JASC 7200
Service difficulty reports · 14,730
Reports filed under 7200 · Engine (Turbine/Turboprop), newest first.
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 jasc_code = '7200' 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 jasc_code = '7200' 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 CA151116003Governor · malfunctioned(CAN) PILOT REPORTS, DURING T/O RUN FLUCTUATIONS ON LT PROPELLER RPM AND TORQUE, ABORTED TAKEOFF AT APPROXIMATELY 90 KTS. FAULT CODES 1504, 1505 AND 968 CHB RETRIEVED FROM CDS FOR ENGINE NUMBER 1. FAULT CODES CLEARED AND ENGINE RUNS PERFORMED, NO ABNORMAL FSDR AALA201511109002Engine · power lossON TAKEOFF ROLL, ADVANCED THRUST LEVERS, NR 1 ENG DID NOT SPOOL UP, REJECTED, SLOW SPEED, TAKEOFF. GOT 'AUTO FLIGHT AUTO THRUST OFF ECAM. RETURNED TO GATE. ACCOMPLISHED OPERATIONAL TEST OF THE ENG & AUTO THRUST SYS ISOLATION IAW AMM TASK 22-30-00-710-003A. SDR CA151117013Engine · malfunctioned(CAN) WHILE COMPLETING THE FLIGHT AND PERFORMING THE PARKING SPOT CHECKLIST, THE ENGINE MODE SWITCHES, WERE SELECTED TO IDLE AND THE CREW IMMEDIATELY RECEIVED A NR 2 DC GENERATOR CAUTION MESSAGE FOLLOWED BY ENGINE OUT AURAL MESSAGE. THE COMPRESSOR SPEED, NG, SDR CA151117012Engine · smoke(CAN) DURING TAKEOFF, THE ENGINE LOST POWER AND SMOKE CAME INTO THE CABIN WITH THE OIL TEMPERATURE NOTED TO BE AROUND 120 TO 140 DEGREES. TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE RAMP. POST EVENT INSPECTION FOUND THE PRESENCE OF OIL IN THE BLEED VALVESDR CA151117008Engine · leaking(CAN) A PROBLEM OF OIL ODOR IN CABIN WAS FIRST REPORTED ON A FLIGHT AND RE-OCCURRED. TROUBLE SHOOTING THE BLEED VALVE AND SWITCHING VALVES WERE REMOVED AND PRESENCE OF OIL WAS FOUND. THE ENGINE WAS CLEANED AND SERVICED AND A GROUND RUN PERFORMED DURING WHICH SDR CALA2015110694798Engine · overtempDURING CLIMB NR 1 ENG HAD EGT EXCEEDANCE, CREW REPORTS IN THE MID 700`S. AHM SHOWS 710.5. DURING CLIMB & HOLDING PATTERN ENG WOULD ONLY PROVIDE 1/3 AMOUNT OF POWER AS RT ENG. REPLACED ENG IAW 71-00 -02. REMOVAL REQUIRED FOR HPT AIRFOILS METALLOGRAPHIC ANALSDR ASAA2015110113589Engine · faultedNR 1 ENGINE "ECONOMIC" FAULT 73-31371 "UPPER EGT SECTORS READING HIGH" FOUND DURING RECENT FAULTS, ESN 894-851, CORRECT/REPAIR WITHIN 500 FLT HOURS. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2015110113588Engine · faultedNR 2 ENGINE: FOUND MSG 75-10392. THE VSV POSITION SIGNAL IS OUT OF RANGE. LONG TIME FAULT. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2015110113587Engine · faultedNR 2 ENGINE: FOUND MSG 75-10442. THE VBV POSITION SIGNAL IS OUT OF RANGE. LONG TIME FAULT. ACFT GROUNDED,ON DEFERRAL.SDR CA151117006Engine · power loss(CAN) THE ENGINE POWER ROLLED BACK IN FLIGHT UNDER UNKNOWN CIRCUMSTANCES. TROUBLESHOOTING IS ON-GOING.SDR 2DYA20151030014Fluid · leakingON TAXI OUT FOR DEPARTURE, MX NOTICED FLUID LEAKING FROM LT ENG. PILOT FROM ACFT BEHIND N251 MADE CONTACT WITH N251 CREW & REPORTED FLUID LEAK. AS ACFT WAS PREPARING TO RETURN TO GATE, PILOT FROM ACFT BEHIND N251 TOLD N251 CREW THAT LT WING & ENG WAS ON FIRESDR DCGA2015FA0000520Engine · making metalENGINE CHIP LIGHT ILLUMINATED DURING TOUR FLIGHT. THE PILOT LANDED ACFT AND CALLED MAINTENANCE. MAINTENACE FOUND METAL FLAKE MEASURING LESS THAN .03125 ON UPPER AND LOWER ENGINE CHIP PLUGS. AFTER CLEANING THE PLUGS A 30 MINUTE GROUND RUN WAS PERFORMED AND THSDR CA151030018Engine · power loss(CAN) THE CREW ABORTED TAKEOFF DUE TO POWER ROLLBACK ON THE NR 2 ENGINE. NO OTHER DETAILS ARE AVAILABLE AT THIS TIME. TROUBLESHOOTING IS ON-GOING.SDR ASAA2015102813549Engine · faultedFOUND FAULT NR 2 ENGINE, MSG NR 77-20862, THE BOTTOM LT EGT SIGNAL, T49553 IS OUT OF RANGE. " ECONOMIC FAULT " TO BE REPAIRED WITHIN 500 FLT HRS. ACFT GROUNDED. ON DEFERRAL.SDR WRNA201511280001Engine · shutdownDEPARTING NR 1 ENG LOST POWER, ALL OF ITS PARAMETERS DISPLAYED IDLE ON ECIAS. POWER RECOVERED IMMEDIATELY, MINUTES LATER SAME ENGINE LOST POWER AGAIN DURING CLIMB OUT. ALL ENGINE DISPLAYED IDLE ON ECIAS BUT THIS TIME POWER WAS NOT RECOVERED. ENGINE CHECKLISSDR WRNA201510290031Engine · shutdownNR 1 ENGINE LOST POWER, ALL OF ITS PARAMETERS DISPLAYED IDLE ON ECIAS. POWER RECOVERED IMMEDIATELY. MINUTES LATER SAME ENGINE LOST POWER AGAIN DURING CLIMB OUT. ALL ENGINE PARAMETERS DISPLAYED IDLE ON ECIAS BUT THIS TIME POWER WAS NOT RECOVERED. ENGINE CHECSDR FDEA201510283394Engine · malfunctionedAFTER TAKEOFF, AFTER 1000' AGL, CLIMB MODE, LT ENG EPR SURGED +/- 0.10% TOTAL OF 0.20 EPR, N1 BOUNCING +/- 10%. QRH ENG LIMIT OR SURGE OR STALL CHECKLIST. AT 50% N1 ENG STABILIZED. INSPECTED PITOT HEADS ON LT SIDE, FOUND TWO HEADS MISSING. INSPECTED RT SSDR CA151030017Engine · power loss(CAN) APPARENTLY THE AIRCRAFT GLIDED DURING THE APPROACH. THE FSR OFFERED ASSISTANCE TO THE OPERATOR AND AUTHORITY. UPDATE #1: THE INVESTIGATOR IN CHARGE REPORTED FSR THAT THE SEQUENCE OF EVENT WAS THE ENGINE LOST POWER DURING FINAL APPROACH, VIBRATION FELT VSDR CA151030013Duct · contaminated(CAN) CUSTOMER HAS REPORTED EXPERIENCING ODOR OF BURNED OIL DURING DESCENT. ODOR REPORTED TO HAVE BECOME STRONGER WHEN TEMPERATURE IS WARMER BUT DID NOT SEEM TO DEPEND ON POWER SELECTION. ACFT IS CURRENTLY AT A MAINTENANCE FACILITY AND DURING INSPECTION OIL SDR ASAA2015102713543Engine · faultedNR 2 ENGINE ECONOMIC FAULT CODE 73-31372 GENERATED ON FLT 2 ONLY OF LAST 10 FLTS. UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. ON DEFERRAL.SDR