JASC 7200
Service difficulty reports · 14,727
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 SWAA2023062670970Engine · hung startENG #1 REQUIRED A RESTART AFTER A HUNG START. 2ND ENGINE START NORMAL INCLUDING ALL INDICATION. APPROX 5 MIN LATER PAX REPORTED FLAMES FROM #1<[01] C/W FIM TASK 71-05-811; NO DEFECTS NOTED. VERIFIED OIL CONSUMPTION WITHIN LIMITS. (.431/HR).SDR AALA202306267387Engine · stalledAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DSM. #2 ENGINE FAIL ON CLIMB AT APPROX 17,000 FEET LOUD BANG AND VIBRATION. IT WAS REPORTED THAT THE #2 ENGINE SUFFERED A LOSS OF OIL PRESSURE AND SUBSEQUENT INFLIGHT SHUT DOWN AFTERSDR QR9R2023062300003Gearbox · failed inspDURING RUN ON TORQUE CHECK OF MOD 1, AFT L/H THREAD INSERT PULLED OUT WITH BOLT. UNABLE TO REPAIR INSERT IAW EMM 70-35-03-470-801-A01. REPLACED MOD 1 ACCESSORY GEARBOX IAW EMM 72-00-61-900-801-A01.SDR DALA2023062205065Unknown · unknownSHIP 3161 WHILE REMOVING THE #2 ENGINE NOSE CONE SPINNER, FOUND 1 HELICOIL BROKEN. REMOVED FROM NOSE CONE. CORRECTIVE ACTION REMOVED AND REPLACED THE FRONT SPINNER CONE IAW AMDS 7221-9601-02. (2828004)SDR 2023FA0000355Engine · damagedENGINE FAILURE DURING NORMAL DESCENT FROM PARACHUTE OPERATIONS. APPARENT TURBINE FAILURE AND ASSOCIATED COWLING DAMAGE. NO INJURIES OR ADDITIONAL AIRCRAFT ISSUES. AIRCRAFT LANDED SAFELY. ENGINE HAS BEEN SHIPPED TO SHOP FOR INSPECTION.SDR TAMF20230620035Engine · leakingENG #2 WAS FOUND WITH A FUEL LEAK IN THE OUTSIDE AREA ON THE LEFT SIDE OF THE IP COMPRESSOR.
THE ENGINE FUEL TUBE P/N FK24001 AND OIL TUBE P/N FW15740 WERE REMOVED AND REPLACED IN ACCORDANCE WITH AIRBUS AIRCRAFT MAITENENCE MANUALS AMM 75-33-51-400-801-A & 72-SDR AALA202306238657Engine · stalledAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO JAX. AFTER TAKEOFF AT APPROX 2000 FT MULTIPLE LOUD BANGS AND AIRCRAFT YAW. POWER WAS REDUCED AND IT WAS DETERMINED THE #2 ENGINE OIL QUANTITY WAS FLASHING AND READING BETWEEN 0.0 ANDSDR AALA202306198657Engine · stalledAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO JAX. AFTER TAKEOFF AT APPROX 2000 FT MULTIPLE LOUD BANGS AND AIRCRAFT YAW. POWER WAS REDUCED AND IT WAS DETERMINED THE #2 ENGINE OIL QUANTITY WAS FLASHING AND READING BETWEEN 0.0 ANDSDR SWAA2023061959908Engine · surgesAT 9;000 FEET ENGINE NUMBER 2 SURGED A LITTLE BIT LATER EGT WENT UP INTO THE RED. #2 ENGINE FAILED. RETURNED TO BNA. NO OVERWEIGHT LANDING.<[01] REMOVED AND REPLACED #2 ENGINE ON MT # 771-00-01 (REM/INST - POWER PLANT). SEE MT FOR ALL COMPLETED WORK AND SIGN-OSDR NACA20230720002Unknown · unknown#2 ENGINE.