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 CHQA20130728197Engine · odorDURING FLIGHT THERE WAS AN OIL BURNING ODOR IN THE COCKPIT WHILE USING BLEED SYSTEM 1 AND BOTH PACK SYSTEMS TURNED ON. THE ODOR WAS ONLY PRESENT IN THE COCKPIT AND CLEARED ON THE GROUND WHILE USING THE APU AS A BLEED SOURCE. LANDED WITHOUT INCIDENT. MX REPSDR YENA20130727162Engine · failedACFT ON 10 MILE FINAL, OBSERVED ECAM ENG 1 COMPRESSOR VANE FAULT AND EGT WAS AT 725 DEGREES , DELARED AN EMERGENCY. R & R ENGINE NR 1 IAW AMM 71-00-20-000-04A. OPS CHECK AND LEAKS OK.SDR CA130921003Engine · flamed out(CAN) SHORTLY AFTER TAKEOFF, THE ENGINE HAD MAGNETIC CHIP DETECTOR, MCD, WARNING. FROM THAT POINT, THE ENGINE STARTED LOSING POWER AND EVENTUALLY FLAMED OUT. THE CREW MANAGED TO SAFELY GLIDE AND LAND THE ACFT WITHOUT FURTHER INCIDENT. NO INJURIES OR ACFT DAMASDR CA130805009Engine · vibration(CAN) DURING CRUISE, THE ENGINES BEGAN TO VIBRATE. THE CREW DECIDED TO SHUTDOWN BOTH ENGINES TO REGAIN CONTROL OF THE ACFT. THE PILOT PERFORMED A RESTART ON BOTH ENGINE AND THEY RETURNED TO NORMAL OPERATION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUTSDR CA130805001Engine · overtemp(CAN) THE US NAVY REPORTED THAT THE ENGINE EXPERIENCED A HIGH TEMPERATURE FLUCTUATIONS JUST AFTER TAKEOFF. THE PILOT ELECTED TO RETURN TO THE BASE. DURING TAXI, THE PMU STATUS MESSAGE ILLUMINATED AND HIGH TEMPERATURE FLUCTUATIONS OCCURRED AGAIN. THE PILOT IMSDR HNAA2013072600432Engine · power lossAFTER TAKEOFF, SHORTLY AFTER GEAR RETRACTION, NR 1 ENGINE MADE A LOUD SOUND, THEN NOTICED NR 1 PROP AT APPROX 400 RPM AND TORQUE 125, PLUS FOR APPROX 30-60 SECONDS BEFORE CREW SHUTDOWN ENGINE, AUTOFEATHER SELECTED AND ARMED. NO UPTRIM INITIATED. INSPECTED NRSDR CA130805005Engine · failed(CAN) DURING REVENUE FLIGHT, THE CREW REPORTED SMOKE IN THE CABIN THAT SMELLED LIKE PLASTIC. THEY ALSO HAD A LAVATORY SMOKE CAUTION INDICATION. THE CREW DISCHARGED THE AFT CARGO FIRE BOTTLE. THEY DECLARED AN EMERGENCY AND LANDED SAFELY, AFTER WHICH THE PASSESDR CA130805004Engine · malfunctioned(CAN) AFTER TAKEOFF AND GEAR RETRACTED, THE NR 1 ENGINE PROPELLER SPEED, NP WENT TO APPROXIMATELY 400 RPM AND THE TORQUE INCREASED MORE THAN 125 PERCENT. THE CREW SHUTDOWN ENGINE AND RETURNED TO THE DEPARTURE POINT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WASDR CA130726008Engine · vibration(CAN) ENGINE WAS SENT FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED AN UNUSUAL SOUND FOLLOWED BY VIBRATIONS AFTER ROLLOUT. SUBSEQUENT TESTING ON THE GROUND REVEALED THE ENGINE HAD UNUSUAL, HEAVY VIBRATIONS VERY LOW IN THE RPM BAND, BEFORE