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 MASA2013032125455Engine · damagedIN CRUISE CREW FELT STRONG AIRFRAME VIBRATION FOLLOWED BY EICAS INDICATION OF FLAME OUT AND ENGINE DEGRADED MESSAGES. THE SYSTEM THEN PERFORMED AN AUTOMATIC RELIGHT. THIS SEQUENCE OF EVENTS OCCURED TWICE. AFTER SECOND RELIGHT THE CREW RETARDED THROTTLE LEVESDR CA130401006Engine · making metal(CAN) CUSTOMER ADVISED THE MAIN OIL PRESSURE WAS FLUCTUATING 20 MIN INTO THE FLIGHT. THE OIL PRESSURE STARTED TO DROP TO 47 PSI THEN THE PILOT ELECTED TO SHUTDOWN AND SECURE THE ENGINE. THE TROUBLESHOOTING FOUND BOTH ENGINE OIL FILTERS WERE CLOGGED WITH BRONZSDR USAA2013032100015Engine · vibrationFLT 1607 EN ROUTE. NR 2 ENGINE VIBRATION HIGH, AT TIMES MOMENTARILY EXCEEDING LIMITS (AMBER INDICATION). HIGHEST READING 4.1. STILL NOTICED VIBRATION AT GROUND IDLE. MX R & R NR 2 ENGINE.SDR CA130401004Engine · power loss(CAN) DURING DESCENT, THE ENGINE POWER ROLLED BACK TO 20 PERCENT UNCOMMANDED. IT RECOVERED BY ITSELF AND THE REST OF THE FLIGHT WAS UNEVENTFUL. THE PILOT DID PRESS THE EVENT BUTTON AND AS SUCH THE TROUBLESHOOTING IS ON-GOING.SDR 39LA2013032200004Engine · vibrationUPON POWER REDUCTION TO FLIGHT IDLE, IN FLIGHT, AT 1600FT AGL, THE NR 1 ENGINE EXHIBITED MASSIVE VIBRATION AND TORQUE/RPM FLUCUATION. NR 1 ENGINE WAS SHUTDOWN IAW EMERGENCY PROCEDURES UPON LANDING.SDR UALA2013032001711Structure · damagedPUDDY ON HONEYCOMB RIGHT SIDE HAS PIECE MISSING. DAMAGE IS AT 8 O'CLOCK POS O F NR 2 ENG FWD LOOKING AFT MEASURES 2.72 INCH BY 1 INCH. REPAIRED ATTRITION LINER IAW MT 72-017.SDR OO0Y20130318002Case · damagedTEE BOLT WAS FOUND WELDED ONTO THE LPT OUTER CASE OD AT 12 O’CLOCK POSITION. CONFIRMED NO REPAIR WAS PERFORMED.SDR UALA2013031901662Liner · damagedNR 2 ENGINE A QUARTER SIZE PIECE OF ATTRITION LINER MATERIAL MISSING. REPAIRED ATTRITION LINER REPAIR.SDR UALA2013031901668Engine · faultyNR 1 ENGINE PROBLEM, RETURNED TO FIELD.SDR UALA2013031801601Engine · malfunctionedOIL LOSS, RTFL. ENG 1 OIL QUANTITY WENT TO ZERO AFTER TAKEOFF WITH PRESSURE DECREASING. CREW CONTACTED TOMC. OIL PRESSURE WAS 217 PSI AND DROPPED TO 179 PSI DURING ARINC PATCH OIL TEMPERATURE WAS IN NORMAL RANGE AT THIS TIME. ESN 724383. REPLACED ENGINE.SDR USAA2013031900002Check Valve · failedFLT 1628 ENROUTE, NR 2 ENGINE FLAMED OUT DURING REVERSE SELECTION ON LANDING. THE FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REPLACED THE NR 2 ENGINE MEC AND FUEL PUMP, PERFORMED THE NR 2 ENGINE VSV ADJUSTMENT, AND CLEARED THE CDP AND CBP WATER SDR CA130430012Engine · power loss(CAN) DURING