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 CA151117005Engine · power loss(CAN) ENGINE HAD 2 SEPARATE EVENTS ON THE SAME ACFT, THE 1ST EVENT WHICH OCCURRED DURING A MISSED APPROACH, THE STUDENT PILOT APPLIED FULL POWER BUT ONLY GOT 800 LB/FT OF TORQUE, FULL POWER SHOULD HAVE BEEN 1970 LB/FT. HE THEN REQUESTED EMERGENCY LANDING IN SDR CA150325016Engine · power loss(CAN) DURING TAKE-OFF RUN, WHEN REACHING 90 KTS, ANALOG TORQUE INDICATION FOR ENGINE NR 2 DROPPED TO ZERO THEN RETURNED TO 90 PERCENT AND DROPPED TO ZERO AGAIN. AT THIS TIME RT ENGINE WENT TO FEATHER AND LT ENGINE WAS UP TRIMMED. PILOT REDUCED POWER AND CONTSDR FDEA201503170948Tube · out of alignmentLEVELING AT FL 340 HAD A LEVEL 2 NR 2 ENGINE FAULT. COMPLIED WITH QRH, UNABLE TO GET SATISFACTORY ENGINE FIRE TEST. RECEIVED FIRE WARNING & COMPLIED WITH QRH FOR ENGINE FIRE SEVERE DAMAGE. WHEN INSPECTING NR 2 ENGINE FIRE LOOPS, FOUND LEFT 7TH STAGE LOW SDR ASAA2015031610985Engine · faultedDURING ACCOMPLISHMENT OF T/C 78273000, NR 2 ENGINE LONG TIME FAULT 73-20772, PS3 SIGNAL IS OUT OF RANGE. ACFT GROUNDED. ON DEFERRAL.SDR CA150325014Engine · shutdown(CAN) THE CREW REPORTED AN IN-FLIGHT SHUTDOWN. THEY WERE FLYING AT FL450 WHEN THEY ENCOUNTERED SEVERE TURBULENCE JUST BEFORE THE IFSD. THEY DESCENDED TO FL 410 AND RESTARTED THE AFFECTED ENGINE BUT THEY NOTICED THAT THE ITT WENT TO YELLOW, APPROXIMATELY 800 SDR 2DYA20150316001Engine · malfunctionedAT 2000FT WITH FLAPS UP & CLIMB POWER SET, EXPERIENCED A VIOLENT SERIES OF EXPLOSIONS FROM RT NR 2 ENG. REDUCED POWER TO IDLE & RETURNED.SDR ASAA2015031210962Engine · making metalWHILE ACCOMPLISHING T/C 78472040, FOUND UNIDENTIFIABLE NON-MAGNETIC PARTICLES LARGER THAN .4" IN FWD SUMP SCAVENGE SCREEN MCD ON NR 2 ENGINE. MM 79-00-00-210-010, STEP 8 NEEDS TO BE ACCOMPLISHED. ACFT GROUNDED. ACCOMPLISHED STEP H8-10. NO ADDITIONAL NR 2 SDR CA150325012Engine · flamed out(CAN) FOLLOWING THROTTLE REDUCTION TO IDLE DURING DESCENT THE ENGINE FLAMED OUT. THE PILOT WAS ABLE TO RESTART THE ENGINE WHICH FLAMED OUT AGAIN TWICE WHILE BRINGING THROTTLE TO IDLE. ALL EVENTS OCCURRED IN EEC MODE.SDR CA150325010Engine · power loss(CAN) ON A FLIGHT AT CRUISE ALTITUDE, PILOT NOTICED LT ENGINE PARAMETERS DECREASING TO LOW POWER. THE CREW ELECTED TO SHUT THE ENGINE DOWN, GROUND CREW FOUND THE P3 LINE SNAPPED OFF AT THE O/S GOVERNOR. FSR TROUBLESHOOTING WITH CUSTOMER.SDR 2015F00046Engine · fireAFTER LANDING, PILOT WAS TAXING AND THE LEFT ENGINE FIRE LIGHT CAME ON, THE ENGINE LOST ALL POWER AND FIRE AND SPARKS WERE COMING OUT OF THE TAIL PIPE. VISUAL INSPECTION SHOWED NR 3 TURBINE WHEEL BLADES MELTED. AFTER REMOVAL AND DISASSEMBLY OF THE ENGINE, ALSDR ANCF2015031101Engine · fodREJECTED TAKEOFF DUE TO FOD ENG 1. ENG 1 IS IN REMOVAL & INSTALLATION PROCESS. BORESCOPE INSPECTION IS DONE ON ENG REMOVED & WILL BE SEND TO MANUFACTURER SHOP FOR INVESTIGATION.SDR CA150325011Engine · flamed out(CAN) FOLLOWING THROTTLE REDUCTION TO IDLE DURING DESCENT THE ENGINE FLAMED OUT. THE PILOT WAS ABLE TO RESTART THE ENGINE WHICH FLAMED OUT AGAIN TWICE WHILE BRINGING THROTTLE TO IDLE. ALL EVENTS OCCURRED IN EEC MODE.SDR CA150325009Engine · power loss(CAN) DURING THE CLIMB PHASE, PASSING 10000FT, THE ENGINE NR 2 TORQUE DROPPED TO 60 PERCENT FROM 86 PERCENT, WITHOUT COMMAND. AFTER 10 SEC THE TORQUE HAS BEEN RESTORED TO NORMAL VALUE. YAW MOMENT PHYSICALLY PERCEIVED DURING THE TORQUE DROP. THE ACFT RETURNED SDR CA150325008Engine · unknown(CAN) IT WAS REPORTED THAT THE LT ENGINE ITT DROPPED BY 35 DEGREES C FOR 2 SEC DURING CLIMB.SDR G1IA20150313001Engine · leakingRIGHT ENG LOST OIL PRESS & TORQUE. ENG SHUTDOWN & SECURED IMMEDIATELY. AFTER LANDING FOUND LARGE AMOUNTS OF OIL LEAKING ON COWLING & GND. FAULT NOT DETECTED AT THIS TIME. WILL AMEND REPORT UPON COMPLETION OF INSPECTION.SDR ASOA20150310017Engine · odorTHE CREW REPORTED AN ACRID ODOR COMING FROM 1 OR BOTH PACKS. DESELECTING PACK NR 1 MITIGATES THE ODOR. MAINTENANCE REPLACED THE NR 1 ENGINE. OPS CHECKS WERE GOOD.SDR CA150325007Engine · power loss(CAN) DURING TAKEOFF ROLL, THE F/O CALLED ABORT DUE TO THE RT ENGINE NOT INDICATING TAKEOFF POWER. THE LT CAME UP TO APPROXIMATELY 91 PERCENT WHILE THE RT ENGINE INDICATED APPROXIMATELY 83 PERCENT. UNABLE TO RECREATE EVENT DURING STATIC RUN UP AFTER EXITING SDR AALA20150306006Engine · bird ingestionAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. ACFT RETURNED AFTER STRIKING A FLOCK OF BIRDS. R & R THE NR 2 ENG. TEAR DOWN REVEALED THE ENG SUSTAINED DAMAGE TO THE FAN BLADES, OUTLET GUIDE VANES & FAN CASE.SDR G1IA20150311001Engine · malfunctionedWHILE ON FLIGHT, IN VMC CONDITIONS AT APPROX 0620 AST FL 270 & AT MOUNTAIN INTERSECTION, EXPERIENCED MECHANICAL IRREGULARITIES OF THE RT ENG. INITIALLY THERE WAS A SLOW FLUCTUATION OF TQ, N1 & FF, JUST SUBSEQUENT TO ENCOUNTERING SOME MILD