GROUND ISDR CA130729013Engine · power loss(CAN) UPON STARTUP, THE CREW RECEIVED A WARNING OF "NO DISPATCH" FOR THE ENGINES. THE ACFT WAS COMPLETELY SHUTDOWN AND RE-BOOTED AND THE ISSUE WAS CLEARED. DURING THE SUBSEQUENT T/O, THE LT ENGINE POWER ROLLED BACK AND THE T/O WAS ABORTED. AS THE ACFT WAS TASDR CA130726016Engine · malfunctioned(CAN) IT WAS REPORTED THAT DURING TAKEOFF, A LOUD BANG CAME FROM THE LEFT ENGINE. TAKEOFF WAS ABORTED AND ACFT TAXIED BACK TO HANGAR. CYAN LT ENGINE MINOR FAULT CAS MESSAGE WAS POSTED BUT NO ABNORMAL ENGINE INDICATIONS WERE NOTED. CYAN DOWNLOAD FADEC CAS MESDR UALA2013072505230Acoustic Liner · damagedNR 2 ENGINE ACOUSTIC LINING ON OTBD FAN SECTION BEHIND BLOCKER DOOR PEELING UP 2 TO 3 FEET. APPROXIMATELY 30 SQUARE INCHES. MEASURED DELAMINATION TO OB "C" DUCT WALL TO BE 24 INCHES LONG AND 2 INCHES WIDE. TO BE WITH IN MT-78-010 LIMITS. TRIMMED OFF LOOSE MATSDR CA130729008Engine · odor(CAN) AFTER TAKEOFF, THE CREW REPORTED OIL ODOR AND THEN SMOKE IN THE CABIN. THEY REDUCED POWER AND THE SMOKE CLEARED. THE FLIGHT RETURNED TO THE DEPARTURE POINT WHERE AN UNEVENTFUL LANDING WAS MADE. THIS IS THE 2ND SUCH EVENT ON THIS ACFT, 1ST EVENT REPORTED SDR CA131021019Engine · power loss(CAN) FOLLOWING A NORMAL CLIMB TO FL190, THE ENGINE TORQUE ROLLED BACK TO ZERO AS THE PROPELLER SPEED DROPPED FROM 1500 TO APPROXIMATELY 500-600 RPM. THE PROPELLER WAS FEATHERED AND THE ENGINE WAS KEPT RUNNING AS THERE WAS NO INDICATION OF FIRE OR SERIOUS ENGSDR CA130729011Engine · power loss(CAN) 16 MINUTES INTO THE FLIGHT, THE CREW NOTICED A SLIGHT YAW OF THE ACFT, FOLLOWED BY AN UNUSUAL PROPELLER SOUND ON THE NR 2 ENGINE. TORQUE WAS INDICATING APPROXIMATELY 104.1 PERCENT AND RPM WAS INDICATING 500-540 RPM. THE CREW CALLED AN UNCOMMANDED AUTOFSDR SIMA20130720001Engine · smokeCREW RECEIVED A "LAV SMOKE" EICAS MESSAGE. F/A REPORTED SMOKE IN THE CABIN AND A WARNING AND HORN ON THE FIRE PANEL IN THE GALLEY. F/A REPORTED THE REAR OF CABIN FILLED WITH SMOKE. DECLARED AN EMERGENCY AND RAN THE AOM VOL 1 CHECKLIST. DIVERTED AND LANDED WISDR FDEA201307201602Pump · failedREJECTED TAKEOFF DUE TO NR 1 ENGINE ROLL BACK AT 95 KTS. R & R THE MEC AND FUEL PUMP.SDR CA130719005Engine · shutdown(CAN) AIRCRAFT HAD UN-COMMANDED SHUTDOWN OF ENGINE NR 1 ON ROTATION. EMERGENCY WAS DECLARED. ACFT LANDED SAFELY, BUT WAS OVERWEIGHT AT TIME OF LANDING.SDR DXTA2013071805451Engine · shutdown10 MINUTES AFTER DEPARTURE, LEFT ENGINE SHUTDOWN INFLIGHT, CLIMBING THROUGH 12,400 THE LT FADEC FAULTY ICAS ILLUMINATED. LT N2 INDICATOR TURNED RED BRIEFLY AND THE ITT HAD A 100 DEGREE SPLIT (L750/R850). 