CA151030011Engine · unknown(CAN) DURING A CLIMBING, RT TURN AFTER TAKEOFF, UPON REDUCING POWER AT APPROXIMATELY 800 TO 900 FT, THE CREW HEARD AND FELT A LOUD NOISE. THE ENGINE PARAMETERS WERE NORMAL. THEY ELECTED TO RETURN TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADE.SDR AALA201510279003Engine · leakingDURING DECENT, CABIN FILLED WITH AN ACRID ODOR. BARELY NOTICED IN THE COCKPIT, BACK VERY STRONG AT REAR GALLEY & BULKHEAD. ODOR RESULTED IN HEADACHES & BURNING NOSES AS REPORTED BY THE CREW. ACCOMPLISHED JC 33L00021001 & TSM TASK 49-00-00-810-831 FOR FUMES SDR CA151030012Engine · shutdown(CAN) DURING CRUISE THE ENGINE SUFFERED AN IN-FLIGHT SHUTDOWN. TROUBLESHOOTING & ENGINE REPLACEMENT IN PROGRESS. NO FURTHER DETAILS OF THE EVENT AT THIS TIME.SDR CA151027001Engine · power loss(CAN) FLIGHT CREW NOTICED LT BLEED FAIL DURING TAKEOFF, JUST AFTER, THE LT TORQUE DECREASED ALONG WITH THE LT PROP RPM. THE ITT STARTED TO INCREASE BEFORE THE CREW SHUTDOWN THE ENGINE. ACFT RETURNED BACK TO THE AIRPORT WITHOUT ANY FURTHER INCIDENT, THE ENGINSDR SWAA2015102645380Engine · malfunctionedINFLIGHT SHUTDOWN, AIR TURN BACK, DECLARED EMER. AT ROTATION, RT ENG SURGED & STALLED, BANGING NOISE, RETARDED THROTTLE. RAN QRH SINGLE ENG & APPROACH. EGT INDICATION WENT RED 965 DEGREES. FLIGHT ATTENDANT REPORTED FLAMES FROM ENG. R & R NR 3 MOTOR ASSEMBSDR FXGA201510280001Engine · contaminatedENGINE CHIP LIGHT CAME ON DURING TAXI. SHUTDOWN ACFT. FOUND LARGE AMOUNT OF METAL PARTICLES ON RGB & AGB CHIP DETECTORS. ALSO PERFORMED ENG OIL FILTER CLEANING & OIL SAMPLE FOUND METAL PARTICLES. WHEN TURNING PROPELLER YOU COULD FEEL GRINDING & RATCHETING SDR CA151030005Engine · overtorqued(CAN) DURING LANDING PHASE, WITH POWER LEVERS SET AT 45, THE RT ENGINE FUEL FLOW AND HIGH PRESSURE COMPRESSOR SPEED, NH, STARTED TO INCREASE WITHOUT ANY PILOT INPUTS, THE ENGINE WENT IN OVERTORQUE CONDITION REACHING 129 PERCENT. THE PILOT INITIATED A GO AROUNSDR WRNA201510210001Engine · malfunctionedDURING APPLICATION OF TAKEOFF POWER, ENGINE NR 1 DID NOT ACCELERATE. DISCONTINUED TAKEOFF.SDR ASAA2015102113445Engine · making metalNON-MAGNETIC METAL PARTICLES FOUND IN NR 2 ENGINE AFT CHIP DETECTOR. ACFT GROUNDED. IAW MM 79-00-00-200-804, STEP 7H, 7, L, 27H, REMOVED NR 2 OIL SCAVENGE FILTER FOR ANALYSIS. INSTALLED NEW FILTER IAW MM 79-21-05. LEAK CHECK GOOD. ELECTRONIC ENGINE CONTROL SDR CALA2015102100864Engine · malfunctionedZERO OIL QTY & LOW OIL PRESS ON NR 1 ENG, FOLLOWED BY ENG SHUTDOWN. COMPLETED SINGLE APPROACH & LANDING. R & R NR 1 ENG IAW TASK CARD 64-7100-1-9800. PERFORMED ENG OPERATIONS CHECK IAW TASK CARD 64-7100-1-9802. ALL CHECKED GOOD.SDR CA151029018Engine · malfunctioned(CAN) DURING MORNING CHECKS, A