MOUNTAIN WAVE TURBULSDR ASAA2015030610885Engine · faultedWHILE ACCOMPLISHING TASKCARD 78273000, FOUND NR 2 ENG SHORT TIME FAULT 75-20802, T25 SIGNALS DISAGREE. ACFT GROUNDED. ON DEFERRAL.SDR CA150325006Engine · overspeed(CAN) DURING CLIMBOUT, FLIGHT CREW OBSERVED ENGINE NR 2 PROPELLER OVERSPEED. FLIGHT CREW ELECTED TO PERFORM AN INFLIGHT SHUTDOWN OF ENGINE NR 2 AND RETURNED TO DEPARTURE AIRPORT. ACFT LANDED UNEVENTFULLY. TECHS WILL BE GOING ONSITE TO PERFORM TROUBLESHOOTINGSDR CA150325003Engine · overtorqued(CAN) ENGINE SUFFERED OVERTORQUE.SDR CA150325002Engine · flamed out(CAN) THE ACFT WAS HOLDING CLEAR OF THE AIRPORT WAITING CLEARANCE TO LAND WHEN THE NR 1 ENGINE BEGAN TO VIBRATE AND LOSE POWER. ENGINE EVENTUALLY FLAMED OUT, AN EMERGENCY WAS DECLARED AND THE A RUN-ON LANDING MADE. FIRE WAS OBSERVED COMING FROM THE NR 1 ENGINSDR CA150325001Engine · shutdown(CAN) ON APPROACH, ACFT EXPERIENCED AN INFLIGHT SHUTDOWN OF THE NR 2 ENGINE. ACFT SUBSEQUENTLY LANDED SAFELY, FSR AWAITING OPERATOR PILOT REPORT TO CONFIRM IF IT WAS A COMMANDED OR UN-COMMANDED IFSD. ON GROUND VISUAL INSPECTION OF THE ENGINE REVEALED NO ANOMSDR CA150310009Engine · malfunctioned(CAN) THE CREW NOTIFIED MAINTENANCE THAT AN ODOR WAS COMING INTO THE ACFT FROM THE RT ENGINE WHEN THE BLEED VALVE WAS ON. MAINTENANCE SUSPECTED A BURNED BLEED AIR GASKET ON THE ENGINE SINCE A NEW GASKET HAD JUST BEEN INSTALLED PRIOR AT THE PHASE INSPECTION. SDR CA150305005Engine · malfunctioned(CAN) SHORTLY AFTER TAKEOFF, A MASTER WARNING WITH INDICATION OF NR 1 ENG OIL PRESS LOW, RED SOUNDED. EXECUTED ENG SHUTDOWN IN FLIGHT DRILL, FOLLOWED BY NR 1 ENG SHUTDOWN INFLIGHT CHECKLIST. MX ALONG WITH REP TROUBLESHOOTS. FOUND FLAKES ON THE RGB CHIP DETESDR CA150306013Engine · making metal(CAN) PILOT REPORTED DURING FLIGHT THE NR 1 ENGINE OIL PRESS FLUCTUATED & STARTED DROPPING BELOW 100 PSI. THE CREW DIVERTED. MECHANIC REPORTED THAT HE PULLED THE OIL FILTER & WHEN HE PLACED THE OIL FILTER INTO SOME CLEANING FLUID, THE CLEAR FLUID WENT BLACK.SDR CA150413006Bearing · failed(CAN) ACFT LOST OIL PRESSURE ON THE RT ENGINE IN FLIGHT. THERE WAS A LOUD "BANG" HEARD AND A FLAME WAS THOUGHT TO HAVE BEEN NOTED COMING FROM THE EXHAUST. THE FIRE BOTTLE WAS BLOWN. IT WAS FOUND THAT THERE WAS NO ENGINE FIRE, NO FUEL LEAKS WERE NOTED AND NSDR QXEA2015030100108Engine · smokeCAPTAIN OBSERVED SMOKE COMING FROM NR 1 ENGINE EXHAUST UPON SHUTDOWN AT THE