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 SWAA2014060228560Engine · faultyDIVERSION, NR 2 OIL QTY DECREASED TO 26%. R & R NR 2 ENG ASSEMBLY IAW MT.SDR CA140616001Engine · making metal(CAN) DURING FLIGHT, THE CREW RECEIVED A CHIP DETECTOR WARNING ON NR 2 ENGINE. POWER WAS SET TO IDLE FOR THE REMAINDER OF THE FLIGHT BUT AS POWER WAS INCREASED ON APPROACH, THE FADEC SHOWED AN EXCEEDANCE MESSAGE AND UNABLE TO CLEAR. POST FLIGHT INSPECTION FOSDR CA140606009Engine · fod(CAN) DURING STATIONARY GROUND RUNS IN SUPPORT OF MAINTENANCE TROUBLESHOOTING PROCEDURES, THE ENGINE EXPERIENCED INTERNAL DAMAGE WITH THE RESULTANT RELEASE OF HIGH-ENERGY PARTICLES. THE INCIDENT IS CURRENTLY UNDER INVESTIGATION WITH FINDINGS TO BE CONVEYED ONSDR CA140602024Engine · vibration(CAN) ENGINE VIBRATION MESSAGE AND MASTER WARNING WERE GENERATED SHORTLY AFTER TAKEOFF. THE PILOT FELT THE VIBRATION, ELECTED TO REDUCE POWER TO MINIMIZE VIBRATION AND PERFORMED AN UNEVENTFUL LANDING. ON GROUND TEST SHOWED NORMAL ENGINE PARAMETERS.SDR SWIA201437868Engine · smokeEXCESSIVE SMOKE COMING FROM RT ENGINE AFTER SHUTDOWN. SMOKE DID NOT SUBSIDE OVER 20 MINUTE PERIOD. NO ABNORMAL ENGINE PARAMETERS NOTED. PERFORMED VISUAL INSPECTION OF RT ENGINE INLET & EXHAUST. NO DEFECTS NOTED. SERVICED RT ENGINE OIL AND FOUND ONLY .5 QUSDR 7AJA20140530001Engine · making metalNUMBER 2 ENG CHIP DETECTOR WARNING ILLUMINATED. ACFT RETURNED TO BASE.SDR CALA2014052791161Engine · odorIAW CREW ON TAKEOFF, GOT AIR BLEED 2 MSG & WITHIN 30 SECONDS SMOKE ALARM IN FWD LAVATORY WENT OFF. CABIN CREW SAID THEY STARTED GETTING SMELL & ODOR AROUND ROW 23 THEN SMELL MOVED FWD TO AROUND ROW 8 & SMELL STARTED TO INTENSIFY. SMELL WAS COMING FROM NR 2 ESDR IPXA2014052883104Compressor · stalledNR 2 ENGINE EXPERIENCED SEVERE COMPRESSOR STALLS. CAPTAIN DECLARED EMERGENCY AND RETURNED TO DEPARTURE. REPLACED NR 2 ENGINE IAW TC5001RR & TC5002RR. OPS CHECKED NORMAL.SDR CALA2014052791164Engine · surgesNUMBER 2 ENG SILENT SURGE. IAW LM8843 & LM8845 FOR WORK DIRECTIVES. ACCOMPLISHED LM8843 & LM8845 & NO DAMAGE OR ABNORMALITIES FOUND.SDR HALA2014052500067Engine · stalledLEFT ENGINE COMPRESSOR STALL AT ABOUT 1500 FT. INSPECTED ENG IAW AMM 72-00-00, FOUND STAGE 5 HPC ENTIRE TIP MISSING, FWD TO AFT, APPROX .2500. R & R NR 1 ENGINE IAW 143-717. OPS & LEAK CHECKED GOOD. OK FOR SERVICE.SDR CA140527002Engine · vibration(CAN) ON DEPARTURE, MCO HAD ENGINE VIBRATION IN GREEN ON CLIMB OVER 290 KTS CREW COULD FEEL IT IN