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 AALA20150217024Blade · failedRT ENG EGT HIGH TEMP INDICATION ACCOMPANIED BY RAPID YAW TO THE RT. RT ENG SHUTDOWN. RETURNED & EMERGENCY DECLARED. LANDING WAS UNEVENTFUL. REPLACED THE RT ENGINE. FOUND HPC DAMAGE, C7 BLADE FRACTURED AT APPROX 2/3 SPAN, DETERMINED TO BE ROOT CAUSE OF FAILSDR DXTA2015021805982Engine · leakingON BREAKING GROUND, PRIOR TO GEAR RETRACTION, FIRST OFFICER CALLED SMOKE IN COCKPIT, SMELLED ELECTRICAL. TURNED PAC'S OFF CHANGED NOTHING. APPEARED TO BE COMING FROM FIRST OFFICER`S SIDE OF COCKPIT. INSPECTED APU NO OIL NOTED. ISOLATED OIL ODOR SOURCE COMSDR MASA2015021612908Engine · power lossNR 2 ENGINE LOST THRUST WITH A HIGH ITT & VIBE CREW SHUTDOWN ENGINE IN FLIGHT, EMERGENCY WAS DECLARED. THERE WAS NO BRACING BY PASSENGERS, ACFT LANDED & TAXIED TO GATE WITHOUT INCIDENT. ENGINE REPLACEMENT WILL BE REQUIRED DUE TO HIGH ITT. THERE ARE NO VISUSDR DALA2015021601246Engine · making metalDURING FLIGHT, DIVERTED DUE TO RT ENGINE OIL FILTER EICAS MESSAGE. INDICATION DID NOT EXTINGUISH WITH THROTTLE AT IDLE. ENGINE WAS SHUTDOWN IAW QRH. MAINTENANCE FOUND OUT OF LIMITS METAL IN MAIN OIL FILTER, MASTER CHIP DETECTOR AND NR 5 BEARING CHIP DETECTORSDR BUEA20150214001Bearing · failedDURING CLIMB TO FL290, AT ABOUT FL220, SMELLED SMOKE, NOTICED THE ITT RISING & WENT INTO RED. PULLED THE THRUST LEVER BACK AND THE NR 2 ENG OUT POPPED PUT ON THE EICAS. DECLARED AN EMERGENCY & DIVERTED. LANDING UNEVENTFUL. AFTER ENG SHUTDOWN A LOSS OF SISDR CA150224010Engine · malfunctioned(CAN) THE PLANE CRASHED SHORTLY AFTER TAKEOFF AS A RESULT OF A REPORTED TECHNICAL ISSUE. PRELIMINARY INFORMATION IS STATING ENGINE TROUBLE OCCURRED JUST AFTER TAKEOFF AND THE CRASH IS DESCRIBED AS A FORCED LANDING.SDR CA150218008Engine · flamed out(CAN) DURING TAXI TO THE DE-ICE BAY NR 1 ENGINE FLAMED OUT WITH NO WARNING INDICATIONS, PRIOR ISSUES OR SOUNDS. TROUBLESHOOTING DID NOT REVEAL ANY COMPONENTS AT FAULT. BORESCOPE OF THE ENG CARRIED OUT WITH NO DAMAGE FOUND. FUEL SYS CHECKED FOR WATER, FILTERSDR FDEA201502120515Engine · vibrationON TAKEOFF, ACFT STARTED VIBRATING VERY BADLY. FELT MORE LIKE AN AIRFRAME FLUTTER RATHER THAN ENG VIBRATION. CHECKED ENG PAGE, ALL NORMAL. CLIMBING THROUGH 2500' PULLED THROTTLES BACK & FLUTTER DECREASED. AS SPEED STARTED TO INCREASE FLUTTER INCREASED. SLSDR CA150224009Engine · making metal(CAN) RT ENGINE CHIP DETECTOR INDICATION ILLUMINATED IN FLIGHT. ACFT RETURNED TO BASE AND LANDED UNEVENTFULLY. THE CREW RETARDED NR 2 ENGINE TO GROUND IDLE, BUT DID NOT SHUTDOWN THE ENGINE. OEI