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 TRBA20130223001Engine · failedCREW REPORTED THAT ON THE ON TAKEOFF ROLL, NR 2 ENGINE TOURQUE WENT TO 95 PERCENT. PREFORMED A HIGH ABORTED TAKE-OFF WHEN SPEED WAS GREATED THAN 70KTS. TAXIED TO GATE, A MOMENTARY FLASH OF LOW ENGINE OIL PRESSUERE WAS SEEN ON BOTH CAP & LOW OIL LIGHT ON NR 2 SDR TRBA20130223002Engine · unserviceableTHE CREW REPORTED THE FOLLOWING: PREFORMED A HIGH ABORTED TAKEOFF WHEN SPEED WAS GREATED THAN 70KTS. SPEED WAS AROUND 70 KTS, T/O WEIGHT WAS 45886. ON INITIAL T/O, POWER LEVERS WERE PLACED IN THE POWER SET NOTS. NORMAL PARAMETERS WERE OBSERVED AS WE CONTINUSDR SIMA20130223002Engine · malfunctionedON FLIGHT 3354 THE CREW REPORTED THAT A FEW SECONDS AFTER ROTATION THE FLIGHT ATTENDANT CALLED TO SAY SHE THOUGHT THERE WAS SMOKE IN THE CABIN AS SHE CALLED THE CREW GOT LAV SMOKE WARNING. COMPLETED THE CHECK LIST SHORTLY AFTER LANDING EICAS WARNING WENT OUT SDR CA130314011Engine · malfunctioned(CAN) ON CLIMB OUT, THE RT ENGINE TORQUE AND FUEL FLOW INDICATORS BEGAN FLUCTUATING, WITH A RISE IN ITT. BY THE TIME THE CAPTAIN CALLED, ALL INDICATIONS HAD REVERTED TO NORMAL AND HE REPORTED THAT THE FLUCTUATIONS LASTED UNDER 2 MINUTES. THE CAPTAIN REQUESTESDR UALA2013022501111Engine · surgesLOUD AIR NOISE AND SURGE DURING TAKEOFF AND LANDING. ON ARRIVAL INBOUND CREW REPORT LEFT ENGINE GOT NOISE AND SURGE DURING TAKEOFF AND DESCENT, CHECKED NO PL FAULT, NO EXISTING FAULT, NO FAULT HISTORY, AND NO EXCEED INDICATION. BOTH ENGINE RUN UP, CHECKED BLSDR V2JA201212180005Engine · failedCLIMBING OUT OF FL260 TO FL310, RT TORQUE DROPPED 20 PERCENT AND IMMEDIATELY ROSE BACK TO 97 PERCENT. A SLIGHT HIGH FREQUENCY VIBRATION WAS THEN NOTICED BY CREW. CLIMB WAS CONTINUED TO FL310. AT FL310 OIL PRESSURE DROPPED BELOW 90PSI ON THE RT ENGINE WITH AUSDR CA130311002Warning Light · illuminated(CAN) ON LANDING, THE LT ENGINE CONTROL FAULT CAS MESSAGE ILLUMINATED. IT WAS CLEARED AFTER THE ENGINES SHUTDOWN. ON NEXT FLIGHT, AT THE TAKEOFF ROLL FULL POWER THE LT ENGINE CONTROL FAULT CAS MESSAGE ILLUMINATED AGAIN. THE PILOT ELECTED TO ABORT TAKE OFF. SDR CA130221001Engine · malfunctioned(CAN) ENGINE WAS RECEIVED FOR INVESTIGATION AND REPAIR AFTER IT WAS DETERMINED THAT A DYNAMOMETER OVERSPEED FAULT CODE OCCURRED DURING TEST AT THE O/H FACILITY DURING. SUSPECT THAT THE ENGINE EXPERIENCED AN NP, PT ROTOR, OVERSPEED OF UNKNOWN MAGNITUDE. THESDR REXA2013022100363Engine · malfunctionedFLIGHT 3723, CREW REPORTED VIBRATION 2 CAUTION ON NR 1 ENGINE AND SHUT DOWN ENGINE DURING FLIGHT. DECLARED EMERGENCY AND LANDED SAFELY. REPLACED LT ENGINE ASSY AND AFT THRUST SHAFT IAW AMM 71-00-00-40-801. OPS