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 CA130531011Engine · flamed out(CAN) DURING FLIGHT AT CRUISE FL360 .78M, ALL ENGINE INDICATIONS WERE NORMAL WHEN A CLIMB WAS INITIATED TO FL380. CLIMBING THROUGH FL370 THE RIGHT ENGINE ROLLED BACK TO IDLE. CONTINUOUS IGNITION WAS ACTIVATED BUT THE ROLL BACK CONTINUED. IN-FLIGHT ENGINE FAILSDR GNMA20130528001Engine · low torquePILOT PERFORMED PRE-FLIGHT CHECKS AND ALL OPERATIONS GOOD. ACFT STARTED DOWN RUNWAY AND LT ENGINE STARTED TO AUTOFEATHER AND ENGINE WOULD NOT GO TO FULL POWER. TAKEOFF WAS ABORTED AND ACFT WAS GROUNDED FOR FURTHER INVESTIGATION OF ENGINE DISCREPANCY.SDR UALA2013053003760Engine · stalledNR 2 ENG STALL, FLT DIVERTED.SDR HALA2013052700071Unknown · unknownRT ENGINE FLUCUATION WAS ONLY AT GROUND IDLE. ALL OTHER POWER SETTINGS NORMAL INDICATIONS IN ALL REGIMES. ACCOMPLISHED FIM TASK 73-21 FAULT TREE 816. NO FAULT FOUND. CONSTANT 28VDC READING, R & R FUEL PUMP IAW AMM 73-11-01. REPLACED MEC IAW MM 73-21-01, ASDR CA130603003Engine · power loss(CAN) DURING REVENUE FLIGHT, THE NR 2 ENGINE TORQUE VALUES WERE FLUCTUATING ERRATICALLY. THE PILOT DECIDED TO RETURN TO DEPARTURE. THE CUSTOMER IS ACTUALLY TROUBLESHOOTING THIS TORQUE ISSUE.SDR WI5R201308230002Blade · missingENGINE WAS FLAGGED FOR A POTENTIAL ISSUE. DURING BLEED SOURCE SELECTION FROM BOTH TO LT, A LOUD NOISE AND A SUDDEN RISE IN ITT ON THE LT ENGINE. TROUBLESHOOTING REVEALED A MISSING 3RD STAGE IP BLADE.SDR T17A20130524513Engine · flamed outENGINE FLAMEOUT IN FLIGHT. DECENDED IN ALTITUDE AND ENGINE WAS SUCCESSFULLY RESTARTED AT FL210.SDR AALA20130522028Engine · faultyCREW REPORTED ODOR THROUGH OUT CABIN AND FLIGHT DECK WITH M2 LAVATORY SMOKE DETECTOR SOUNDING. EMERGENCY DECLARED FLIGHT RETURNED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENGINE DUE TO OIL THROUGH OUT COMPRESSOR SECTION. SYS GROUND CSDR N6WA2013052203Engine · malfunctionedOBSERVED POWER LOSS ON NR 2 ENGINE AT ROTATION. OBSERVED ENGINE SURGING N1 FROM 80 TO 70 PERCENT, HEARD POPPING SOUND, SHUTDOWN ENGINE IAW QRH. R & R NR 2 ENGINE IAW AMM 71-00-00, SP-09 FOR COMPLETION OF RUNS AND RII'S.SDR CA130530001Engine · power loss(CAN) DURING DESCENT, THE PILOT REPORTED THAT THE ENGINE TORQUE DROPPED TO ZERO. SUBSEQUENT POWER LEVER MOVEMENTS HAD NO EFFECT AND THE ENGINE FLAMED OUT. APPROXIMATELY 12 SECONDS LATER, THE AUTO-RELIGHT RESTORED ENGINE POWER AND THE FLIGHT RESUMED NORMALLY. SDR CA130521014Engine · malfunctioned(CAN) DURING TAKEOFF, THE