSDR MASA2009122000356Engine · malfunctionedASH FLT 2748 TUS-PHX. RETURNED TO FIELD DUE TO LT ENGINE HIGH OIL TEMP 260 DEGREES IN FLIGHT ENGINE SHUT DOWN. MX R2 NR 1 ENGINE.SDR CA091102012Filter · crushed(CAN) FOUND APU LUBE OIL FILTER CRUSHED WHILE CARRING OUT TASK RJ9-49-360-706 (REPLACMENT OF OIL FILTER). FILTER REPLACED.SDR CA091013006Radome · delaminated(CAN) ON APPROACH, THE ACFT HAD A BIRD STRIKE TO THE RADOME WHICH CAUSED DELAMINATION DAMAGE TO THE LWR RADOME STRUCTURE. THE RADOME WAS REPLACED AND THE ACFT RELEASED TO SERVICE.SDR MASA2009100100304Fadec · malfunctionedASH FLT 2643 CLT - SDF, ACFT RETURNED TO FIELD & DECLARED AN EMERGENCY DUE TO LEFT FADEC CAUTION. MX REMOVED AND REPLACED LT FADEC.SDR CA091002007Pcu · malfunctioned(CAN) FL390, EICAS IB SPOILERON, IB FLT SPLRS, AP TRIM IS LWD CAUTION MSGS. FLIGHT SYNOPTIC PAGE SHOWS RT WING INBD MFS FULLY DEPLOYED, AIRPLANE TURNED VIOLENTLY ROLL LT, IAS REDUCED BY DRAG, AP DISC, THRUST INCREASED TO CLIMB TO MAINTAIN SPEED, ALL QRH CHECKLSDR CA090930003Tube · cracked(CAN) RT WING FLUX VALVE DRAIN TUBE FOUND CRACKED FROM POSSIBLE WATER FREEZING AND ALLOWED FUEL TO ESCAPE THE RT WING. LINE REPLACED.SDR MALA090115Proximity Sensor · out of adjustUPON RETRACTING THE LANDING GEAR ON DEPARTURE, A GEAR DISAGREE MESSAGE ON EICAS WARNING CYCLING ON/OFF 3 TIMES AND REMAINED ON UNTIL LANDING GEAR WAS SHOWING ALL 3 GEAR DOWN AND LOCKED, RETURNED TO DEPARTURE. NOSE GEAR WAS NOT SHOWING FULLY RETRACTED. ENTERESDR MASA2009080700252Engine · flamed outASH FLT 2743 ELP-PHX. RTF DECLARED EMERGENCY FOR LT ENGINE FLAME OUT. LANDED SAFE WITH NO ISSUE, ITT WENT TO 1094 DEG C FOR 696 SECONDS. MX REMOVED AND REPLACED LT ENGINE.SDR CA090727006Line · broken(CAN) AFTER IN FLIGHT TEST OF ACFT ADG MX NOTICED AN AUDIBLE HISS COMING FROM THE CREW OXYGEN SERVICE POINT. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE CAPILARY LINE (P/N S7047-7) OFF THE BACK OF THE CREW OXYGEN SERVICE POINT GAUGE WAS FRACTURED ATSDR CA090723002Ahrs · unserviceable(CAN) FLIGHT ABORTED - LOSS OF AHRS NR 2 INFORMATION ON CLIMB. FLT IB 8712 MAD/LYS CLIMBING TO FL 350: FOLLOWING EICAS/PFD MESSAGES APPEARED: PITCH FEEL FAULT (STATUS) YD 2 INOP (STATUS) PFD: FD-ATT-MAG RED FLAG NR 2 MFD: MAG RED FLAG NR 2 A/P DISCONNECT ATTSDR CA090808001Window · crackedAT FLT LEVEL 250 PILOTS SIDE WINDOW CRACKED. CREW DESCENDED TO FLT LEVEL 100 AND LANDED. MX REPLACED WINDOW. ADR MHUT-09-20327514 RAISED. SIDE WINDOW LH PPG NP139322-11 08203H3860.SDR CA090720005Connector · burned(CAN) CONNECTOR