10-15 SECONDS LATER THE LT ENGINE SHUTDOWN. LT ENGINSDR CA130805007Engine · malfunctioned(CAN) AIRCRAFT LANDED AFTER POWER COULD NOT BE REDUCED. JUST PRIOR TO LANDING THE ENGINE WAS SHUTDOWN. FSR TO FOLLOW UP ON INVESTIGATION OF FCU WHICH MAY HAVE CONTRIBUTED TO THE EVENT, 140 HRS SINCE INSTALLED.SDR CA130729002Engine · power loss(CAN) AFTER DROPPING A SLINGED LOAD, THE NR 2 ENGINE FROZE AT HIGH TORQUE FOR 20 SEC. THE NR 1 ENGINE REDUCED POWER ACCORDINGLY BUT THE MAIN ROTOR OVERSPED TO 104 PERCENT. TROUBLESHOOTING IS ON-GOING.SDR CA130729007Engine · malfunctioned(CAN) THE ACFT WAS AT ABOUT 600 FT AFTER TAKEOFF WHEN THE TORQUE, FUEL FLOW AND POWER TURBINE SPEED BEGAN TO DECREASE ON THE NR 2 ENGINE. THE PROPELLER AUTO-FEATHERED AND THE CREW SHUTDOWN THE ENGINE, CLIMBED TO 1500 FT, COMPLETED THE CHECKLIST ITEMS AND DECLSDR CA130729001Torque Sensor · failed(CAN) TWO REJECTED TAKE OFFS WERE REPORTED DUE TO THE AUTOMATIC TAKEOFF POWER CONFIGURATION SYSTEM NOT ARMING. THE PILOT SAW THAT THE ENGINE ANALOG TORQUE GAGE INDICATED ZERO. TROUBLESHOOTING LED TO THE REPLACEMENT OF THE TORQUE SENSOR, AUTOFEATHER UNIT AND SDR UALA2013071605001Flex Hose · deterioratedNR 2 ENGINE LPT-HPT, TCC, ACC COOLING FLEX HOSE ( AT 3 O'CLOCK POS) DETERIORATED. HOSE BRANCHES OFF THE IGN COOLING DUCT. REPLACED TUBE ASSY.SDR CA130729006Engine · overtemp(CAN) DURING TAKEOFF OPERATION, THE NR 2 ENGINE WAS APPROACHING THE ITT LIMIT OF 800 DEGREES C. TAKEOFF WAS ABORTED AND THE ACFT WAS RETURNED TO THE RAMP.SDR REXA2013071301357Engine · failedSHORTLY AFTER TAKEOFF AND AT 4400 FT, RT ENGINE MADE A LOUD NOISE AND N2 WENT TO ZERO. SHORTLY AFTER, A HOT ICON POSTED. EMERGENCY DECLARED AND RETURNED TO DEPARTURE.SDR EVCA20130722045Engine · power lossPILOT STATED AFTER TURNING FINAL TO BASE, THE ACFT EXPERIENCED A PARTIAL ENGINE LOSS OF POWER (SIMILAR TO ROLLING THE ENGINE TO FLIGHT IDLE). THE ACFT WAS APPROX 80 TO 100 FT ABOVE THE GROUND AT ABOUT 40 KTS. THE PILOT MADE AN EMERGENCY LANDING WHICH RESULTESDR YENA20130711148Engine · failedDURING TAKEOFF ROLL, NR 1 ENGINE FAILURE OCCURED AT BRAKE RELEASE, APPROX 20 KNOTS BELOW VMCG. FLIGHT CREW PERFORMED A REJECTED TAKEOFF. R & R NR 1 ENGINE IAW AMM 71-00-20-000-04A, ALL OPS CHECKS AND HIGH POWER ASSURANCE RUNS WITHIN LIMITS.SDR CA130805002Engine · malfunctioned(CAN) DURING CRUISE, THE ENGINE TORQUE SUDDENLY DROPPED TO ZERO AS DID THE POWER TURBINE SPEED. THE PILOT REDUCED POWER TO FLIGHT IDLE AND MOVED THE ACFT POWER MANAGEMENT SYS TO MAX CLIMB TORQUE. AFTER A FEW SECONDS, THE ENGINE PARAMETERS CAME BACK TO NORMAL.SDR AALA20130710004Engine · vibrationLT