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 2010FA0000000Bearing · failedDURING FLIGHT INBOUND, THERE WAS AN IN FLIGHT SHUTDOWN OF THE NR 2 ENGINE. THE ENGINE UNDERWENT A MPI/CZI INSP 80.8 HOURS PRIOR TO THE FAILURE. TEARDOWN INSP REVEALED A FAILURE OF THE UPPER TOWER SHAFT BEARING. THIS WAS AN ORIGINAL BEARING THAT UNDERWENT CZI SDR C2XA09TY277Engine · leakingON SHORT FINAL LAV SMOKE DETECTOR WENT OFF AND HAD SMOKE IN THE CABIN. REMOVED AND REPLACED NR 2 ENG IAW TASK CARD 6271001. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR C2XA09229Engine · smokeFLIGHT 3060 - EWR - FLIGHT CREW REPORTED NR 1 ENGINE EMITTING AN UNUSUAL AMOUNT OF SMOKE AFTER BEING SHUTDOWN. EWR MX RAN ENGINE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. NO SMOKE NOTICED AFTER SHUTDOWN.SDR C2XA09IA328Engine · leakingDEN - FLIGHT 5663, AFTER T/O CHECKLIST, THE CREW REPORTED A LAV SMOKE WARNING. THE AIRCRAFT RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT FERRIED TO CLE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINSDR C2XA09IA330Engine · leakingCLE - DURING MAINTENANCE INSPECTION, AN OIL HAZE IN THE CABIN WAS REPORTED WITH 31 ENGINE HIGH OIL PRESSURE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR 2010FA0000038Planetary Gear · mismanufactured2ND STAGE PLANET GEARS HAVE ON THE INTERNAL BORE A PRESS FIT BUSHING (PN E3035030). THIS BUSHING HAS ITS BORE COATED OR SPRAYED WITH BRONZE MATERIAL INTRODUCED BY SB 1404. DURING OUR INSP WE OBSERVED THAT THIS BRONZE COATING HAD ROTATED FROM ITS ORIGINAL POSISDR MASA2009122000356Engine · malfunctionedASH FLT 2748 TUS-PHX. RETURNED TO FIELD DUE TO LT ENGINE HIGH OIL TEMP 260 DEGREES IN FLIGHT ENGINE SHUT DOWN. MX R2 NR 1 ENGINE.SDR UALA2009122103941Engine · malfunctionedNO FUEL CONFIG LT W-FUEL IMBALANCE OF 2000 NR R TANK LIGHT. NR 2 ENG BURNS 300 NR MORE THAN NR 1 CHRONIC REPLACED FQIS. OP CHKS NORMAL.SDR QMLA122009049Engine · failedENROUTE TO HOSPITAL, WHILE DESCENDING, NOTICED THE TORQUE OF THE NR1 ENG HAD DROPPED TO ZERO. THE NR1 ENG PARAMETERS WERE CONSTANT AT ABOUT 75-80 PERCENT NG AND APPROX 650 DEGREES C MGT. IMMEDIATELY VERIFIED THAT BOTH THROTTLES WERE COMPLETELY OPEN. AS APPLISDR DXTA2009122103903Fuel Control · malfunctionedAPPROX 1 HR INTO FLT AT FL410, RT N1 READ 2 % LOWER THAN LT N1. RT ENG N1 DID NOT RESPOND TO THROTTLE. RT N1 ROLLED BACK TO 55 %, WITH FURTHER REDUCTION TO 35 %. ALL ENG INDICATIONS LOW BUT WITHIN LIMITS. AT APPROX 18600 FT-7 RAT RT ENG SPOOLED UP/ BACK TO NSDR SWIA200923300Module · crackedRIGHT ENGINE LPT MODULE CRACKED. (FLT 6458) REPLACED