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 AALA201506089014Engine · dirtyFLIGHT 515 EN-ROUTE, UPON DEPARTURE, BOTH ENGS EXCEEDED LIMITS ON EGT. TOGA DEPARTURE WITHIN PERFORMANCE LIMITS. EGT'S BOTH ABOVE 800. AN OPERATIONAL DECISION WAS MADE TO BRING THE ACFT BACK. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED AN ENGSDR CA150615001Engine · malfunctioned(CAN) THE CREW REPORTED PROBLEMS WITH THE LT ENG & SHUT THE ENG DOWN. THE ACFT LANDED SAFELY. THE PILOT REPORTED THAT THE ENG 1 ABRUPTLY INCREASED TORQUE, THE ACFT YAWING SHARPLY TO THE RT, & THEREFORE THEY DECIDED TO CUT THE ENG. DURING INVESTIGATION WHEN SDR HALA2015060405015Engine · vibrationRETURNED TO DEPARTURE DUE TO NR 1 ENGINE, N1 VIBRATION CLIMBED TO 3.9 DURING CLIMB THRU FL 360-380, REDUCING POWER N1 STABILIZED AT 1.5 IN TURN CLIMBED TO 1.7. TROUBLESHOOT IAW TSM 77-00-00-810-814-A22. VIBRATION DUE TO FAN LUBE AND WITHIN LIMITS FOR QC MONISDR CA150615003Engine · faulty(CAN) PILOTS REPORTED SMOKE IN CABIN AFTER TAKEOFF, 1500 - 2000 FEET. CREW PUT MASK ON & LANDED. ENG HAD A RECENT HSI. THE TROUBLESHOOTING SHOWED OIL AROUND THE INNER DIAMETER OF THE FAN DISC & IN THE EXHAUST BREATHER OUT PORT & ON THE FMU DRAIN. OIL CONSUSDR KCSA2015060206Engine · vibrationAFTER ROTATION, CREW NOTICED A VIBRATION. NR 3 ENGINE VIBRATION INDICATOR DISPLAYED HIGH. ALL OTHER ENGINE INDICATIONS WERE NORMAL. VIBRATION DISAPPEARED AFTER REDUCING BELOW TAKEOFF POWER SETTING. OPERATED NR 3 ENGINE AT IDLE THRUST FOR REMAINDER OF FLIGHT. SDR CA150615002Engine · unknown(CAN) CUSTOMER REPORTED THAT ON GND WHILE TAXIING, THE PILOT LOST THROTTLE INPUT ON LT ENG. SHUTDOWN & RESTARTED AT THE END OF THE RUNWAY & IT WORKED FINE. DURING TROUBLESHOOTING, MECHANIC WAITED FOR AN HOUR TO START THE ENG & ENG RESPONDED WELL. AFTER WARMSDR CA150615007Engine · leaking(CAN) DURING SCHEDULED FLIGHT, PILOT EXPERIENCED SIGNIFICANT TORQUE & OIL PRESS DROP WHICH CAUSED HIM TO DIVERT TO THE NEAREST AIRFIELD. A SUCCESSFUL EMER LANDING WAS MADE DURING WHICH THE LOW OIL PRESS WARNING ILLUMINATED DURING THE LANDING SEQUENCE. POST FSDR CA150602025Engine · making metal(CAN) WHILE AT CRUISING ALTITUDE THE PILOT OBSERVED THE RED ENG CHIP LIGHT IN THE HELICOPTER WARNING PANEL. KEPT THE POWER ON THE ENG & BEGIN A DESCENT TO A CLEARING ON A LOGGING ROAD. THE INSPECTION OF THE THREE NON-ELEC CHIP PLUGS REVEALED NUMEROUS CHIPS ASDR ASAA2015053111926Engine · faultedDURING ACCOMPLISHMENT OF T/C 78273000, FOUND NR 2 ENGINE SN 894-475, MAINTENANCE MSG 75-20802 T25 SIGNALS DISAGREE, SHORT TERM FAULT. MUST BE CORRECTED WITHIN 50 FLIGHT HOURS. ACFT GROUNDED. REF FIM TASK 75-33 TASK 805, EEC BITE TEST GOOD, VERIFIED FAULT MSSDR