OPERATION WAS APPROXIMATELY 25 MINUTES. CHIP DETECTOR REMOVED &SDR CA150217010Warning Light · illuminated(CAN) NUMBER 2 ENGINE CHIP CAS MESSAGE ILLUMINATED IN FLIGHT & STAYED ON.SDR CA150213002Engine · malfunctioned(CAN) PILOT REPORTED THAT AFTER TAKEOFF OUT OF KONT CLIMBING OUT OF FL 180 THEY HEARD A LOUD BANG ON RIGHT ENGINE AND NOTICED N1 ON RIGHT ENGINE DROP TO HALF OF LEFT ENGINE AND FELT THE A/C YAW. HAPPENED VERY QUICK AND THEN EVERYTHING CAME BACK TO NORMAL REST SDR CIER2201502111115Engine · shutdownRIGHT ENGINE SHUTDOWN IN FLIGHT AT 27.000 FT.SDR CA150224008Engine · leaking(CAN) DURING APPROACH, CREW REPORTED OIL ODOR IN COCKPIT AND PROCEEDED WITH AN EMERGENCY LANDING. FLIGHT COMPLETED AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED OIL ON HP COMPRESSOR AND ICC CASE.SDR CA150224011Seal · leaking(CAN) THERE WAS A STRONG OIL ODOR, ESPECIALLY DURING DESCENT. ODOR WAS STILL PRESENT IN THE COCKPIT AFTER LANDING. OIL WAS PRESENT IN BLEED SHROUD AFTER FLIGHT. THE RT ENGINE WAS REPLACED DUE TO NR 2 BEARING SEAL LEAK.SDR CA150224007Engine · malfunctioned(CAN) ACFT EXPERIENCED THE RT PROPELLER GOING TO FLAT PITCH SHORT FINAL, WITH ASSOCIATED YAW OF 35-40 DEGREES. FULL RUDDER AUTHORITY WAS UNABLE TO CORRECT THE YAW. A GO-AROUND WAS INITIATED. GIVEN THE VFR CONDITIONS THE ACFT RETURNED IN THE PATTERN FOR A SECSDR CA150224006Engine · malfunctioned(CAN) DURING CRUISE, FLUCTUATION OF TORQUE WAS WITHIN 5 PERCENT. AT TOP OF DESCENT ENGINE NR 2 TORQUE DROPPED TO ZERO AND ITT DROPPED BELOW 350, DEGREE C. THE PILOT COMPLETED IFSD PROCEDURES AND ACCOMPLISHED A SUCCESSFUL SINGLE ENGINE LANDING. MFCU AND FUELSDR ASAA2015020710578Fault Code · activatedWHILE ACCOMPLISHING TC 78273000, FOUND FAULT CODE 77-10852, "THE BOTTOM RT EGT SIGNAL, T49552 IS OUT OF RANGE ECONOMIC FAULT FAULTED ON NR 2 ENGINE. ACFT GROUNDED. REPLACED NR 2 ENGINE.SDR 29GA2015021000004Engine · out of adjustLT ENGINE AUTO COARSEN ON FINAL WITH AUTO COARSEN LIGHT ILLUMINATED. PERFORMED AUTOCOARSEN SYSTEM ADJUSTMENT TEST, AUTO COARSEN SYSTEM TEST NORMAL.SDR 29GA2015021600004Engine · out of adjustLEFT ENGINE AUTO COARSEN ON FINAL WITH AUTO COARSEN LIGHT ILLUMINATED. PERFORMED AUTOCOARSEN SYSTEM ADJUSTMENT TEST, AUTO COARSEN SYS TEST NORMAL.SDR ASAA2015020610577Fault Code · false activationNR 2 ENGINE SHOWS FAULT 73-31372, ECONOMIC, UPPER EGT SECTORS READING HIGH. LEG 3, ACFT GROUNDED. PERFORMED TC78273000. NO FAULTS FOUND ON NR 2 ENGINE.SDR ASAA2015020610574Warning Light · false activationENROUTE AT CRUISE THE NR 2 BLUE "ENG VALVE CLOSED" LIGHT ILLUMINATED AND STAYED ON BRIGHT