- DURING ACCOMPLISHMENT OF AD 200-16-51 WAS FOUND RH 5TH STAGE ENGINE BLEED VALVE CORRODED AND STUCKED P/N 3202222-1 AND S/N 2243. "REMOVED AND REPLACED RH 5TH STAGE ENG BLEED AIR CHECK VALVE IAW B737 AMM 36-11-35 PAG 401-408. PERFORMED LEAK CHECK IASDR QR9R2023061400001Engine · warning message#1 AND #2 ENG PA DIS CAUTION LIGHTS ILLUMINATED IN FLT WITH A 4.5% DIFFERENCE BETWEEN THE BOTH ENGINES N1. REMOVED AND REPLACED #2 ENGINE.SDR DXTA2023061488650Accelerometer · failedRIGHT ENGINE ENGINE VIBRATION INDICATION: DESCENDING OUT OF 35000 THE RIGHT N2 VIB MESSAGE ILLUMINATED ON THE RIGHT N2 DIAL FOR ABOUT 10 SECONDS. DID NOT SEE ANY OTHER INDICATIONS ALTHOUGH IT DID SOUND LIKE A VERY SLIGHT CHANGE IN ENGINE HUM OCCURRED. THE VIB SDR HALA2023061400033Unknown · unknownON CLIMBOUT LEFT ENGINE COMPRESSOR STALL. RETURNED BACK TO AIRPORT ATB. FOUND LEFT ENGINE NOSE CONE MISSING PROTECTIVE COATING. PERFOMED INSPECTION AFTER HIGH POWER SURGE PER AMM 72-00-00-200-801 UP TO STEP 2.D.(3) MECH 19196 06/14/23 COMPLETED REMAINING STEPSSDR CALA2023061401851Engine · vibrationDURING CLIMB HIGHVIBRATION NUMBER 2 ENGN1 INDICATION 9.9 E2 PHOTOS ATTACHED UPDATING LOGPAGE TO REFLECT SDR. REPLACED #2 ENGINE. SEE JC 31-7100-9-0001 FOR APPLICABLE SIGNOFFS. ALL RII TASKS ACCOMPLISHED FOR E2 ENGINE CHANGE REF JC 31-7100-9-0001 AND RII GMM 09SDR 2023F00187Gearshaft · abnormalON FEBRUARY 10, 2023 THIS AGB WAS RECEIVED BY STS MAINTENANCE ORGANIZATION (EASA FR.145.0229) FOR AN OVERHAUL (NOT RELATED TO THIS EVENT) FROM CUSTOMER ROLLS-ROYCE NORTH AMERICA. THIS AGB WAS NEVER SERVICED BY STS BEFORE. DURING DISASSEMBLY, IT WAS OBSERVED TSDR GTIA2023060937248Engine · failedENG 1 FAILURE ON CLIMB 5100 FT-ENGINE CHANGE IN PROGRESSSDR SWAA2023061257222Engine · fireAFTER ENGINE SHUTDOWN;SMALL FIRE ON #1 ENGINE EXHAUST;AT 5:00 POSITION.<REMOVED AND REPLACED #1 ENG. PER MT771-00-01 REF TTG8Q00LJY44SDR CALA2023060901793Filter Element · warning messageENG FUEL FILTER R EICAS ADVISORY THE FUEL FILTER IS APPROACHING OR AT A FILTER BYPASSING CONDITIO N. DIFFERENTIAL PRESSURE TRANSDUCER MEASUREMENT FOR THE RIGHT E NGINE FUEL FILTER IS ABOVE THE IMPENDING BYPASS OR THE BYPASS LI MIT. THE CONFIRMATION TIMER FORSDR CALA2023060901789Engine · unknownON INITIAL TAKEOFF ROLL USING A-T, AT ABOUT MID POWER RANGE, THE RIGHT ENGINE FAILED TO CONTINUE TO ACCEL AND CREW HEARD COMPRES SOR STALL INCL WHITE EXAUST FUMES DURING FAILURE. THEY REPORTED NO ENGINE EXCEEDANCES. STATUS PAGE SHOWS "ENG CONTROL R" AND "EN G SDR CALA2023060701765Panel · unknownPDA 1 REF LP 4785250, FLAGGING PDA. NO 1 ENG FAN STATOR CASE OUTER ACOUSTIC LINER BETWEEN 4 & 6 O''CLOCK FACING AFT DEBONDED. TOTAL SURFACE OF DEBONDING IS 47" X 12" = 564 " SQ. FOUND ON WALKAROUND.SDR DALA2023060704641Unknown · unknownSHIP 3256 -ATB- RETURNED TO MSP DUE TO HIGH ENGINE VIBRATION ON NBR 2 ENGINE @ APPROX. 