PLUG J114, P114 BEHIND THE GALLEY HEATER PANEL ON THE G1 GALLEY WAS FOUND SMOKING AND BADLY BURNED. ALSO, WIRE BUNDLE WAS BADLY BURNED AS THE TERMINAL BLOCKS, ETC ALSO STARTED TO BURN THE INSULATION ON THE CEILING. AIRLINE IS IN THE PROCESS OSDR CA090808002Autopilot Sys · malfunctionedREPORTING TO FLIGHT OPERATIONS: AFTER ROTATION F/O CALLED FOR "GEAR UP, SPEED MODE". AFTER PRESSING SPEED MODE BUTTON THE FMA REFERENCE REPORTED CLB 40 AND THE FLIGHT DIRECTOR SLOWLY BEGAN COMMANDING A HIGHER PITCH ATTITUDE THAN NORMAL. ACFT WAS BEING HANDFLSDR CA090630001Hinge · cracked(CAN) DURING ROUTINE MX A SPECIAL INSP OF FLOTATION VALVE (PN BA690-95100-1, IPC 21-32-02, FIG 1-5) WAS CALLED UP IAW TASK RJ9-21-32-02-DVI-801-FCD. HINGE FOR FLOATATION VALVE WAS FOUND CRACKED DURING THIS INSP. HINGE WAS REPLACED IAW TASK RJ9-21-32-02-RP-80SDR CA090624003Quick Disconnect · loose(CAN) AFTER LANDING, FLIGHT CREW REPORTED THAT ACFT REQUIRED A LOT OF PWR TO TAXI AND THE LT SIDE BRAKES SEEMED TO BE DRAGGING. ONCE CLEAR OF RUNWAY THEY STOPPED ON TAXIWAY AND TWR CONFIRMED THAT THEIR NR 1 MAIN WHEEL WAS FLAT. MX WAS DISPATCHED TO ACFT ANDSDR CA090623001Hinge · worn(CAN) DURING TRANSIT CHECK IT WAS NOTED THAT THE FLOATATION VALVE WAS MISSING. INVESTIGATION FOUND THE VALVE RELOCATED AMONG THE ELEVATOR CABLES. IT WAS FOUND TO HAVE WORN THROUGH ITS PIANO HINGE. PIANO HINGE WAS STILL ATTACHED TO MOUNTING SIDE OF THE HINGESDR CA090624005Windshield · cracked(CAN) AT FL 170 - 250/290 KIAS, RT WINDSHIELD CRACKED. FLIGHT DIVERTED. MX REPLACED RT WINDSHIELD. WINDSHIELD (NP 139321-13 06201H6258) CRACKED, PART NOT SEEN.SDR CA090606003Compressor · fod(CAN) ON T/O ROLL, RT N1 DROPS FROM 86 PERCENT TO 50 PERCENT. TAKEOFF ABORTED. MX INSP REVEALED FOD DAMAGES ON FAN AND COMPRESSOR. A CIRCULAR CUT WAS FOUND ON NR 4 WHEEL TIRE. IT IS SUSPECTED THAT AN FOREIGN OBJECT EMBEDDED IN THE NR 4 WHEEL TIRE RELEASED FROMSDR REXA200900057Compressor · contaminatedDURING CLIMBOUT THE SMOKE AFT LAV ILLUMINATED. AFT CABIN ATTENDANT REPORTED AN ODOR BUT NO SMOKE ALTHOUGH THE SMOKE DETECTOR ACTIVATED. THE FLIGHT CREW DONNED OXYGEN MASKS, PERFORMED THE QRH AND REQUESTED A RETURN TO DEPARTURE. AN OTHERWISE NORMAL APPROACH ASDR CA090602002Transceiver · failed(CAN) PILOT REPORTED RECEIVE FAILURE IN FLIGHT ON MAY 26, 2009. MX FUNCTION CHECK WAS PERFORMED, UNABLE TO DUPLICATE PROBLEM. RECEIVE PROBLEM REPORTED AGAIN ON MAY 27, 2009 AND PROBLEM VERIFIED. REPLACEMENT VHF COMM REMOVED FROM C-GSUW AND INSTALLED INTO ACFT.SDR