COCKPIT CREW NOTICED A LOUD NOISE FOLLOWED BY RAPID THRUST CHANGES ON THE ENGINE NR 2. THERE WAS NO ENGINE VIB INDICATION ON THE EICAS DISPLAYED.SDR UALA2013052203541Engine · failedRIGHT ENGINE PRI CONT STATUS. MESSAGES P(S) 351-23 ANS P(S) SVA OR FCU-EEC DID NOT SHOW WHEN IN ALT MODE. INF- :MESSAGES DISPLAYED ON EPCS PAGE WERE: P351-19 & HCC-EEC. RDF-P :REPLACED EEC STATOR AND EEC. NO HELP, FAULTS ONLY ON RH EICAS COMP ON PRI SIDE. TRSDR CA130529002Engine · making metal(CAN) DURING APPROACH, THE MASTER WARNING WENT OFF FOR A LT ENGINE LOW OIL PRESSURE. THE ENGINE THEN FLAMED OUT WITHOUT ANY CREW INPUT. THE ENGINE WAS SECURED AND A SINGLE ENGINE LANDING WAS ACCOMPLISHED AT DESTINATION. POST FLIGHT INSPECTION FOUND NUMEROUS SDR HALA2013052000063Engine · malfunctionedATB NR 1 ENG FAILURE, AUTO SHUTDOWN. ACFT MADE AN UNEVENTFUL LANDING AT THE ORIGINAL DEPARTURE STATION. REMOVED AND REPLACED NR 1 ENGINE. OP'S & LEAK CHECKED OK. OK FOR SERVICE.SDR CA130614003Engine · malfunctioned(CAN) THE CUSTOMER REPORTED A REJECTED TAKEOFF DUE TO ABNORMAL PARAMETER TORQUE FROM ENGINE NR 2 REACHING ONLY 72 PERCENT INSTEAD OF 90 PERCENT. THE SPEED WAS BELOW 70KTS. THE ON GROUND INVESTIGATION FOUND THE FAULT CODE 62 ON ENGINE NR 2 ELECTRONIC ENGINE CSDR CA130529001Engine · smoke(CAN) SHORTLY AFTER TAKEOFF, SMOKE CAME RUSHING INTO CABIN HOWEVER, NO ODOR WAS NOTICED. THE CREW TURNED OFF ALL BLEEDS AND THE SMOKE STOPPED ACCUMULATING, BUT REMAINED IN THE CABIN. THE ACFT DIVERTED TO WEST PALM BEACH WHERE A SAFE EMERGENCY LANDING WAS MADSDR CA130521012Engine · malfunctioned(CAN) CAPTAIN REPORTED LT TL JAM IN FLIGHT AT FL350 AT 92.5 PERCENT N1. DESCENT CONTINUED WITH TL JAMMED AT HIGH ENGINE N1 AND IAS 320 KNOTS. CONSIDERATION TO ENGINE FIRE PUSH WAS GIVEN, HOWEVER AT 7000 FT ALTITUDE TL FREED. LANDING CONDUCTED 2 ENGINES OPS.SDR CA130603004Engine · making metal(CAN) THE PILOT REPORTED THAT 5 MINUTES AFTER TAKEOFF DURING CLIMB HE FELT A SLIGHT VIBRATION AND THE OIL PRESSURE WENT MOMENTARILY IN TO THE YELLOW RANGE. THE PILOT MADE RIGHT TURN TO RETURN TO HOME BASE WITH THE LOP WARNING LLUMINATED AND A GROWL NOISE BEINGSDR 2013FA0000294Engine · making metalDURING FLIGHT, PILOT HEARD INCREASING "RUMBLING" NOISE. PILOT LANDED TO THE NEAREST LANDABLE SIDE APPROX 2 MIN AFTER THE NOISE STARTED. RUMBLING DECREASED SIMULTANEOUSLY WITH ENGINE LOAD. ENGINE CHIP CAUTION ILLUMINATED AT THE END. ENGINE HAS NOT BEEN RUN SDR CALA2013051500299Stator Vane · leakingOBSERVED FUEL