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 AALA20160310001Engine · failedTHE INBD CREW REPORTED ODOR & HAZE IN THE CABIN, CAUSING EYES TO WATER & WAS DIFFICULT TO BREATHE. ACCOMPLISHED SIC 21-96-01 & FOUND LT ENG TO BE THE SOURCE OF THE ODOR. R & R THE LT ENG IAW SIC 71-91-99 & BOW. LEAK CHECK & OPERATIONS CHECKED GOOD. ACCOMPLSDR FDEA201603050852Engine · flamed outREPEAT WRITE UP, AT START OF TAXI, NR 2 ENG FLAMED OUT. RAMP TOWER REPORTED SMOKE COMING FROM THE ENG, SO WE SHUT IT DOWN & DISCHARGED ONE FIRE BOTTLE. SMOKE STARTED TO DISSIPATE, DID NOT FIRE SECOND BOTTLE.SDR WX0A2016030773099Engine · failedDURING THE TAKEOFF THE CREW NOTED A LOUD BANG FOLLOWED BY ALL PARAMETERS FLASHING ON THE RT ENG. FIRST OFFICER CALLED THE ABORT AT 100 KTS AFTER SEEING ALL OIL QTY GONE & DASHES ON THE N1. THERE WAS SMOKE IN THE CABIN AT THE TIME OF THE EVENT. THE CREW DECLSDR UIEA2016030500115Unknown · not reportedIN CRUISE AT FL 350, THE RT ENG COMPRESSOR STALLED AT LEAST 3 TIMES. WE REDUCED POWER & CONTINUED. NO ADDITIONAL STALL AT REDUCED POWER. PERFORMED TEST IAW AMM 71-01-00, PERFORMED MINOR ADJUSTMENTS. COMPLIED WITH TEST 10 & 9 WITHIN TEST 8. NO ADJUSTMENTS SDR ASOA2016030314549Engine · shutdownRIGHT ENGINE AUTO SHUTDOWN DUE TO LIGHTNING STRIKE. R & R RT ENGINE ACFT RETURN TO SERVICE.SDR CA160303001Engine · unknown(CAN) FLIGHT DIVERTED DUE TO ENGINE PROBLEMS. NO SPECIFIC INFO PASSED WITH REGARDS TO WHAT ENGINE ISSUE WAS NO INFO PROVIDED WITH REGARDS TO WHETHER A MAYDAY OR PAN WAS DECLARED.SDR FDEA201603020808Engine · fireAFTER NORMAL 3 ENG START, BEGAN TAXI, GOT LVL 0 ALERTS. RAMP 1-3, RAMP 2-3, AIR 1-3 ISOL & ANTI-ICE ENG 2 DISAGREE. EXTERNAL RADIO CALLS FOR SMOKE & FLAME ON ENG 2. ALL ENG INDICATIONS NORMAL. PULLED 2 FIRE HANDLE & BLEW AGENT, STILL REPORTS OF FLAME. MOTSDR QMLA2016030116015Engine · making metalDURING A ROUTINE INSPECTION 300 HR, MECHANIC REMOVED THE FITTING TO INSPECT THE NR 6 - 7 NOZZLE. METAL WAS FOUND IN & AROUND THE SCREEN. THIS IS NONFERROUS METAL. THE OIL PUMP IS COMING APART. THE ENG IS REMOVED & WAITING FOR NEW ONE TO ARRIVE. OIL SAMPLESDR WX0A2016030173094Engine · failedON TAKEOFF ROLL AT ABOUT 20 KIAS AT 1.86 EPR LT ENG BEGAN TO COMPRESSOR STALL. R & R NR 1 ENG IAW WO 289702 OPERATIONS, LEAK CHECK & TRIM CHECKED OK. REFER TO TC 71-080-003, TC 71-070-001, M739 FOR INDIVIDUAL SIGN OFFS. RECORDS TRACKING ENTRY.SDR CA160302005Engine · malfunctioned(CAN) PILOT REPORTED AN UNCOMMANDED ACCELERATION. THE AIRCRAFT MADE IT BACK TO THE POINT OF DEPARTURE AND LANDED SAFELY, HOWEVER, THE LANDING WAS OFF THE ACTIVE RUNWAY ON A NEW RUNWAY