CA090507001Unknown · failed(CAN) UPON ENTERING ACFT FOR FIRST TIME, CREW NOTICED STRONG ODOR IN FRONT HALF AND FLIGHT DECK. MAIN BATTERY WAS ON WHEN CREW GOT TO THE ACFT, AC POWER WILL NOT ENGAGE, ALL GENERATOR COME ON LINE BUT WILL NOT POWER THE TRU’S. REPLACED BOTH DCPC’S WITH SERVICSDR CA090501003Radome · damaged(CAN) THE RADOME AND THE LT HORIZONTAL STABILIZER TIP FAIRING. SUFFERED LIGHTNING STRIKE DAMAGE ISSUED REO 690-51-00-036 (FERRY FLIGHT DISPOSITION FOR LIGHTNING STRIKE DAMAGE ON ACFT STRUCTURE).SDR CA090423001Window · cracked(CAN)"F/O SIDE WINDOW BROKE ON TAXI- IN" "REMOVED AND REPLACED THE F/OS SIDE WINDOW IAW AMM 56-12-01 AND RII 56-220-1000. PRESURIZED ACFT IAW AMM 56-11-01. NO LEAKS DETECTED. SIDE WINDOW- (RT).SDR CA090413004Windshield · cracked(CAN) THE FLIGHT CREW NOTICED AT THE GATE THE F/O WINDSHIELD HAS A SMALL CRACK IN THE UPPER LT CORNER. THE F/OS WINDSHIELD WAS REMOVED AND REPLACED IAW AMM 56-11-01. 601R33033-18 0434143807 TSO: 12007.5/CSO: 7645SDR CA090324002Engine · flamed out(CAN) METEOROLOGICAL CONDITION WAS: RAIN MODERATE, ICE MODERATE. DURING THE APPROACH PHASE AT 7000 FEET, SPEED 220 KNOTS, LIGHTNING STRIKE IMPACTED THE ACFT. FOR FEW SECONDS RT ENG FLAME OUT OCCURRED AND R FLAMEOUT CAUTION MESSAGE WAS DISPLAYED ON EICAS, AFTESDR CA090402004Duct · ruptured(CAN) CROSSOVER DUCT HAS RUPTURE AT EXPANSION BELLOWS ON OPPOSITE SIDE FROM FIRE WIRES. PART IS TRACKED AS EXPEDABLE.SDR CA090312011Control Rod · loose(CAN) ON CLIMBOUT, MOVED THE YOKEBACK AND FORTH FELT A BIND IN THE CONTROLS AND HAD LIMITED PITCH CONTROL OF THE ACFT. RETURNED TO RDU. RETORQUED PILOTS ELEVATOR CONTROL ROD LEVER P/N BA670-90454-3ASSY AND PERFORMED 2 FCFS, REFER TO IPC 27-31-12 FIGURE 1 ITESDR CA090312012Window · cracked(CAN) AT FL 370 HEARD POP NOISE AND THE LT SIDE WINDOW CRACKED. NO PRESSURIZATION PROBLEMS. WE DESCENDED TO LOWER ALTITUDE AND COMPLIED WITH QRH. THE LT SIDE WINDOW WAS REMOVED AND REPLACED.SDR CA090226001Warning Light · illuminated(CAN) ON FINAL APPROACH WHEN GEAR SELECTOR WAS SELECTED DOWN, GEAR DID NOT RESPOND. RECEIVED A "GEAR DISAGREE" AURAL MESSAGE AND WARNING. AFTER DISCUSSIONS WITH TECH, MADE A RETURN TO DEPARTURE. WHEN APPROACHED AIRPORT, MADE AN ALTERNATE GEAR EXTENSION AND SDR CA090118005Duct · damaged(CAN) CLIMBING THROUGH FL 300 "COWL A/ICE DUCT L" WARNING ON ED1 FOLLOWED CHECKLIST PROCEDURE WARNING MESSAGE REMAINED ENGINE SHUTDOWN AND SINGLE ENGINE OPERATIONS CHECK LIST APPLIED DIVERTED TO SDF AFTER ENGINE WAS SHUT DOWN WARNING MESSAGE CAME ON AND