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 = 'CF650E2' 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 = 'CF650E2' 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 UIEA200300061Fire Loop · malfunctionedDURING DESCENT INTO ANC, NR 2 ENGINE HAD A FIRE WARNING PASSING THROUGH 16000 FT AT IDLE POWER. NR ENGINE (A) LOOP IS PLACARDED INOPERATIVE. PERFORMED EMERGENCY FIRE CHECK LIST AND SHUTDOWN ENGINE. FIRE HANDLE WAS PULLED AT 1946Z, TT EDP IN DEPRESSURIZE MODSDR UIEA200300060Engine · making metalIN CRUISE, ENGINE NR 3 COMPRESSOR STALLS WITH N1, N2 AND EGT FLUCTUATION. PERFORMED ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECK IAW FLIGHT HANDBOOK 3.70.1. SHUTDOWN ENGINE AND RETURNED. FUEL DUMPED 6,000 KGS. VISUAL INSPECTION OF NR 3 ENGINE, FOUND METASDR UIEA200300058Engine · shutdownINFLIGHT ENGINE SHUTDOWN IN CRUISE NR 2 ENGINE N1 SPOOLED DOWN FROM 102 PERCENT TO 55 PERCENT. ALL OTHER INDICATIONS NORMAL. ENGINE WOULD NOT RESPOND TO THRUST LEVER MOVEMENT. ENGINE SHUTDOWN AS PRECAUTION AT 07:55 UTC. C/A: FOUND DEBRIS IN EXHAUST. BOROSSDR UIE2003F00001Warning System · malfunctionedDURING TAKEOFF AT APPROXIMATELY 75 KNOTS, PILOTS LEADING EDGE FLAP INDICATED UNSAFE WITH F/E LT WING PANEL LEADING EDGE FLAP INDICATORS ALSO INDICATING UNSAFE. NO WARNING HORN WAS HEARD AT ANY TIME DURING TAKEOFF. VISUALLY AND MANUALLY CHECKED ALL LEFT WING SDR P5CA0300954Engine · malfunctionedON START UP NO (N1) INDICATION ON NR 1 ENG RESET C/13 NO HELP. DEFERRED NR 1 ENG (N1) IAW MEL 77-1-2.SDR P5CA0300944Exciter · inoperativeNR 4 ENG START NO INGITION. REPLACED NR 4 ENG NR 1 EXCITER BOX: DEFERRED NR 4 ENG NR 2 IGNITION SYS.SDR UIEA200300055Engine · stalledDOV/RMS DIVERSION TO JFK, IN CRUISE AT FL350 NR 1 ENGINE BEGAN TO SHUDDER/STALL WITH DROP OF N1 ONLY. PULLED THRUST LEVER BACK. IT THEN DID IT AGAIN AND CONTINUED TO DO IT. SHUT DOWN ENGINE IAW QRH. DIVERTED TO JFK. NO FUEL DUMPED. REMOVED AND REPLACED NSDR UIEA200300040Connector · looseDURING CRUISE, NR 4 ENGINE NACELLE TEMP INDICATOR SHOWED 5.9. STARTED FLUCTUATING TO 6.5, EVENTUALLY READING 7.0. ACCOMPLISHED ABNORMAL PROCEDURES IAW 3.26.10. AIRCRAFT DIVERTED. NO FUEL DUMPED. TROUBLESHOOTING FOUND 1 CONNECTOR LOOSE ON LT LOWER DETECTORSDR UIEA200300032Engine · malfunctionedDURING TAKEOFF NR 3 ENGINE HAD EXCEEDANCE OF PEAK TEMPERTURE OF 994 DEGREES FOR A 91 SECOND DURATION. THRUST LEVER WAS RELATIVE TO THE SAME POSITION AS OTHERS. TAKEOFF N1 WAS 113.5 DUE TO EXCEEDING 990 DEGREES THE ENGNE WAS SHUT DOWN. APPROXIMATELY 23,000 KSDR UIEA200300033Mec · malfunctionedRMS/FRU - REJECTED TAKEOFF, ON TAKEOFF ROLL, NR 1 ENGINE WOULD PRODUCE ONLY 108.0 N1 WITH FIREWALL THRUST. 