2,000 FEET, PEAK 7.2. AIRFRAME VIBRATION ASSOCIATED WITH EVENT. VIBRATION LESSENED WITH THRUST REDUCTION. CORRECTIVE ACTION: PERFORMED VISUAL INSPECTION OF FAN INLET AND ENGSDR SWAA2023060656173Engine · failed#2 ENG FAIL & ASSOCIATED LOUD BANG ON T/O ROLL. ABORTED T/O AT <80KTS A/C ABORTED TAKEOFF @ 80 KTS DUE TO #2 ENG FAILURE AND ASSOCIATED LOUD BANG ON TAKEOFF ROLL. REPORTED ENGINE DEBRIS ON RUNWAY. EMERGENCY EQUIPMENT MET THE AIRCRAFT AND GAVE ALL CLEAR FOR RETSDR UIEA2023060540560Plug · unknownENG #2 BORSCOPE, PLUG AP-9 DAMAGED(<P>REMOVED & REPLACED ENG #2 BORESCOPE PLUG AP-9 IAW 767-300 AMM 72-00-00. NO FURTHER DEFECTS NOTED.</P>)SDR AALA202306237431Engine · stalledAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO LAS. ON TAKEOFF FROM SLC, FLIGHT CREW HEARD LOUD BANG AND BRIEF SHUDDER AT 800' AGL. #2 ENGINE HAD BRIEF OVERTEMP FOR 5-10 SECONDS,THEN RETURNED NORMAL. CREW SUSPECTED BIRD STRIKE ANSDR AALA202306067431Engine · stalledAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO LAS. ON TAKEOFF FROM SLC, FLIGHT CREW HEARD LOUD BANG AND BRIEF SHUDDER AT 800' AGL. #2 ENGINE HAD BRIEF OVERTEMP FOR 5-10 SECONDS,THEN RETURNED NORMAL. CREW SUSPECTED BIRD STRIKE ANSDR CALA2023060501755Engine · damagedBIRD HIT LEFT ENG ON TO EGT WENT INTO RED. PERFORMED VISUAL INSPECTION OF #1 ENGINE AND FOUND BIRD WAS INGESTED INTO CORE AT 4 OCKLOCK POSITION OF ENGINE FIRST STAGE INLET GUIDE VANES, REQUIRES FURTHER INSPECTION. SDR REPORTING EGT PIC UPDATE. REMOVED AND REPLSDR QMLA2023060420043Unknown · unknownUPON DEPARTURE FROM KPDK, ENG CHIP LIGHT ILLUMINATED ON THE WARNING PANEL. IT WENT OUT AFTER A FEW SECONDS. LANDED AS SOON AS POSSIBLE BACK TO KPDK AND SHUT DOWN ENGINE, CHECKED THE CHIP PLUGS AND THERE WAS NOTHING ON THEM. GROUND RUN THE AIRCRAFT WITH NO LISDR ASAA2023060143423Blade · peelingREF ASA T/C # 78472010 CFM56-7 FAN BLADE LUBRICATION FOUND #2 PLATFORM RUBBER SEAL PEELED OFF. GROUNDED - YES. REMOVED AND REPLACED TWO PLATFORMS ON THE #2 ENGINE PER TASK CARD 78472010 AND PERFORMED VIBRATION SURVEY PER B737-800 AMM 71-00-00. CHECKS GOOD.SDR COEA2023053103976Engine · low pressureFLIGHT 8744, ENROUTE GEG - YKM - DISCREPANCY: AIRCRAFT LOST OIL PRESSURE AND ENGINE TORQUE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. ONCE ON THE GROUND THE PILOT REPORTED OIL ALL OVER THE ENGINE COWLING AND WINDSHIELD. ENGINE REPLASDR AALA202305317032Unknown · unknownAIRCRAFT WAS NOT GROUNDED: ON TAKEOFF FROM JFK, AIRCRAFT HIT BLOWN TIRE DEBRIS FROM PRIOR DEPARTING AIRCRAFT. EMERGENCY DECLARED ON APPROACH TO AUS. AIRCRAFT LANDED