ASAA2015053111925Engine · faultedNR 2 ENGINE SHOWS MAINTENANCE MESSAGE 73-30312. THE START SWITCH SIGNAL AND BUSS DATA DISAGREE, SHORT TERM FAULT, FAULT MUST BE CLEARED WITHIN 50 HOURS. ACFT GROUNDED. NO HISTORY LAST 90 DAYS. ACCOMPLISHED FIM 73-24T813, INITIAL EVAL & REPAIR CONFIRMATION SDR UHLA201505290417Engine · shutdownCLIMBING THROUGH 11,000 FT, A LOUD BANG CAME FROM ENGINE 2 FOLLOWED BY YAW AND AN IMMEDIATE LOSS OF POWER. EMERGENCY WAS DECLARED AND RETURNED FOR LANDING. THE ENGINE STILL HAD N1 ROTATION AND ALL PARAMETERS WERE NORMAL. R & R E2.SDR FDEA201505291661Sensor · malfunctioned20 MILES, PLANE IN CLEAN CONFIG, GOT SERIOUS VIBRATION. CHECKED ENG INSTRUMENTS & SAW NR 2 ENG WAS 15% LESS ON N2 COMPARED TO OTHER ENGS. EGT STARTED TO CLIMB, SAW 690 DEG BEFORE WE SHUT DOWN ENG. DID FULL QRH PROCEDURE FOR ENG FIRE SEVERE DAMAGE. PULLED SDR CA150604009Engine · unknown(CAN) IFSD OF ENGINE IN CRUISE.SDR ASAA2015052711882Engine · faultedWHILE PERFORMING TC 78273000, FOUND FAULT CODE MSG NR 73-31441 AND 73-31611. ACFT GROUNDED. CLEARED FAULTS FIM 73-24, TASK 815, AMM TASK 73-21-00-700-804, FIM TASK 73-73, TASK 804 AND AMM 73-21-00-700-804. FAULTS HAVE BEEN CORRECTED.SDR CALA2015052700454Engine · vibrationAT FL 360 RT ENG VIB WENT INTO AMBER BAND TWICE, MAX 2.7. FOLLOWED QRH, PROBLEM DID NOT RETURN DURING DIVERSION REF FIM 71-05-00-815-808-ROO. INSPECTED MAG CHIP DETECTORS & OIL FILTERS. FOUND TO BE CLEAN. RAN ENG, OPERATIONS CHECKED NORMAL. ACFT OK FOR SERSDR CALA2015052700453Engine · fireAFTER ENG RUNNING FOR 5 MINUTES TOWER ADVISED US WE HAD FLAMES COMING OUT OF NR 1 ENG. NO FIRE INDICATION IN COCKPIT. WE DID A PRECAUTIONARY SHUTDOWN OF THE ENG & RETURNED TO GATE. R & R NR 1 ENG REF WC 29-7100-1-0900 & 29-7100-1-4900. OPERATIONS & LEAK CHSDR ASAA2015052511851Engine · faultedWHILE ACCOMPLISHING T/C 78273000, FOUND FAULT CODE NR 73-30311 ON ENGINE NR 1. THIS IS A SHORT TIME FAULT. ACFT GROUNDED. ACCOMPLISHED INITIAL EVALUATION FOR NR 1 ENG START SWITCH TESTS, ALL TESTS PASS. INITIAL EVALUATION HAS SHOWN THAT THE FAULT IS NOT ACTSDR CA150604004Engine · power loss(CAN) AFTER DEPARTURE, FIRST ENGINE LOST POWER FOLLOWED BY THE LOSS OF THE SECOND ENGINE WITHIN 20 MINUTES. THE PILOT PERFORMED A FORCED LANDING AROUND 20 NM OUT OF DESTINATION AIRPORT. ALL 7 PASSENGER AND 2 CREW ON BOARD SUFFERED MINOR INJURIES.SDR CA150604003Engine · power loss(CAN) AS FLIGHT IDLE POWER WAS SET DURING LANDING APPROACH, THE RT ENGINE CONTINUED TO DECELERATE WELL BELOW FLIGHT IDLE. THE POWER LEVER WAS ADVANCED AND POWER RECOVERED TO A SETTING ABOVE FLIGHT IDLE. THE ENGINE DID NOT FLAME OUT, NOR WAS THERE AN INADVERTESDR CA150525009Engine · overheated(CAN) ENGINE OVERHEAT FOR 1 