AND LEAK CHECKED GOOD. ALL REQUIRED BRAKE IN RUSDR USAA2013022200001Engine · vibrationIN CRUISE FL 340 NR 2 N1 VIRBRATION BRIEFLY EXCEEDED 5 UNITS, THRUST REDUCED TO KEEP VIBRATION BELOW 5. VIBRATION LEVELS RETURNED TO NORMAL AT 11-12 THOUSAND FEET. PERFORMED VIBRATION SUMMARY, NO DEFECTS NOTED, INSPECTED FOR FOD DAMAGE, NONE FOUND, INSPECTEDSDR CA130311003Engine · flamed out(CAN) DURING DESCENT IN BAD WEATHER, ENGINE NR 1 FLAMED OUT, FOLLOWED BY A SUCCESSFUL RELIGHT. FLIGHT CONTINUED AS NORMAL AND THE ACFT MADE AN UNEVENTFUL LANDING.SDR YENA20130220049Engine · fireFLT 615 JFK-JAX, ENGINE NR 2 TAILPIPE FIRE EXTINGUISHED WITH PURPLE K DRY AGENT. REMOVED AND REPLACED NR 2 ENGINE ASSY PER TASK CARDS E190-71-00-01-400-801 + E190-71-00-01-000-801. LEAK CHECKS AND ENGINE RUNS ACCOMPLISHED, ALL OPS CHECK NORMAL.SDR UALA2013021900999Engine · shutdownAIRCRAFT RETURN TO GATE, PER CREW, AFTER NORMAL LEFT ENGINE STARTED AND STARTED RIGHT ENGINE. CREW NOTICE LEFT GENERATOR TRIPPED AND SAW THAT LEFT ENGINE AUTO-SHUT DOWN BY ITSELF. CHECKED EPCS PAGE, NO FAULTS DISPLAYED. NO FAULTS FOUND ON EICAS. NO ENGINE SDR UIEA2013021900092Engine · making metalFOUND METAL CHIPS IN TAIL PIPE OF NR 1 ENGINE. R & R NR 1 ENGINE IAW AMM 71-00-00 ENG RUN & LEAK CHECKS SATISFACTORY.SDR CA130225011Unknown · unknown(CAN) UPON RELEASING THE PROPELLER BRAKE, PILOTS HEARD AN ABNORMAL ENGINE SOUND AND SUBSEQUENTLY ODOR OF SMOKE IN THE COCKPIT & CABIN. THERE WERE PASSENGERS WERE ONBOARD, AND THEY EXITED THE ACFT IAW THE NORMAL EXITING PROCEDURES. TROUBLESHOOTING ONGOING.SDR SWIA201332842Engine · failedSMOKE TOILET EICAS MSG ON TAKEOFF AT 100 KNOTS. BLEEDS FROM ENGINES. ABORTED TAKEOFF. (FLT 4464) REMOVED AND REPLACED RIGHT ENGINE. P/N: CF34-3B1 S/N ON: 873691 S/N OFF: 872710.SDR CA130218009Engine · shutdown(CAN) AFTER NORMAL APPROACH AND LANDING, NR 1 ENGINE AUTO SHUTDOWN PRIOR TO EXITING THE RUNWAY ENVIRONMENT. UNABLE TO TAXI TO GATE ON SINGLE DUE TO SIGNIFICANT SNOW ON TAXIWAYS AND RAMPS. ACFT TOWED TO GATE. ASR TO FOLLOW.SDR UALA2013021800971Engine · making metalDUE TO METAL DEBRIS FOUND ON MAIN GEARBOX AND MAIN OIL FILTER, ENGINE MUST BE REPLACED PRIOR TO NEXT DEPARTURE. REPLACED NR 2 ENGINE PER MM. ENGINE S/N OFF 726665 S/N ON 727132.SDR QMLA2013021613025Engine · making metalPILOT REPORTED ENGINE CHIP LIGHT ILLUMIINATED JUST AFTER LANDING AND RETURNING TROTTLE TO IDLE. MX WAS CALLED AND A LARGE AMOUNT OF FLAKES WERE FOUND ON BOTH THE UPPER AND LOWER ENGINE CHIP DETECTORS. SOME FLAKES EXCEEDED THE MAXIMUM ALLOWABLE IAW MM 72, PARA SDR CA130225009Engine · leaking(CAN) THE OIL ODOR IN CABIN OCCURRED DURING THE DESCENT. A BORESCOPE INSPECTION SHOWED TRACES OF