AREA UNDER CONSTRUCTION. NO INJURIES, NO AIRFRAME DAMAGE WAS FOUND.SDR 2016FA0000103Warning Message · activatedWHILE MOVING THROTTLES FORWARD FOR TAKEOFF AT ABOUT 30 PERCENT, LT ENGINE ITT RAISED TO 940 DEGREES FOLLOWED BY THE LT CHIP DETECTOR WARNING LIGHT.SDR SWAA2016022549436Engine · malfunctionedAIR TURN BACK, LOUD BANG ON TAKEOFF, FOLLOWED BY LOUD AIR NOISE IN AIR. ALL OTHER INDICATIONS NORMAL. R & R NR 1 ENG ASSEMBLY IAW MT.SDR ASAA2016022015593Engine · faultedWHILE ACCOMPLISHING TASK CARD 78273000, ENGINE 2 LOGGED ECONOMIC FAULT 73-31372, UPPER EGT SENSORS READING HIGH. ACFT GROUNDED. ACCOMPLISHED FAULT ISOLATION IAW FIM 73-11, TASK 801. RAN ENGINE NR 2 AT IDLE FOR 5 MIN, ALL T49.5 PARAMETERS WERE IN RANGE, DIDSDR SWIA201641901Engine · flamed outNR 2 ENGINE FLAMED OUT AFTER TAKEOFF. ATTEMPTED TO RELIGHT ENGINE, UNSUCCESSFUL. CREW DECLARED AN EMERGENCY AND DIVERTED. CABIN WAS BRACED AND THE ACFT LANDED SAFELY. TAXIED TO THE GATE UNDER ITS OWN POWER. R & R RT ENGINE ASSY. OPS CHECKS AND LEAK CHECKS SDR AALA201602239001Engine · leakingAIRCRAFT WAS GNDED. DIRTY SOCK & MUSTY SMELL FROM TAKEOFF THRUST TO IDLE AT TOUCHDOWN. SEEMS TO BE ASSOCIATED WITH HIGHER THRUST SETTINGS. THE ODOR RESULTED IN THE CABIN CREW NOT BEING ABLE TO CONTINUE DUE TO ILLNESS. FOUND THE NR 1 ENG FWD SUMP DRAIN LEAKSDR CA160302001Engine · malfunctioned(CAN) DURING TAXI, THE PILOT NOTICED THE NR 2 ENGINE ACCELERATING ON IT`S OWN. THE PILOT WAS ABLE TO STOP THE ENGINE ACCELERATION AND RETURNED TO DEPARTURE GATE SAFELY. THE FOLLOWING TROUBLESHOOTING WAS PERFORMED. WHEN THE ELECTRICAL POWER WAS PUT ON, NR 2 MANSDR CA160301012Engine · power loss(CAN) IN CRUISE, THE PILOT NOTICED THE LEFT ENGINE PARAMETERS DROP TO IDLE. POWER LEVER WAS BROUGHT TO IDLE DETENT THEN PUSHED BACK WITH NO RESPONSE. ENGINE KEPT IN IDLE WHILE AIRCRAFT WAS DIVERTED. IT LANDED WITHOUT INCIDENT.SDR CA160301009Engine · leaking(CAN) THE CUSTOMER REPORTED THAT ON A STRAIGHT AND LEVEL FLIGHT, THE ROTOR SPEED DECAYED IN ELECTRONIC ENGINE CONTROL MODE WHICH RESULTED IN THE PILOT SELECTING MECHANICAL MODE. PILOT THEN ROLLED INTO MANUAL MODE AND REPORTED NR AT 90 PERCENT. THE ACFT LANDEDSDR ASAA2016021715560Engine · shutdownAFTER ENGINE SHUTDOWN NR 2 ENGINE BLUE "COWL VALVE OPEN" REMAINED ILLUMINATED BRIGHT BLUE. ACFT GROUNDED. RAN NR 2 ENGINE, PERFORMED OPS CHECK ENGINE ANTI-ICE NR 2 ENGINE, OPS CHECKED GOOD IAW AMM 30-21-00, NO DISCREPANCIES NOTED.SDR ASAA2016021715559Engine · malfunctionedNR 1 ENGINE WOULD NOT START, WHEN START LEVER RAISED TO IDLE FF APPROXIMATELY 1.75, BOTH FUEL SHUTOFF LIGHTS GO OUT. AFTER A