BLUE NR 1 ENG FUEL FLOW 2.64, NR 2 ENG FUEL FLOW 2.63 ALL ENGINE PARAMETERS NORMAL NO OTHER INDICATION OF ANY ENGINE ABNORMALITY. MAINTENANCE & DISPATCH NOTIFIED VIA SATSDR CA150224005Engine · separated(CAN) THE ENGINE LOST POWER ON TAKEOFF. THE ENGINE WAS RIPPED FROM THE FUSELAGE AND THERE WAS TAIL AND WING DAMAGE.SDR SIMA20150204002Engine · failedLAVATORY SMOKE AFTER TAKEOFF, AOM 1 PROCEDURE COMPLIED WITH. FLIGHT ATTENDANT REPORTS SMOKE & FUMES IN CABIN. R & R NR 2 ENGINE IAW WC 71-000-00. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD. PERFORMED ETN-EM-72-034 FOR NEW ENG. NO SMOKE OR ODOR PRESENT.SDR AALA20150204012Engine · malfunctionedDURING CLIMB RT ENG OIL PRESSURE INCREASED TO 60 PSI, OIL QTY DROPPED TO ZERO & ENG SHUTDOWN. RETURNED & EMERGENCY DECLARED. LANDING UNEVENTFUL. R & R RT ENG POWER PLANT ENGINEERING REPORTS INTRUSION OF HOT AIR INTO THE NUMBER 4 & 5 BEARING COMPARTMENT WHICSDR DALA2015020400899Engine · failedFLIGHT RETURNED TO DEPARTURE WITH THE NR 1 ENGINE HAVING PROBLEMS. FLIGHT CREW REPORTED ALL PARAMETERS WENT TO -0-. THE NR 2 ENGINE WAS SHUTDOWN. MAINTENANCE FOUND METAL IN TAIL PIPE AND HAVE REPLACED THE ENGINE.SDR CA150224004Engine · failed(CAN) THE CUSTOMER CONTACTED THE FSR TO REPORT ENGINE IFSD, LOUD BANG FOLLOWED BY POWER LOSS. THE PILOT PERFORMED AN EMERGENCY LANDING ON A BEACH. POST-EVENT INSPECTION REVEALED THE COMPRESSOR FREE TO ROTATE, UNABLE TO TURN PROPELLER BY HAND, EXHAUST DUCT DISDR CA150224003Engine · malfunctioned(CAN) ENGINE SUFFERED AN IFSD AT 41,000 FT AND THE CREW PERFORMED A MANUAL RELIGHT. PILOT REPORTED COMPRESSOR SURGE EVENT WHEN TRYING TO GET FROM 41000 FT TO 43000 FT DUE TO WEATHER CONDITIONS. DESCENDED TO 37000 FT AND ENGINE RECOVERED AFTER REDUCING POWER SSDR CA150224002Engine · unresponsive(CAN) ENGINE WOULD NOT DECELERATE ON APPROACH. NO THROTTLE RESPONSE ON APPROACH AFTER 2HR FLIGHT. SUSPECT FROZEN P3 LINE.SDR JJBA20150203012Engine · malfunctionedWHILE IN DESCENT, BOTH ENGINES WENT TO FULL POWER BY THEMSELVES. PERFORMED ENGINE RUNS ON LT & RT ENGINE AT DIFFERENT POWER SETTINGS. PERFORMED GVI OF LT & RT PROP ASSEMBLY. NO DEFECTS NOTED.SDR ASAA2015020310540Fault Code · activatedNR 1 ENGINE HAS MAINTENANCE MESSAGE FAULT 76-31361. THE START LEVER SIGNALS DISAGREE, LONG TERM FAULT. ACFT GROUNDED. OPENSDR N6WA2015020301Engine · power lossHIGH N1 VIBRATION ON NR 2 ENG, N1 DROPPED TO 50 % & RETURNED TO NORMAL ABOUT 5 SECONDS LATER. PERFORMED GVI OF NR 2 ENG INLET, EXHAUST & FAN BLADES. INSPECTED FOR PRESENCE OF CHIP DETECTOR CONTINUITY, NO DIC FOUND. PERFORMED GND POWER RUN WITH