THE REAR GALLEY, BACK END CREW CAME DUE SHAKING SO BADLY.SDR FDEA201405241153Engine · making metalWHILE LEVEL AT FL370, RECEIVE A LEVEL 2, NR 3 ENGINE OIL FILTER ALERT. COMPLIED WITH QRH DIRECTIVE & SHUTDOWN NR 3 ENGINE. ALL OTHER ENGINE INDICATIONS WERE NORMAL. REMOVED MAIN CHIP DETECTOR & FOUND LARGE QTY OF LARGE METAL PARTICLES. REMOVED OIL FILTERSDR SWIA201437851Engine · overtempREJECTED TAKEOFF DUE TO ITT EXCEEDENCE ON LT ENGINE DURING T/O ROLL. COMPLIED WITH OVER TEMP INSPECTION IAW CARD.SDR CA140602023Engine · flamed out(CAN) IN THE CLIMBOUT, THE FLIGHT ENCOUNTERED SOME ICE AND TO TURBURLENCES AND THE LT ENGINE SUDDENLY FLAMED OUT. AUTO RE-LIGHT ACTIVATED END THE ENGINE RE-LIT PERFECTLY WITH NO ABNORMAL INDICATIONS.SDR CA140602021Engine · overheated(CAN) THE PILOT SHUTDOWN NR 1 ENGINE FOR HIGH OIL TEMPERATURE AND THEN THE NR 2 ENGINE RUN IN OEI. THE ON GROUND PRELIMINARY FINDINGS FROM THE TROUBLESHOOTING REVEALED THAT NR 1 ENGINE OIL TEMPERATURE PEAKED AT 132.375 OC AND WAS ABOVE 130OC FOR 2 MINUTES 41 SDR JJBA20140523014Unknown · malfunctionedNR 1 ENG TORQUE FLUCTUATED 10-20% DURING DESCENT WHEN POWER WAS SET TO APPROXIMATELY 15 & 20%.SDR CA140602020Engine · malfunctioned(CAN) DURING REVENUE FLIGHT, THE PILOT INDUCED AN IFSD DUE TO TORQUE FLUCTUATION. ON GROUND, THE AFU WAS REPLACED AND THE MAINTENANCE CREW REPORTED TORQUE LIMITED TO 60 PERCENT DURING GROUND RUN. ELECTRONIC ENGINE CONTROL, MFCU AND FUEL PUMP WERE SWAPPED WITHSDR CA140602017Engine · power loss(CAN) DURING CLIMBOUT THROUGH 2000 FT, THE PILOTS NOTICED THE NR 1 ENGINE TORQUE SLIGHTLY ROLL BACK, FOLLOWED BY A LOUD BANG. THE PILOTS PERFORMED THE SHUTDOWN PROCEDURES AND THE ACFT WAS LANDED SAFELY. DURING LANDING, THE REDUCTION GEAR BOX MAGNETIC CHIP DETSDR CA140523004Engine · smoke(CAN) SMOKE IN CABIN DURING DESCENT. MAINTENANCE, STARTING THE RT ENGINE, SMOKE OBSERVED FROM THE ENGINE ITSELF. THE ENGINEERS HAVE ISOLATED THE OIL LEAK TO THE DRAIN PIPE INDICATED BELOW. BORESCOPE INDICATED EXTENSIVE OIL WETTING EVIDENT AT THE 3RD STAGE LSDR FDEA201405211114Engine · stalledNR 1 ENGINE HAD A SUSPECTED STALL ON ROLLOUT. TOWER REPORTED LT ENGINE ON FIRE. STOWED THRUST REVERSERS BY 60 KIAS & STOPPED ACFT, SHUTDOWN ENGINE, NO OTHER FIRE INDICATIONS, VISUALLY CONFIRM NO SMOKE. ON SHUTDOWN IN RAMP ADC 1 FAULT OCCURRED & STAYED ON. SDR CA140603009Magnetic Plug · damaged(CAN) AT A SM EVENT, SIGNIFICANT METAL WAS NOTED ON THE M05 MAG PLUG AND THE MAG PLUG. NO CHIP LIGHT