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 SWAA060817Engine · failedAIR TURNBACK / IN FLT SHUTDOWN / DECLARED EMERGENCY. NR 1 ENG FAILURE AT 10,500 FT DURING CLIMB, EGT IND 830 DEGS AND RISING. REMOVED AND REPLACED NR 1 ENG PER MT.SDR U30A200600008Bearing · spalledSDR WRITTEN TO CLOSE SDR U30A200600003, WHICH READ: FLT 1013 CUN-STL; SHORTLY AFTER T/O, CREW REPORTED VIBRATION, POPPING SOUNDS COMING FROM NR 2 ENG. ENGINE ROLLED BACK TO IDLE. CREW MANINTAINED IDLE CONDITION (ENGINE PARAMETERS WERE NORMAL AND OIL QUANTITY GSDR U30A200600003Engine · malfunctionedSHORTLY AFTER TAKE OFF, CREW REPORTED VIBRATION AND POPPING SOUNDS COMING FROM NR 2 ENGINE. ENGINE ROLLED BACK TO IDLE. CREW MAINTAINED IDLE CONDITION (ENGINE PARAMETERS WERE NORMAL & OIL QUANTITY GOOD). CREW DECLARED AN EMERGENCY & RETURNED TO CUN, AND LANDEDSDR CHQA200600036Engine · damagedFLIGHT 7796 - ORD-BUF - SHORTLY AFTER SELECTING CLIMB THRUST, NR 2 ENGINE INDICATED AN ABNORMALLY HIGH ITT AND THE FUEL FLOW WAS SIGNIFICANTLY HIGHER THAN ENGINE NR 1. IMMEDIATELY REDUCED THRUST ON NR 2 ENGINE UNTIL ITT WAS BACK IN GREEN. DECIDED THE ENGINE SDR CA060403009Engine · power lossDURING CLIMB, THE ENGINE EXPERIENCED AN UNCOMMANDED LOSS OF POWER. THE AIRCRAFT CRASHED ON ATTEMPTING TO RETURN TO POINT OF DEPARTURE. P&WC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR AALA20060163Engine · making metalLAX - INFLIGHT HAD TO SHUT DOWN LEFT ENGINE IN CRUISE AT ALTITUDE FLIGHT LEVEL 380 DUE TO NO OIL PRESSURE AND NO OIL QUANTITY INDICATION. LEFT ENGINE WINDMILLED APPROXIMATELY 30 MINUTES BEFORE LANDING. LANDED AT LAX WITHOUT INCIDENT. FOUND EXCESSIVE OIL IN SDR DL76L060176Engine · smokeSMOKE IN FWD HALF OF CABIN AND SOME IN COCKPIT. PERFORMED ENGINE RUN/ DUCT BURNOUT PER MM, NO TROUBLE FOUND. INSPECTED E/E, NO TROUBLE FOUND.SDR DLM90060169Engine · hot startON DESCENT, NR 1 ENGINE EGT PEGGED AT TOP OF RED RANGE 881 DEG WITH OIL PRESS AT 260 PSI AND OIL TEMP 96 DEG. NO OTHER UNUSUAL INDICATIONS. RETARDED TO IDLE WITH NO IMPROVEMENT. SHUT ENGINE DOWN IAW QRH. REPLACED ENGINE.SDR UPS06M46420Engine · flamed outENG FAILURE, JUST AFTER COMING OUT OF REVERSE THRUST NR 3 ENG FLAMEOUT. VISUALLY INSP'D NR 3 ENG, NO DEFECTS NOTED. RAN ENG, ALL INDICATIONS NORMAL. NO ALERTS. OK FOR SERVICE. HEAVY SNOW ON RNWY AT LANDING.SDR VNAA0603004Fan Blade · lack of lubeDURING CRUISE AT FL340 THE RT ENGINE FAN VIB INDICATED APPROXIMATELY 2.5 FOR 1 SECOND THEN FLUCTUATED CONTINUOUSLY AND WAS ABNORMALLY HIGH. THE CREW REPORTED SLIGHT YAWING DURING VIBRATIONS. THE FLIGHT DIVERTED TO DAY AND LANDED WITHOUT INCIDENT. AFTER TROUSDR CA060403011Engine · power lossTHE ENGINE EMITTED A LOUD NOISE FOLLOWED BY AN UNCOMMANDED INFLIGHT SHUTDOWN. THE AIRCRAFT DEPARTED THE RUNWAY ON LANDING RESULTING IN SIGNIFICANT AIRFRAME DAMAGE. P&WC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR CA060403006Engine · flamed out(CAN) INFLIGHT THE ENGINE EMITTED A LOUD NOISE, INTERTURBINE TEMPERATURE INCREASED AND THE ENGINE FLAMED OUT. A DEAD-STICK LANDING WAS CARRIED OUT RESULTING IN SIGNIFICANT AIRCRAFT DAMAGE. MFG WILL INVESTIGATE AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NSDR AALA20060143Engine · shutdownDEN - RIGHT ENGINE FAILED AFTER TAKEOFF AT ABOUT 300 FEET ABOVE GROUND LEVEL. RIGHT HAND ENGINE EXHAUST GAS TEMPERATURE AT ROTATION WAS ABOUT 570 DEGREES. ENGINE FIRE/DAMAGE/SEPARATION CHECKLIST FOLLOWED, HAD N1 AND N2 BUT NO RESTART. LANDED DEN WITHOUT INCISDR CA060403005Engine · making metal(CAN) IN FLIGHT, THE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED AND THE ENGINE WAS SHUTDOWN. SUBSEQUENT INSPECTION REVEALED METALIC DEBRIS IN THE ENGINE OIL. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE EXTABLISHED. (TC NR 20060403005)SDR WRLA2006006Fan Blade · damagedDURING CLIMB, FLIGHT CREW NOTED FAN VIBRATION REACHED 3.2. AIRCRAFT RETURNED TO SNN (EINN). UPON ARRIVAL NR 2 ENGINE WAS INSPECTED. FAN INSPECTION FOUND MULTIPLE FAN BLADES AND EXIT GUIDE VANES DAMAGED DUE TO SUSPECTED FOREIGN OBJECT DAMAGE. R/R NR 2 ENG FASDR AMTA200600143Engine · fluctuatesRT ENGINE, (.1) EPR LOWER AND 40 DEGREES C, EGT HIGHER THAN THE LT ENGINE WITH OTHER PARAMETERS MATCHING. PRIOR TO DESCENT EPR FLUCTUATED (.15) EPR TOWARDS THE NORMAL (HIGHER SETTING). REDUCED THRUST TO MID POINT AND ENG STABILIZED. (K)SDR CALA0600071Engine · failedTHE NR 2 ENGINE GAVE OFF A LOUD BANG AFTER TAKEOFF FROM SJO. THE BANG WAS FOLLOWED BY A RAPID RISE IN EGT AND LOSS OF THRUST. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO SJO WHERE IT LANDED WITHOUT INCIDENT. A WALKAROUND INSPECTION FOUND SDR DHL2006793001Engine · malfunctionedENG NR 1 WOULD NOT MAKE T/O EPR WT 151.0, 75KTS +10 PA340 BRAKE ENERGY NORMAL. PERFORMED ENGINE TRIM IAW JRH 7.7 ALL PARAMETERS NORMAL. OPS CHECK GOOD.SDR ASMF200602008Engine · bird ingestionPILOT REPORTED THAT DURING CRUISE AT 410 FLIGHT LEVEL THE VIBRATION INDICATION OF THE LEFT ENGINE WAS 0.1 AND OF THE RIGHT ENGINE WAS 1.7. THE RIGHT ENGINE WAS CHECKED IAW M/M 71-00-00 DETECTING A BIRD STRIKE. THE ENGINE WAS CHECKED IAW M/M 05-51-18, AN FOD SDR CA060228016Engine · flamed outON DESCENT, THE ENGINE FLAMED OUT AND THE PROPELLER FEATHERED. A RE-LIGHT ATTEMPT WAS UNSUCCESSFUL. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR ASOA06217Engine · shutdownDURING DESCENT, THE RT ENGINE AUTOMATICALLY SHUTDOWN AND FEATHERED. THE CREW ATTEMPTED TO RESTART THE RT ENGINE BUT WAS UNSUCCESSFUL. THE QRH WAS COMPLIED WITH AN AN EMERGENCY WAS DECLARED. A SINGLE ENGINE LANDING WAS PERFORMED SAFELY. REVEALED THAT THE EESDR C7WA200600003Engine · fodIN FLIGHT, AT FL 28.0, NR 2 ENGINE COMPRESSOR STALLED. ENGINE WAS IN STABLE OPERATION, NO BLEED AT 1.80 EPR. EPR DROPPED TO 1.4 EGT RUNS 80 TO 100 HOTTER THAN ENGINES 1 AND 3 IN ALL PARAMETERS OF FLIGHT. INSPECTION ON NR 2 ENGINE REVEALED HEAVY FOD DAMAGE. SDR CA060227003Engine · failedDURING DESCENT AN OPERATOR EXPERIENCED AN INCIDENT IN SEVERE TURBULENCE WHERE BOTH PROPELLERS/ENGINES WERE OVERSPEED. THE NR 1 ENGINE HAD THE TORQUE SHAFT BREAK AND THE POWER TURBINE BLADES SEPARATE. BOTH PROPELLERS/ENGINES TO BE REPLACED.SDR CA060227022Engine · failedTHE ENGINE EXPERIENCED AN UNCOMMANDED IN-FLIGHT SHUT DOWN AFTER TAKEOFF. SUBSEQUENT INSPECTION REVEALED DEBRIS IN THE ENGINE EXHAUST. P&WC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR AWXA200600358Engine · malfunctionedPHX - ENGINE ANOMALY - CREW REPORTED A MOMENTARY ENGINE STALL ON THE NR 1 ENGINE AT ALTITUDE, WITH ASSOCIATED ECAM MESSAGE. MAINTENANCE INSPECTED AND BORESCOPED IAW AIRBUS TROUBLE SHOOTING MANUAL 71-00-00-810-803. FOUND STAGE 6 BLADE MISSING 50 PERCENT AND NSDR CA060227019Engine · malfunctionedON APPROACH, THE ENGINE WAS FOUND NOT TO RESPOND THE THROTTLE LEVER INPUT. THE PILOT ENGAGED THE FUEL CONTROL MANUAL OVER-RIDE AND REGAINED AUTHORITY OVER THE ENGINE. P&WC WILL MONITOR THE INVESTIGATION OF THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTASDR 06FDEA0798Engine · failedPRECAUTIONARY SHUTDOWN NR 2 ENGINE DUE TO VIBRATION. AIRCRAFT ON GROUND REPORTED SEEING SPARKS COMING FROM NR 1 ENGINE, HOWEVER HAD SEVERE VIBRATION ON NR 2 ENGINE. FAN HAS FOD AND BLADES BROKEN IN HALF, SECOND STAGE DAMAGED, THIRD STAGE IS ALSO DAMAGED, SDR 2006FA0000245Engine · making metalLT ENGINE OIL PRESSURE STARTED FLUCTUATING. PILOT RETURNED TO AIRPORT. MAINTENANCE CHECKED OIL FILTER AND FOUND METAL IN OIL. ENGINE REMOVED AND SENT TO REPAIR FACILITY. (K)SDR MWEA060018Engine · frozenRIGHT ENGINE PRESSURE RATIO DID NOT ADVANCE PAST 1.02, ALL OTHER INDICATIONS NORMAL. DISCONNECTED PT7 LINES AT CROSSBRIDAL AND DETERMINTED THAT THE LINES WERE OBSTRUCTED WITH ICE BETWEEN BRIDAL AND PT7 TRAP, RAN ENGINES, OPERATIONS CHECKED GOOD.SDR MWEA060016Engine · frozenCREW NOTICED NO ENGINE PRESSURE RATIO INDICATION ON RIGHT ENGINE. THAWED OUT RIGHT ENGINE PT7 SYSTEM, REMOVED AND REPLACED PT7 MOISTURE TRAP.SDR AALA20060137Drain