RIGHT ENGINE.SDR ZZDA2009407Engine · malfunctionedLOUD NOISE FROM LEFT ENGINE FOLLOWED BY COMPRESSOR STALL ALERT, THEN HIGH LEFT ENGINE TGT. REMOVED AND REPLACED NR 1 ENG ON W/O 208109 TASK CARD 603. AUTO LAND ACCOMPLISHED ON W/O 208109 TASK CARD 625.SDR CA100101003Engine · overtemp(CAN) DURING CLIMB AT FL 150 , CREW REPORTED THE ITT ENG NR 1 RAISING IN THE RED BAND AT 1000 DEG. CREW COMPLIED WITH QRH AND SHUTDOWN THE LT ENGINE. THE CREW ELECTED TO DO AN AIR TURNBACK AND LANDED TO DEPARTURE AIRPORT. MX FOUND EXCEEDANCE REPORT IN MDC AT SDR CA091222004Engine · smoke(CAN) A NOISE FROM THE ENGINE FOLLOWED BY WHITE SMOKE FROM THE EXHAUST. MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION IS AVAILABLE. (TC NR 20091222004)SDR DL738091987Engine · contaminatedATB STRONG ODOR AND FUMES IN CABIN AND COCKPIT AFTER TAKEOFF. RETURNED TO DEPARTURE RAN ENG'S AND BOTH PACKS. OPERATED ALL GALLEYS. OPERATED ALL BLEEDS APU AND ENGINES. NO ODOR NOTED. FOUND CONSIDERABLE AMOUNT OF GLYCOL IN ENG INTAKES. SUSPECT ENG INGESTED GLSDR IXXA090072OEngine · power lossDURING TAKEOFF FROM WSAP NR 4 ENG FAILED TO PRODUCE TAKEOFF PWR. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PERFORMED POWER RUN AND ACCELERATION CHECK. OPS CHECK GOOD IAW ERH 72.01.1. ACFT WAS RETURNED TO SERVICE.SDR DLM88091969Engine · failedRT ENG PWR LOSS AFTER TAKEOFF. FOUND METAL IN TAIL PIPE, REQUIRES ENGINE CHANGE. REPLACED RT ENG.SDR CHQA200900262Engine · bird ingestionTHE FLIGHT CREW REPORTED A BIRD STRIKE ON ROTATION AT ABOUT 20FT. E2 ITT FLUCTUATED 100 DEGREES FOR 3 OR 4 MINUTES AFTERWARDS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION IAW EMB 140 AMM 5-50-08 WITSDR C2XA09IA310Engine · leakingIAH - FLIGHT 2379, THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS WITH AN ASSOCIATED SMOKE SMELL ON CLIMBOUT. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWOSDR CA091221003Engine · unknown(CAN) CREW HEARD SURGE NOISE WITH MESSAGE ON CAS. EDU DOWNLOAD DID NOT REVEAL ANY FAULTS. MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION IS AVAILABLE. (TC NR 20091221003)SDR CA091221002Engine · damaged(CAN) THE PROP WAS HARD TO TURN AND THE NL TURNED WITH THE PROP. WHEN THE NH ROTOR WAS ROTATED THE NL ALSO TURNED. THE ENGINE WILL BE REMOVED FOR REPAIR. MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION IS SDR DXTA2009121403895Check Valve · faultyAFTER STARTING BOTH ENGINES AND CALLING FOR TAXI CLEARENCE. THE TOWER INFORMED US THAT THERE WAS GRAYISH SMOKE COMING OUT OF ONE OF THE ENGINES (THEY THOUGHT THE LT SIDE, BUT COULD NOT BE 100 PERCENT CERTAIN) ALL