DROP OF TORQUE BUG OCCURRED ON NR 2 ENGINE. THIS LED TO THE REPLACEMENT OF THE FADEC BEFORE THE ACFT WAS DISPATCHED. DURING A SUBSEQUENT FLIGHT, AN ENGINE SHUTDOWN OCCURRED UNDER UNKNOWN CIRCUMSTANCES. POST FLIGHT INSPECTION REVSDR CA151030003Engine · smoke(CAN) DURING FLIGHT, SMOKE ENTERED THE CABIN AND COCKPIT. THE CREW ELECTED TO DIVERT. AN UNEVENTFUL LANDING WAS MADE. POST FLIGHT INSPECTION REVEALED A SIGNIFICANT PRESENCE OF OIL IN HIGH PRESSURE SHUT OFF VALVE (HPSOV) AND ASSOCIATED DUCTING AS WELL AS LOW OISDR CA151030001Engine · malfunctioned(CAN) AN IFSD OCCURRED ON THE ABOVE AIRCRAFT. THE FLIGHT WAS DIVERTED AND IT LANDED SAFELY SINGLE ENGINE. NO OTHER DETAILS ARE AVAILABLE AT THIS TIME.SDR CA151021007Engine · smoke(CAN) FLIGHT CREW NOTICE SMOKE IN THE COCKPIT AND THE SMOKE DRILL WAS PERFORMED, BOTH FLIGHT CREW DONNED THEIR MASKS AND CONFIRMED THAT BOTH ON 100 % OXYGEN. THE BALANCE OF THE SMOKE DRILL ITEMS CARRIED OUT INCLUDING THE OPENING OF THE FORWARD OUTFLOW VALVE TOSDR CALA2015102094684Strut · defectiveABORTED TAKEOFF, POSSIBLE COMPRESSOR STALL, UNUSUAL NOISE. EDM DOES NOT CONFIRM A STALL OCCURRED. POWER ASSURANCE RUNS ACCOMPLISHED. LT & RT LOWER STRUT ASSEMBLIES REPLACED.SDR CA151029016Engine · contaminated(CAN) DURING DESCENT, WHEN BOTH POWER LEVERS WERE MOVED TO IDLE, A SIGNIFICANT AMOUNT OF SMOKE APPEARED IN COCKPIT WITH SMOKE FUME ODOR. AN UNEVENTFUL LANDING FOLLOWED AT DESTINATION. POST FLIGHT INSPECTION FOUND OIL INSIDE THE GAS GENERATOR AND INTERCOMPRESSOSDR EPUA20151022002Fuel Control · failedPILOT REPORT LOSS OF POWER & TORQUE FLUCTUATION IN CLIMB, LASTING FOR APPROX 5 SECONDS, THEN POWER SMOOTHED OUT. PILOT ELECTED TO RETURN TO DEPARTURE AIRPORT WITHOUT INCIDENT & REPORTED THE PROBLEM. INSPECTED ENG & ACFT FUEL SCREENS, FILTERS & SUMPED ALL FUESDR R61A201510170727Engine · power lossCREW NOTED THAT THE NR 2 ENGINE WAS NOT PRODUCING FULL POWER. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES IAW AMM WITH NO DEFECTS NOTED. ACFT IS GOOD FOR SERVICE.SDR CA151026007Engine · making metal(CAN) AIRCRAFT LOST NR 2 ENGINE OIL PRESSURE AFTER TAKEOFF OIL PRESS WARNING LIGHT ILLUMINATED, NR 2 ENGINE IN-FLIGHT SHUTDOWN CARRIED OUT, ACFT RETURNED TO DEPARTURE AIRPORT. MOC REPORT THE FOLLOWING, OIL PX DROPPED, OIL PX WARNING LIGHT, OIL TEMP HIGH 108C-SDR FDEA201510163252Cable · damagedREJECTED TAKEOFF DUE TO NR 3 ENGINE NOT SPOOLING UP TO TAKEOFF POWER. REJECT SPEED LESS THAN 80 KIAS NR 1 & 2 APPROX 103% N1, NR 3 STOPPED ACCELERATING AT APPROX 96 % N1 WHERE THROTTLE POSITION HAD NO FURTHER EFFECT. TROUBLESHOT IAW FIM 71-00-00-2 FIM AND ISDR AN3R2015101600001Bearing · failedENGINE REMOVED FROM ACFT AND SENT FOR EVALUATION. THIS LAST MAJOR ENGINE