SECOND DURING START UP. RETURNED TO GATE FOR MX INVESTIGATION. ENG IS RETURNED TO SERVICE WITH NO FURTHER TROUBLESHOOTING.SDR ASAA2015052211837Engine · faultedWHILE CONDUCTING WO 298788, TC 78273000, MSG 73-21371 "UPPER EGT SECTORS READING" ON ENGINE 1. ECONOMIC FAULT. MUST BE CORRECTED IN 500FLT HRS. ACFT GROUNDED. ACCOMPLISHED EEC TEST, EEC TEST PASSED, NO EEC FAULTS. ALSO ACCOMPLISH EEC INPUT MONITORING FOR EGSDR CA150604001Engine · malfunctioned(CAN) CUSTOMER REPORTED THAT DURING FLIGHT N1 AND N2 SPEED FLUCTUATION AND ERRATIC ACCELERATION.SDR CA150603005Engine · shutdown(CAN) WHILE CRUISING IN FLIGHT, LT ENGINE EXPERIENCED AN INFLIGHT SHUTDOWN. THE PILOT THEN CARRIED OUT THE SINGLE ENGINE OPERATION AND AFTER CONFIRMING NO DAMAGE, FIRE OR SMOKE FROM THE ENGINE, THE PILOT PROCEEDED TO RESTART THE ENGINE SUCCESSFULLY. THE ACFT CSDR CA150910001Spring · distressed(CAN) ON APPROACH ABOUT 20 MM BEFORE TOUCHDOWN WHEN THE CREW DONNED THEIR OXYGEN MASKS REPORTING SMOKE IN COCKPIT AND CABIN. THE ACFT CONTINUED FOR A SAFE LANDING. THE ENGINE WAS SENT TO PLANT 5 FOR INVESTIGATION AND REPAIR. THE EVENT IS ASSOCIATED WITH TSDR CA150603003Warning Message · illuminated(CAN) IT WAS REPORTED THAT DURING FLIGHT, THE ENGINE NO DISPATCH CAS MESSAGE ILLUMINATED. THE CREW ELECTED TO DIVERT AND PERFORMED AN UNEVENTFUL LANDING.SDR CA150603002Engine · malfunctioned(CAN) WHILE IN CRUISE, ENGINE WENT TO MAX TORQUE BUT STILL IN GREEN, NOSE GEAR WHEN TOP OF GREEN, NO EXCEEDANCES. PILOT TRIED TO REDUCE POWER BUT NO RESPONSE WHEN PLA MOVED. PROP LEVER STILL HAD SOME CONTROL AS DID CONDITION LEVER. PILOT ELECTED TO SHUTDOWN SDR AALA20150518012Engine · fodDURING CLIMB, FLIGHT CREW REPORTED HOT PLASTIC, VARNISH ODOR & SMOKE IN COCKPIT. TURNED OFF RECIRCULATION FAN & SMOKE DISSIPATED. ATTEMPTED PACK BURNOUT PROCEDURE IAW AMM 21-20-02-201 DURING WHICH BLACK SMOKE & SPARKS WERE OBSERVED EXITING NR 1 ENGINE TAIL CSDR AALA20150518006Engine · bird ingestionDURING CLIMB A HARD BIRD STRIKE DOWN THE LT SIDE OCCURRED. THE LT ENGINE EXPERIENCED A VIBRATION SPIKE OF 1.4 N-3. RETARDED THROTTLES & VIBRATIONS CEASED. NOTED EVIDENCE OF CORE INGESTION IN THE NR 1 ENGINE. PERFORMED INSPECTION CARD 05-96-14 & FOUND NR 1 SDR CA150602011Engine · failed(CAN) CUSTOMER REPORTED THAT DURING TAKEOFF ROLL THE ACFT WAS SHAKING & ALL NR 2 ENG PARAMETERS WERE FLUCTUATING, ERRATIC. THE PILOT ELECTED TO PERFORM IFSD OF NR 2 ENG, TURNED AROUND & LANDED TO THE AIRPORT OF ORIGIN WITHOUT INCIDENT. AFTER LANDING, DURING SDR SWAA2015052239929Engine · failedINFLIGHT SHUTDOWN & DECLARED EMER. NR 1 ENG FAILED AT 3000 AGL. PROCEEDED BY COMPRESSOR STALL ROLLED BACK. AFTER SHUTDOWN RED LIGHT EGT 950 DEGREE, COOLED