FEW SECONDS THE ENGINE VALVE CLOSED ILLUMINATED, NO LIGHT OFF. ACFT GROUNDED. PERFORMED ELECTRONIC ENGINE CONTROL BITE PROCEDURE IAWSDR CA160301001Engine · power loss(CAN) DURING CRUISE, AIRCRAFT EXPERIENCED RIGHT HAND ENGINE TORQUE DROP FROM 64% TO 11% THEN BACK TO NORMAL. PILOT FELT A YAW AND 5 TO 8% TORQUE DROP WERE INTERMITTENTLY FELT THROUGHOUT THE FLIGHT. AIRCRAFT LANDED AT DESTINATION UNEVENTFULLY. GROUND INSPECTIONSDR QMLA201601316010Engine · making metalENGINE REMOVAL DUE TO CHIP EVENTS IN SUMP CHIP DETECTOR.SDR ASAA2016021315439Engine · faultedWHILE ACCOMPLISHING T/C 78273000 NR 2 ENGINE MAINT FAULT 77-10852, BOTTOM RT EGT SIGNAL T495S2 IS OUT OF RANGE, ECONOMIC FAULT. ACFT GROUNDED, ON DEFERRAL.SDR CA160216012Engine · power loss(CAN) CUSTOMER REPORTS ON TAKE-OFF ENGINE ROLLED BACK ON POWER. CUSTOMER INSTANTLY REDUCED POWER AND ABORTED TAKEOFF AND DID NOT SEE WHAT INSTRUMENTATION WAS READING. NO DAMAGE, INJURIES OR INCIDENT REPORTED.SDR CA160216010Engine · surges(CAN) DURING TAXIING, IN PREPARATION OF A REPOSITIONING FLIGHT, THE PILOT HEARD A LOUD NOISE REPORTED AS A COMPRESSOR SURGE. ENGINE POWER WAS PULLED BACK TO IDLE AND THEN SHUTDOWN. AIRCRAFT RETURNED TO THE HANGAR. THIS WAS THE SECOND EVENT. THE PREVIOUS TAXI RSDR ASAA2016020815343Engine · faultedWHILE ACCOMPLISHING T/C 78273000, FAULT CODE APPEARED ON NR 1 ENGINE 77-20871, THE TOP LT EGT SIGNAL, T495S4, IS OUT OF RANGE, ECONOMIC FAULT. MUST BE CORRECTED IN 50 HOURS. GROUNDED. ACCOMPLISHED ENGINE 1 ELECTRONIC ENGINE CONTROL MONITORING OF T49.5 INPUTSDR SWAA2016020948763Engine · failedAIR TURN BACK, IN FLIGHT SHUTDOWN, DECLARED EMER. NR 1 ENG FAILURE. R & R NR 1 ENG IAW MT.SDR ASAA2016020615307Engine · faultedNR 1 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION TRENDING HIGH. HARDWARE INSPECTION AND FAN LUBE REQUIRED. ACFT GROUNDED. ACCOMPLISHED NR 1 ENGINE FAN LUBE IAW TASK CARD 78472002.SDR 29GA2016020800002Engine · failedTHE OIL PRESSURE LIGHT CAME ON 50 FT OFF THE GROUND FOLLOWED BY THE CHIP DETECTOR LIGHT. THEN A BUNCH OF LIGHTS CAME ON AND THEN THE ENGINE STARTED PRODUCING A LOUD BANGING NOISE. THE CAPTAIN SAID HE SHUT THE ENGINE DOWN AND DID AN AIR RETURN. R & R NR 2 ESDR CA160208001Engine · contaminated(CAN) ENGINE WAS RECEIVED FOR INVESTIGATION OF OPERATED METAL IN OIL. DUE TO THE TIME ACCUMULATED BY THE ENGINE THE OPERATOR ALSO ELECTED TO PERFORM AN O/H OF THE TUBOMACHINE AND REDUCTION GEARBOX.SDR ASAA2016020514986Engine · vibrationNR 2 ENGINE TREND DATA SHOWS AN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE REQUIRED. ACFT GROUNDED. ACCOMPLISHED NR 2 ENGINE FAN