OIL ON THE HP IMPELLER. TROUBLESHOOTING ON GOING.SDR CA130225001Engine · stopped(CAN) FOLLOWING AN AGRICULTURAL APPLICATION WHILE RETURNING TO THE AIRPORT. THE ENGINE STOPPED AND THE ACFT CRASHED IN A FARM FIELD.SDR 39LA2013021800023Detector · unserviceableTHE NR 2 ENGINE FIRE AUDIO CAME ON AND THEN WENT OUT, NO OTHER INDICATIONS WHERE PRESENT. AFTER 30 SECONDS THE NR 2 ENGINE FIRE LIGHT AND AUDIO CAME ON FOR 2 SECONDS AND THEN WENT OFF WITH NO FURTHER INDICATIONS. AFTER THE FIRE LIGHT AND AUDIO CAME ON AGAIN SDR ASAA2013021593898Engine · fluctuatesAT CRUISE FL 200, FLUCTUATION IN NR 1 ENGINE N1 NOTED. COMPLIED WITH QRH PROCEDURES, REDUCED THRUST RETURNED N1 TO NORMAL CONDITION FOR DURATION OF FLIGHT. ACCOMPLISHED STEPS E. (4) & (5) OF FIM TASK 73-06, 809 IAW EA 800-71EA-09794 STEP 9. NO DISCREPANCIESDR CA130225008Engine · malfunctioned(CAN) THE ENGINE SHOWED UNCOMMANDED POWER ACCELERATION DURING THE TAKEOFF. THE PILOT USED THE BRAKES TO BRING DOWN THE SPEED AND BOTH BRAKES CAUGHT FIRE. INVESTIGATION IS ONGOING.SDR QMLA2013021313027Engine · failedAT START OF APPROACH, HAD A PROUNOUNCED YAW FOLLOWED BY NR 2 ENGINE LOW LIGHT COMING ON, OBSERVED ENGINE RPM CLIMB TO 110 PERCENT AND DROP OFF, ENGINE RPM FELL BELOW 20 PERCENT AS WELL. AUDIBLE WARNING ACTIVATED, LOST NR 2 ENGINE. DIVERTED TO AIRPORT AND EXECSDR ASOA20130213015HEngine · smokeAFTER TAKEOFF THE CREW REPORTED A LAVATORY SMOKE INDICATION IN FLIGHT. THE ACFT RETURNED AND LANDED WHERE MX DETERMINED THE SOURCE OF THE SMOKE TO BE THE NR 2 ENGINE. THE ACFT WAS FLOWN UNDER A SPECIAL FLIGHT PERMIT TO WHERE THE NR 2 ENGINE WAS REPLACED, ENGSDR HALA2013021300020Engine · malfunctionedRT ENGINE EPR, N1, N2, F/F ALL FLUCTUATE. CLIMB EPR 1.5 PERCENT, N1 .5 PERCENT, N2 .2 PERCENT, F/F 200LBS LESS IN CRUISE.SDR HNAA2013021300051Engine · smokeSMOKE IN CABIN REPORTED AFTER ENGINE START. R & R NR 2 ENGINE IAW WC 71-00-01R.SDR CA130225006Engine · odor(CAN) DURING THE PREPARATION FOR A FLIGHT, AFTER THE BLEED SELECTION WAS ON, LOW POWER, DISC OR START/FEATHER, IMMEDIATELY A BAD ODOR WAS NOTICEABLE OUT OF THE AIR CONDITION. THE ENGINE WAS STOPPED AND THE ODOR CEASES SLOWLY AND NO ODOR WAS NOTICEABLE WITH THSDR DALA1304221702Engine · failedRT ENGINE FAILED AT FL 360 0, OIL PRESSURE, 0 OIL QTY 18 QTS. ENGINE WIND MILLED 5-8 MINS BEFORW SHUTDOWN. WIND MILL PARAMETERS N1 20-25 PERCENT, N2 0.0 PERCENT. REPLACED ENGINE NR 2.SDR FDEA201302120329Unknown · vibrationENGINE VIBRATION NOTED IN CRUISE FLIGHT. CLIMB WAS NORMAL. AS POWER WAS REDUCED AT TOP OF CLIMB, VIBRATION WAS NOTED AND DETERMINED TO BE ENGINE NR1. VIBRATION WAS MOST PROMINENT AT APPROX 95 PERCENT NI. AT LOW POWER SETTINGS VIBRATION