113.0 N1 WAS THE DESIRED POWER SETTING. ABORTED TAKEOFF AT 80 KTS, NR 1 N1 APPEARED TO SPIN UP SLOWER THAN THE REST. ALL OTHER ENGINES APPEARED NORMALSDR UIEA200300020Trunnion · lack of lubeNOSE LANDING GEAR WOULD NOT EXTEND NORMALLY. EXTENDED OK WITH ALTERNATE SWITCH. LUBRICATED NOSE LANDING GEAR TRUNNIONS PER MM 12-21-01. JACKED AIRCRAFT PER MM 7-11-02. RESET ALTERNATE GEAR SYSTEM PER 32-36-00 AND ACCOMPLISHED NOSE LANDING GEAR SWING PER 32SDR UIEA200300017Warning Light · illuminatedINFLIGHT ENGINE SHUTDOWN, DURING CRUISE, NR 4 ENGINE SHUTDOWN IN FIGHT DUE TO 'OIL FILTER BYPASS LIGHT. OIL TEMPEARTURE AND PRESSURE NORMAL AT 49 PSI/120 DEGREES AND N2 AT 94 PERCENT. WITH THRUST AT IDEL (75 PERCENT N2) PRESSURE WAS 30 PSI AND TEMPERATURE ROSDR P5CA0300782Igniter · defectiveRETURN TO BLOCKS DUE TO NR 4 ENG FAILED TO START. REPLACED BOTH IGNITER PLUGS TESTED OK. DEFECTED IGNITER PLUG NR 2 POS NR 1 SYS PREV DEFERRED.SDR UIEA200300007Engine · inoperativeDURING CLIMB OUT AT APPROXIMATELY 18,800 FT, NR 3 ENGINE HAD THREE LOUD BANGS. WHEN THROTTLE WAS RETARDED BANGS STOPPED. THRUST LEVER REMAINED AT IDLE FOR REMAINDER OF THE FLIGHT. THE ONLY INDICATION NOTICED WAS THAT THE N1 WAS AROUND 76 PERCENT AT ONE POINSDR P5CA0300717Cable · faultyNR 4 ENGINE COMPRESSOR STALL AT TOP OF DESCENT - EGT 700 DEGREES, N1 20 PERCENT LESS THAN OTHER ENGINES. STALL CLEARED AT 33.0. REPLACED NR 4 ENGINE VSV RETURN CABLE PER MM 75-30-00. BOROSCOPED ENGINE IAW AMM 72-00-00. ENGINE RUN CARRIED OUT AS PER AMM 71-SDR P5CA0300716Seal · leakingAFTER FUELING WAS COMPLETED, A STEADY DRIPPING OF FUEL ONTO #2 ENGINE FROM #2 PYLON WAS NOTICED. FOUND LEAK COMING FROM SEALANT ON FWD SPAR ON #2 ENGINE PYLON. INSTALLED FUEL LEAK SEAL IAW BMM 28-11-00 & PAC SERVICE FUELING MANUAL 4-05-02, ITEM 7. NO LEAKS NOTSDR P5CA0200712Frame · crackedA 2 INCH CRACK FOUND, NR 3 ENGINE, TURBINE MID FRAME HOT SECTION AT NR 7 TIME (10 O'CLOCK POSITION). CRACK WELDED IAW GE SOPM 70-41-00. REF EDA 7254E001.SDR P5CA0200709Duct · separatedNR 4 ENG - FIRE INDICATION AFTER TAKEOFF IN CLIMB. PRECAUTIONARY ENGINE SHUTDOWN & FUEL DUMP PERFORMED. FIRE BOTTLE NOT REQUIRED. FOUND 8TH STAGE BLEED CROSSOVER DUCT SEPARATED FROM DUCTING SYSTEM. REPLACED WITH CROSSOVER DUCT & PRECOOLER DOWNSTREAM DUCT. SDR P5CA0200708Coupling · looseDURING CRUISE AT FL 310, #4 ENG OIL QTY WENT FROM 3.5 TO ZERO IN APPROX. 15 MIN. OIL PRESS STARTED FLUCTUATING; OIL TEMP IN GREEN BAND (PERFORMED PRECAUTIONARY SHUTDOWN) WINDMILL RPNM 26%, N2 23%, OIL TEMP BELOW GREEN, OIL PRESS 10 PSI. EMERGENCY DECLARED & SDR UIEA200200061Line · crackedAIR TURN BACK, NR 1 HYDRAULIC SYSTEM LEAKING. QUANTITY STOPPED AT 2 GALLONS AFTER PLACING EDP SWITCH TO DEPRESS. ADP WORKED NORMAL AFTER 20 MINUTES IN CONTINUOUS ADP PRESSURE DROPPED TO ZERO. FOUND LINE