JASC 7200
Service difficulty reports · 14,726
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 IPXA2025082060238Engine · overtempDIVERSION, EMERGENCY DECLARED, DURING CLIMB PASSING APPROXIMATELY 20,000 FT WITH EPR'S MATCHED AT CLIMB POWER WE NOTICED RIGHT HAND ENGINE EGT AMBER AT 800 DEGREE AND CLIMBING. IN ADDITION, N1 AND FUEL FLOW WERE SEE ATTACHED PAGE. PERFORMED FIM TASK 73-21-00/SDR DALA2025082106238Engine · bird ingestionSHIP 3228 DISC: MULTIPLE BIRD STRIKES ON FINAL APPROACH TO CHS EVIDENCE OF BIRDSTRIKE TO NR 2 ENGINE SMELLS IN CABIN. SMOKE/FUMES QUESTIONARE FORM SUBMITTED. C/A : C/W BIRD STRIKE INSPECTION IAW AMM 05-51 FOUND EVIDENCE OF BIRD STRIKE IN #2 ENGINE. C/W WITH BISDR CALA2025082208056Control Unit · faultedRTO DUE TO LEFT ENG SURGE AND STALLDEBRIEF FROM CREW PUSHING THROTTLES UP TO 70% N1 LH ENG SLOW TO ACCELERATE. ENGAGED AUTO THROTTLE AND ENGINE SPOOLED UP AND THENN1 ROLLED BACK TWICE TO 90% N1. F/O MAY HAVE SEEN EXCEEDANCE BUT NO RED BOX SHOWING. CREW HAD NO SDR QMLA2025081320086Engine · faultedWHILE AT CRUISE FLIGHT THE NR 1 ENGINE TORQUE BEGAN TO RAPIDLY RISE WITH INCREASED ENGINE NOISE AND RISING ROTOR RPM. DURING THAT SAME TIME THE AIRCRAFT BEGAN A YAWING MOTION. IMMEDIATELY ADJUSTED POWER AND MANUALLY
ADJUSTED THROTTLE NR 1 TO REGAIN CONTROL ASDR YENA2025081400838Engine · failedFLT#547, ISP-MCO. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO JFK, AFTER T.O. ENG #2 FAIL. OPENSDR ABXA20250813175Manifold · crackedON TAXI R ENG HAD VIBRATIONS FROM 2.8 TO 3.3. WHEN ADDING TAXI THRUST VIBRATION INDICTIONS UP NTO 4.9 AND STARTED BEING VARIABLE- VIBRATION FELT IN AIRFRAME. AIRCRAFT RETURNED TO BLOCKS. (BTB). PERFORMED D.V.I OF RT ENG & FOUND UPPER & LOWER LPT COOLING AIR SDR ANCF2025081400224Engine · vibrationENG 1 FAIL REQUEST TO DOWNLOAD FDR DURING INITIAL TAKEOFF, WHEN T.O THRUST WAS APPLIED. A LOUD BANG FROM THE ENG 1 LEFT SIDE WAS HEARD, FOLLOWED BY AN ENG FAIL ECAM, VIBRATIONS COMING FROM THAT SIDE COOLD BE FELT.SDR ANCF2025081323Engine · bird ingestionDURING TAKE OFF ROLL BIRD STRIKE ON ENGINE ONE VIBRATION 2,7 ON ENGINE ONE AND N1 AND LOUD NOISE (2.7 VIBRATION ON N1 ENGINE NUMBER ONE) NO MAYDAY NO PAN PAN SUST PRIORITY DURING RETURN DURING CRUISE EGT DIFFERENCE 30 ° C ON ENGINE ONE LANDING WEIGHT 63.1 TSDR DALA2025081306041Engine · fireATB- -IFSD- LEFT ENGINE FIRE ON TAKEOFF, PERFORMED ENGINE IFSD. FOUND SEVERE DAMAGE TO THRUST REVERES AND CORE COWLS. REPLACED LEFT ENGINE.SDR 2025FA0000565Shaft · corrodedCORROSION PITTING REMAINED ON THE SHANK NUT HOLE LOCATION 30 OF ESN 26028 IPC REAR STUB SHAFT AFTER MACHINED TO THE MAXIMUM LIMIT IAW RR EM FRSC383. PART