WAS LESS AND NO VIBSDR EHAA20130211002Engine · power lossFIFTEEN MINUTES INTO THE FLIGHT, THE NR 1 ENGINE EXPERIENCED A MOMENTARY POWER LOSS OF ABOUT TEN PERCENT TORQUE. ALL THE GAUGES INDICATED THE SAME AND THE ACFT YAWED IN THAT DIRECTION. THIS LASTED ONLY A SECOND OR TWO, BUT A FEW MINUTES LATER THE SAME THING SDR FDEA201302110317Actuator · failed"ON TAKEOFF ROLL AT APPROX 100KTS FELT NOTICEABLE THUD AND LOSS OF THRUST FOLLOWED BY AN ENGINE FAIL LIGHT -ANOTHER ACFT REPORTED FLAMES COMING FROM THE TAIL PIPE ON NR 2 ENGINE ON TAKEOFF -ALL ENGINE INDICATIONS NORMAL AFTER REJECT. NR 2 ENGINE TAILPIPE AND SDR DXTA2013021105280Solenoid · failedAFTER APPROX 15 MINUTES INTO FLIGHT, ALTITUDE FL180, THE LT ENG EFC CIRCUIT BREAKER TRIPPED, THE LT EFC ANNUNCIATOR ILLUMINATED WITH ASSOCIATIATED LOSS OF THRUST ON LT ENGINE AND A STRONG ODOR OF BURNED ELECTRICAL NOTED. THE ODOR CLEARED QUICKLY. REPLACED SDR CA130225003Engine · making metal(CAN) DURING THE TAKEOFF PROCEDURE, WHEN THE PILOT PASSED FROM FLIGHT IDLE TO FULL POWER, THE PILOT HEARD A LOUD NOISE AND HE DECIDED TO REDUCE POWER AND TAXIED THE ACFT BACK TO THE TERMINAL. DURING THE ON-GROUND INVESTIGATION, THE TECH FOUND METAL IN THE EXHSDR CA130218006Engine · failed(CAN) ON CLIMBOUT, FELT A BIG BANG- LT ENGINE N1 WENT TO 30 PERCENT AND ITT WAS AROUND 920 C. FOLLOWED QRH PROCEDURES AND SHUTDOWN LT ENGINE AND RETURNED TO ORIGIN. AFTER EXTENSIVE TROUBLESHOOTING MAINTENANCE R & R THE LT ENGINE.SDR SWIA201332792Engine · failedFELT A BIG BANG - LEFT ENGINE N1 WENT TO 30 PERCENT AND ITT WAS AROUND 920°C, SHUT DOWN THE LEFT ENGINE. (FLT 2958) REPLACED LEFT ENGINE IAW AMM P/N: CF34-3B1 S/N ON: 873869 S/N OFF: 873127 P/N: 755469E S/N ON: 1832/4738.SDR CA130212019Engine · malfunctioned(CAN) DURING THE SHORT FINAL, THE ACFT EXPERIENCED AN UNCOMMANDED ENGINE ACCELERATION. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE ACFT LANDED SUCCESSFULLY. THE ACFT WAS TOWED OFF OF THE RUNWAY.SDR UALA2013021100777Liner · missingNR 2 ENGINE, LOOKING FORWARD AT THE 8 O`CLOCK FAN POSITION IS A MISSING SECTION OF ATTRITION LINING. THIS MEASURED SECTION MISSING IS 1.5 X 2 IN. REPAIRED AND APPLIED ADHESIVE IAW MT72-017.SDR CA130214021Engine · failed(CAN) ON FEBRUARY 7, 2013, ACFT EXPERIENCED AN UNREPORTED STALL EVENT AT APPROXIMATELY FL340 FOLLOWED BY A FAILURE OF THE LT ENGINE. THE LT ENGINE INCURRED A CATASTROPHIC CONTAINED FAILURE OF THE HPT. THERE WAS NO DAMAGE FOUND IN THE COMPRESSOR SECTION. THE SDR CA130208007Blades · damaged(CAN) PILOT HAD JUST COMPLETED POWER CHECK FOLOWING DAY OF HELISKI OPS AND WHEN MECHANIC EXITED THE AIRCRAFT DURING ENGINE COOL DOWN HE HEARD A LOUD BANG FOLLOWED BY A