CRACKED AT CLAMP IN SAILBOAT AREA. REMOVED AND REPLACSDR UIEA200200052Mec · inoperativeWHILE CLIMBING THROUGH 13,500 FEET AND ACCELERATING THROUGH 310 KTS, NR 4 ENGINE ROLLED BACK TO IDLE ACCOMPANIED BY A NOTICEABLE YAW. INSTRUMENTS CONFIRMED NR4 ENGINE HAD INDEED ROLLED BACK. AUTO THROTTLES WERE ENGAGED AT TIME. USING CLIMB POWER BUT NO THROSDR UIEA200200051Transponder · failedDURING INITIAL CLIMB, TRANSPONDER FAIL LIGHT ILLUMINATED WITH NR 1 SET SELECTED. SELECTED NR 2 TO NO AVAIL. CIRCUIT BREAKER CHECKED OK. DIVERTED. C/A: REPLACED MODE S TRANSPONDER IAW MM. TEST CARRIED OUT. OPS CHECK SATISFACTORY. ALSO ATC TRANSPONDER NRSDR UIEA200200049Sensor · malfunctionedNOSE GEAR DOOR LIGHT (RED) AND GEAR LIGHT REMAINED ON AFTER GEAR LEVER WAS RAISED. ATTEMPTED TO CORRECT PER FHB PROCEDURES TO NO AVAIL. AIR TURN BACK REQUIRED. JETTISONED APPROXIMATELY 70,000 KGS OF FUEL. LIFTED THE AIRCRAFT AND TROUBLESHOT PER MM. ALL GESDR UIEA200200050Module · leakingNR 1 HYDRAULIC LOW QUANTITY LIGHT CAME ON AFTER TAKEOFF. HYDRAULIC QUANTITY DROPPED TO ZERO. APPROXIMATELY 30 SECONDS LATER THE EDP AND ADP PRESSURE LIGHTS BEGAN TO FLASH. SHUT SYSTEM DOWN IAW PROCEDURES. EDP PUMP SWITCH PLACED TO SUPPLY OFF POSITION AT 08SDR P5CA0200699Compressor · stalledCLIMBING THROUGH 15,000 FT NR 3 ENGINE COMPRESSOR STALLED. EGT WAS 100 DEGREES CELCIUS. LOWER THAN OTHER MOTOR & N2 WAS LOWER WITH NACELLE ANTI-ICE ON. TROUBLESHOT ENGINE PER MM 71-00-43, PERFORMED INSPECTION PER MM 72-00-00 & BORESCOPE OF ENGINE IAW MM 72-SDR UIEA200200036Battery · overheatedDURING PREFLIGHT, THERE WAS STRONG BURNING SMELL IN COCKPIT. TROUBLESHOT, NR 3 ACM MAKING A NOISE, DEFERRED. DURING CRUISE AFTER 2.5 HOURS OF FLIGHT, BURNING ODOR RETURNED IN COCKPIT. AFTER SEARCHING FOR SOURCE IT WAS NOTICED NR 1 GEN KVAR/KW METER WAS READSDR UIEA200200035Control Unit · failedON CLIMBOUT, NR 3 AND NR 4 BUS TIES OPENED. SPLIT BUS SYSTEM OPEN. NR 3 GENERATOR WAS DISCONNECTED. NR 4 GENERATOR CHECKED GOOD VOLTS/ FREQ. NR 3 BUS LOST POWER AND COULD NOT REPOWER. DUMPED 17.0 KGS OF FUEL PRIOR TO LANDING. REMOVED AND REPLACED RIGHT SDR UIEA200200030Window · inoperativeL1 WINDSHIELD LOWER AFT ELECTRICAL CONNECTION WAS PRODUCING SMOKE. SYSTEM TURNED OFF. SMOKE EV AC CHECKLIST COMPLETED. C/A: REPLACED L1 WINDOW PER MM 56-11-01 REPLACED LEFT WINDOW HEAT CONTROLLER PER MM. WINDOW HEAT CONTROLLER (PN 657154-5).SDR UIE2002000026Switch · intermittentON DESCENT A STRONG ELECTRICAL ODOR COMING OUT OF GASPERS. ELECTRICAL SMOKE OR FIRE CHECK LIST INITIATED. AFTER NR 6, SMOKE STOPPED. AIRCRAFT IN THIS CONFIGURATION AND LANDED. FOUND MELTED INSULATION AT WING ILLUMINATION LIGHT SWITCH TERMINAL. LIGHT INTERSDR Q2S2002F00002Duct · blownAIR TURNBACK, ON TAKEOFF, AT 2500 FEET