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 REXA2013011300152Engine · malfunctionedON FLIGHT 4134 (IAH - MEM) WHILE CLIMBING THROUGH 5,000FT HEARD A POP AND LOST THRUST (BOTH AT THE SAME TIME). NO INDICATIONS OF SPOOL, ITT WAS WITHIN LIMITS, ENGINE FAILURE. CREW SUSPECTED FLAMEOUT AND ATTEMPTED TO RESTART PER QRH. ENGINE DID NOT RELIGHT. SDR CA130128006Engine · malfunctioned(CAN) THE ACFT HAS BEEN PARKED OUTSIDE IN COLD WEATHER, AFTER THE LAST FLIGHT. IT WAS STARTED UP ON SUNDAY THE 15TH WHEN THE RUN AWAY OCCURRED APPROXIMATE 5 MIN AFTER THE START UP. THE ENGINE WAS RUNNING AT IDLE SPEED WITH THE PROPELLER IN FEATHERED POSITIOSDR ASAA2013011193644Shim · wornNR 1 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. CHECKED INLET AND EXHAUST FOR EVIDENCE OF FOD IAW MM 71-00-00-800-802. ACCOMPLISHED NR 1 ENGINE FAN LUBE IAW TASK CARD 78472002. INSPECTED ALL PLATFORM SEALS AND HARDWARESDR CA130128002Engine · making metal(CAN) PILOT GOT A CHIP DETECT ALARM ON ON THE NR 2 ENGINE. CREW APPLIED IMMEDIATELY AN ENGINE SHUT OFF PROCEDURE AND TERMINATED FLIGHT OEI AT CAEN WHICH IS LOCATED AT CHALAIR AVIATION MAINTENANCE SHOP WHERE THE PLANE IS MAINTAINED. AFTER LANDING ON GROUND INVESDR CA130111002Engine · malfunctioned(CAN) ALTITUDE FL210, AIRSPEED 210 KIAS TEST POINT ATS RELIGHT OF LT ENGINE PREAMBLE: FOLLOWING A SUCCESSFUL WINDMILL RELIGHT OF THE ACFT LT ENGINE IT WAS AGAIN SHUTDOWN IN THE FIRST STEP OF THE ATS RELIGHT PROCEDURE. DURING THE WINDMILL RELIGHT PROCEDURE ITSDR CA130110004Engine · failed(CAN) THE ENGINE MATED TO REDUCTION GEARBOX WAS RECEIVED FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED CATEGORY 4 HP VANE DAMAGE AND AN IN-FLIGHT SHUTDOWN. THE OPERATOR REPORTED THAT THE ENGINE LOST POWER DURING FLIGHT AND OIL PRESSURE DROPPED TO 0SDR YENA20130110009Engine · overtempFLT 677 JFK-LAX, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO PHX. AT CRUISE FL 360 LOUD BANG ACCOMPANIED BY IMMEDIATE LOSS OF POWER AND EGT OVER LIMIT ENGINE ONE. REMOVED AND REPLACED ENGINE NR 1 AS PER A320-71-00-20-400-040. ALL OPERATIONAL CHECKS OK.SDR SIMA20130110001Engine · power lossON FLIGHT 3422 THE CREW ABORTED TAKEOFF DUE TO GREATER 80 KNOTS TAKEOFF POWER LOSS ON NR 2 ENGINE AND LOSS OF NR 2 ITT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET FADEC 2A AND 2B, CLEAN CONNECTOR CHECK CORROSION ON CONNECTOR PER ROLLS ROYCE FIM 77-21-00-81SDR SIMA20130109038Frame · corrodedLT ENGINE FRAME FLANGE CORRODED OUT OF LIMITS. R & R LT ENGINE IAW WC 71-000-00.SDR USAA2013011100001Engine · malfunctionedFLIGHT 796, PHL-TLV - SHORTLY AFTER DEPARTURE THE FLIGHT CREW WAS ADVISED OF AN ODOR IN THE CABIN WHICH RESEMBLED A "HOT, ELECTRICAL" SMELL. THE ODOR DID NOT DISSIPATE, SO THE FLIGHT CREW CHOSE TO RETURN TO PHL AS A PRECAUTION. AN EMERGENCY WAS DECLARED AND SDR A6WA201301094006Engine · malfunctionedFLIGHT DEPARTED NORMALLY FROM DCA. CLIMBING BETWEEN 2000-3000FT MSL, WHEN THRUST LEVERS WERE ADVANCED FROM 85% N1 TO CLIMB SETTING OF AROUND 90% N1 CREW EXPERIENCED A SIGNIFICANT VIBRATION. CREW OBSERVED RIGHT ENGINE ITT SPIKE TO 980 