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 = 'CF348E5A1' 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 = 'CF348E5A1' 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 CA110420008Warning Message · activated(CAN) FLIGHT EXPERIENCED AVNX MAU 2A FAIL EICAS MSG. NOSE WHEEL STEERING WILL BE INOPERATIVE. TOW INTO GATE WILL BE REQUIRED. FIM 45-45-00-810-941-A CARRIED OUT, FAIL/FAULT MESSAGE CLEARED. CONSIDERED TRANSITORY MAU 2A CHECKED SERVICEABLE.SDR CA110418005Slat System · malfunctioned(CAN) CREW ADVISED FLIGHT DISPATCH OF A SLAT FAIL INBOUND. ON APPROACH TO RUNWAY 22, CREW SELECTED FLAPS CONFIG 2. SLAT FAIL MSG, CREW ADVISED ATC AND DID A GO-AROUND. ATC VECTORED THE FLIGHT AFTER THE GO-AROUND, THE QRH WAS COMPLETED, CREW LANDED RUNWAY 22 SDR CA110415005Floorbeam · corroded(CAN) DURING A CPCP VISIT, AREAS OF CORROSION WERE FOUND.SDR CA110330002Actuator · failed(CAN) AFTER TAKEOFF, THE FLIGHT EXPERIENCED A BRAKE CONTROL FAULT AND WERE UNABLE TO RETRACT THE LT MAIN GEAR. THE FLIGHT DECLARED A PAN-PAN AND RETURNED WITH ALL GEAR SHOWING DOWN AND LOCKED. THE FLIGHT LANDED WITHOUT FURTHER EVENT. LT DOWNLOCK STAY ACTUATSDR CA110324005Actuator · failed(CAN) CREW REPORTED FLAP FAIL MESSAGE ON APPROACH. A GO AROUND WAS CONDUCTED AND THE QRH CHECKLIST WAS COMPLETED BEFORE THE FLIGHT CONTINUED ONTO DESTINATION. REPLACED TRIPPED ACTUATOR AT 3L POSITION IAW J/C E17-27-51-01-000-801A AND E17-27-51-01-400-801-A. SDR CA110318007Ram Air Turb · failed(CAN) DURING RAT AUTO DEPLOYMENT TEST RAT FAILED. FOUND RAT BLADES IN UNLOCKED POSITION, JAMMED IN RAT COMPARTMENT DURING DEPLOYMENT. RAT ASSEMBLY CHARGED & TESTED IAW AMM 24-23-01, SERVICEABLE.SDR CA110201009Bracket · broken(CAN) ENGINE OIL DRAIN ATTACHMENT POINT BROKEN OFF.SDR CA110121001Attach Bolt · shortDURING AN N1 CHECK ON THE ACFT, A PYLON INSP FOUND THAT THE AFT FIXED FAIRINGS WERE MISSING SEVERAL ITEMS OF ATTACH HARDWARE. IN THE LT PYLON FIXED FAIRING, BOTH FWD PIP PINS HAD FALLEN OUT, AS HAD ONE OF FOUR MID-POINT ATTACH BOLTS. THE MISSING HARDWARE WAS FSDR CA110117001Oven · smokeCABIN CREW REPORTED WHITE SMOKE FROM THE AFT GALLEY OVEN. CIRCUIT BREAKER PULLED.SDR CA110110005Uplock · failedNOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT RETURNED TO POINT OF DEPARTURE/OVERWEIGHT LANDING APPROX 1800KGS, R/I UPLOCK ON SPEC FOUND MOSITURE IN UPLOCK, PER 32-32-03-000-801-A AND 32-32-03-400-801-A. UPLOCK BLED, 50 FLIGHT CONTROL ACTUATIONS 18 GEAR SDR