WAS REJECTED BY RR TV255302 (CSN: 2473 SDC) WHICH IS RETIRED BEFORE ITS DECLARED LIFE IN TLM (7123 SDC).SDR DALA2025081806141Seal · leakingDIRTY SOCK ODOR DETECTED ON SHORT FINAL AGTER ENGINE HAD BEEN AT IDLE/LOW POWER FOR A SIGNIFICANT TIME. REPLACED BOTH ENGINE INLET COVER SEALS AND PERFORMED DUCT BURNOUT LEVEL B DECONTAMINATION A321 NEO AMM 21-00-00-615-803-A & AMM 36-10-00-615-805-A. (LP 73SDR UIEA2025080901117Engine · vibrationNR 2 ENG EXCESSIVE VIBRATION 4.5 N1. NO CHANGE WHEN THROTTLE REDUCED AT CRUISE LEVEL. VIBRATION FELT THROUGH RUDDER PEDALS. MAX RECORDED 5.0(<P>#2 ENG 2 EACH BALANCE WEIGHT REMOVED, ENG #2 VIB TRIM BALANCE PERFORMED IAW AMM 71-00-00 & AMM 72-31-00. RESULT MAX SDR IXXA2025080117038Engine · faultedUPON LANDING HEARD A LOUD BANG AND FLASH OF LIGHT BOTH FROM THE LEFT SIDE OF AIRCRAFT. NO OTHER IRREGULAR ITEMS NOTED. ACCOMPLISHED EXTERIOR INSPECTION WITH NO DAMAGE, DEFECTS, OR ANY OTHER ABNORMALITIES NOTED. ACCOMPLISHED LEFT ENGINE VARIABLE STATOR VANE ANDSDR NI6R202508100063Engine · flamed outPILOT REPORT: WE WERE ORBITING THE FIRE AT 10,500' IN A RIGHT TURN, WITH BOTH ENGINES STABILIZED AT 200 HORSEPOWER EACH AND FUEL FLOWS AT 200 LBS./HR. EACH WHEN I FELT A YAWING MOTION THAT I INITIALLY THOUGHT WAS WAKE TURBULENCE. LOOKING AT THE ENGINE INSTRUMESDR DALA2025080805955Engine · odorDIRTY SOCK SMELL NOTICED ON TAKEOFF ROLL AND EARLY CLIMB OUT. REMOVED AND REPLACED NR 1 ENGINE IAW AMDS 7100-9901-LT.SDR YENA2025080800817Engine · odorFLT#8385, BOS-JFK. REF LP # 4339985 ITEM # 1(DIRTY SOCK ODOR AFTER APPLICATION OF T.TO THURST AND DURING DECENT WITH IDLE POWER) DIRTY SOCK SMELL. RAN ENG 1 AND 2. WHILE ENGINES RUNNING ISOLATED L AND R PACKS TO DISCOVER OIL SMELL APPARENT WHILE ON ALONE. SMELSDR UIEA2025080501089Engine · faultedLOW SPEED REJECTED, #1 ENG 2.5-3.0 BELOW REQ T/O THRUST. EGT #1 EXCEED 952 SOLID RED BOX AROUND EGT. RED BOX FOR 5 SECONDS(<P>MX IN WORK WHILE IN AOGM FOR RTO ENG 1 EGT LIMIT. AOGM ETR: 10AUG25</P>)SDR DALA2025080605884Engine · vibrationSHIP 3022 - ATB - RETURNED TO MSP DUE TO #2 ENGINE HIGH VIBRATIONS WITH AUDIBLE RUMBLE. CORRECTIVE ACTION: FOUND DAMAGE TO FAN BLADES FROM BIRD STRIKE. REPLACED BLADES NBR 2, 20 AND 3, 21. (LP 7827314)SDR 2025FA0000536Engine · fireFOLLOWING A REPAIR CARRIED OUT, THE ENG WAS SENT FOR TESTING. ENGINE UNDERGOING TESTING (TEST 003) , & FLAME COMING OUT OF UPPER LT UNDERCOWLING OBSERVED. ITP THROTTLE OPERATOR DECELERATED & ACTIVATED THE FIRE EXTINGUISHER BOTTLE. AFTER THE INCIDENT, ENG WASSDR AALA202508087634Solenoid Valve · faultyAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THAT WHILE AT FL340 IN SMOOTH AIR, #1 ENGINE