LEAKING WHILE TAXI FOR TAKEOFF. REPORTED SUSPECTED FUEL LEAKING FROM NR 2 ENG, LEFT VSV LEAKING. SCEPTRE DOES NOT RECOGNIZE EMP C4547. REMOVED AND INSTALLED NR 2 ENG LT VSV ACTUATOR IAW AMM 75-31-01-0 00-801-F-00. OPS CHECK GOOD. ROTABLE PARTSSDR CALA2013051500297Vane · leakingGROUND CONTROL REPORTED SUSPECTED FUEL LEAKING FROM NR 2 ENGINE LEFT VSV LEAKING. REMOVED AND INSTALLED NR 2 ENGINE LT VSV ACTUATOR IAW AMM 75-31-01-0 00-801-F-00. OPS CHECKED GOOD.SDR CA130527001Engine · shutdown(CAN) DURING TAXIING, THE ENGINE HAD AN UNCOMMANDED SHUTDOWN. THE FLIGHT WAS CANCELLED AND THE ACFT RETURNED TO THE HANGAR FOR TROUBLESHOOTING WHICH IS ON-GOING.SDR NACA2013051000001Engine · failedNR 1 ENGINE FAILURE IN FLIGHT, ENGINE SHUT DOWN. REMOVED AND REPLACED ENGINE DUE TO TURBINE FAILURE.SDR FDEA201305100956Engine · surgesLEFT ENGINE EPR SURGED. .10 EPR DURING TAKE OFF ROLL WITH AUTOTHROTTLES ENGAGED. REJECTED TAKE OFF AT 80 KNOTS. PERFORMED IP/HP COMPRESSOR AIRFLOW CONTROL TEST MM REF 71-00-00-5-3 RAN ENGINES TO HIGH POWER AND LT ENGINE EPR WAS STEADY NO SURGING ACFT OK FOSDR CA130513007Engine · malfunctioned(CAN) THE PILOT WAS ON THE RUNWAY GETTING READY TO TAKEOFF. BOTH ENGINE THROTTLES WERE PUSHED TO MAX CRUISE BUT ONLY RT ENGINE WAS REACTING. AFTER 5 SEC WITHOUT ANY RESPONSE FROM LT ENGINE THE PILOT REVERT THROTTLES TO IDLE. AFTER SUCCESSFUL ENGINE GROUND RSDR UALA2013050903250Actuator · leakingNR 2 ENGINE STATOR VANE ACTUATOR LEAKING FUEL. REPLACED SVA PER AMM, OPS AND LEAK CHECK NORMAL.SDR AALA20130508037Transmitter · inoperativeLAX - INFLIGHT FAT-DFW. CREW REPORTED LEFT ENGINE COMPRESSOR STALL FOLLOWED BY SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE PRESSURATION TRANSMITTER. SYSTEMSDR UALA2013051003267Probe · bindingNR 1 ENGINE HPT SECOND STAGE ROTATING AIR SEAL PROBE BOSS WAS DIFFICULT TO REMOVE. REQUIRED PRYING AND TWISTING TO REMOVE. COULD NOT FULLY INSTALL NEW UNIT. BOSS HANGS UP ON THE LAST INCH OF INSTALLATION. BORESCOPED HOLE. NO DEBRIS FOUND. REPLACED TCA PROSDR VNAA2013050700004Engine · failedCREW REPORTED AIRCRAFT HAD SMOKE IN THE CABIN. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LEFT ENGINE AND OXYGEN EQUIPMENT PER AIRCRAFT MANUALS. CHECKS WERE PERFORMED PER THE AIRCRAFT MANUALS ANDSDR REXA2013050700870Engine · vibrationAIR TURNBACK DUE TO N2 VIBRATION AND IFSD.SDR QMLA2013050613063Sump · making metalDURING THE 20 HOUR INSPECTION OF THE CHIP DETECTORS IAW 13-7900-E0-432 FOUND METAL CHIP ON THE SUMP CHIP