CA101115017Slat System · failed(CAN) THE AIRCRAFT ENCOUNTERED A SLAT FAILURE DURING APPROACH. SF ACE 1 AND 2 INHIBITS CLEARED IAW AMM 45-45-00-970-805-A/200. OPS CHECK FOUND SATISFACTORY IAW 27-56-00-710-810-A/200.SDR CA101116001Slat System · failed(CAN) WHEN EXTENDING FLAPS 0 TO 1, EICAS MESSAGE "SLAT FAILURE". QRH ACTIONED, NIL FIX. UNEVENTFUL LANDING RWY 31 - NO HANDLING DIFFICULTIES NOTED. FLIGHT CONTROL SYSTEM RESET ALL FLIGHT CONTROL MESSAGES ON CMC CLEARED. NO CORRESPONDING MAINT FIM MESSAGES OSDR CA101110001Unknown · smoke(CAN) CREW ADVISED FLIGHT DISPATCH THAT 2 PASSENGERS REPORTED A STREAM OF SMOKE FROM THE IFE SCREEN LOCATED AT 13F. THE POWER WAS REMOVED, SMOKE STOPPED/DISSIPATED. FOUND AT 13F WITH BAD ELECTRICAL SMELL. CHECKED CONNECTOR UNDER SEAT J32 IT WAS SECURELY CONSDR CA101108005Tire · failed(CAN) ON POST FLIGHT/DI INSPECTION (NEXT AM) NR 3 MAIN TIRE WAS FOUND TO BE DEFLATED AND ONE INNER RIB/STRIP OF RUBBER MISSING 3/4 AROUND TIRE. APPEARS TO HAVE SEPARATED CLEANLY FROM CARCASS SIGNS OF IMPACT ON TRAILING EDGE OF INBOARD FLAP AND FLAP SEAL AS WESDR CA101108001Wire Harness · failed(CAN) APPROACH TO RWY05 SLAT FAILURE (SLAT FAIL MSG WHEN FLAP 1 SELECTED), GO AROUND AND LANDED 05 SECOND ATTEMPT, EMERGENCY EQUIPMENT WERE ON STANDBY. RT SLAT HARNESS W611 AND W612 REPLACED AS PER AMM 27-83-07. CKS SERVICEABLE, P/N 171-00186-401 (RT SLAT NRSDR CA101030001Actuator · failed(CAN) FLIGHT EXPERIENCE A FLAP FAILURE ON APPROACH. A GO AROUND WAS CONDUCTED AND SUBSEQUENT LANDING WAS CARRIED OUT. IFS AND THE DUTY PILOT WERE ADVISED. CHANGED NR 3 RT FLAP ACTUATOR AS PER AMM 27-51-01-000-801A OPERATIONAL CHECKED SERVICEABLE.SDR CA101021001Rod End · bentDURING TASK 37-24-23-11-001-01, GENERAL VISUAL INSP OF THE RAM-AIR TURBINE MANUAL RELEASE SYS FOUND THE ROD END OF THE RAT DOOR ACTUATION ROD BENT. (PROBABLE DAMAGE CAUSED BY FORK END ASSY BEING VERY STIFF TO ROTATE). RAT DOOR ACTUATION ROD END REPLACED AND ASDR CA101022003Converter · failedDURING CRUISE THE PILOT NOTICE THE AUXILIARY WARNING LIGHT WAS ON, ON THE ENG CONTROL PANEL, AN INDICATION OF POWER LOSS ON 1 CHANNEL, IN A DUAL CHANNEL SIGNAL DATA CONVERTER. ALL ENG INSTRUMENTS N1,N2, FF, ITT, FP, OP, & FUEL TOTALIZER GO THROUGH BOTH CHANNSDR CA101004002Powerplant · failedSHORTLY AFTER TAKEOFF THE CREW REPORTED THE LT ENGINE HAD FAILED. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO POINT OF DEPARTURE. LANDING WEIGHT WAS BELOW MAXIMUM.SDR CA100928015Flex Hose · burstBURST IN FLEX NEAR QUICK DISSCONNECT FITTING END, LOSS OF HYD PRESSURE AND FLUID.SDR CA100922006Screw · undertorquedACFT 379, DURING N01 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSCREEN FASTENERS FOUND THE SCREWS BELOW MINIMUM TORQUE. SCREWS WERE RETORQUED IAW AMM 56-11-00-04.SDR CA100924002Wire Harness · burnedFOUND HARNESS PEVIOUSLY REPAIRED, WHEN RE-INSPECTED FOUND EVIDENCE OF BURNED HARNESS BEYOND LIMITS. DAMAGE TO HARNESS CAUSED BY PRECOOLER GASKET FAILURE. (SDR20100728002/003 AND 201000802002)SDR CA100924004Wire Harness · burnedFOUND HARNESS PEVIOUSLY REPAIRED, WHEN RE-INSPECTED FOUND EVIDENCE OF BURNED HARNESS BEYOND LIMITS. DAMAGE TO HARNESS CAUSED BY PRECOOLER GASKET FAILURE.SDR CA100920005Flap System · malfunctionedON APPROACH, THE CREW RECEIVED AN ECAM MESSAGE "FLAP LOW RATE". THE QRH WAS FOLLOWED AND WHEN DESCENDING THROUGH 400 FT AGL, WHEN THE AUTO PILOT WAS DISCONNECTED, THE ACFT BEGAN DRIFTING HIGH AND REQUIRED MORE MANUAL FORCE THAN NORMALLY REQUIRED. A NORMAL LASDR CA100909001Circuit Card · failedFLIGHT ENCOUNTERED A DUEL BLEED FAILURE, 20 MINUTES AFTER DEPARTURE, FLIGHT RETURNED TO POINT OF DEPARTURE FOR MX INVESTIGATION.SDR CA100907001Screw · looseACFT 376, DURING NR 1 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSCREEN FASTENERS FOUND SCREWS BELOW MINIMUM TORQUE VALUES ON RT WINDSHIELD AT POSITIONS 78, 80, 82 AND 83. REPEAT SDR FOR WINDSHIELD FASTENERS.SDR CA100907004Screw · undertorquedDURING NR 01 CHECK, WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSHIELD FASTENERS FOUND SCREWS BELOW MINIMUM TORQUE VALUES ON RT WINDSHIELD AT LOCATIONS 1, 6, 13, 33, 43, 56, 60, 64, 68, 76, 79 AND 80. REPEAT SDR FOR MFG WINDSHIELD FASTENERS.SDR CA100728002Wire Harness · burnedWHILE PERFORMING J/C Z419-001ACR-U, DURING THE INSP, PAY PARTICULAR ATTENTION TO HOT AIR LEAKS FROM THE PRE-COOLER ON ELECTRICAL CABLES. WIRING HARNESS W606 AND CLAMPS IN RT PYLON ARE HEAT DAMAGED FROM HOT AIR LEAKAGE AT PRECOOLER.SDR CA100728003Wire Harness · burnedWHILE PERFORMING J/C Z419-001ACR-U "DURING THE INSP, PAY PARTICULAR ATTENTION TO HOT AIR LEAKS FROM THE PRE-COOLER ON ELECTRICAL CABLES" --WIRING HARNESS W607 AND CLAMPS IN RT PYLON ARE HEAT DAMAGED FROM HOT AIR LEAKAGE AT PRECOOLER.SDR CA100802002Gasket · failedGASKET LEAKING DAMAGED W606 AND W607 WIRE HARNESS. . IT APPEARS TO BE MADE OF A THIN PIECE OF METAL SANDWICHED BETWEEN PRESSED PAPER COVERED IN A CARBON POWDER.SDR