A SIMULATED FORCED LANDING, THE PILOT STATED THAT HE CLIMBED TO FL35 AND INITIATED SPIRAL TURNS FOR A LT TRAFFIC APPROACH TO THE RUNWAY. DURING FINAL APPROACH, THE ACFT STARTED DESCENDING AT A HIGHER RATE THAN EXPECTED. THE PILOT ATTEMPTED TO INSDR UALA2013031401513Rub Strip · damagedCHUNK MISSING OUT OF FAN RUB STRIP NR 1 ENGINE 6 O'CLOCK POSITION. A 1.5 X 1.5 X .25 SECTION MISSING AT 6 O`CLOCK ON ATTRITION LINER. DEFECT IS WITHIN LIMITS PER MT 72-017. MUST BE REPAIRED WITHIN 5 CYCLES OR 10 HOURS.SDR ANCF2013031300152Engine · slowDURING TAKE OFF, WHEN THRUST LEVERS WERE ADVANCED BETWEEN FLEX AND TOGA, ECAM WARNING SHOWED ENGINES THRUST LEVERS NOT SET, ENGINES DID NOT SPOOL UP RAPIDLY AS EXPECTED IN A NORMAL TAKEOFF, DECIDED TO ABORT TAKEOFF. GROUND RETURN WAS PERFORMED AND PERFORMEDSDR CA130318009Engine · vibration(CAN) ON A REVENUE FLIGHT, DURING ACCELERATION TO TAKEOFF, THE PILOT HEARD A RUMBLING NOISE FROM THE LT ENGINE AND FELT THE VIBRATION. THE ACFT RETURNED TO THE HANGAR AND UNLOADED PASSENGERS. THE SAME SCENARIO WAS REPEATED ON A GROUND RUN. VISUAL INSPECTIONSDR QXEA2013031200581Engine · malfunctionedNR 2 ENGINE OIL PRESSURE WAS AEE AT IE THEN STARTED DROPPING FOLLOWED BY MASTER WARNING OIL TEMP REMAINED NORMAL. LT ENGINE RUNNING PRESSURE STABALIZED AT 15 PSI. ON APPROACH NR 2 PROP STARTED TO ROLL BACK ON THREE OCCASIONS. OIL PRESSURE DROPPED TO ABOUT 3SDR UALA2013031401547Engine · surgesNR 2 ENGINE SURGE. DETECTED BY BOEING AHM. SURGE OCCURED ON GROUND DURING MAINT ENGINE RUN. REF FIM 71-05-00 PG 105. PERFORMED VISUAL INSPECTION OF NR 2 ENGINE INLET, EXHAUST AREAS, ALSO VISUALLY INSPECTED 2. 5 AND 2.9 BLEED PORTS NO DEFECTS OR OBSTRUCTIOSDR VGCA20130312001Regulator · damagedNR 2 ENGINE RPM FLUCTUATION IN FLIGHT. FOUND REGULATOR DAMAGED.SDR CA130318008Engine · leaking(CAN) SHORTLY AFTER TAKEOFF, THE PILOT OBSERVED AN LOW OIL PRESSURE INDICATION ON THE RT ENGINE AND HE ELECTED TO SHUT IT DOWN BEFORE RETURNING TO THE DEPARTURE POINT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. POST FLIGHT INSPECTION FOUND AN OIL LEAKSDR CA130318007Engine · power loss(CAN) DURING REVENUE FLIGHT IN CRUISE, THE LT ENGINE REDUCED POWER APPROXIMATELY 10 PERCENT, FROM A N1 SPEED, 90.6 PERCENT TO 80.6 PERCENT. NO ENGINE WARNING LIGHTS ILLUMINATED. AFTER A FEW MINUTES THE ENGINE RESUMED POWER BY ITSELF. TROUBLESHOOTING IS ON-GOSDR CA130318006Engine · malfunctioned(CAN) BEFORE T/O, AFTER 2 MINUTES OF RUNNING TIME AT IDLE, THE ENGINE SHUT ITSELF DOWN UNCOMMANDED. SMOKE WAS SEEN COMING OUT OF THE ENGINE AT THE TIME. TROUBLESHOOTING IS ON-GOING.SDR SIMA20130311003Engine · malfunctionedFOR FLIGHT 3291 - THE CREW REPORTED THEY PULLED THE NR 1 FIRE HANDLE AND DISCHARGED BOTTLE "A" BECAUSE SAME PERSONEL CHANGED ENGINE ON FIRE INDICATION. THE CREW REPORTED NO EICAS FIRE INDICATIONS. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED E1 INSPECTISDR UALA2013031201473Engine · oil consumptionNR 1 ENGINE ESN 717999 HAS REACHED AMBER LEVEL FOR OIL CONSUMPTION, BEFORE DEPARTURE OPEN COWLING AND CHECK FOR VISIBLE LEAKS. ACP ENGINE INSP FOR OIL LEAK. NO LEAKS FOUND. OIL CONSUMPTION WITHIN LIMITS.SDR AALA20130311020Engine · failedJFK - CREW REPORTED FUEL ODOR THROUGH OUT CABIN ON DESCENT. EMERGENCY DECLARED FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT JFK ON 03/11/2013. SYSTEM GROUND CHECK NORMAL OPERATION.SDR USAA2013031400005Engine · contaminatedON THE START ARRIVAL TO FLL, CREW REPORTED A COMPLETE ENGINE FAILURE OF ENGINE NR 1 WITH APPARENT SEVERE DAMAGE. FLIGHT DIVERTED TO KMCO AFTER DECLARING AN EMERGENCY. FOLLOWED ORH PROCEDURES AND MADE AN UNEVENTFULL SINGLE ENGINE LANDING (PRECAUTIONARY) AT KSDR CA130401001Engine · failed(CAN) APPROXIMATELY 2 MINUTES AFTER LEVELING OFF AT 300 FT, A NOISE WAS HEARD FROM NR 1 ENGINE ACCOMPANIED BY THE FOLLOWING INDICATIONS: N1 DROOP, ENG 1, N2 DROOP, ENG 2, TORQUE SPLIT, FLICKERING N1, ENGINE CHIP, ENG 1, SMOKE IN COCKPIT AND CABIN COLLECTIVE ASDR CA130318004Engine · malfunctioned(CAN) SHORTLY AFTER T/O, A LOUD NOISE WAS HEARD FOLLOWED BY A POWER LOSS AND BURNED OIL ODOR IN THE CABIN. THE ENGINE WAS SECURED AND THE ACFT RETURNED TO THE DEPARTURE POINT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. NO OTHER INFO IS AVAILABLE. THSDR CA130318003Engine · power loss(CAN) AFTER A NORMAL STARTUP, APPROXIMATELY 10 SECONDS INTO TAXI, THE LT ENGINE FAN SPEED N1 DROPPED TO 12 PERCENT AND THE ENGINE TEMPERATURE ROSE TO 900C. TROUBLESHOOTING IS ON-GOING.SDR UALA2013031101445Engine · bird ingestionEVIDENCE OF BIRD STRIKE INGESTION IN NR 2 ENGINE. PERFORMED VISUAL INSPECTION OF ENGINE 2 ESN V10991 AND INLET COWL PER MT72-021. NO DAMAGE OBSERVED. BIRD DEBRIS OBSERVED ON SPLITTER FAIRING. ACP BORESCOPE OF NR 2 ENGINE, NO LIMITING DEFECTS NOTED. REF AMSDR QMLA2013030713033Engine · making metalCHIP LIGHT NR 2 ENGINE. REMOVED CHIP DETECTOR, DETERMINED TO BE A MINOR EVENT IAW MM. PERFORMED GROUND RUN FOR PRECAUTIONARY MEASURES, NO DEFECTS NOTED.SDR CA130306001Engine · fire(CAN) PRELIMINARY, THE ACFT HAD NR 2 ENGINE FIRE WARNING AFTER TAKEOFF. BOTH BOTTLES WERE DISCHARGED. AFTER LANDING, THERE IS EVIDENCE OF AN