GATE. FOUND NR 1 ENG OVERSERVICED WITH OIL. DE-SERVICED NR 1 AND NR 2 ENG OIL TO PROPER LEVELS, REF AMM TASK 12-10-71-210-802. GROUND RAN ENGINES AT VARIOUS POWER SETTINGS WITH BLEEDSSDR RAIA201503010005Engine · contaminatedSMOKE IN COCKPIT AFTER TAKEOFF, RETURNED TO BLOCK. MAINTENANCE PERFORMED SMOKE TROUBLESHOOTING, FOUND TRACES OF DE-ICE FLUID IN ENGINE INLETS, CLEANED AND REMOVED DE-ICE FLUID, OPS CHECKS AND NO OTHER DEFECTS NOTED, OPS CHECK GOOD.SDR VNAA2015022700024Engine · damagedCREW REPORTED LT N2 VIBRATION MESSAGE WHILE ON RUNWAY. WHEN SETTING TAKEOFF POWER, CREW HEARD LOUD POP FOLLOWED BY GRINDING SOUND COMING FROM LT SIDE OF ACFT. CREW REJECTED TAKEOFF, SHUTDOWN LT ENGINE AND RETURNED TO GATE. MAINTENANCE INSPECTED LT ENGINE AND SDR CA150408019Engine · flamed out(CAN) ENGINE FLAMED OUT WHILE TAXIING BACK TO RAMP AFTER COMPLETION OF FLIGHT.SDR HQPR2015FA0000080Drive Gear · failedDURING FLIGHT PILOT NOTICED A N2 PERCENT ROTOR/ENGINE TACHOMETER FLUCTUATION. OPERATING PERCENT IS 103.0 PERCENT AND WOULD INCREASE 1 TO 2 PERCENT ABOVE OR 1 TO 2 PERCENT BELOW DEPENDING ON THE POSITION OF THE COLLECTIVE WHEN APPLYING OR DECREASING POWER DEMASDR CA150306005Engine · malfunctioned(CAN) OIL SMELL IN CABIN ON APPROACH. DURING DISCUSSION WITH CUSTOMER, IT WAS FOUND OUT THAT MOP HAS A TENDENCY TO INCREASE. CUSTOMER REPORTED TO HAVE ADJUST MOP, TO DECREASE IT, 2 TIMES SINCE OH. MOT WAS ALSO FOUND TO FLUCTUATE & INCREASE WITH THE EVENT OFSDR CA150303005Engine · shutdown(CAN) IN FLIGHT SHUTDOWN AFTER LANDING, THE OIL QUANTITY WAS NORMAL. NO FINDINGS HAVE BEEN FOUND SO FAR EXCEPT SLIGHT OIL LEAK EVIDENCE ON RT ENGINE COWLING. INVESTIGATION ON-GOING.SDR CA150408024Engine · shutdown(CAN) THE RT ENGINE SHUTDOWN IN FLIGHT DURING DESCENT. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGATION.SDR CA150306003Engine · shutdown(CAN) AIRCRAFT EXPERIENCED A LEFT ENGINE SHUTDOWN DURING DESCENT. THE ENGINE SHUTDOWN AS THROTTLE SETTING WAS REDUCED TO IDLE DURING DESCENT THROUGH APPROXIMATELY 5000 MSL. THE PILOT THEN ACTIVATED THE IGNITERS & THE LEFT ENGINE SPOOLED UP TO IDLE POWER & OPSDR CA150306002Engine · malfunctioned(CAN) DURING APPROACH AT 3000 FT WITH N1 AT APPROXIMATELY 47%, ENGINE 2 LOW OIL PRESS WARNING SOUNDED. OIL PRESS WAS AT ABOUT 3 PSI, ITT WAS CLIMBING ABOVE 200 DEGREES, N1 & N2 HAD ROLLED BACK SLIGHTLY FROM ORIGINAL SETTING. ITT CONTINUED TO CLIMB TO APPROXISDR