ENGINE PARAMETERS APPEARED NORMAL. REMOVED ANSDR DL77L091958Engine · failedNR 1 ENG FAILED BORO INSP/C NBR 1 ENG REPLACED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.SDR CA091221001Engine · odor(CAN) CREW NOTED OIL ODOR IN CABIN. MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION IS AVAILABLE. (TC NR 20091221001)SDR HALA2009120800575Engine · malfunctionedETOPS SIGNIFICANT SYS - ENG NR 1 EPR 106.1; N1 97.6; EGT 723; N2 96.9; FF 4.8 FUEL FLOW IN NR 1 ENG 3-4 HUNDRED LBS HIGHER. ENG NR 2 EPR 106.1; N1 95.5; EGT 706; N2 95.9;FF 4.5. INSP THROTTLES FOR BINDING, PLAY OR OTHER DEFECTS. NONE NOTED. PERF HIGH POWER SDR C2XA09RI203Engine · damagedFLIGHT 3046 - PHL - DURING DESCENT, FLIGHT CREW REPORTED BIRD STRIKE, CAUSING E2 EXCEEDANCE, ITT WENT INTO RED AND ENGINE SHUTDOWN. FLIGHT CREW DECLARED EMERGENCY AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 ENGINE AND PERFORMED OPERATIONALSDR CA091215010Engine · unknown(CAN) PILOT REPORTED HEARING A GRINDING NOISE AND SHORTLY AFTERWARD NG WENT TO ZERO. ENGINE WILL BE TRANSPORTED TO MANUFACTURER FOR INVESTIGATION. MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION IS AVAILABSDR AXSA701FX120309Engine · failedDURING CLIMB THROUGH 7500FT WITHOUT WARNING THE ENGINE MADE A VERY LOUD GRINDING/SQUEALING NOISE FOR APPROX 3 SECONDS AND PWR WAS IMMEDIATELY LOST. THE PILOT WAS ABLE TO SUCCESSFULLY LAND IN A FIELD WITH NO DAMAGE TO THE ACFT. MX EXTERNAL EVALUATION OF THE ENSDR UALA2009120403751Engine · making metalEXCESSIVE METAL PARTICLES FOUND ON NR 1 ENG MASTER CHIP DETECTOR AND MAIN GEARBOX CHIP DETECTOR. NR 1 ENG NO ROTATION. DUE TO REPORT OF ENGINE NOT CRANKING AT START ALONG WITH PMA-N2 MSG AS REPORTED BY SFOEP, MX FOUND EXCESSIVE METAL PARTICLES ON NR1 ENG MASSDR HALA09F00132Inlet Bullet · dentedOPEN - ETOPS SIGNIFICANT SYS - FOUND DAMAGE IN NR 1 ENG INLET CONE 2 DENTS 5 INCHES APART IN SAME SEGMENT. 1 DENT 1.3 X .047 DEEP 1 DENT .7 X .021 DEEP DIMENTIONS EXCEED SRM 54-13-01-1A 1-1 ALLOWABLE LIMITS PER DETAIL 1- OK TO CONTINUE IAW M105FILE NR 593048.SDR BSYA2009057AEngine · failedAIRCRAFT EN ROUTE FROM BIH TO VCV WHEN BOTH ENGINES QUIT AT 16,000FT. AFTER DESCENDING 2,000FT PILOT WAS ABLE TO GET BOTH ENGINES RUNNING AGAIN AND THEN RETURNED TO BIH. MAINTENANCE CHECKED FUEL, FUEL WAS OK. RAN AIRCRAFT, NO PROBLEMS NOTED. FLIGHT DEPT THSDR HALA09F00133Engine · power lossETOPS SIGNIFICANT SYS - BOTH ENG APPEARED TO LOSE ENG THRUST. ENG PARAMETERS NORM FOR THRUST OBTAIN PLS SEE ACARS MESSAGE SEND TO MOC ON OUR T/S. PREFORMED FIM 22-00-02-1 FIG 101- NO FAULTS