CLEARESDR CA090109008Handle · broken(CAN) ON ARRIVAL AT DESTINATION AIRPORT, THE MAIN CABIN DOOR HANDLE SNAPPED OFF WHEN GROUND CREW ATTEMPTED TO OPEN DOOR. MAIN OUTER DOOR HANDLE REPLACED AND ACFT RETURNED TO SERVICE.SDR CA081229004Handle · broken(CAN) WHEN GROUND CREW ATTEMPTED TO OPEN AIRCRAFT FOR MORNING DEPARTURE, OUTER DOOR HANDLE SNAPPED OFF IN HIS HAND. MAINTENANCE INSPECTED AND REPLACED MAIN CABIN DOOR HANDLE ASSEMBLY AND FUNCTION CHECKED AS PER MANUFACTURERS MAINTENANCE MANUAL. AIRCRAFT RETUSDR CA081217002Landing Gear · inoperative(CAN) LANDED WITHOUT LT MLG NOT FULLY EXTENDED. THE FLT CREW ATTEMPTED TO EXTEND GEAR, BUT NEVER GOT A LT MLG GREEN DOWN AND LOCKED INDICATION. THEY CYCLED THE GEAR 3 TIMES, BUT STILL WERE UNABLE TO GET GOOD INDICATION. THEY PERFORMED A MANUAL EXTENSION ANDSDR CA081208010Thrust Reverser · malfunctioned(CAN) BOTH THRUST REVERSERS FAILED TO STOW AFTER LANDING. RT T/R FOUND DEPLOYED APPROX 1/2 WAY. LT T/R FOUND DEPLOYED JUST A CRACK FROM STOWED POSITION. ONCE NOSE OLEO SERVICED, RESET T/R STOW USING OPERATIONAL CHECK OF T/R REF:AMM 78-30-00 P 201 TASK 78-30SDR CA081204001Pipe · chafed(CAN) MX FOUND NR1 ENGINE MOTIVE FLOW PIPE CHAFED LEAKING FUEL. PIPE WAS REPLACED, ENGINE RUNS AND LEAK CHECKS COMPLETED SATISFACTORY. CAUSE OF CHAFING COULD NOT BE CONFIRMED. IT WAS REPORTED THAT THE NEAREST DRAIN LINE WAS AT LEAST .5 INCH AWAY AND ALL SEEMEDSDR COMA2008120290001Fan Blade · damagedEN ROUTE FROM ORD TO JFK NR 2 ENGINE N1 VIBE. ACFT IN ICING CONDITIONS. FOLLOWED QRH FOR ICING BUT VIBE CONTINUED TO CLIMB, PERFORMED IFSD OF NR 2 ENGINE. EMERGENCY DECLARED, ACFT DIVERTED TO FWA LANDED SAFELY. REMOVED AND REPLACED 3 SETS OF DAMAGED FAN BLSDR CA081106007Power Unit · burned(CAN) NOT ACCEPTING AC EXTERNAL OR APU GEN AC. MX DETECT A BURNED CONTACTOR. CURRENTLY ACFT EXTERNAL AVAILABLE LIGHT IS ON. ACFT ONLY MAINTAINS POWER FOR 3 SECONDS, AND KICKS OFF. MFG HAS ISSUED A CONCESSION SL STATING NO OBJECTION TO FERRY PROVIDED THE FOSDR CA081027004Bracket · loose(CAN) INBD MLG RT DOOR ATTACHMENT BRACKET ON STRUT FOUND LOOSE DURING HEAVY MAINT VISIT. REFERENCE: CMM 32-11-05, FIGURE 1, PAGE 1019, ITEM 290. IT IS WORTH NOTING THAT THIS IS THE 2ND TIME, IN THE MONTH OF OCTOBER 2008, THAT THIS ISSUE HAS BEEN RAISED. PREVSDR CA081009008Wire · chafed(CAN) FLIGHT ATTENDANT REPORTED A BURNING ODOR IN THE CABIN. THE ACFT LANDED UNEVENTFULLY. THE CAUSE OF THE ODOR WAS TRACED TO CHAFED WIRE ABOVE THE FORWARD LAVATORY.
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