MAINTENANCE THAT WAS ACCOMPLISHED WAS A MAJOR PERIODIC INSPECTION PERFORMED ON 1/6/2008. TOTAL ENGINE TIME AT THAT TIME WAS 6408.3 HOURS AND THE ENGINE HAS OPERATED A TOTAL OF 1222.4 HOSDR CA151029011Engine · shutdown(CAN) DURING DESCENT THROUGH APPROXIMATELY 2500, THE ENGINE SHUT ITSELF DOWN FROM A SETTING OF 5-10 PERCENT ABOVE FLIGHT IDLE. THE WARNING INDICATIONS CAME ON WITH LOSS OF OIL PRESSURE, FUEL FLOW, N2 ETC. THERE WERE NO PROBLEMS SEEN DURING THE PREVIOUS 4.5 HRSDR 2015FA0000494Engine · making metalDURING GROUND RUN AFTER THE FIRST START OF THE DAY THE ENGINE CHIP LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE UPPER AND LOWER ENGINE PLUGS AND FOUND 1 SLIVER ON THE UPPER PLUG. A 30 MINUTE GOUND RUN WAS PERFORMED AND THE PLUGS WERE RECHECKED AND FOUND CLEANSDR FDEA201510143211Engine · faultyDURING CLIMB OUT PASSING FL 260, NR 3 N1 WENT TOWARD ZERO WHILE ACFT EXPERIENCED MODERATE VIBRATION. MOVED THROTTLE TO IDLE EGT & N2 APPEARED NORMAL & WERE SIMILAR TO 1 & 2 ENG, WHEN NR 3 THROTTLE WAS ADVANCED FROM IDLE, MODERATE VIBRATIONS WERE FELT. RAN SDR CA151029002Bearing · failed(CAN) DURING LANDING, A FIRE WARNING SOUNDED IN THE COCKPIT. THE PILOT DISCHARGED BOTH FIRE BOTTLES AND THE FIRE WARNING WENT OUT. GROUND INSPECTION REVEALED THAT NR 6 AND 7 BEARING EXTERNAL AREA SHOWED EVIDENCE OF FIRE AND WET OIL. THE TURBOMACHINE CHIP DSDR CA151013007Engine · fire(CAN) IT HAS BEEN REPORTED THAT THE CREW WERE PRESENTED WITH A NR 2 ENGINE FIRE DURING LANDING. THE CREW STOPPED THE ACFT ON RUNWAY AND ACTIVATED THE ENGINE FIRE EXTINGUISHER BOTTLE. MECHANICS ADVISE IT LOOKED LIKE A POSSIBLE OIL FIRE.SDR Z3EY2015FA0000551Bolt · missingDURING INDUCTION INSPECTION, IT WAS NOTED THE FRONT VSVA CRANKSHAFT HOUSING SUPPORT BRACKET WAS MISSING ONE MOUNTING BOLT AND THE BRACKET WAS HANGING DOWN BY 2-3MM. THE CUSTOMER CONFIRMS THAT THEY HAVE NO RECORD OF MAINTENANCE BEING PERFORMED IN THIS AREA. CSDR CA151029006Engine · malfunctioned(CAN) DURING TAKE-OFF, THE CREW FELT A BUMP FROM RIGHT SIDE OF THE AIRCRAFT. THE MASTER WARNING SYSTEM ANNOUNCED HIGH PRESSURE COMPRESSOR SPEED (NH) DROP WITH ENGINE ELECTRONIC CONTROL AND ENGINE PROPELLER CONTROL FAULTS. TAKE-OFF WAS ABORTED, POWER LEVER MOVESDR CA151013003Engine · malfunctioned(CAN) AIRBORNE RETURN TO DEPARTURE AIRPORT SHORTLY AFTER TAKEOFF DUE TO A MECHANICAL ISSUE WITH EGT EXCEEDED. ENGINE NR 1 REPLACED IAW TASK CARD 2-271A-01.SDR HALA2015101200209Engine · power lossAT 3500' HAD A LOSS OF NR 1 ENGINE POWER, EVENTUALLY LED TO A ENGINE GAUGES WERE ALL RED & WE SHUTDOWN ENGINE & F/A'S REPORT SURGING IN CABIN. AN UNEVENTFUL LANDING WAS MADE AT THE DEPARTURE. ENGINE CHANGE IN WORK.
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