IMMEDIATELY. R & R NR 1 ENG IAW MT.SDR ASAA2015051711762Engine · faultedPERFORMED T/C 78273000, NR 1 ENGINE HAD ECONOMIC FAULT 77-20861, "THE BOTTOM LT EGT SIGNAL, S495S3 IS OUT OF RANGE, FAULT OCCURS FIRST 2 LEGS OUT OF 4 SHOWN. ACFT GROUNDED, ON DEFERRAL.SDR ASAA2015051711760Engine · making metalNR 1 ENGINE CHIP DETECTOR FOUND WITH CONTAMINATION. ACFT GROUNDED. DETERMINED MATERIAL TO BE MAGNETIC M-50 BEARING METAL. TECH SERVICES CONFIRMED AND VERIFIED, INITIATED INVESTIGATION AT STEP 7B, EXAMINE ENGINE STARTER MAG PLUG REF AMM 79-00-00-200-804-F00SDR CA150602010Engine · overtemp(CAN) REPORTED THAT DURING A TRAINING FLIGHT, ENGINE NR 1 OVERTEMPED WHEN GOVERNOR WAS SWITCHED FROM AUTO TO MAN WITH N1 AT 70 PERCENT. GROUND INSPECTION PERFORMED AND DEBRIS FOUND AT ENGINE NR 1 EXHAUST AREA WITH DENTS NOTED IN THE EXHAUST DUCTS, FIELD SERVISDR CA150806008Blade · damaged(CAN) DURING SCHEDULED MAINTENANCE AFTER HAVING A FOD INCIDENT ON THE OTHER ENGINE, IT WAS DECIDED TO REMOVE THE PROTECTIVE SCREEN AND INSPECT THE COMPRESSOR FOR FOD DAMAGE. THE FIRST STAGE COMPRESSOR BLADES WERE FOUND WITH HEAVY IMPACT DAMAGE. THE SECOND AND SDR SWIA201541178Engine · flamed outRT ENGINE FLAME OUT DUE TO LIGHTNING STRIKE ON APPROACH. INTERROGATED MDC AND NO FAULT FOUND RELATED TO ISSUE. RAN RT ENGINE AND NO FAULTS FOUND IAW FIM. RIGHT ENGINE OPS CHECK GOOD.SDR MTNA05152015001Engine · smokeON CLIMBOUT, AT APPROXIMATELY 2600 FT OF FLIGHT, THE PILOT REPORTED SMOKE COMING INTO THE COCKPIT FROM THE RT SIDE VENT. ALSO NOTICED AN ODOR OF BURNING OIL. ALL ENGIME INSTRUMENTS INDICATION WERE NORMAL. THE PILOT ELECTED TO RETURN TO AIRPORT. THE ACFT LANSDR 2015FA0000215Engine · overtempSHORTLY AFTER TAKEOFF, THE CO-PILOT REPORTED ITT ABOVE THE 730 DEGREE REDLINE ON ENGINE NR 1. POWER WAS IMMEDIATELY REDUCED ON THE LT ENGINE TO WITHIN LIMITS. OIL PRESSURE ON ENGINE ONE WAS ABOUT 60 PERCENT OF THE OIL PRESSURE ON ENGINE NR 2, HOWEVER THE OILSDR CA150602008Engine · failed(CAN) WHILE PULLING THE BUCKET LOAD FROM WATER, THE PILOT HEARD A COMPRESSOR STALL, FOLLOWED BY A YAW AND LOAD GROWLING NOISES. PILOT LOOKED AT THE GAUGES AND NOTICED NG DROPPING AND ITT CLIMBING. PILOT RELEASED THE LOAD, ROLLED THE ENGINE DOWN TO IDLE AND MSDR A6WA2015051942730Engine · malfunctionedRT ENGINE INDICATING 125 - 127 PSI IN CLIMB OUT & CRUISE. REDUCED THRUST TO 80% N1 & 86% N2 OIL PRESS PSI. INDICATES 86 PSI AT IDLE ON GROUND. REPLACED RT ENGINE. ALL CHECKED GOOD.SDR CALA2015051593782Engine · shutdownAT CRUISE ALTITUDE, ENG 1 UNCOMMANDED SHUTDOWN WITH ENG 1 FAIL ECAM. FOLLOWED FM PROCEDURE & SELECTED ENG 1 MASTER SWITCH TO OFF. DID NOT FEEL OR HEAR COMPRESSOR STALL. REPLACED ENG IAW AMM M T71-017.SDR