NOTED. PREFORMED MCDP TEST 30-NO FAULTS. PREFORMED FMC TEST 01-TMC TESDR FDEA200912024328Ecu · malfunctionedLEAVING FL 180 ON DESCENT NR 3 ENG RPM LOW INDICATION. N1 20 PERCENT,N2 50 PERCENT, EGT 400. NO OBVIOUS DAMAGE TO ENGINE. ATTEMPTED RE-START AND ENGINE RE-STARTED BUT INDICATIONS ONLY WENT BACK TO N1 20 PERCENT, EGT 400, AND N2 50 PERCENT. ENG HUNG THERE SDR 2009FA0001048Bearing · failedS.O.A.P. SAMPLE REVEALED A TRACE OF CARBON STEAL, ALUMINUM AND GRIT (CARBON/GRIT) WITH MAJOR AMOUNTS OF M50 WITH SHINY PLATELETS. THE FILTER WEIGHT WAS 7,806 MGS. THE ENGINE WAS DISASSEMBLED IAW THE CURRENT MM AS REQUIRED TO ACCESS ALL BEARINGS. DISASSEMBLYSDR A6WA200940781Engine · fluctuatesON CLIMB ABOVE 10000 FT RT ENG FLUCTUATIONS, APPROX 2 PERCENT N1 AND N2, 200 LBS F/F AND 20/30 DEG ITT FOR SEVERAL MIN, THEN ENG STABILIZED, ON DESCENT AND APPROACH MULTIPLE REPEAT EPISODE OF FLUX EXPERIENCED FDR EVENTS NOTED. EMERGENCY DECLARED, LANDED WITHOSDR EIAA200900132Engine · malfunctionedNR 3 ENGINE SURGE/STALL AT MAX TAKEOFF POWER. EGT EXCEEDANCE 1088 DEG CELSIUS. REMOVED AND REPLACED NR 3 ENGINE PER WORKCARDS F7201, F7204, F7207, F7209. OPS & LEAK CHECK GOOD.SDR USAA2009112593230Engine · flamed outFLT 1019 - MHT TO CLT - EMERGENCY LANDING - ON TAKEOFF THE NR 2 ENGINE HAD A COMPRESSOR STALL AND THE AIRCRAFT RETURNED TO MHT. AN EMERGENCY WAS DECLARED, EMERGENCY VEHICLES WERE DISPATCHED. THE AIRCRAFT LANDED AND TAXIED TO GATE WITHOUT FURTHER INCIDENT. REPLSDR CA091215008Engine · smoke(CAN) DURING FLIGHT, THE CUSTOMER REPORTED SMOKE IN THE CABIN. PRELIMINARY INSPECTION FOUND OIL RESIDUES BEHIND THE FAN, ENGINE IS LIKELY TO BE REMOVED AND MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION ISSDR QXEA2009113001011Engine · odorBURNING ODOR THROUGHOUT CABIN AND COCKPIT AFTER BLEED SELECTOR WENT TO NORM AT 1000' LAV SMOKE DETECTOR SOUNDED. BOTH BLEED 1 AND 2 WERE ON AND PACKS WERE IN AUTO. ODOR SUBSIDED BEFORE WE COULD ISOLATE IT'S SOURCE VIA E/A CHECKLIST. RETURNED TO FIELD. LANDINGSDR IPXA09157957Engine · unserviceableINSPECTION TYPE:N/A AT FL 330 ECAM ADVISORY-LOW OIL QTY NR 1 ENGINE. ECAM AND OIL QTY GAUGE BOTH INDICATED OIL QUANTITY 0 ON NR 1 ENGINE. NR 1 ENGINE PRES AND TEMP NORMAL THROUGHOUT FLIGHT. CONTINUED TO RUN ENGINE AND IT PERFORMED WITHIN LIMITS IN ALL PWR RSDR HNAA2009112400337Engine · malfunctionedDURING CLIMB OUT NR 1 ENG TORQUE FLUCTUATED FROM 90 PERCENT TO 50 PERCENT THEN BACK TO 90 PERCENT WITH NO ASSOCIATED CAUTION LIGHTS. INSPECTED AND FOUND C/B J7, NOT PULLED AND COLLARD IAW MEL 73-2. NR 1 ENG ECU PREVIOUSLY ON MEL REFERENCE