Valve · inoperativeORD - AFTER TAKEOFF LEFT ENGINE COMPRESSOR STALLED AT APPROXIMATELY 2000 FEET ABOVE GROUND LEVEL AT CLIMB POWER. ENGINE POWER REDUCED AND STALL CLEARED. NO OTHER INDICATIONS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE FIRST STAGSDR DL757060136Engine · fodDURING TAKEOFF SUSPECT LEFT ENGINE INGESTED FOD. ENGINE DID HAVE A COMPRESSOR STALL WITH AN INDUCED YAW AFFECT. EGT STARTED CLIMBING. FLT CREW FOLLOWED QRH PROCEDURES AND SHUT DOWN THE ENGINE AND RETURNED TO LIR. REPLACED ENGINE.SDR 2006FA0000235Engine · unknownOIL TEMP 112, OIL PSI 50, MASTER CAUTION LIGHT CAME ON OIL SMELL IN CABIN. SHUT NR 3 ENGINE DOWN LANDED AT AIRPORT. CAUSE UNKNOWN AT THIS TIME REMOVE ENGINE FOR INSPECTION AND REPAIR, INSTALLED RENTAL. (K)SDR UPS06546154Engine · flamed outAT V2 R EEC AND R ENG LIM EICAS ON DESCENT, R ENG COMPRESSOR STALL. INCREASED THRUST TO ELIMINATE ENG STALL. REDUCED THRUST AGAIN TO MAKE DESCENT CLEARANCE. SOON AFTER R ENG FLAMEOUT, R ENG LP PUMP STATUS MSG DISPLAYED. CREW DECLARED AN EMERGENCY. PERFORMSDR CA060227020Engine · power lossON DESCENT, THE ENGINE WAS REPORTED TO EMIT A GRINDING NOISE ACCOMPANIED BY AN UNCOMMANDED POWER LOSS. THE ENGINE WAS SHUT DOWN IN FLIGHT AND A SINGLE-ENGINE LANDING ACCOMPLISHED AT POINT OF DESTINATION. GROUND INSPECTION REVEALED INTERNAL ENGINE DAMAGE. P&SDR CHQA200600028Engine · smokeFLIGHT 3201 - LGA-RDU - ON CLIMB-OUT, RECEIVED "LAV SMOKE" INDICATIONS AND STRANGE ODOR. FLIGHT ATTENDANT SAW SMOKE AT ROWS 10 AND 11. RETURNED TO FIELD. RAN QRH, INDICATIONS WENT AWAY ON DESCENT TO LANDING. NO OTHER SIGNS NOTED. MAINTENANCE FERRIED TO INSDR MWEA060013Engine · damagedCREW HEARD LOUD NOISE AND FELT A VIBRATION FROM ENGINE. FOUND FAN BLADE DAMAGE DUE TO FOREIGN OBJECT. REMOVED AND REPLACED ENGINE.SDR YENA200609Engine · stalledNR 1 ENG STALL DURING CLIMB THRU 4000 FT/250K. LOUD BANG-ROLLBACK. ENG RECOVERED NORMALLY. CONFIRMED NR 1 ENGINE STALL CAUSED BY WAKE TURBULANCE. NO EGT EXCEEDENCES NOTED. PERFORMED TSM TASK 71-00-10-710-019A, 71-00-00-810-808. ACCOMPLISHED BOROSCOPE, FUSDR CA060227014Engine · flamed outTHE ENGINE FLAMED OUT DURING TAXI. SUBSEQUENT INVESTIGATION COULD NOT DUPLICATE THE PROBLEM. THE ENGINE FUEL FILTER WAS REPLACED, THE AIRFRAME RIGGING CHECKED AND THE AIRCRAFT RETURNED TO SERVICE.SDR QXEA200600452Engine · unknownSEA FLIGHT 2100, NR 1 NP WOULD NOT ACCELERATE WHEN TAKEOFF POWER APPLIED REMAINED ABOUT 800 RPM. INSPECTED NR 1 ENGINE MTC 97670002 RIGGING ALL NORMAL, PERFORMED TC 9720016 NO DEFECTS NOTED, ALL PARAMETERS WITHIN LIMITS. NO PARTS REPLACED. AIRCRAFT RETURNEDSDR QXEA200600448Engine · power lossON