EXPERIENCED AN ENGINE STALL. THE ECAM WAS ACCOMPANIED BY A BRIEF AND ISOLATED "BUMP" SIMILAR TO TURBULENCE. NO NOTICEABLE DECREASE IN THRUST WAS EXPERIENCED AND ENGINE PARSDR CALA2025080607384Engine · stalledC/W NR 2 ENGINE STALL INSPECTION IAW AMM 71-00-00-200-805-G00. PILOT OBSERVED VSV LAG WITH FUEL FLOW ON ONE OCCURANCE WITH LOSS OF THRUST , ON SECOND OOCCURANCE NOTED VSV LEAD ON FUEL FLOW . AT TIME OF OCCURANCES ALTITUDE WAS AT 35000 CLIMBING TO 36000. REPOSDR DALA2025073105754Engine · faultedDURING MTC DIRECTED #1 MANUAL ENGINE START, THE EGT EXCEEDED START LIMIT MOMENTARILY WITH AN ENG 1 START FAULT EGT OVER LIMITS MESSAGE, APPROXIMATED TO BE AROUND 723 OC FOR 2 - 3 SECONDS, RETURN TO GATE. GVI INLET AND EXHAUST. NO DAMAGE FOUND. REQUIRED BOROSCSDR IPXA2025072856371Acoustic Liner · brokenBROKEN ACOUSTIC LINER, NR 2 ENG FAN CASE MIDDLE 7:00 AREA. OK TO WORK.SDR CALA2025073107128Check Valve · faultedSTARTING ENGINE NR 2 WAS 2 1/2 MINS TO STARTER CUTOUT WITH STRONG EXHAUST ODOR IN CABIN. NR 2 ENGINE OPERATED IAW AMM 71-00-00-712-021-N00. DURING ENGINE OPS, INSPECTION OF CABIN CARRIED OUT IAW AMM 05-51-56-940-801-C1 TO IDENTIFY ODOR. NO UNUSUAL ODORS PRESSDR 2026F00041Engine · damagedUNKNOWN INTERNAL ENGINE COMPONENT CAUSING BURNING OF OIL AFTER ENGINE OVERHAUL AND REPLACEMENT OF ALL 4 TURBINE WHEELS. FIRST OCCURRENCE RECORDED AFTER SMOKE WAS OBSERVED COMING FROM THE EXHAUST WHEN THE AIRCRAFT WAS AT IDLE AND DURING SHUTDOWN AFTER A FLIGHTSDR 2025FA0000832Engine · failedENGINE FAILURE IN CLIMBSDR CALA2025072406883Engine · malfunctionedAT TO POWER SET ENG 1 DO UNT ONLY WENT TO 1.2EPR PULLED LEFT. ENG2 EPR NORM AT 1.46. PREFORMED FAULT ISOLATION REF FIM TASK 75-24-00-810-802B TO STEP 3.B.1 AND FOUND FAULT CODE HCCWAF. ACCOMPLISHED TEST NR 11 : HIGH POWER ASSURANCE TEST REF AMM TASK 71-00-00SDR SWAA2025072193105Blade · bent#1 ENGINE #18 BLADE DAMAGED DUE TO BIRD STRIKE AND SHOWS SIGNS OF BIRD INGESTION INTO THE COMPRESSOR SECTION. PERFORMED DVI; BORESCOPE AND BLADE PAIR REMOVAL AND REPLACEMENT IAW MT 772-21-19 AND 772-21-22 REFER TO TTG8Q01431JL AND TTG8Q0142NUK. AND BORESCOPESDR SWAA2025072193239Engine · power lossCLIMBING THROUGH 10000 FEET HEARD LOUD BANGS; AIRCRAFT SHOOK; OBSERVED N1 REDUCED TO APPROX 60% N1. REDUCED POWER AND ENGINE INDICATIONS RETURNED TO NORMAL. DID NOT DECLARE EMERGENCY. ENGINE NUMBER 1. REMOVED AND REPLACED #1 ENGINE PER [AMM 71-00-02-401-NG/ SDR UIEA2025071900978Engine · damagedENG #3 SEVERE DAMAGE. NO OIL QUANTITY. REMOVED AND REPLACED #3 ENGINE IAW AMM 71-00-02-004-001-J00. PERFORMED ENGINE TEST RUN IAW AMM 71-00-00-700-801-J00 TEST #3. ALL OPS SATISFACTORY AND NO LEAKS