CREW. NO DEFSDR UIEA2015020200062Acoustic Panel · damagedDURING WALK AROUND INSPECTION FOUND LT ENG FAN MID OUTER LINER ACOUSTIC PANEL PEELING & MISSING EXPOSING HONEYCOMB. DIMENSION 31 INCHES LONG X 1.2 INCHES WIDE, FOUND WITHIN LIMITS FOR CONTINUING SERVICE IAW AMM 72-00-00-206-167-H00 TABLE 640 & 642. LIMIT 10 SDR CA150202010Engine · stalled(CAN) INCIDENT DETAILS, AFTER LANDING & EXITING RUNWAY, NR 2 ENGINE STALLED. ENG 2 FADEC TEST CARRIED OUT, NIL FAULT. NIL EVIDENCE OF ANY DAMAGE IN INTAKE OR EXHAUST, AREA INSPECTED, NO ABNORMALITY. NR 2 ENGINE STARTED WITHOUT ANY FAULT, NIL NOTED IN PFR, CSDR CA150923008Engine · noisy(CAN) THE CREW REPORTED 3 POWERFUL DISTINCT NOISES ASSOCIATED WITH A SLIGHTLY LONGITUDINAL MOVEMENT OF THE AIRCRAFT DURING CLIMB PHASE. DURING THIS TIME THEY ALSO REPORTED THAT MOVEMENT OF THE POWER LEVERS HAD NO EFFECT ON THE ENGINES RESPONSE FOR A VERY SHORTSDR ASAA2015013010496Fault Code · false activationWHILE PERFORMING T/C 78273000 FOUND ECONOMIC FAULT MESSAGE 73-31372, UPPER EGT SECTORS READING HIGH ON NR 2 ENGINE. ACFT GROUNDED. ACCOMPLISHED TC 78273000, FAULTS NOT PRESENT.SDR CA150204010Engine · failed(CAN) THE ENG WAS RECEIVED FOR REPAIR & INVESTIGATION AFTER THE OPERATOR REPORTED A FLAME OUT DURING CRUISE & INFLIGHT SHUTDOWN. DURING THE OPERATOR TROUBLESHOOTING A LOUD MECHANICAL GRINDING NOISE WAS NOTED TO BE COMING FROM THE ANGLE DRIVE AREA OF THE TURBOSDR AWKA201501300001Engine · failedWHILE ON DEPARTURE & CLIMBING THROUGH FL190 THE FLIGHT CREW NOTED A LOUD BANG & VIBRATION, FOLLOWED BY A RED RT ENG EXCEEDANCE CAS MSG & THEN AN AMBER RT ENG VIBRATION MSG. THE PIC RETARDED THE RT ENG THROTTLE LEVER & THE VIBRATION DECREASED, BUT WHEN SLIGHTLSDR RAIA20151250001Engine · malfunctionedNR 1 ENGINE SHUTTERED AND OIL TEMP AND ITT INCREASED, OIL QTY WENT TO 3 AND EICAS SHOWED E1 EXCEEDENCE, ENGINE WAS SHUTDOWN. MAINTENANCE REPLACED NR 1 ENGINE, OPS CHECKED GOOD.SDR CALA2015012793024Engine · vibrationAT CLIMB POWER ENG 2 N1 VIB 2.7 WITH ENG 1 AT 0.4. ALSO ENG 2 EGT 570 DEGREES & ENG 1 AT 519 DEGREES. ACCOMPLISHED ON SHOT TRIM BALANCE IAW MT71-010, MM 72-31-11 & MM 71-00-00. TESTED NR 8. ALL INDICATIONS NORMAL, MAX N1 VIBE WAS 0.4 AT 85%.SDR DXTA2015012605968Engine · overspeedNR 2 ENGINE OVERSPEED 105.1 N1. FL400, ISA + 4, MACH.75 THROTTLE DID NOT CONTROL ENGINE. OVERSPEED SELECTED ON NR 2 ENGINE COMPUTER. PILOT MANUALLY SHUTDOWN ENGINE. PUNGENT OIL ODOR JUST PRIOR TO ENGINE SHUTDOWN. TROUBLESHOT CAUSE OF NR 2 ENGINE N1 OVERSPEESDR CA150205003Engine · malfunctioned(CAN) PILOT REPORTED THAT DURING THE DESCENT, WHEN