SAFELY. MAINTENANCE ACCOMPLISHED ENGINE FOREIGN OBJECT DAMAGE AND BIRDSTRIKE INSPECTION PER AMMSDR DALA2023053104365Unknown · unknownSHIP 3410 ODOR EVENT CAUSED BY RIGHT ENGINE. CORRECTIVE ACTION: REMOVED & REPLACED EXTERNAL GEARBOX BREATHER SHAFT ASSEMBLY. (2790177)SDR DXTA2023053087310Engine · bird ingestionAFTER ROTATION LESS THAT 20 AGL, RT ENG INGESTED A LARGE BIRD, CLIMBED TO BURN FUEL, RAN CHECKLISTS & BRIEFED THE RETURN TO LANDING PLAN. THROUGHOUT THE FLIGHT, THE RIGHT ENGINE PRODUCED POWER AND ITS PARAMETERS WERE QUITE CLOSE TO THE LEFT ENGINE: N1 WAS EQUSDR A6WA202305288615Engine · damagedITT ON RIGHT ENGINE INCREASED TO 840C ON 85% N1 ON BOTH ENGINES, WITH VIBRATIONS AT FLIGHT LEVEL 190. REDUCED POWER VIBRATION ON N2 TWICE FOR 1 SEC EACH. AND N1 VIBE AT 2.7MIL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED BOROSCOPE INSPECTION OF RH ENGINE COLD SSDR 2023F00252Platform · brokenHIGH VIBRATION ON ENGINE #2 (INDICAION REACHED 4.5) DURING TAKEOFF. PROBLEMA CAUSED BY PLATFORM -FAN BL DETACHMENT.SDR ASAA2023052643389Hook · wornWHILE PERFORMING T/C SBCFM56-7B-1074-1 ON THE #2 ENG, ESN 804633 NOTED THAT THE STAGE 3 J-HOOK WAS WORN COMPLETELY THROUGH @ THE 12 O'CLOCK POSITION. GROUNDED - YES. REMOVED #2 ENGINE. TRANSFERRED DEFECTS TO SHOP W/O #1955720.SDR 2023FA0000572Bearing Race · brokenTORQUE SENSOR BEARING INNER RACE FAILED [PN: 3103585-1 TSN: 1,319.2, CSN: 898].SDR ASAA2023052443360Engine · damagedWHILE ACCOMPLISHING ASA SBCFM56-7B-72-1074-1. FOUND ON STAGE 3 SLAB PIN AT THE 9 O'CLOCK POSITION LIBERATED. CAUSING DAMAGE TO THE J-HOOK AND SPOOL. REQUIRES ENGINE CHANGE ON #1 ENG S/N 804245. GROUNDED - YES. REMOVED ENGINE S/N 804245. REFERENCE ASA SHOP W/O SDR AALA202305257102Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAS. ON TAKEOFF #2 ENGINE HAD OVER TEMPERATURE INDICATION. THE AIRCRAFT LANDED SAFELY AT LAS WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 77-00-00-810-849-A EGT 962 24 SECOSDR AALA202305252598Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAS. ON TAKEOFF #1 ENGINE HAD OVER TEMPERATURE INDICATION. THE AIRCRAFT LANDED SAFELY AT LAS WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 77-00-00-810-849-A EGT 971 21 SECSDR CALA2023052401621Engine · making metalENG OIL SYS R ENGINE OIL PRESSURE IS LOW INDICATING PROBLEM WITH ENGINE OIL PU MP. FIM TASK REF : G73-90-F8-04A-421C-A CMC MSG# 7332682 FLIGHT STATUS: A INTERMITTENCE CODE: M PH: CRUISE NARRATIVE: ELECTRONIC ENGINE CONTR OL CHAN-B (RIGHT ENG) CMC MSG# 7332682 SDR AALA202307286816Actuator · warning messageAIRCRAFT WAS GROUNDED: AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. AFTER TAKEOFF THURST IN CLIMB DETENT ECAM MESSAGE