OBSERVED. REF W/O 149634.SDR DALA2025072305534Engine · fireSHIP 1812 - ATB- -IFSD- LEFT ENGINE FIRE ON TAKEOFF, PERFORMED ENGINE IFSD. CORRECTIVE ACTION: FOUND SEVERE DAMAGE TO THRUST REVERES AND CORE COWLS. ENGINE CHANGE AND REPAIRS IN PROGRESS.SDR DALA2025072205513Engine · unknownSHIP 3502 - RTB - DUE TO PASSENGER AT SEAT 20J NOTICED SMOKE COMING FROM THE BOTTOM OF THE #2 ENGINE AND ADVISED THE FA. THE FA CONTACTED THE FLIGHT DECK AND THE TAKEOFF WAS REJECTED. PERFORMED GVI AND RAN #2 ENGINE FOR 5 MINS. CONFIRMED NO SMOKE FROM EXHAUSSDR DALA2025071805434Engine · failedSHIP 3305 #1 ENG FAIL AT FL380 MACH 0.82 SMOOTH AIR. CHANGED ENGINE #1 IAW A330 AMDS JIC 7100-9901-01. (7314738).SDR YENA2025071700732Engine · stalledFLT#637, JFK-STI. (AIRCRAFT PERFORMED AN AIR TURN-BACK TO JFK AND AN EMERGENCY WAS DECLARED) "ENG 2 STALL DURING CLIMB ENG AUTO RELIGHT AND RESUMMED FULL POWER (NO IFSD); REF LOG PAGE 4310981 (INSTALLED BORO PLUG PORT C IAW AMM 72-00-00) BOROSCOPE FINDINGS FOUSDR AALA202507172094Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ABQ DUE TO THE FLIGHT CREW REPORTING THAT ON TAKEOFF #2 ENGINE OVERTEMP OCCURRED, FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND SHUT DOWN THE ENGINE. THE AIRCRAFT LANDED SAFELY AT ABSDR AALA202507152094Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ABQ DUE TO THE FLIGHT CREW REPORTING THAT ON TAKEOFF #2 ENGINE OVERTEMP OCCURRED, FLIGHT CREW ACCOMPLISHED ECAM PROCEDURES AND SHUT DOWN THE ENGINE. THE AIRCRAFT LANDED SAFELY AT ABSDR DALA2025071505302Engine · odorAIRCRAFT 5010, ON DESCENT THROUGH 14,000 FT BEGAN SMELLING AN ODOR, CONFIRMED WITH JUMPSEATERS SMELL. ALL 4 DONNED O2 MASKS. ODOR PERSISTED THROUGH DESCENT. 1 JUMPSEATER HIT DELUTER ON MASK SHORT FINAL TO SEE IF FUMES DISSIPATED. STATED FUMES WERE STRONGER. TASDR SCNA20250714257Engine · failedSEVERE ENGINE DAMAGE #2 CLIMBING OUT OF 14,000 FT REDLINE EGT NO ROTATION N2 N1 14% FA'S REPORTED ALOT OF SPARKS MODERATE VIBRATION. REMOVED AND REPLACED #2 ENGINE REF TASK CARD # 710000000 ACCOMPLISHED ENGINE RUN TEST 9 AND TEST 5 REF AMM 71-00-00 ALL SYSTESDR YENA2025071600729Engine · failedFLT#2922, NAS-JFK. (AIRCRAFT PERFORMED AIR TURNBACK TO NAS) "ENGINE #2 BANG AND SEIZE. INSPECTED ENGINE #2 IAW AMM 05-51-26 FOUND NO AIRFRAME DEFECTS ENGINE #2 METAL, DEBRIS FOUND IN EXHAUST REMOVED AND REPLACED #2 ENGINE IAW AMM 71-00-20-400-040. REFERENCE SDR SWAA2025071491117Engine · failedENGINE FAILURE AFTER DEPARTURE AT 3000. R&R #1ENGINE IN REF MT 771-00-01. OPS & LEAK CHECK GOOD. AIRCRAFT OK TO CONTINUE IN SERVICE.SDR CALA2025071606622Seal · faultedNR 1 ENGINE HAS EXPERIENCED AN INCREASE IN OIL CONSUMPTION. ACCOMPLISH A SNIFF CHECK OF OIL FOR FUEL ODOR, IAW AMM 12-13-01-130-803-002, STEP F.