ENGINE VIBRATION ON CLIMB OUT. REPLACED LT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR UALA2013071104854Liner · unsecureNR 1 ENGINE AT APPROX 9 O'CLOCK HAS SECTION OF ATTRITION LINER HAS LIBERATED. AFFECTED AREA IS ACTUALLY A PREVIOUSLY REPAIRED AREA THAT IS LOOSE.SDR CA130715011Engine · vibration(CAN) DURING CLIMB AFTER T/O, THE CREW RECEIVED A MASTER WARNING AND FELT VIBRATIONS ORIGINATING FROM THE NR 1 ENGINE. POWER WAS REDUCED, VIBRATION LEVELS DID REDUCE AND THE ACFT RETURNED TO THE DEPARTURE POINT WHERE AN UNEVENTFUL LANDING WAS MADE. POST FLIGSDR UALA2013070904768Engine · unknownDURING NR 1 ENGINE AUTO START, N1 STAYED STAGNANT AT APPROX 30 PERCENT, ENGINE NEVER STARTED. RAMP REPORTED FLAMES FROM TAIL PIPE, EEC NEVER AUTO CRANKED, NO ECAM MESSAGES. CHECKED INLET AND EXHAUST FOUND NORMAL. STARTED ENGINE TWICE IAW JRH2-40-1. FOUNDSDR CA130715010Engine · fluctuates(CAN) T/O WAS ABORTED DUE TO UN-COMMANDED POWER FLUCTUATIONS. NO OTHER DETAILS ARE AVAILABLE AT THIS TIME.SDR CA130715009Engine · malfunctioned(CAN) DURING TAXI BEFORE T/O, AFTER THE THRUST REVERSERS WERE CYCLED, THE ENGINE STARTED VIBRATING AND THE LOW OIL PRESSURE WARNING CAME ON. THE ENGINE WAS SHUTDOWN. UPON A RE-START ATTEMPT, THE ENGINE HUNG AT 25 PERCENT. SUBSEQUENT VISUAL INSPECTION OF THE SDR SIMA20130707008Carbon Seal · leakingFOUL ODOR WHEN NR 1 PACK WAS SELECTED AND ON ENGINE BLEED SOURCE ODOR IS LESS WITH APU BLEED SOURCE, AND GONE WITH THE PACK OFF. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED ETN-EM-72-034 AND DETERMINED ENGINE NR 1 BLEED TO BE THE SOURCE OF ODOR. FOLLOWING THSDR CA130715008Engine · overheated(CAN) DURING T/O, AS THE THROTTLE WAS ADVANCED TO MAX POWER, THE ENGINE TEMPERATURE ROSE IN THE OVERTEMP AREA AND THE PILOT ABORTED THE T/O, RETURNING TO THE GATE SAFELY. DATA READOUT CONFIRMED THAT AN OVERTEMP OCCURRED. TROUBLESHOOTING IS ON-GOING AND FOCUSISDR CA130715005Engine · power loss(CAN) DURING TAXI BEFORE T/O, THE ENGINE COULD NOT MAINTAIN LOW IDLE AND WAS UNRESPONSIVE TO THROTTLE MOVEMENTS. THE FLIGHT WAS CANCELLED AND THE ACFT TAXIED BACK TO BASE WHERE EXTENSIVE TROUBLESHOOTING ON-GOING.SDR UALA2013070804722Panel · damagedON 2 SRV WALK AROUND FOUND THREE GOUGES ON INLET COWL ACOUSTIC PANELS AT 7, 5 AND 10 O'CLOCK POSITIONS.SDR QMLA2013070513093Engine · making metalDURING A SCHEDULED ZONE INSPECTION, THE MECHANIC FOUND THE CHIP DETECTORS FOR THE NR 2 ENGINE WITH SMALL AMOUNTS OF METAL CHIPS ON ALL DETECTORS. HE THEN REMOVED THE OIL FILTER TO FIND METAL CHIPS AS WELL. AN OIL SAMPLE AND CHIPS WERE SENT TO LAB FOR TESTINGSDR CALA2013090490970Engine · bird ingestionDUE TO FAN BLADE DAMAGE ON NR 2 ENGINE CAUSED BY BIRD STRIKE. ACCOMPLISHED INSPECTION OF THE FAN BLADES PER AMM TASK 72-31-11-200-010-B 13. FOUND ONE BLADE WITH ALLOWABLE DEFLECTION LIMIT & EVIDENCE OF AN AREA OF 'RUB ON THE ATTRITION LINER.SDR CALA2013083090887Engine · malfunctionedCREW REPORTS HEARING & FEELING A SLIGHT VIBRATION (LIKE LOUD LAV MOTOR FLUSHING), FOLLOWED BY LT ENGINE OIL FILTER EICAS MESSAGE. CREW FOLLOWED QUICK REFERENCE HANDBOOK & REDUCED THROTTLE & LIGHT REMAINED ILLUMINATED. AS CREW STARTED ENGINE SHUTDOWN PROCEDURSDR CALA2013082990853Engine · shutdownNR 1 ENGINE INFLIGHT SHUTDOWN.SDR CA130715004Engine · malfunctioned(CAN) DURING DESCENT, THE ENGINE ACCELERATED UNCOMMANDED AS THE TORQUE, FUEL FLOW AND COMPRESSOR SPEED ACCELERATED OVER A 2 SECOND PERIOD. THE ENGINE THEN STABILIZED JUST ABOVE NORMAL OVER THE NEXT 8 TO 10 SECONDS AND THE APPROACH AND LANDING WERE PERFORMED WSDR CA130709012Engine · contaminated(CAN) ON APPROACH FLIGHT, CREW NOTICED A CHIP DETECTOR WARNING LIGHT ON THE RT ENGINE. ACFT LANDED WITHOUT A PROBLEM, MAINTENANCE WAS NOTIFIED. COWLS WERE REMOVED, CHIP PLUG PULLED, METAL WAS FOUND ATTACHED TO MAGNETIC PINS ON PLUG. ENGINE WAS REMOVED AND O/SDR CA130703004Engine · making metal(CAN) DURING FLIGHT, NG STARTED TO DETERIORATE, SLOW UN-COMMANDED DECELERATION. WHILE THE FUEL FLOW, WF AND TEMPERATURE, ITT, STARTED TO CLIMB. A COMMANDED FLIGHT SHUTDOWN WAS PERFORMED AFTER THE ENGINE TEMPERATURE REACHED 1027 OC WITH NG AT APPROXIMATELY 45 PSDR QMLA2013070213090Engine · power lossACFT DEPARTED. 7 MINUTES INTO FLIGHT, 1600 FT MSL, CLIMBING TO 2000 FT, FADEC FAULT CAUTION ILLUMINATED. BETWEEN 10 & 15 SECONDS LATER ACFT EXPERIENCED A VIOLENT LEFT YAW OF APPROX 45 DEGREES. AN AUTOROTATIVE DESCENT IMMEDIATELY INITIATED. DURING DESCENTSDR ASAA2013070295451Counterweight · failedLT ENGINE VIBRATION AT CRUISE 1.1, N,86.1 LT & RT. ACFT GROUNDED. ACCOMPLISHED TEST 14B FAN TRIM BALANCE NR 1 ENGINE SOULTION POS 13, REMOVE P-14 INSTALLED P09, POS 15, REMOVED P-14 INSTALLED P09, POS 21. REMOVED P-08, INSTALLED P-14, POS 28. REMOVED P08 INSDR QMLA2013070213088Engine · making metalENG CHP SEGMENT ILLUMINATED IN FLIGHT AND POWER WAS REDUCED TO LAND AS SOON AS POSSIBLE WHERE AARF RESCUE WAS ON STANDBY. LANDED AT HOME PAD WITHOUT FURTHER INCIDENT AND NOTIFIED MX. MX FOUND SMALL FLAKE ON CHIP DETECTOR AND SEVERAL FLAKES IN OIL FILTER BOWLSDR CA130715002Engine · malfunctioned(CAN) A LOUD NOISE FOLLOWED BY ENGINE SHUTDOWN OCCURRED. NO OTHER DETAILS ARE AVAILABLE AT THIS TIME.
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