ENGINE 2 EGT OVER LIMIT. CREW FOLLOWED ECAM PROCEDURES RETARDED #2 THRUST LEVER UNTIL EGT WITHIN LIMITS APPROX 3% N2 LESS THANSDR AALA202307287487Solenoid Valve · defectiveAIRCRAFT WAS GROUNDED: AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. AFTER TAKEOFF THURST IN CLIMB DETENT ECAM MESSAGE ENGINE 2 EGT OVER LIMIT. CREW FOLLOWED ECAM PROCEDURES RETARDED #2 THRUST LEVER UNTIL EGT WITHIN LIMITS APPROX 3% N2 LESS THANSDR AALA202307283610Solenoid Valve · defectiveAIRCRAFT WAS GROUNDED: AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. AFTER TAKEOFF THURST IN CLIMB DETENT ECAM MESSAGE ENGINE 2 EGT OVER LIMIT. CREW FOLLOWED ECAM PROCEDURES RETARDED #2 THRUST LEVER UNTIL EGT WITHIN LIMITS APPROX 3% N2 LESS THANSDR AALA202307282209Solenoid Valve · defectiveAIRCRAFT WAS GROUNDED: AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. AFTER TAKEOFF THURST IN CLIMB DETENT ECAM MESSAGE ENGINE 2 EGT OVER LIMIT. CREW FOLLOWED ECAM PROCEDURES RETARDED #2 THRUST LEVER UNTIL EGT WITHIN LIMITS APPROX 3% N2 LESS THANSDR AALA202307287566Bleed Valve · defectiveAIRCRAFT WAS GROUNDED: AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. AFTER TAKEOFF THURST IN CLIMB DETENT ECAM MESSAGE ENGINE 2 EGT OVER LIMIT. CREW FOLLOWED ECAM PROCEDURES RETARDED #2 THRUST LEVER UNTIL EGT WITHIN LIMITS APPROX 3% N2 LESS THANSDR AALA202307280927Solenoid Valve · defectiveAIRCRAFT WAS GROUNDED: AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. AFTER TAKEOFF THURST IN CLIMB DETENT ECAM MESSAGE ENGINE 2 EGT OVER LIMIT. CREW FOLLOWED ECAM PROCEDURES RETARDED #2 THRUST LEVER UNTIL EGT WITHIN LIMITS APPROX 3% N2 LESS THANSDR AALA202305196816Unknown · unknownAIRCRAFT WAS GROUNDED: AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW. AFTER TAKEOFF THURST IN CLIMB DETENT ECAM MESSAGE ENGINE 2 EGT OVER LIMIT. CREW FOLLOWED ECAM PROCEDURES RETARDED #2 THRUST LEVER UNTIL EGT WITHIN LIMITS APPROX 3% N2 LESS THANSDR DXTA2023051886460Unknown · unknownSMOKE IN COCKPIT / CABIN: IRRITATING CHEMICAL/OIL LIKE ODOR FROM WEMAC AIR OUTLETS JUST AFTER TAKEOFF AT HIGH ENGINE POWER SETTINGS SUCH AS T/O AND CLB POWER. APU IS DEFERRED. RETURNED TO FIELD. COMPLIED WITH ENVIRONMENTAL CONTROL SYSTEM BLEED AND TRIM AIR DUSDR M17F2023060500001Engine · failedENGINE #1 FAILS DURING ENGINE START ON THE GROUND, QRM PROCEDURESDR CALA2023051501505Engine · fireRTO DUE TO FLAMES REPORTED FROM ENGINE #1 BY ANOTHER AIRCRAFT. REJECTED BELOW 100KIAS. REF TASK05-51-07-210-801, INSPECTED TIRES AND BRAKES FOUND NO IS OK FOR SERVICE. EVIDENCE OF HEAT DAMAGE. TIRE PRESSURES WERE ALL IN NORMAL RANGE. PER TASK DUE TO GROSS WEIG
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