DEPARTURE APPROX 100FT, NR 2 ENGINE TORQUE DROPPED 80% 3-5 SEC, AIRCRAFT YAWED TO RIGHT. NR 1 ENGINE CONTINUED TO OPERATE. NR 2 ENGINE 99.5%, OPERATED NORMALLY REMAINDER OF FLT. MX DOWNLOADED EED FAULT CODES FOUND BOTH NR 1 & 2 ENGINES HAD CODES 94 21 76SDR ARWA20060202Engine · vibrationSHUT-DOWN NR 3 ENGINE IN FLIGHT DUE TO VIBRATION. COMPLIED WITH ALL CHECKLIST. C/W RED BORDER NR 019421 NR 3 ENGINE P-679000 REPLACEMENT. COMPLY WITH RED BORDER NR 019421; REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH MAINTENANCE MANUAL 71-00-00. OPESDR GUUA02080601Tube · crackedMIA/MCO DURING FLIGHT LEFT ENGINE FUEL FLOW AND TORQUE WENT TO ZERO. ENGINE SHUT ITSELF DOWN, SECURED ENGINE. DIVERTED TO PBI. REPLACED P3 AIR TUBE ASSEMBLY BETWEEN FUEL CONTROL AND P3 AIR FILTER.SDR KPVA20064Engine · malfunctionedON TAKEOFF ROLL, NR 2 ENGINE DID NOT PRODUCE AND INCREASE IN POWER. AFTER EXITING RUNWAY, NR 2 ENGINE MANUAL LIGHT ILLUMINATED. RESET BOTH ENGINE ECU CIRCUIT BREAKERS IAW GMM CHAPTER 13 PAGES 3.11-3.12 SECTION X PAR A&B.SDR CA060224005Engine · failedIN(CAN) AIR OPERATOR: MODULE 3: CENTRIFUGAL COMP. INDUCER PN 0292251370 S/N 1260FT LIFE LIMIT 14000CYC ACTUAL 14711CYC. CENTRIFUGAL COMP. IMPELLER PN 2292252980 S/N 1019FB LIFE LIMIT 14000CYC ACTUAL 14711CYC. REF: MM NR 29201931, CHAP 05-10-03 PAGE 9 (OCT 20SDR CA060227016Engine · power lossDURING DESCENT, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A LOSS IN POWER. A SINGLE-ENGINE LANDING WAS ACCOMPLISHED. PWC WILL MONITOR INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR CHQA200600026Engine · power lossFLIGHT 6392 - ORF-CVG - DEPARTED WITHOUT INCIDENT, BOUND FOR CVG OVER MOL VOR, EXPERIENCED POWER LOSS ON ENGINE NR 2 FROM APPROXIMATELY 86 PERCENT N1 TO 54 PERCENT N1 WITH ALL OTHER INDICATIONS IN GREEN. REQUESTED ALTITUDE LESS THAN 25,000 FEET. DIVERTED TO SDR MASA200600354Engine · overtempASH 6330 BFL - PILOT ABORTED TAKEOFF DUE TO NR 2 ENGINE HIGH ITT. MOC COORDINATING WITH ENGINE SHOP FOR DISPOSITION. AC CURRENTLY OUT OF SERVICE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE.SDR CA060808011Engine · malfunctioned(CAN) EXPERIENCED THE RT ENGINE IFSD, JUST AFTER THE LIGHTNING STRIKE TODAY. PIC DID NOT TRY TO RESTART THE ENGINE DURING THE FLIGHT, BUT AFTER THE LANDING WE COULD START THE ENGINE. THERE IS NO VISIBLE DAMAGE ON THE OUTSIDE OF THE ENGINE, WE WILL DO THE BSSDR TRBA2006013Engine · unknownWHILE ON GROUND BEFORE TAXIING, SMOKE COMING OUT OF THE RT ENGINE EXHAUST PIPE. MAINTENANCE PERSONNEL CONDUCTED VISUAL CHECK OF THE ENGINE. NO FIRE EVIDENCE WAS NOTED. (K)
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