BLADE LUBE, VIBRATION SURVEY TEST 7 AND FAN REBALANCE, VIBRATION LEVELS BELOW .9.SDR DXTA2016022606190Engine · unserviceableCLIMBING THROUGH 11,000', THE MASTER WARNING LIGHT FLASHED & THE RT LOW OIL PRESS ANNUNCIATOR ILLUMINATED. THE RT OIL PRESS TAPE WAS AT ZERO, LESS THAN 5 SECONDS. CREW GOT OUT CHECKLIST, BUT RT OIL PRESS RETURNED TO NORMAL AFTER POWER WAS REDUCED. NO VISIBSDR CA160204002Module · cracked(CAN) DURING PRESSURE TEST OF THE RBSS, A LEAK WAS REPORTED IN THE INTERNAL CAVITY OF THE HUB. CLOSE EXAMINATION AND A CRACK TEST, FPI, FOUND A CRACK APPROXIMATELY 3" LONG RUNNING AXIALLY FROM THE FRONT TO THE BACK OF THE SLOT. THE LEAKAGE ON PRESSURE TEST WASDR CA160203001Engine · overtemp(CAN) AT TAKEOFF POWER APPLICATION, THE RT ENGINE OIL PRESSURE SPIKES ABOVE RED AND THEN SLOWLY LOWERS TO NORMAL RANGE. THE RT ENGINE THRUST SPIKE WAS CAUSING YAW TO LEFT. BOTH THROTTLES WERE MOVED TOGETHER AND THE LT ENGINE ITT WENT SOLID RED BAR DURING CLISDR VQIA2016020120005Actuator · failedACFT EXPERIENCED A NR 1 ENGINE COMPRESSOR VANE FAULT ON ECAM, THE FLIGHT CREW ELECTED TO RETURN TO DEPARTURE. UPON ARRIVAL TECHS ACCOMPLISHED TSM 75-30-00-810-801-A. THE VBV BALL SCREW ACTURATOR WAS FOUND FAULTY AND REPLACED IAW AMM 75-31-50, THE ASSOCIATED SDR CA160201006Engine · smoke(CAN) ENGINE SMOKING WHEN THROTTLE REDUCED TO IDLE AND BELOW.SDR SWAA2016020148487Engine · stalledABORTED TAKEOFF, TAKEOFF THRUST WAS SET AT APPROX 60KTS. THERE WAS A BANG & THE ACFT YAWED LT. AFTER BANG FIRST OFFICER NOTED EGT OVER TEMP LIGHT ILLUMINATED. AFTER STOPPING ACFT, N1 & N2 INDICATED O FIREBALL OUT OF REAR OF NR 1 ENG, WAS SEEN BY COMMUTING PSDR ANCF2016012901Engine · failedDURING TAXI OUT, THERE WAS A SMELL FROM THE AIR CONDITIONING NOZZLE END, CLIMB POSTING 11000FT ENG 1 FAIL, NO INDICATION OF NR 2. ENG 1 WAS REMOVED & INSTALL A NEW ONE. ENG 1 PN CFM56B & SN 569969.SDR CA160201004Lock Nut · wrong part(CAN) UPON DISASSEMBLY OF THE AFFECTED ENGINE AND MODULE ASSY IT WAS DISCOVERED THE PART NUMBER OF THE NO 7 BEARING LOCKNUT REMOVED WAS NOT FOUND IN THE OEM APPROVED IPC. THE PART NUMBER OF THE PART REMOVED WAS 4019T66P01 WHILE THE APPROVED PART NUMBER LISTED SDR CA160203015Engine · surges(CAN) DURING THE CLIMB THROUGH FL230, THE CREW NOTICED A RT ENGINE POWER SURGE. TORQUE INDICATIONS WERE OBSERVED DEVIATING BY APPROXIMATELY 1500 FOOT-POUNDS WITH FLAMES EMANATING FROM THE EXHAUST STACK. THE POWER SETTING WAS REDUCED, THE ENGINE CONTINUED TO SSDR CA160203014Engine · malfunctioned(CAN) ON FOUR SEPARATE OCCASIONS, THE CREW EXPERIENCED A REDUCTION OF TORQUE ON THE RIGHT ENGINE. ON ALL