ENGINE FIRE IN NR 2 ENGINE. FIRE WARNING AT 20,000 FT, 47 PASSENGER ON BOARD. PASSENGER DEPLANED ON RUNWAY. NO SMOKESDR VNAA2013030600007Engine · malfunctionedCREW REPORTED LEFT ENGINE OIL PRESSURE CLIMBED TO APPROXIMATELY 133 PSI ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RESDR CA130318001Engine · failed(CAN) DURING CLIMB THE LT ENGINE HAD AN UNCOMMANDED SHUTDOWN FOLLOWED BY OIL ODOR AND SMOKE IN CABIN. THE CREW FEATHERED AND SECURED ENGINE BEFORE RETURNING TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. TROUBLESHOOTING IS OSDR CA130311010Engine · fire(CAN) AN ENGINE FIRE WARNING WAS ANNUNCIATED ON THE RT 2 ENGINE, APPROXIMATELY 20 MINUTES AFTER DEPARTURE. THE CREW SECURED THE ENGINE AND DISCHARGED BOTH FIRE BOTTLES, RETURNING TO DEPARTURE. A SINGLE ENGINE LANDING WAS UNEVENTFUL. IT WAS REPORTED THAT A LOSDR 39LA2013030800004Engine · malfunctionedIMMEDIATLY AFTER TAKEOFF AT APPROX 97 PERCENT NG THE NR 1 NG BEGAN TO FLUCTUATE 3-4 PERCENT. NOTICED THE NR 1 NF BEGIN TO FLUCTUATE AS WELL NR 1 FUEL PRESSURE AND T5. ALL INDICATIONS ON NR 2 ENGINE WERE NORMAL. APPROXIMATE 40 PERCENT TORQUE SPLIT WAS NOTED SDR QXEA2013030500537Engine · fireACFT FIRE WARNING INDICATION ON NR 2 ENGINE AT 20,000. ENGINE SHUTDOWN INFLIGHT. FIRE BOTTLES USED. FIRE WARNING REMAINED ON AFTER BOTH BOTTLES USED. LANDING UNEVENTFUL. FIRE DAMAGE NOTED IN NACELLE AFTER LANDING. OPENSDR UALA2013030401265Vane · damagedNR 2 ENGINE HAS 1 STG VANE ID PLATFORM FILLET RADIUS BURN THRU LOCATED 3 O'CLOCK POSITION THAT EXCEEDS ADDITIONAL REDUCED INSPECTION LIMITS PER MM 72-00-00. REPLACED NR 2 ENGINE IAW AMM.SDR AALA20130302009Engine · failedPLS - INFLIGHT SJU-MIA. CREW REPORTED HYDRAULIC OVERTEMP INDICATION AND LOSS OF RIGHT HYDRAULIC QUANTITY FOLLOWED. RIGHT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED PLS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICESDR ANCF2013030200149Engine · bird ingestionBIRD STRIKE ENGINE 2 AT TAKEOFF IN BGA HIGH VIBRATION DURING CLIMB N1 6.0. IN ACCORDANCE WITH AMM TASK 72-00-00-200 006-A AND SUBTASKS 72-00-00-220-172-A (B1) 72-00-00-280-057-A BOROSCOPE INSPECTION OF THE STAGE 4 LP TURBINE BLADES, HPC STAGES 1, 3 AND 8 CONBSDR CA130228002Engine · vibration(CAN) THIS ENGINE WAS SENT TO THE O/H FACILITY FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED AN IN-FLIGHT SHUTDOWN. THE OPERATOR REPORTED THE ENGINE WAS SHUTDOWN 4.5 MILES BEFORE LANDING DUE TO SEVERE VIBRATION, LOW ITT, AN EXPLOSIVE SOUND AND A BURSDR UALA2013022801217Engine · faultyDIRTY SOCK ODOR IN COCKPIT AFTER DEPT PASSING THROUGH 