LOG PAGE 036751, ISDR WX0A070480Engine · failedUPON CLIMBOUT IN A RIGHT TURN A LOUD POP WAS HEARD AND THE ACFT LURCHED. NR 1 ENGINE N1 AND N2 SPOOLED DOWN AND EGT ROSE TO JUST UNDER 800 DEGREES. PERFORMED EQRH, SEVERE ENGINE DAMAGE CHECKLIST. MAINTENANCE DEPARTMENT PERSONNEL REMOVED AND REPLACED THE 31 SDR IXXA090067OEngine · vibrationDURING CRUISE, THE CREW NOTICED AN ABNORMAL VIBRATION FROM THE NR 2 ENG, THEN A LOSS OF OIL PRESSURE AND OIL QUANTITY. SHUTDOWN NR 2 ENG AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT.SDR 2009FA0000960Fuel Control · contaminatedA CT-58 FUEL CONTROL UNIT (FCU) PN 725725-5 SN 29172)) , STATOR VANE ACTUATOR (SVA) PN
4004T63G10 SN KTR4579BR)) , AND PILOT VALVE (PV) PN 6028T23G01 SN KTR3098BR)) WERE
DELIVERED BY THE NTSB AND CARRIER FOR INSPECTION. INITIAL DISASSEMBLY OF THE FCU,
SVA, SDR CA091209003Bearing Race · failed(CAN) THE ACFT CAME IN FOR A CHIP LIGHT SNAG AND WHEN THE MX DEPARTMENT INSPECTED CHIP DETECTOR IT WAS NOTED TO HAVE QUITE A BIT OF METAL ON THE DETECTOR. ENG SHOP WAS NOTIFIED AND IT WAS DETERMINED THAT A REPAIR WAS NECESSARY AT THAT TIME. GEARBOX WAS REMOVSDR UALA2009111703584Engine · separatedCREW REPORT: LEFT ENGINE WOULD NOT SHUTDOWN WITH FUEL CONTROL SWITCH, PULLED FIRE HANDLE TO SHUT DOWN. FOUND NR 1 ENG, INTERMEDIATE PRS CHECK VLV SEPARATED FWD SIDE. LOW STAGE HOT AIR DAMAGED MULTIPLE WIRES UNDER VLV ON WIRE BUNDLES "W3506"AND "W3538" BELONSDR CBR2010F00000Engine · power lossWHILE IN CRUISE FLIGHT, RETURNING FROM SIGHTSEEING TOUR, PILOT NOTICED THE N2/NR LOWER THAN NORMAL. THE PILOT MADE SEVERAL COLLECTIVE ADJUSTMENTS IN AN ATTEMPT TO BRING THE RPM UP, WHICH RESULTED IN A FURTHER DECAY OF THE RPM TO 94 PERCENT. AFTER RADIO CONSUSDR AALA20091116ORD01Engine · failedON FINAL NUMBER ONE ENGINE BEGAN TO VIBRATE AND SURGE. MOVED THROTTLE TO IDLE. LANDED WITHOUT INCIDENT. FOUND METAL IN TAILPIPE. REPLACED NUMBER ONE ENGINE ON 17 NOV 2009 AT ORD.SDR AALA20091116DFW01Engine · making metalRIGHT ENGINE COMPRESSOR STALL AT CRUISE FOLLOWED BY THE NUMBER TWO ENGINE OIL FILTER BYPASS INDICATION. CREW SHUT DOWN NUMBER TWO ENGINE AS PRECAUTION. LANDED DFW WITHOUT INCIDENT. FOUND HEAVY METAL DEPOSITS IN CHIP DETECTORS. REPLACED NUMBER TWO ENGINE ONSDR MDG2009Engine · shutdownPILOTS REPORTED ENG SHUTDOWN DURING FLIGHT. MX REPORTED UPON INSP THAT THERE WAS A GRINDING SOUND INTERNAL TO THE ENG WHEN THEY TRIED TO ROTATE THE ENG BY THE STARTER. ENG WILL BE REMOVED AND SENT TO THE O/H SERVICE CTR FOR EVALUATION FOR REASON OF FAILURE.
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