OCCASIONS, THE POWER LEVER WAS FREE TO MOVE BUT MOVEMENT HAD NO EFFECT. THEY ALSO NOTED THAT ON ALL OCCASIONS, THE TORQUE BEGINS TO REDUCE AT LOW OAT AND OSDR WX0A2016020373085Engine · failedABORTED TAKEOFF, HEARD THUMPING NOISE & RT ENG EGT WAS FLASHING. HAPPENED AT 50 KTS. R & R RT ENG IAW TC 71-080-003.SDR CALA2016012800076Engine · fireFLIGHT ATTENDANT REPORTED LOUD BANG FROM LT ENG AS POWER WAS BEING APPLIED ON TAKEOFF ROLL. ACFT BEHIND REPORTED SEEING FLAME FROM LT ENG. NO ABNORMAL INDICATIONS ON COCKPIT GAUGES. ACCOMPLISHED AMM 71-00-00-210-801-F00 & FIM 71-05-00-810-805-F00 STEPS 1 - SDR DALA2016012700697Engine · failedDURING FLIGHT, AT 2,500 FT, THE LT ENGINE HAD A COMPRESSOR STALL AND CREW SHUTDOWN. CREW FOLLOWED PROCEDURES IAW QRH AND THEN DIVERTED. MAINTENANCE FOUND METAL IN TAILPIPE DURING EVALUATION. REPLACED ENGINE.SDR CA160203012Engine · malfunctioned(CAN) DURING CRUISE AT FL430, A SUDDEN AND STRONG VIBRATION WAS FELT AND THE MASTER CAUTION CAME ON INDICATING LT ENGINE VIBRATION. THE WAS ACCOMPANIED BY A RAPID RISE IN OIL PRESSURE. THE ENGINE POWER WAS RETARDED, VIBRATIONS LEVEL REDUCED BY THE OIL PRESSUSDR CA160203011Engine · malfunctioned(CAN) WHILE STARTING THE ENGINES WITH INTENT TO PERFORM A TEST FLIGHT, FOLLOWING THE 500 HRS INSPECTION REQUIREMENTS, ON SELECTION OF BLEEDS TO MAX., A STRONG OIL ODOR WAS PRESENT. THE ACFT TAXIED WITH THE ODOR CONTINUING FOR A FURTHER 5 MINUTES. THE CREW TRISDR CALA2016012595029Engine · oil consumptionDIRTY SOCK ODOR WHEN ACFT REACHED CRUISE, AFTER LEVEL OFF IN FLIGHT DECK & FIRST REAR CABIN, THEN IN FIRST CLASS, HAZE IN FLIGHT DECK WAS INCREASING. SHUT OFF THE UPPER RECIRC FAN & ODOR SEEMED TO INTENSIFY, THE UPPER WAS SELECTED BACK ON THEN THE LOWER WAS SSDR CA160203008Engine · malfunctioned(CAN) AT 50 FEET, DURING TAKE-OFF, THE PILOT ABORTED AS A PRECAUTION DUE TO A POPPING NOISE OF UNDETERMINED ORIGIN. THE AIRCRAFT LANDED SAFELY. TROUBLESHOOTING IS ON-GOINGSDR CA160126004Valve · malfunctioned(CAN) PILOT WAS FLYING AN ENGINE BREAK IN FLIGHT AFTER OVERHAUL. WHEN THE AIRCRAFT REACHED 5000 FEET THE PILOT ADVANCED THE THROTTLE FROM 65% TO 75% AS PART OF THE ENGINE BREAK IN PROCEDURES. AT THIS POINT THE ENGINE BEGAN TO LOOSE POWER. WHILE RETURNING TO AISDR CALA2016012895062Engine · oil consumptionDIRTY SOCK ODOR WHEN ACFT REACHED CRUISE, AFTER LEVEL OFF, IN FLIGHT DECK & FIRST REAR CABIN, THEN IN FIRST CLASS. HAZE IN FLIGHT DECK WAS INCREASING. NR 1 ENG HAS OIL IN THE TAIL PIPE & 9 QTS OF OIL ADDED, HIGH OIL CONSUMPTION. REPLACED NR 1 ENG IAW AMM 71
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