ILLUMINATION HAD OCCURRED DURING OPERATION, HOWEVER IT APPEARED TO BE IMMINENT. FILTERS AND OIL WERE CHANGED AND A 20 MIN GROUND RUN WAS CARRIED OUT IAW THE SDR CA140602019Engine · malfunctioned(CAN) PILOT ABORTED TAKEOFF DURING TAKEOFF ROLL DUE TO UNCOMMANDED ACCELERATION. PILOT SECURED THE ENGINE AND RETURNED TO RAMP.SDR VNAA2014051700011Engine · surgesCREW REPORTED LT ENGINE BEGAN TO SURGE IN POWER IMMEDIATELY AFTER TAKEOFF, DROPPING AND SPIKING UP TO 5 PERCENT N1. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED GROUND ENGINE RUN AND FOUND LT ENGINE N1 SURGING ABOVE 80 PERCENT N1SDR SWIA201437609Engine · failedLEFT ENGINE OVERTEMP, CREW PULLED POWER BACK, THEN PUSHED UP. ENGINE OVERTEMPED AGAIN THEN FLAMED OUT. FOUND LT ENGINE COMPRESSOR DAMAGE, STAGE 4 AFT. REPLACED LEFT ENGINE OIL PRESSURE TRANSMITTER AND LT ENGINE.SDR CA140619013Engine · failed(CAN) AS REPORTED BY THE FBO WHO IS HANDLING THE REPAIR OF THE ENGINE, A POWER LOSS OCCURRED WITH FLAMES COMING OUT OF THE EXHAUST. THE AIRCRAFT APPARENTLY LANDED SAFELY. THE ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THE FBO REPORTED SIGNIFICANSDR SOKF20140516004Engine · power lossDURING TAKEOFF FROM SAL TO GUA THE ACFT REJECTED THE TAKEOFF DUE NR 1 ENG DID NOT ACCELERATE ON TAKEOFF POWER. IAW TROUBLESHOOTING MANUAL 71-00-00-810-807A PERFORMED ACCELERATION CHECK IAW AMM 71-00-00. ALL PARAMETERS WERE FOUND NORMAL. THE ACFT RETURNED TOSDR HALA2014051500064Guide Vane · damagedDURING NR 1 ENGINE BOROSCOPE, FOUND LOOSE & MISSING HARDWARE FROM 1 OUTLET GUIDE VANE. REPLACED HARDWARE IN FAN OUTLET GUIDE VANE IAW AMM 72-21 OK FOR SERVICE.SDR ASOA20140513071Engine · smokeTHE CREW REPORTED THAT THE CABIN AND FLT DECK FILLED WITH SMOKE DURING CLIMB. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CALA2014051300591Engine · malfunctionedAPPROXIMATELY 1:45 EN ROUTE FROM LAX TO KONA WE GOT THE LAVATORY SMOKE ADVISORY MSG. FIRST OFFICER RAN CHECKLIST. RETURNED TO LAX, APPROXIMATELY 30 MIN LATER WE NOTICED HIGH OIL TEMP & LOW OIL PRESS BUT STILL IN AMBER. ALSO LOW OIL QTY APPROXIMATELY 10 QTS SDR CA140602010Engine · overheated(CAN) JUST AFTER TAKEOFF, THE PILOT OBSERVED A HIGH ITT. THE HIGH ITT CAME BACK EVERY TIME PILOT RETARDED AND SLOWLY INCREASED THE THROTTLE. THE PILOT ELECTED TO DIVERT. DURING THE REST OF THE FLIGHT HE KEPT THE THROTTLE AT A REDUCED THRUST TO KEEP THE ITT LSDR CALA2014051391008Engine · making metalOIL PRESS INDICATION, ENG RED CREW COMMENTS. LOW OIL