GRINDING NOISE. SHUT ENGINE DOWN AND DISCOVERED A PROBLEM NEAR THE FRONT OF THE ENGINE. BOSDR VNAA2013020700005Engine · malfunctionedCREW REPORTED IN-FLIGHT SHUTDOWN OF NUMBER ONE ENGINE. SHAKER / PUSHER ACTIVATED AND FLIGHT SPOILER EXTENDED. NUMBER ONE ENGINE ITT AT 998 DEGREES WITH NO OIL PRESSURE. CREW DECLARED EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ANSDR ASAA2013020793850Unknown · unknownDIAGNOSTICS REPORTS NR 1 ENGINE CORE VIBRATION DATA INTERMITTENTLY REPORTS ZEROS FROM THE FRONT AND REAR SENSORS. AAVM STILL LOGS LOSS OF N2 SIGNAL, ALSO CDS LOGGED 31-63150, ENGINE 1 N2 RPM INVALID ON BOTH DEUS AS INTERMITTENT AND ON VARIOUS FLT LEGS. VERIFSDR CA130225005Engine · power loss(CAN) CUSTOMER REPORTED A POWER ROLLBACK ON THE LT ENGINE. DFDR DATA WAS EVALUATED BY CUSTOMER ENGINEERING AND IT WAS IDENTIFIED AS AN UNCOMMANDED AUTOFEATHER EVENT. THE AUTOFEATHER CONTROL UNIT (AFCU) WAS REPLACED.SDR CA130212017Engine · malfunctioned(CAN) DURING THE DESCENT AT 20K FT, THE PILOT REPORTED A HIGH FUEL FLOW AND TORQUE FLUCTUATIONS. THEY FLEW TO A LOWER ALTITUDE TO ELIMINATE A POSSIBLE ICING CONDITION WITHOUT CHANGE. THEY DIVERTED THE FLIGHT WHERE A UNEVENTFUL LANDING WAS PERFORMED. DURING SDR CA130212016Compressor · stalled(CAN) DURING THE TAKEOFF PROCEDURE, LOUD NOISE OCCURRED DURING THE ACCELERATION ASSOCIATED WITH A SEVERE VIBRATION NOTED BY THE PASSENGERS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE FBO. THE CREW HEARD WHAT THEY FELT SOUNDED LIKE A COMPRESSOR STALL, TSDR 39LA2013020600014Engine · power lossDURING THE TAKEOFF ROLL, IT WAS DETERMINED THAT THE RT ENGINE WAS NOT MAKING THE PREDICTED POWER. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT AND ACFT WAS TAXIED BACK TO THE RAMP FOR MX.SDR CA130212020Engine · fod(CAN) HAD A CHIP CAUTION ON RT ACCESSORIES GEARBOX DURING A FLIGHT. THE CREW SHUTDOWN AND SECURED THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. THE ON GROUND INSPECTION REVEALED DEBRIS ON MAGNETIC CHIP DETECTOR. NO OTHER CONTAMINATION ON OIL FILSDR UALA2013020400663Engine · malfunctionedFIRST START OF NR 2 ENGINE, ENGINE EGT WAS APPROACHING 535 DEG, N2 WAS HANGING AT ABOUT 42 PERCENT, START ATTEMPT WAS ABORTED. AFTER COOL DOWN SECOND START WAS ATTEMPTED, EGT STAYED WITHIN LIMITS, BUT ENGINE HUNG WITH ERRATIC FUEL FLOW. FUEL FLOW WOULD REACHSDR UALA2013020400662Engine · surgesON ARRIVAL FLT 941-29. CREW REPORTED THE LEFT ENGINE SURGED AND RUMBLED ON THREE DIFFERENT OCCASIONS. ALL THREE AT FLT LVL 28.0. AUTOTHROTTLES ON. ENGINE HAD NO EXCEEDENCES, EGT REPORTED TO BE HIGHER AND CLIMBING DURING ALL THREE EVENTS. ALSO DURING TAXI
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