MSL, WITH TAKEOFF POWER AT 113.0 N1, NR 2 ENGINE FIRE LIGHT AND BELL CAME ON. NACELLE INDICATOR BOTH A AND B READ 6.5 SHUTDOWN ENGINE IAW QRH. DUMPED 18,700 LBS OF FUEL. NO EVIDENCE OF FIRE FOUND ON INSPECTION OF ENGINSDR IUEA02016Pin · misalignedDURING WALK AROUND DAILY CHECK, INSPECTION FOUND NR 4 ENGINE PYLON MIDSPAR FUSE PIN ALIGNMENT STRIPES MISALIGNED BY 0.5 INCH. CLOSER INVESTIGATION POINTS TO POSSIBLE FUSE PIN FAILURE. THIS AS PER MM. FURTHER INSPECTION FOUND SPRING BEAMS CRACKED, REPLACEMSDR 2001F00268Engine · failedAT FLT 310, NR 2 ENGINE FAILED. PROCEEDING FAILURE CREW COULD SMELL OIL SMELL, THEN ENGINE QUIT. N2 WENT TO ZERO ALSO ZERO OIL PRESSURE. N1 APPROXIMATELY 22 PERCENT. A/C DIVERTED TO BKK. (M)SDR P5CA0401104Fire Loop · inoperativeNR 2 ENGINE A-LOOP INOP IN FIRE TEST MODE. TRANSFERRED TO DMI 32697 AND PLACARD PER MEL 26-1.SDR UIEA00053Turbine · failedATB - FLT 3120 - CREW HEARD A LOUD BANG FROM RIGHT SIDE OF AIRCRAFT, THEN NR 4 ENGINE SHUTOFF. UPON RETURN TO LAX, IT WAS DISCOVERED THAT NR 4 ENGINE TURBINE SECTION HAS FAILED AND THE ENGINE HAS INTERNAL DAMAGE. SEVERAL BLADES FOUND DAMAGED DURING BORESCOPESDR UIEA00049Engine · flamed outFLT 9027 - BOM-MAA - NR 2 ENGINE FLAME OUT AT FL370. ALL ENGINE INDICATIONS WERE NORMAL AND ENGINE WAS RUNNING FINE. ACCOMPLISHED IN FLIGHT RESTART AT FL290. MAINTENANCE CHECKED ENGINE INLET AND EXHAUST AREA AND NO DEFECTS WERE FOUND. INSPECTED ENGINE TUBISDR 20001212AP005Support Bracket · brokenNR 1 ENGINE FIRE LOOP SUPPORT TUBE AT 12:00 JUST ABOVE THE HIGH PRESSURE TURBINE IS BROKEN. REMOVED AND REPLACED FIRE LOOP SUPPORT BRACKETS IAW AMM 26-11-01. (M)SDR 20001212AP006Support Bracket · crackedNR 2 FIRE LOOP SUPPORT BRACKET AT 1:00 POSITION ABOVE THE DIFFUSER AT THE ELECTRICAL CONNECTION TO THE LOOP IS CRACKED. REMOVED AND REPLACED FIRE LOOP SUPPORT BRACKETS IAW AMM 26-11-01. (M)SDR 20001212AP007Support Bracket · crackedNR 3 FIRE LOOP SUPPORT BRACKET AT 1:00 POSITION ABOVE THE DIFFUSER AT THE ELECTRICAL CONNECTION TO THE LOOP IS CRACKED. REMOVED AND REPLACED FIRE LOOP SUPPORT BRACKETS IAW AMM 26-11-01. (M)SDR 20001212AP008Support Bracket · crackedNR 4 ENGINE FIRE LOOP MOUNT TUBE AT 12:00 POSITION ABOVE HIGH PRESSURE TURBINE CRACKED. REMOVED AND REPLACED FIRE LOOP SUPPORT BRACKETS IAW AMM 26-11-01. (M)SDR UIEA0018Duct · separatedFLT 7150 - GYE - ON TAKEOFF AT 400 AGL, NR 1 ENGINE EXPLODED AND HAD AIRCRAFT VIBRATION. LEVELED AIRCRAFT AT 817 FEET. ADVISED TOWER HAD AN ENGINE FIRE AND DECLARED AN EMERGENCY. DUMPED 30K FUEL AND RETURNED TO GYE. ON ARRIVAL, DETERMINED THAT NR 1 ENGINE SDR 20000728SH009Compressor · crackedAFTER ENG AND MODULE DISASSEMBLY, ENG SHOP INSP GROUP FOUND DEBLADED HPC11-14TH SPOOL-SHAFT A VISIBLE CRACK. A SEPARATED