CA100719001Bolt · loose(CAN) CAPT`S WINDSHIELD ANCHOR NUTS AT TORQUE POSITIONS 69, 61, 59, 49 SPINNING WHEN TORQUE IS APPLIED TO SCREWS. DISCOVERED DURING SPECIAL INSPECTION SP3-024.SDR CA100722003Window · looseDURING ACFT CHECK, WHILE PERFORMING, J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSCREEN FASTENERS, FOUND 1(12) SCREWS AT POSITIONS 37, 22, 14, 8, 42, 44, 69, 65, 61, 53, 67, AND 75 SPINNING AND UNABLE TO TORQUE ON CAPT`S WINDSCREEN, AND 1 FASTENER AT POSITION SDR CA100812006Screw · looseDURING NR 1 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSCREEN FASTENERS FOUND WINDSHIELD SCREWS LOOSE (UNDERTORQUED) AT THE FOLLOWING POSITIONS: LT: 31,40,59,78,80, RT: 38,39,46,48,50,54,56,70,72,76,78,80, REPEAT FINDING. (SEE SDR`SSDR CA091210005Slat System · failed(CAN) SLATS FAILED ON APPROACH, EMERGENCY EQUIPMENT REQUESTED. MX RT OTBD SLAT SKEW SENSOR 2-3 FAILED AND REPLACED.SDR CA091210003Slat System · failed(CAN) SLATS FAILED ON APPROACH, FLIGHT CREW REQUESTED EMERGENCY EQUIPMENT, COMPLETED GO AROUND AND QRH. LANDED WITHOUT FURTHER INCIDENT. MX SF-ACE 1 & 2 CB`S RESET, CMC CLEARED NIL FURTHER.SDR CA091116004Flap System · failed(CAN) FLIGHT CREW:AFTER NORMAL LANDING FLAPS SELECTED 0 ECIAS FLAP FAIL AND INDICATOR AMBER. SLATS 0 AND GREEN.SDR CA091214002Link · broken(CAN) ACFT EN ROUTE, HAD A RT NOSE GEAR AFT DOOR OPEN MESSAGE. UPON ARRIVAL, MX INSP REVEALED THAT THE ATTACHING DOOR ROD`S TAB WASHER WAS BROKEN. THIS LEAD TO THE BREAKING OF SAFETY WIRE AND ALLOWING THE ROD TO TURN FREELY.SDR CA091021001Pulley · damaged(CAN) DURING B02N01 CHECK IT WAS DISCOVERED THAT THE LT AND RT AILERON PULLEYS BETWEEN RIB 2 AND RIB 4 IS OUT OF ALIGNMENT WITH THE CABLE RUN. AILERON PULLEY SUPPORT BRACKETS P/N 170-32541-001 AND 170-32541-002 MIS-ALIGNED WITH CABLE RUN CAUSING PREMATURE WEASDR CA091021004Wire Harness · burned(CAN) DURING B02N01CHECK INSPECTION OF RT ENGINE PYLON, MECHANICS DISCOVERED RH PYLON FADEC WIRING HARNESS BURNED IN THE AREA AFT OF THE ENGINE BLEED PRE-COOLER ASSY. FURTHER INVESTIGATION REVEALED PART OF GASKET P/N 170-166603-001, ITEM 30 IPC 36-11-08 FIG.01SDR CA090908007Girt Bar · malfunctioned(CAN) ON ARRIVAL, THE FLIGHT ATTENDANT HAD DIFFICULTY OPENING THE L1 DOOR. MAINTENANCE NEEDED TO BE CALLED TO UNHOOK THE GIRT BAR FROM THE FLOOR FITTINGS. MODIFICATION SB 170-52-0031 HAS BEEN ACCOMPLISHED ON THIS ACFT, TO MODIFY THE DOOR HANDLE MECHANISM SO THSDR CA090625005Cable · broken(CAN) UPON