DEGREES C AND DRAMATIC ESDR CA130128001Engine · power loss(CAN) NH UNCOMMANDED CHANGE FROM 65 PERCENT TO 75 PERCENT IN HOTEL MODE, PROP BRAKE UNABLE TO KEEP PROP STATIONARY.SDR ASMF201301003Engine · unknownAIRCRAFT RETURNED TO PLATFORM, LEFT ENGINE WOULD NOT START. FLIGHT CREW ACCOMPLISHED THE QRH 7.14 PROCEDURE, CONFIRMING FAILURE. MX PERSONNEL PERFORMED THE LT ENGINE START IAW MM 74-00-00 AND ENGINE LEAKING INSPECTION IAW MM 73-21-00, NO CONFIRMING FAILURE.SDR O9IA2012010700013Engine · power lossDURING CLIMB, CREW WAS BEGINNING LEVEL OFF AT 3000 FT. ATC REQUESTED CLIMB TO 4000 FT. CREW ADVANCED POWER TO APPROX 600HP. EXPERIENCED A COMPLETE POWER LOSS FROM LT ENGINE JUST AFTER BEGINNING OF CLIMB. NO INDICATIONS FROM INSTRUMENTS PRIOR. CREW MAINTASDR SIMA20130106004Plug · defectiveON FLIGHT 2812 THE FLIGHT ATTENDANT REPORTED ENGINE 1 SMOKING AFTER SHUTDOWN. THE FIRST OFFICER INSPECTED AND FOUND THE SAME SMOKE CONTINUED FOR SOMETIME. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED E1 SHAFT PLUG (AFT) IAW EMB 140 EO EM-72-7SDR CA130117004Engine · malfunctioned(CAN) DURING REVENUE FLIGHT, A FEW MINUTES AFTER TAKEOFF, THE PILOT NOTICED AN HIGH OIL PRESSURE IN THE RED BAND. THE PILOT REDUCED POWER AND EACH SUBSEQUENT TENTATIVE TO INCREASE POWER, THE MOP WAS CLIMBING IN THE RED ZONE. THE ENGINE WAS SHUTDOWN BY THE PILSDR GTIA20130104518Engine · fluctuatesPOWER FLUCTUATION DURING TAKEOFF. DURING CLIMB AT F 50 ACFT SUDDENLY YAWED ENGINE NR 1 EPR DROPPED TO ZERO ALONG WITH N1 THEN RECOVERED IT APPEARS THE ENGINE LOST POWER THIS OCCURRED THREE TO FOUR TIMES THROUGH FL 70 WHERE DESCISION TO TURN BACK WAS MADE, DURSDR UALA2013010300033Engine · fodREPLACE NR 1 ENGINE ON ACCNT FOD DAMAGE. REMOVED OLD ENGINE, AND INSTALLED NEW ENGINE PER AMM. NEW ENGINE STILL REQUIRES HOOKUPS AND EXTERNAL COMPONENTS PER AMM.SDR CA130117008Engine · shutdown(CAN) 1 ENGINE EXPERIENCED AN IN-FLIGHT SHUTDOWN DUE TO AN UNCOMMANDED AUTOFEATHER .SDR CA130117006Engine · fluctuates(CAN) DURING REVENUE FLIGHT, THE ENGINE FUEL FLOW AND THE TORQUE WERE FLUCTUATING. THE PILOT ELECTED TO FOLLOW THE EMERGENCY PROCEDURE AND SECURED THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED.SDR CA130117003Engine · shutdown(CAN) DURING TAXI AFTER NORMAL ENGINE START THE NR 1 ENGINE SHUTDOWN ON ITS OWN. BEFORE SECOND ENGINE START ATTEMPT, EXECUTED A SHUTDOWN AND START CHECKLIST, BUT THE NR 1 ENGINE N2 NEVER WENT ABOVE 41 PERCENT.SDR UALA2012123107464Engine · making metalNR 1 ENGINE FAIL ON CLIMBOUT. NR 1 ENGINE CHIP DET CHECK ICN OFF FLT 890-31, 2706-1 ENGINE 222172 CHECK MAGNETIC CHIP DETECTORS FOR CONTAMINATION MM 79-22-01 P601. THIS IS DUE TO IN FLIGHT SHUTDOWN WITH MESSAGES THAT COULD BE CAUSED BY GEARBOX OR BEARING FAISDR CA130116004Engine · fire(CAN) DURING REVENUE FLIGHT, IFSD EVENT OCCURRED FOLLOWING AN ENGINE FIRE WARNING. AN UNEVENTFUL EMERGENCY SINGLE ENGINE LANDING WAS PERFORMED SUCCESSFULLY. DURING INSPECTION AND FOUND BURNED MARKS ON BOTH SIDES OF THE ENGINE NR 1 NACELLE.SDR CHQA20121226478Engine · leakingCREW REPORTED, RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER 1 ENGINE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR N6WA20121226001Engine · malfunctionedRIGHT ENGINE DEGRADED, CAUTION MESSAGE ON TAKEOFF. PERFORMED 3 ENGINE STARTS AND CLEARED FAULTS IAW AMM 72-00-00.SDR E3MA20121220004Engine · shutdownDURING APPROACH INTO A LANDING ZONE, THE NR 2 ENGINE SHUTDOWN. INDICATIONS ON THE CAD WERE A "FLI DEGRADE" AND A DELTA N1. THERE WAS NO TORQUE INDICATION ON THE VEMD.SDR CHQA20121222477Plug · damagedCREW REPORTED, RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THE FLIGHT ATTENDANT CONFIRMED A HAZY PRESENCE IN THE REAR OF THE CABIN AND THE CREW RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE SMELL TO ENGINE 1 AND THESDR AALA20121221011Engine · failedCLE - CREW REPORTED LEFT ENGINE FAILED AT ROTATION AND SHUTDOWN (SINGLE ENGINE TIME 25 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED CLE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT CLE ON 12/24/2012. SYSTEM GROUND CHECK NSDR 39LA2012122100001Unknown · unknownAT V1 AND CLIMB OUT NR 2 ENGINE TORQUE FLUCTUATED PLUS OR MINUS 5 PERCENT FROM TORQUE SETTING. FLUCTUATION WAS NOT AN INDICATOR ISSSUE. MALFUNCTION CONTINUED TO OCCUR WITH ENGINE CONTROL UNIT (ECU) SET TO NORMAL. NO OTHER INDICATIONS NOTED. PERFOMRED ENGINE SDR CA130116007Engine · malfunctioned(CAN) AFTER TAKEOFF AND WHILE LEVELING OFF, THE PILOT OBSERVED RAPID RISE OF ITT AND TORQUE ON NR 1 ENGINE. THE PILOT SHUTDOWN THE ENGINE AND LANDED BACK AT POINT OF DEPARTURE WITHOUT ANY FURTHER INCIDENT.SDR USAA2012122100003Engine · malfunctionedON TAXI IN, CREW REPORTED A NR 1 ENGINE OVERTEMP AND AUTO SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW J/C 26L40071004. OPS GROUND CHECK IAW 26L00071015 GOOD AT THIS TIME.SDR YENA20121218679Engine · malfunctionedFLT 1430 LGB-SFO, DECLARED EMERGENCY AND AIR RETURN TO LGB DUE TO OIL PRESSURE LOST ON ENGINE NR 2 DURING CLIMBOUT. REMOVED AND REPLACED ENGINE NR 2 AS PER TASK CARD A320-71-00-20-000-040. OPS CHECK GOOD.SDR WI5R20121218Blade · brokenDURING A PRE-BUY BOROSCOPE INSPECTION, IT APPEARED THAT AN IP ROTOR BLADE HAD BROKEN OFF AND GONE THROUGH THE CORE OF THE ENGINE. THIS WAS CONFIRMED UPON DISASSEMBLY. BLADE ON THE 3RD STAGE OF THE IP ROTOR WAS MISSING.SDR SWAA2012122110812Engine · malfunctionedON CLIMB POWER SET LARGE FLUCTUATIONS ON N1 AND N2. REMOVED AND REPLACED ENGINE PER MM.SDR ASOA2012122002686Engine · malfunctionedRT ENGINE VIBRATION, ITT SPIKE, AND LOOSE OF POWER AT ROTATION. FOLLOWED QRH AND RETURNED FOR LANDING. EMERGENCY DECLARED, ACFT RETURNED. R & R NR 2 ENGINE.SDR CA121228006Engine · shutdown(CAN) THE ACFT SUFFERED AN IFSD OF 1 ENGINE UNDER UNKNOWN CIRCUMSTANCES. COMPRESSOR DAMAGE WAS REPORTED. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION IS AVAILABLE.SDR JIKA2012121801Engine · malfunctionedDURING FLIGHT BETWEEN KHWD AND KBUR AT CRUISE ALTITUDE THE PILOT REPORTED THAT THE LEFT ENGINE SUDDENLY LOST POWER WITH NO WARNING OR NEGATIVE TRENDING INDICATIONS. ENGINE SPONTANEOUSLY STARTED SMOKING AND FLASHES OF LIGHT OF WHAT APPEARED TO BE SPARKS OR FIRSDR CA121218001Engine · shutdown(CAN) IN FLIGHT SHUTDOWN. THE PARAMETERS OF THIS ENGINE WERE NORMAL AT THE MOMENT OF SHUTDOWN.SDR CA130103008Engine · making metal(CAN) INFLIGHT ENGINE CHIP LIGHT. LANDED WITHOUT FURTHER EVENT.SDR CA121213001Engine · malfunctioned(CAN) DURING FLIGHT AT 1000 FT. PILOTS DID THE AFTER TAKEOFF CHECKS AND THE TORQUE WOULD NOT REDUCE WITH THE POWER CONTROL LEVER FROM AROUND 40 PSI. GEAR WAS LOWERED TO REDUCE AIR SPEED AND OPD RADIOED TO RETURN TO DEPARTURE AIRPORT IMMEDIATELY. A MAYDAY WASSDR HALA2012121000233Engine · hung startLEFT ENGINE HUNG START, N1 18.37. EGT 740. N2 56.47 F/F 1,200. REPLACED LT ENGINE MEC & LEAK CHECKED IAW AMM 73-21-01. REPLACED LT ENGINE T2 SENSOR IAW AMM 73-21-05. REPLACED CIT SENSOR. COMPLIED WITH ALL COMPONENT REPLACEMENT TESTS IAW AMM 71-00-00 TESTS SDR CA130222001Engine · overtemp(CAN) DURING TAKEOFF, THE ENGINE EXPERIENCED HIGH ITT, ON RED LINE. TAKEOFF WAS ABORTED. A DATA COLLECTION UNIT DOWNLOAD WAS CARRIED OUT AND IT SHOWS THAT THE ITT REACHED 754 C. TROUBLESHOOTING IS ON-GOING.SDR CA121210002Engine · odor(CAN) DURING DESCENT THE CREW NOTICED A STRONG CHEMICAL ODOR PERMEATING THROUGH THE FLIGHT DECK, ALSO THROUGH THE FORWARD PORTION OF THE PASSENGER CABIN. THE CREW DONNED THEIR OXYGEN MASKS FOR THE FINAL PORTION OF THE DESCENT AND APPROACH. ENGINE 1 REPLACESDR UALA2012120607050Engine · stalledNR 2 ENGINE STALL, RTFL. NEED TO ACP OVER WEIGHT LANDING CHECK. FLIGHT CREW REPORTED SMOOTH LANDING WITH A SINK RATE LESS THAN 200FPM. SAMC TEXT: REF MM 05-51-11. ACCOMPLISHED AMM 05-51-11, ALL CHECKS OKAY.SDR CHQA20121205451Engine · leakingCREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THEY REPORTED NO VISIBLE SMOKE WAS PRESENT, HOWEVER AN ODOR WAS PRESENT IN THE CABIN. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TASDR ASMF201212007Engine · smokeDURING ENGINE START, SMOKE WAS DETECTED FROM RT ENGINE. MX PERFORMED ENGINE LEAKING INSPECTION IAW MM 72-00-00, DETECTED OIL LEAK IN THE RT ENGINE FUEL PUMP DRAIN. RT ENGINE WAS RUN IAW MM 71-71-00, TESTS NR 3A/3B AND MM 79-00-00, NO LEAKS WERE DETECTED. ASSDR GTIA2012120517Engine · shutdownFLT 301 IS AIR RETURN TO DEPARTURE AFTER NR 2 ENGINE WAS SHUTDOWN IN FLIGHT IAW COM PROCEDURE, EMERGENCY DECLARED, & LANDED SAFELY.SDR CA121228001Engine · power loss(CAN) DURING CLIMB, A LOUD NOISE WAS HEARD, FOLLOWED BY A POWER LOSS AND LOW OIL PRESSURE WARNING. THE ENGINE WAS SHUTDOWN AND SECURED AND THE ACFT RETURNED TO THE DEPARTURE POINT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. NO DETAILS ON ENGINESDR CA121211002Engine · failed(CAN) FLIGHT CREW REPORTED THAT DURING CLIMB OUT FROM BEDFORD MA, ENROUTE TO FL, AT APPROXIMATELY 2000 FT ENGINE NR 1 MADE A LOUD POP NOISE AND SHUTDOWN. AFTER 2 FAILED INFLIGHT RESTARTS CREW ELECTED TO DIVERT AND ACCOMPLISHED SUCCESSFUL SINGLE ENGINE LANDINGSDR UHLA2012120400422Engine · leakingBURNT SMELL FROM AIR CONDITIONING SYSTEM DURING FLIGHT. LOSS OF 2 QTS OF OIL FROM E2. REMOVED AND REPLACED NR 2 ENGINE DUE TO OIL LEAKING, OPS CHECK GOOD.
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