CA150602006Engine · malfunctioned(CAN) PILOT REPORTED AFTER LANDING THE ACFT, & TAXING OFF THE RUNWAY HE PULLED THE CLA FROM HIGH TO LOW IDLE & THE ENG SHUTDOWN. HE ATTEMPTED TO RESTART THE ENG, BUT ABORTED THE START AS ITT REACHED 800 C. THE MECHANICS ALLOWED THE ENG TO COOL & AGAIN TRIED SDR CA150602004Engine · leaking(CAN) DURING TEST FLIGHT AFTER EXTENSIVE AIRFRAME SCHEDULED MX, A HEAVY OIL SMELL IN CABIN WAS DETECTED. PROCEEDED WITH TEST FLIGHT AS THERE WERE NO ASSOCIATED SMOKE & VAPOR & ACFT LANDED UNEVENTFULLY. AFTER PRELIMINARY INSPECTION, OPERATOR REPORTS OIL PRESESDR CALA2015051100386Engine · vibrationON CLIMB OUT, PASSING FL 350, NR 2 ENG VIBRATIONS JUMPED TO 5.0 WITH ACCOMPANYING NOISE & VIBRATIONS. LANDED WITH NR 2 AT IDLE, SHUTDOWN AFTER LANDING & SINGLE ENG TAXI TO GATE. REPLACED NR 2 ENG IAW MM 71-00-02 & TASK CARD 29-7100-1-0900. RAN ENG, ALL PARASDR CA150525007Engine · power loss(CAN) PILOT REPORTED THAT AFTER TAKEOFF WHILE THROTTLING BACK TO CRUISE SETTING, ENG EXPERIENCED A ROLL BACK TO IDLE. PILOT PROCEEDED TO LAND THE ACFT & DURING LANDING THE ACFT SLIDE SIDEWAYS WHICH BENT THE AIRFRAME BUT STAYED UP ON THE MAIN LANDING WHEELS. SDR VNAA2015051000013Engine · fluctuatesCREW REPORTED RT ENGINE N1 FLUCTUATING FROM 80.8 TO 93.0 IN CLIMB AT FL190. CREW LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED ENGINE SPEED CONTROL SYS IAW MINIMUM EQUIPMENT LIST, MEL. ACFT RELEASED FOR SERVICE.SDR CA150602005Engine · overtorqued(CAN) INFLIGHT SHUTDOWN DUE TO ENG OVER TORQUE UP TO 75%. ONGOING POWER SECTION & PROPELLER REPLACEMENT. THE ACFT TO BE FERRIED TO MAIN BASE FOR AUTO FEATHER SYS CHECK.SDR PG9A2015F00064Engine · warning lightDURING CRUISE FLIGHT, ENROUTE, PILOT RECEIVED A WARNING INDICATION FROM ENGINE CHIP LIGHT ILLUMINATION CAUTION PANEL AND FOLLOWED THE FLIGHT MANUAL AND LANDED.SDR CA150525006Engine · overtemp(CAN) DURING TAKEOFF ROLL, ENGINE TEMPERATURE WENT TO RED AREA INDICATION, APPROX. 720 DEGREES C. THIS LASTED FOR 5-8 SECONDS UNTIL CREW REDUCED POWER AT 400 FT CREW ELECTED TO DIVERT TO ALTERNATE AIRPORT AND PERFORMED AND UNEVENTFUL LANDING.SDR CA150525005Engine · vibration(CAN) DURING APPROACH, PILOT REPORTED UNUSUAL VIBRATION, LOW OIL PRESSURE ALARM AND ITT CLOSE TO 1000 DEGREES C ON RT ENGINE. PILOT ELECTED TO SHUTDOWN ENGINE. ACFT LANDED UNEVENTFULLY. GROUND INSPECTION FOUND SEVERE DAMAGE ON 2ND STAGE PT BLADES. ENGINE RSDR CA150525004Engine · failed(CAN) UNCONFIRMED REPORTS SUGGEST THE ACFT WAS ATTEMPTING AN EMERGENCY LANDING AFTER THE PILOT HAD REPORTED THE ACFT WAS SUFFERING ENGINE PROBLEMS. THE ACFT CAME DOWN IN A RIVER A SHORT TIME LATER AND WAS SUBMERGED.
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