PASSING FL250, THEY HEARD A NOISE ON THE ENGINE NR 2, WHILE BOTH ENGINES WHERE BELOW CRUISE POWER. THE AIRCRAFT DIVERTED. DURING THE TROUBLESHOOTING, BOTH ENGINE SPOOLS (LOW AND HIGH POWER) ROTATED NORMALLY. ASDR ASAA2015012210402Shim · worn24 EA FAN BLADE SHIMS ON NR 1 ENG REQUIRE REPLACEMENT. ACFT GROUNDED. R & R 24 EA FAN BLADE SHIMS ON NR 1 ENG IAW TASK CARD 78472002.SDR ASAA2015012210401Engine · faultedFAULT CODE 73-31372, UPPER EGT SECTORS READING HIGH FOUND FOR NR 2 ENG ON T/C 78273000. ACFT GROUNDED. WHILE PERFORMING THE RE-ACCOMPLISHMENT OF TC 78273000, FOUND NO FAULTS FOR THE NR 2 ENGINE. THIS PLT IS CLEARED AS AN INTERMITTENT FAULT.SDR CA150205006Engine · failed(CAN) FOLLOWING THE REPLACEMENT OF THE LEFT PROPELLER PALE A TEST FLIGHT WAS PERFORMED. DURING THE FLIGHT TEST, THE CREW STARTED THE ENGINE FAILURE PROCEDURE AND IN FLIGHT RELIGHT PROCEDURE WITHOUT RESULT. AFTER A SECOND ATTEMPT TO RELIGHT THE ENGINE WITHOUT SSDR CA150205002Engine · shutdown(CAN) AN UN-COMMANDED NR 1 ENGINE IN FLIGHT SHOWNDOWN OCCURRED DURING TAKE-OFF. IT WAS REPORTED A LOT OF NOISES, THEN 2 SECONDS LATER THEY HEARD "BANG" AND THE ENGINE STOPPED. SPEED WAS <60KT AND POWER SETTING WAS NOT SET 90 YET.SDR 2015FA0000057Carbon Seal · failedDURING DESCENT, CREW NOTICED SLIGHT RISE IN OIL TEMP AND PRESSURE IN NR 1 ENGINE, AND STARTED TO GET OIL SMELL AND HAZE IN THE CABIN. CREW SHUTDOWN NR 1 ENGINE AND DEPLOYED O2 MASKS AS A PRECAUTION AND LANDED WITH NO FURTHER PROBLEMS. SUBSEQUENT VISUAL INSPESDR VNAA2015011600026Engine · vibrationWHILE DESCENDING THROUGH 20,000 MSL, CREW REPORTED A VIBRATION AND THAT LT ENGINE INTERTURBINE TEMPERATURE (ITT) SPIKED AND ENGINE SHUTDOWN. ATTEMPT TO RELIGHT ENGINE WAS UNSUCCESSFUL. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSDR QMLA2015011615004Engine · contaminatedDURING THE FIRST FLIGHT SINCE ENG FLUSH, THE COCKPIT & CABIN FILLED WITH SMOKE. THE SMOKE WAS CONSISTENT WITH THE SMELL FROM RUNNING THE HEATER AFTER AN ENG FLUSH. INSPECTED BOTH ENGS FOR LEAKS & BURNED WIRING WITH NO DEFECTS NOTED. THIS WAS THE FIRST FLIGHSDR CA150120019Oil System · low pressure(CAN) HAD AN IFSD EVENT ON NR 1 ENGINE. AFTER THE CREW RECEIVED A LOW OIL PRESSURE WARNING 15-20 MIN AFTER TAKE-OFF. THE ENGINE REMOVED AND EN ROUTE TO SHOP.SDR CA150120018Engine · making metal(CAN) SHORTLY AFTER TAKE-OFF, WHILE GEARS WERE BEING RETRACTED, NR 2 ENGINE TORQUE WENT FROM 90 TO 70 PERCENT. APPROXIMATELY 5 SECONDS LATER, THE TORQUE DROPPED TO 40 PERCENT, THEN TO ZERO. FOLLOWED PROCEDURES AND SAFELY LANDED BACK AIRPORT OF ORIGIN. THE PREL
Back to JASC 7200