PRESS AFTER LOW OIL QTY PRECEDED BY HIGH ENG VIBRATION. REPORTED OIL LINE CRACKED AT TOP OF SERVO FUEL HEATER, IPC 79-21-51-03 ITEM 030, DUE TO HIGH N2 VIBES & METAL PARTICLES IN TAIL PIPE, IAW PTT SEQ 120SDR FDEA201405120985Engine · malfunctionedNR 3 ENG WOULD NOT ADVANCE TO MAX POWER, EPR OF 1.61, AUTO THROTTLES ADVANCED ENGINES 1 & 2 TO 1.61 EPR, NR 3 STOPPED AT 5% - 6% BELOW 1 & 2. THROTTLE NR 3 STOPPED 1/2 KNOB BEHIND NR 1 & 2. MANUALLY ADVANCED NR 3 THROTTLE UP, EPR & N1 SETTINGS WOULD NOT ADSDR N6WA2014051202Engine · vibrationLEFT ENG VIB AT 2.9 AT ONE POINT. INSPECTED ENG FAN BLADES FOR STIFFNESS & FOR ICE, SHOOK FAN BLADES & PERFORMED ENG RUN IAW AMM 72-21-02 ANS 71-00-00.SDR CA140602009Engine · power loss(CAN) ON THE CLIMBOUT, AT APPROXIMATELY 19,000 FT, THE TORQUE INDICATION ON NR 2 ENGINE WENT TO ZERO, NO OTHER ENGINE PARAMETERS CHANGED. SHORTLY AFTER THAT THE NR 2 ENGINE FUEL PRESS CAUTION LIGHT CAME ON. THE CREW ELECTED TO SHUTDOWN THE ENGINE, DECLARED ASDR CHIR201405141535Impeller · damagedCREW REMOVED ENGINE FOR FAILURE TO PASS POWER ASSURANCE. HOT END OF ENGINE WAS REMOVED AND PLASMA SPRAY WAS NOTED COMING FROM AIR DIFFUSER. EXCESSIVE DAMAGE WAS OBSERVED THROUGHOUT GP SECTION INCLUDING BURNING OF SECOND STAGE NOZZLE AND LOSS OF MULTIPLE FIRSDR UHLA2014050900353Engine · vibrationINFLIGHT, NR 1 ENGINE HIGH LP VIBRATION UP TO 5.0, HP VIBRATION 1.7. VIBRATION CAN BE HEARD AND FELT. DIVERTED, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R NR 1 ENGINE.SDR CALA2014050990988Engine · surgesENGINE L SURGE AUTO EVENT ON SHUTDOWN CORRELATED TO 71-60431. ACCOMPLISHED FIM TASK 71- 05-819, IAW C3. NO CORRECTIVE ACTION REQUIRED.SDR CA140602018Gearbox · making metal(CAN) THE PILOT SHUTDOWN THE ENGINES AND ABORTED THE TAKEOFF DUE TO A CHIP DETECTOR INDICATION ON THE COMBINING GEARBOX.SDR CA140513004Engine · fire(CAN) AFTERSHUT DOWN THE PILOT NOTICED FLAMES COMING FROM ENGINE NR 2 EXHAUST AND MOTORED THE ENGINE IAW FLIGHT MANUAL TO PUT OUT THE FIRE. THIS ACTUALLY MADE THE FLAMES INCREASE AND THE FIRE WAS PUT OUT WITH THE ONBOARD FIRE EXTINGUSHER.SDR FDEA201405070960Engine · overtempPASSING 1200 FT, NR 3 ENGINE EGT WENT TO 969 C, PULLED THROTTLE BACK, TEMP STABILIZED, BUT WITHIN MINUTES STARTED FLUCTUATING INTO THE AMBER TOWARDS RED. PULLED THROTTLE TO IDLE & LT RED WITH THROTTLE AT IDLE. NR 3 ENGINE EGT EXCEEDANCE. ACCOMPLISH A BOROSCSDR QXEA2014005070039Fadec · malfunctionedIN DESCENT NR 1 ENG FADEC CAUTION AND POWERPLANT MESSAGE ILLUMINATED. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND FAULT CODE 912 ON NR 1 ENGINE, CH A & B. CLEARED IAW AMM TASK 73-21-00-070-801 & 61-20-36-070-801. REPLACED NR 1 FADEC AS A PRECAUTIONARY MEASDR SWAA2014050827784Engine · malfunctionedDIVERSION, INFLIGHT SHUTDOWN & DECLARED EMERGENCY. NR 2 ENG OIL QTY DROPPED TO 0 PRESS. DROPPED & LOW OIL PRESS LIGHT CAME ON. OIL TEMP CLIMBED TO 120 DEGREES, SHUT DOWN ENG. R & R NR 2 ENG IAW MT.SDR FDEA201405020914Engine · failedAT FL 390, ACFT SHUDDERED WITH A ASSOCIATED POP. EGT WENT INTO RED, FOR RT ENGINE. IMMEDIATELY BROUGHT RT THROTTLE TO IDLE. EGT WAS IN THE RED APPROX 15 SECONDS AFTER THROTTLE WAS AT IDLE, MOTOR RAN NORMALLY AT IDLE. CAPTAIN STATED THAT HE OBSERVED THE SDR HCM2014F00000Engine · making metalDURING FLIGHT, ENGINE CHIP LIGHT ILLUMINATED AND PILOT MADE A PRECAUTIONARY LANDING. MECHANIC INSPECTED ENGINE CHIP PLUGS. A SIGNIFICANT AMOUNT OF METAL WAS FOUND ON THE ELECTRIC PLUG, MODULE 01 CHIP PLUG AND THE ENGINE OIL TANK CHIP PLUG. IT WAS DETERMINESDR JIKA2014050201Engine · contaminatedDURING CRUISE, PILOT TURNED ON ENGINE DE-ICING SYS, RT ENGINE EGT EXCEEDED LIMITS & RT ENGINE FUEL BYPASS LIGHT ILLUMINATED. ENGINE REDUCED TO FLIGHT IDLE BUT RT ENGINE EGT NOT RESPONSIVE & RT ENGINE BYPASS LIGHT REMAINED. ENGINE SHUTDOWN, DECLARED AN EMERGSDR WI5R2014050200001Blade · detachedLT ENGINE HAD AN INTERMITTENT LOW RUMBLING NOISE AT GREATER THAN 80 PERCENT N1. DISASSEMBLY OF THE ENGINE HAS REVEALED IP ROTOR LIBERATED 1 OF THE 1ST STAGE BLADES.SDR SCNA20140501046Engine · failedDURING CLIMBOUT, A LOUD BANG AND FLASH, NR 2 ENGINE FAILURE. RETURNED TO DEPARTURE.SDR CA140602007Engine · power loss(CAN) ENGINE NR 1 ANALOG TORQUE DROPPED DURING INITIAL TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND UNABLE TO CONFIRM IF UNCOMMANDED AUTOFEATHER TOOK PLACE. ENGINE NR 1 AUTOFEATHER UNIT AND AUTOMATIC TAKEOFF POWER CONTROL SYSTEM, ATPCS, WERE ISOLATED IAW MINIMUSDR JJBA20140429006Engine · power lossON SHORT FINAL NR 1 ENG TORQUE WENT TO 80% PERCENT, ENG WAS SHUT DOWN. RESET BETA LOCKOUT BREAKER & ENG PERFORMANCE IAW 71-00-00. OPERATIONS CHECKED SATISFACTORY AT THIS TIME OCF REQUIRED.SDR CA140602014Engine · flamed out(CAN) DURING CRUISE, THE ENGINE FLAMED OUT FOLLOWED BY A LOUD NOISE. THE ENGINE WAS SECURED AND THE CREW RETURNED TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. THE ENGINE HAS BEEN REPLACED AND ACFT RETURNED TO SERVICE.
Back to JASC 7200