CA150306001Engine · flamed out(CAN) THE ENGINE EXPERIENCED A FLAME OUT AT 8000 FEET DURING MANEUVERS FOLLOWED BY A SUCCESSFUL AUTO RELIGHT & ENGINE RESTART. THE AIRCRAFT LANDED UNEVENTFULLY. THE FIELD SERVICE REPRESENTATIVE IS EN ROUTE TO THE CUSTOMER. FAULT ISOLATION IS IN PROGRESS.SDR TAMF2015FA0000067Blades · damagedDURING THE 360 OF THE ACFT, DETECTED A FOD AT LT ENGINE, WITH FAN BLADES NR 8, 9, 22 DAMAGED, NICKED, AND INLET COWL WITH DAMAGE IN THE ACUSTIC PANELS. A VISUAL INSPECTION OF THE LOW PRESSURE COMPRESSOR WAS PERFORMED AND IS NOT REQUIRED A BOROSCOPE INSPECTIONSDR N6WA2015022202Engine · vibrationLEFT ENG VIBRATION IT, YELLOW, STARTED AT 8000 FEET COULDN'T MAINTAIN CLIMB THRUST. INSPECTED NR 1 ENG FAN BLADES FOR FREE & FOR DEFECTS. PERFORMED THE VIBRATION CHECK IAW AMM 71-00-00-720-806. NR 1 ENG OPERATED WITHIN LIMITS.SDR CA150305011Engine · shutdown(CAN) ENGINE SHUTDOWN ON DESCENT.SDR 2015FA0000098Housing · crackedDURING STRIP OF ENGINE, IT WAS NOTED THE FRONT BEARING HOUSING HAD 2 CRACKS IN THE REAR PANEL.SDR ASOA20150219014Engine · leakingTHE CREW REPORTED LAVATORY SMOKE WARNING MESSAGE AND SMOKE IN THE CABIN. MAINTENANCE REPLACED THE NR 2 ENGINE. OPS CHECKED WERE GOOD.SDR HDNA201502190004Engine · making metalON STARTUP NR 1 ENG CHIP LIGHT ILLUMINATED. UPON INSPECTION OF CHIP DETECTORS FOUND UPPER DETECTOR TO HAVE EXCESSIVE AMOUNTS OF METAL. R & R TURBINE.SDR CA150224016Engine · overtorqued(CAN) THE CREW EXPERIENCED AN AIR TURN BACK TO BASE DUE TO ENGINE NR 1 OVER-TORQUE UP TO 106.3 PERCENT DURING CLIMB. AN UNEVENTFUL LANDING WAS MADE.SDR CA150224014Engine · power loss(CAN) IAW TECHNICIAN REPORT, WHILE ON RUNWAY THE PILOT WAS UNABLE TO REACH TAKEOFF POWER AND ELECTED TO ABORT TAKEOFF. THE RIGGING, P3/PY LINES, WERE CHECKED WITH NO FAULT. CUSTOMER IS SUSPECTING A STUCK OPEN BLEED VALVE, BOV, AND WILL INSPECT P3 AIR FILTERSDR N6WA2015021804Engine · malfunctionedBANG HEARD ON TAKEOFF ON LT SIDE OF ACFT. ALSO, BRIEF APR INDICATION ON LT ENG AT ROTATION IN WIND SHEAR CONDITIONS. R & R NR 1 ENG IAW AMM 71-00-00.SDR N6WA2015021801Engine · failedBANG HEARD DURING TAKEOFF ON LT SIDE OF ACFT. ALSO, BRIEF APR INDICATION ON LT ENGINE AT ROTATION IN WIND SHEAR CONDITIONS. R & R NR 1 ENGINE IAW AMM 71-00-00.SDR 9EKA20150218009Firewall · crackedON A SCHEDULED INSPECTION, NR 2 ENG TO MGB FIREWALL FEED THROUGH FOUND CRACKED.
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