(1). ACCOMPLISH FIM 71-05 TASK 805, STEPS D.(1) TO D.(4) TO TROUBLESHOOT FOR HOC. PERFORMED TEST NR 6, PART POWER SDR DALA2025071405285Engine · faultedSHIP 9558 - RTO - CREW REPORTED WITH AUTO-THROTTLE ENGAGED AT 60KNTS RIGHT THROTTLE RETARDED. P30 FAULT, INSPECTED FOR LEAKS/BLOCKAGE WITH NO FINDINGS. REPLACED RIGHT ENGINE EEC, NO HELP. REPLACED #2 ENGINE.SDR FDEA202507121184Engine · failedAT FL360 STARTING THE DESCENT WE RECEIVED A LVL 2 SELECT FADEC ALTN ALERT ON ENG 2. STARTED THE QRH CHECKLIST WE RECEIVED A LVL 2 ENG 2 RPM LO ALERT. COMPLETED THE FADEC CHECKLIST AND GOT THE FADEC BACK. THEN COMPLETED THE ENG 2 RPM LO CHECKLIST WITH ASDR SWAA2025071590378Engine · failedENGINE FAILURE AFTER DEPARTURE @ 3000'SDR CALA2025071406520Engine · faultedRT ENG OVRHT LIGHT ILLUMINATED ON CLIMBINSPECTED CORE AREA OF #2 ENGINE FOUND CORE UPPER FIRE LOOP TOUCHING SENSE LINE TO PRSOV, ADJUSTED POSITION OF CLAMP, RAN ENGINE. OVERHEAT LIGHT CAME ON AFTER 3 MINUETS AT 85% N1, WENT OUT AFTER THROTTLE BACK TO 83%, THENSDR DXTA2025071404208Engine · faultedDURING CRUISE AT FL430 WITH RAT OF -39 RECEIVED AN AMBER ENG CNTRL FAULT L CAS MESSAGE. ALONG WITH THIS CAS MESSAGE WE RECEIVED THE R ENG. THE ENG CNTRL FAULT QRH PROCEDURE (U1) COMPLETED. PROCEDURE INDICATED TO LAND AND CONTINUED TO DESTINATION. DURING DESCESDR AALA202507179372Engine · flamed outAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FLAMEOUT OF ENGINE NUMBER 1 AFTER LEVELING OFF AT FL370. THERE WAS NO OTHER INDICATIONS THAN A "ROLL BACK" OF N1 AND COMMAND SYSTEM-A DISCONNECTING. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SDR 2025FA0000497Turbine Wheel · shearedOVERTORQUE INSPECTION (117% FOR 1 SEC). THE PROP BOX AND ACCESSORY GEARBOX ASSEMBLIES WERE DISMANTLED, INSPECTED AND RE-ASSEMBLED IAW ROLLS ROYCE MANUAL INSTRUCTIONS. THE TURBINE SHAFT TO PINION GEAR COUPLING WAS INSPECTED WITH NO REJECTABLE FINDINGS. THEREFORSDR AALA202507149372Engine · flamed outAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FLAMEOUT OF ENGINE NUMBER 1 AFTER LEVELING OFF AT FL370. THERE WAS NO OTHER INDICATIONS THAN A "ROLL BACK" OF N1 AND COMMAND SYSTEM-A DISCONNECTING. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SDR DXTA2025071404204Engine · vibrationIN FLIGHT, AT CRUISE, THE RIGHT ENGINE AMBER VIBRATION DISPAYED AT 2.7. PER QRH, AFTER PULLING BACK POWER, VIBRATION INDICATOR REDUCED BACK TO GREEN BUT AT AN ELEVATED READING OF 2.5 TO 2.6. A SLIGHTLY SLOWER CRUISE SPEED WAS REQUIRED TO KEEP INDICATOR IN
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