7000 FT. LASTED ABOUT 5 MINUTES. REPLACED NR 1 ENGINE PER AM M 71-00-02. COMPLETED INSPECTION OF NR 3 BEARING & PNEUMATIC DUCTS, AND SPINNER. NO OIL FOUND. DRAINED GEARBOX, ONLY TWO QTS FROM GEARBOX. SDR CA130228001Engine · malfunctioned(CAN) THE ENGINE WAS RECEIVED FOR INVESTIGATION AND REPAIR AFTER IT WAS DETERMINED THAT A DYNAMOMETER OVERSPEED FAULT CODE OCCURRED DURING TEST AT THE PREVIOUS SHOP VISIT.SDR VNAA2013022700017Engine · failedCREW REPORTED A HIGH ITT AND VIBRATION WITH LOSS OF POWER IN NR 2 ENGINE. CREW RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE NR 2 ENGINE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFTSDR SIMA20130227006Engine · failedFLIGHT 4132, CREW REPORTED JUST AFTER VR, FUMES AND HAZE BECAME EVIDENT IN COCKPIT. BY APPROX. 500FT, FLIGHT ATTENDANT CHIMMED AND NOTIFIED CREW OF SMOKE IN CABIN. EICAS LAVATORY SMOKE WARNING ILLUMINATED. EMERGENCY PROCDURES PERFORMED PER AOM - 1. FLIGHSDR WAIA2013F00098Engine · hung startFLIGHT CREW EXPERIENCED A "HUNG START" ON NR 2 ENGINE AT 40 PERCENT NG DURING START. ENGINE WAS SHUTDOWN AND MX WAS NOTIFIED. REMOVED P3 FILTER HSG ASSY; CLEANED AIR FILTER HSG DRAIN VALVE. REINSTALLED P3 FILTER HSG IAW MM CHAPTER 73-10-07. PERFORMED OPS CHSDR YYFA20130225001Unknown · unknownART FIRED ON TAKEOFF, RT ENGINE CAME UP FASTER THAN THE LT ENGINE.SDR CA130401009Engine · power loss(CAN) ON A LOCAL SKYDIVERS FLIGHT IN VMC CONDITIONS, WHILE CLIMBING, THE ACFT SUSTAINED A SIGNIFICANT LOSS OF POWER AT 1,000 FT. MAINTAINING FLIGHT WAS NO LONGER POSSIBLE SO THE CAPTAIN DECIDED TO RETURN TO THE AERODROME AND, REALIZING THAT THE ACFT WOULD NOTSDR CA130311007Engine · making metal(CAN) DURING TAKEOFF ROLL, CREW NOTICED NR 2 ENGINE TORQUE INCREASED TO 95 PERCENT, THE PLA WAS PULLED BACK TO 82 PERCENT, AND THEN MOVED UP TO 89 PERCENT TO MATCH OPPOSITE ENGINE. DURING THE INCREASE OF TORQUE, ITT INCREASED TO 775C. TAKEOFF WAS ABORTED AND SDR DXTA2013030805312Engine · vibrationRT ENGINE VIBRATION WITH ASSOCTAED RISE IN ITT - APPROX 2 HRS INTO FLIGHT AT FL430 THE NR 2 ENGINE, N2 VIBRATION MOVED FROM 5 PERCENT TO 30 PERCENT SCALE THE ITT WENT FROM 809 TO 826 N2 WENT FROM 99.0 TO 100.4. AFTER A FEW MINUTES EVERYTHING RETURNED TO NORMASDR YENA20130224052Engine · failedFLT 575 SWF-MCO, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO JFK. AT APPROX 30,000FT ON CLIMBOUT ENGINE 2 LP VIB REACHED 4.7. LEVELED OFF PER QRH PULLED NR 2 ENGINE LEVER TOWARD IDLE. LP VIB WENT TO 5.7 COMPRESSOR STALLING BEGUN OCCURING. ALSO RAN QRH
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