PLUG THAT EXCEDED THE LIMITS CALLED OUT IN MM.SDR JJBA20130506001Mfc · failedCREW REPORTED THAT NR 1 ENGINE TORQUE WAS FLUCTUATING EXCESSIVELY ABOVE 70 PERCENT TORQUE SETTING. THE ACFT RETURNED TO THE FIELD AND THE MX CREW REPLACED THE NR 1 MFC.SDR UALA2013050603140Engine · stalledSTALL DISPLAYED ON UPPER ECAM SCREEN DURING OFF IDLE ACCELERATION. ENGINE NOT SHUTDOWN. STALL OCURRED AT 210 DURING LEVEL OFF. RAN CHECKLIST. DID NOT REOCCUR. HEARD AUDIBLE STALL. TROUBLESHOOT PER TSM 71-00-00-810-809-A. REPLACED INEENG PER MT 71-01-SDR USAA2013050700008Actuator · inoperativeRIGHT ENGINE HIGH EGT DURING TAKEOFF, AT APPROXIMATELY 800 FT, HEARD A BANG, RIGHT ENGINE EGT EXCEEDED MAXIMIUM TEMPERATURE OF 635 DEGREES. REMOVED AND REPLACED VSV ACTUATOR. PERFORMED BORESCOPE INSPECTION WITH NO FINDINGS. REMOVED AND REPLACED NR 2 ENGINE OUSDR 2013FA0000668Bearing · failedENGINE CHIP LIGHT, DURING FLIGHT, PILOT HEARD INCREASING "RUMBLING" NOISE. LANDED TO THE NEAREST LANDABLE SITE, APPROX 2 MIN AFTER THE NOISE STARTED. RUMBLING DECREASED SIMULTANEOUSLY WITH ENGINE LOAD. ENGINE CHIP CAUTION ILLUMINATED AT THE END. AFTER REMOSDR 2013FA0000667Bearing · failedENGINE CHIP LIGHT DURNG FLIGHT, PILOT HEARD INCREASING "RUMBLING" NOISE. LANDED TO THE NEAREST LANDABLE SITE, APPROXIMATELY TWO MINUTES AFTER THE NOISE STARTED. RUMBLING DECREASED SIMULTANEOUSLY WITH ENGINE LOAD. ENGINE CHIP CAUTION ILLUMINATED AT THE END. SDR CA130508007Engine · shutdown(CAN) DURING ACFT PUSH BACK, PILOTS REPORTED BOTH ENGINES SHUTDOWN. THE ACFT RETURNED TO GATE. MAINTENANCE INTERROGATED MDC AND NFF, NO OTHER EICAS MESSAGES THAT COULD BE ASSOCIATED WITH DUAL ENGINE SHUTDOWN WERE PRESENT ON THE EICAS. MAINTENANCE ATTEMPTED ENSDR ASMF20130523007Unknown · vibrationCAPTAIN REPORTED THAT DURING CLIMB, THE LT ENGINE VIBRATION REACHED 2.8 UNITS AND DURING CRUISE THE VIBRATION WAS STABILIZED IN 2.3 UNITS. AIRCRAFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A TRIM BALANCE IAW AMM 71-00-00, TASK 71-00-00-700-847-G01, ASDR CA130502002Engine · shutdown(CAN) THE CREW REPORTED THE LT ENGINE SPOOL BACK AND AN UNCOMMANDED SHUTDOWN AFTER 30 MINUTES OF FLIGHT DURING CRUISE AT FL 330. DURING THE SHUTDOWN, THE CREW PERFORMED THE EMERGENCY CHECK LIST AND DESCENDED TO FL210 WHERE THEY PERFORMED A START. THE DURATIOSDR CA130527003Engine · fire(CAN) DURING TAKEOFF RUN, 10 KT BEFORE V1, THE FIRE ALARM ON ENGINE NR 2 CAME ON. THERE WAS SMOKE ON ENGINE EXHAUST BUT NO FIRE WAS VISIBLE. PILOT FIRED THE