ARRIVAL AT THE GATE, S/D MADE THE ANNOUNCEMENT TO DISARM DOORS. FA AT BACK DID SO AND CONTACTED THE SD TO SAY IT WAS DONE. UPON LEAVING THE ACFT, CREW HEARD A HISSING SOUND AS S/D TRIED TO ENTER THE R2 DOOR. ONCE SLIDE DEPLOYED BOTH CREW MEMBESDR CA090326001Coffeemaker · smoke(CAN) COFFEE MAKER STARTED TO SMOKE DURING CLIMB OUT, FA TURNED OFF POWER FROM THE GALLEY CB PANEL. SHE INFORMED THE FLIGHTDECK WHO ALSO TURNED OFF GALLEY POWER FROM THE FLIGHTDECK. THE SMOKE CLEARED BUT A BURNING SMELL LINGERED IN THE CABIN. THE CREW DECIDED SDR CA090320002Bearing · damaged(CAN) AILERON CONTROL COLUMN FOUND TO BE STIFF IN THE AIR. THE CAUSE WAS FOUND TO BE ONE OF THE SEALED BRGS. ENTIRE TORQUE TUBE ASSY HAS BEEN REPLACED.SDR CA090127004Disk · damagedTRANSCRIPTION FROM EMAIL RECEIVED FROM ENGINEERING DEPT, FAILED WITH 2048 LANDINGS SINCE INSTALLATION, MPN: 90000583-1PR WITH SN: APR05-0595 FOUND THE DAMAGE WAS FOUND AFTER REMOVAL OF THE WHEEL TO REPAIR FLAKING PAINT WHICH WAS IDENTIFIED IN THE 14TH OF JANUASDR CA090121001Lockwasher · broken(CAN) WARNING MSG IN F/DCK "LANDING GEAR NOSE DOOR OPEN DURING CLIMB" CREW PERFORMED FIM PROCEDURE, NO FURTHER FAULTS FOUND AND A/C OK FOR FURTHER FLIGHT. MAINTENANCE FOUND RT AFT NLG DOOR ACTUATING ROD EYE END LOCK TAB WASHER TAB BROKEN AND ROD ADJUSTER BACKSDR CA090119007Aileron · stuck(CAN) AS THE FLIGHT CREW COMPLETED THEIR FLIGHT CONTROL CHECK, DURING TAXI OUT FROM THE GATE, THE CREW DETERMINED THAT THE AILERONS WERE JAMMED. THE ACFT TAXIED BACK TO THE GATE FOR MX ACTION.SDR CA090119003Actuator · malfunctioned(CAN) ON DEPARTURE, LT MLG WOULD NOT RETRACT.SDR CA090127001Brake Assy · failedTRANSCRIPTION OF EMAIL RECEIVED FROM MRO: BRAKE PN 90000583-1PR SN MAR05-0550 AC PO C129RAER006 THIS BRAKE WAS RECEIVED IN PRETTY BAD CONDITION. IT LOOKS LIKE 2 ROTORS AND 1 STATOR FAILED DURING OPERATION. ATTACHED ARE SOME PICTURES OF THE BRAKE AND PIECES OSDR CA081120003Brake Sys · disintegrated(CAN) DURING PUSHBACK, GRND PERSONNEL REPORTED SMOKING BRAKES. FOUND NR3 BRAKE ROTORS HAD FAILED. REPLACED BOTH NR3 WHEEL AND BRAKE ASSY IAW AMM 32-49-05 AND 32-49-11. S/N OF THE BRAKE IS JAN05-0530.SDR CA081104004Fitting · broken(CAN) ON PUSHBACK, RECEIVED FLIGHT CONTROL- NO DISPATCH MESSAGE. INVESTIGATION FOUND THE RUDDER UPPER FTG LUG BROKEN. RUDDER PCU ACTUATOR WAS INSTALLED 2007-05-17. CAUSE WAS FOUND TO BE MISSING SLIDING BUSHING, P/N 170-62218-003, IPC 27-21-05 FIG.01 ITEM 170.
Back to GE CF34-8E5A1