PIECE OF 12TH STAGE DOVETAIL PRESSURE SURFACE EDGE (REAR SIDE) APPROX 1.5 INCHES LONG CIRCUMFERENTIALLY STARTING FROM A CRACK. PART PARAMSDR UIEA9998Eicas · malfunctionedFLT AZ9162 - MXP-ORD - ON TAKEOFF ROLL AT 20 KNOTS, THE FLT CREW SAW A MOMENTARY RED FLASH ON THE EICAS. BELIEVED TO BE A FIRE WARNING MESSAGE, BUT IT WAS TOO QUICK TO READ. TAKEOFF WAS ABORTED WITHOUT EXCEEDING TAXI SPEED AND A/C RETURNED TO BLOCKS. WHEN ASDR UIEA9997Valve · stuckFLT GT57 - NR 2 ENGINE FIRE WARNING ILLUMINATED AFTER TAKEOFF. IT OCCURRED DURING CLIMB WITH CLIMB POWER SET. BOTH NACELLE TEMPS WERE 8.5. ENGINE SECURE DIAW FHB. DECLARE EMERGENCY AND JETTISONED 14 KGS OF FUEL. LANDING WAS UNEVENTFUL. FOUND NR 2 ENGINE SDR UIEA9975Ignitor · erodedFLT 2087 - ANC-KIX - DURING DESCENT THROUGH 4000 FT, NR 1 ENGINE FLAMED OUT. FLIGHT CRWE DID NOT ATTEMPT TO RE-START ENGINE. AIRCRAFT LANDING AT KIX UNEVENTFUL. MAINTENANCE PERFORMED TROUBLESHOOTING AS PER MM 71-00-42. NO FAULTS FOUND. BOTH IGNITERS WERE SDR UIEA9805Turbine · failedANC - AFTER TAKEOFF AT FL 310, NR 2 ENGINE FLAMED OUT IN CRUISE. ATTEMPTED RE-START ENGINE AND NO HELP. NO N2 INDICATION. AIRCRAFT DUMPED FUEL AND HAD UNEVENTFUL RETURN TO ANC. DURING INSPECTION OF ENGINE AT ANC, FOUND EVIDENCE OF METAL IN THE TAIL PIPE ANSDR UIEA9802Engine · failedATB - FLT C1315 - ANC/TPE - NR 3 ENGINE FAILURE (FLAMEOUT) DURING CRUISE, FL 290, .84M..ENGINE VIBRATION NORMAL. ACCOMPLISHED ENGINE FAILURE SHUTDOWN CHECKLIST. AFTER CHECKLIST, N1 = 26.8, N2 = 0, F/F = 100, OIL PRESSURE = 0. FUEL DUMPED AND RETURNED TO ANCSDR UIEA9704Engine · failedCREW REPORTS: ABORTED TAKEOFF FLT SK5086/06, SHJ/GOT...DURING TAKEOFF, FLIGHT CREW REPORTED A LOUD BANG AT 90-100 KNOTS AND ABORTED TAKEOFF DUE NR 1 ENGINE FAILURE (SN 528419). INSPECTION OF ENGINE REVEALED AFT CENTERBODY DEPARTED AIRCRAFT. LPT BLADE PENETRSDR UIEA9601Scavenge Pump · failedBANKOK/TAIPEI, CI346/07 - EN ROUTE, INCURRED NR 1 ENGINE SHUT DOWN IN FLIGHT-DESCENT PHASE FOR LOSS OF OIL PRESSURE AND N2 RPM. ON ARRIVAL, CHECKED MAIN OIL SCREEN AND CHIP DETECTORS ALL OK. FOUND LUBE AND OIL SCAVENGE PUMP DRIVE SHAFT SHEARED. DRAINED ENGISDR UIEA9502Blade · fractureENGINE, SN 455833, TEAR DOWN REVEALED CONSIDERABLE TURBINE DAMAGE. HPT STAGE 1 BLADES METALLURGICAL ANALYSIS FOR PRIMARY FAILURE MODE. ONE BLADE FOUND WITH FAILURE PATTERNS IN THE TRAILING EDGE AREA. BLADE, PN 9299M30G09R, SN KTWD2263, REPAIR HISTORY M1K-M2SDR UIEA9504Shut-Off Valve · failedON LEVEL OFF FROM A CLIMB TO F350, THE NR 4 ENGINE FLAMED OUT FOR NO APPARENT REASON. AIRCRAFT DIVERTED INTO JFK. FOUND NR 4 ENGINE FUEL SHUT OFF VALVE FAILED. REPLACED FUEL SHUT OFF VALVE ACTUATOR PER MM 76-11-04. OPS AND RUN-UP OK. ENGINE INLET, TAIL PI
Back to GE CF6-50E2