FIRE EXTINGUISHERS AND ABORTED TAKEOFF. ACFT WAS TAKEN TO HANGAR WHERE DAMAGE WAS NOTICED ON POWER TSDR CA130502001Engine · power loss(CAN) SHORTLY AFTER T/O, A LOSS OF ENGINE POWER OCCURRED AND THE A/C MADE A FORCED WHEELS UP LANDING IN AN OPEN FIELD. NO ONE ON BOARD WAS SERIOUSLY INJURED. THE A/C SUFFERED DAMAGE TO THE PROPELLER AND LOWER FUSELAGE. OFFER OF ASSISTANCE WILL BE MADE TO THE DSDR 2013FA0000325Engine · failedRIGHT ENGINE EGT INCREASED. FIRE LIGHT ACTIVATED AND THEN PERFORMED EMERGENCY SHUTDOWN PROCEDURES.SDR DALA1311640668Engine · failedRT ENGINE FAILED ON TAKEOFF AT 1000 FT AGL. REPLACED ENGINE IAW 6T103.SDR CA130513001Engine · power loss(CAN) DURING FLIGHT, THE CREW RECEIVED AN ENGINE CONTROL FAIL CAUTION WARNING. DURING ACCOMPLISHMENT OF THE CHECKLIST FOR THIS MESSAGE THEY DISCOVERED THAT THEY HAD NO THROTTLE RESPONSE OR CONTROL OVER THE RT ENGINE. THE CREW SHUT THE ENGINE DOWN AND LANDED SDR CA130502007Engine · bird ingestion(CAN) DURING CLIMB, ACFT EXPERIENCED STRONG VIBRATION ON RT ENGINE, CREW RETURN TO GROUND SAFE AND DISCOVER RT ENGINE HAD A BIRD STRIKE.SDR JIKA2013042701Engine · failedDURING CRUISE AT 16000 FT, THE PILOT GOT A R CHIP DETECT LIGHT. WHILE MONITORING THE ENGINE THE TORQUE INDICATION FLUCTUATED, AND THE ENGINE FAILED. DECLARED AN EMERGENCY AND DIVERTED. REVIEW OF THE ENGINE TEAR DOWN REPORT REVEALED THAT THE PROBABLE CAUSE SDR JIKA2013042601Engine · contaminatedDURING CRUISE AT 10000 FT, THE PILOT SELECTED BLEED AIR ON, AND THE CO-PILOT SELECTED WINDOW DEFROST. AT THIS POINT, WHAT APPEARED TO BE SMOKE CAME OUT OF THE DEFROST VENTS. THE PILOT SELECTED BLEEDS OFF, DECLARED AN EMERGENCY AND RETURNED TO SALT LAKE CITY SDR CA130430013Engine · power loss(CAN) DURING TAKEOFF OPERATION, AT FULL POWER, 97 PERCENT TORQUE, THE ENGINE NR 1 HAD AN UNCOMMANDED AUTOFEATHER. THE PILOT REDUCED POWER TO IDLE. THE TAKEOFF WAS ABORTED AND THE ACFT WAS RETURNED TO THE RAMP. FDR WAS SENT TO EVALUATE THE MAXIMUM POWER OBTASDR UALA2013042502896Rub Strip · damagedNR 1 ENGINE HAS A SMALL HOLE IN FAN BLADE RUB STRIP AT THE 6:00 POSITION. FOUND PREVIOUS REPAIR COMING APART, HOLE OF APPROX ONE HALF INCH IN DIAMETER. NO FURTHER ACTION REQUIRED.SDR CA130513003Engine · flamed out(CAN) THE OPERATOR REPORTED THE ENGINE FLAMED OUT WHILE TRANSITIONING FROM REVERSE TO IDLE AFTER LANDING. THE ACFT WILL BE FERRIED FOR AN INVESTIGATION WITH THE PRESENCE OF MFG REP. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE
Back to JASC 7200