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 00008Engine · flamed outDURING CLIMB THROUGH FLT LEVEL 43.8 LT ENGINE FLAMED OUT. AT FL250 AIRSTART PERFORMED AND CONTINUED FLT AT 370.SDR C1HA200296001Engine · malfunctionedON RUNWAY ADVANCED THROTTLE TO 1.4 CHECK PARAMETERS GOOD, CONTINUED THROTTLE ADVANCE FORFLEX POWER, LOUD BANG FROM NR 2 ENGINE, ENGINE FAIL LIGHT ILLUMINATED AND PACKS TRIPPED. ACCOMPLISHED THOROUGH EXAMINATION OF ENGINE NR 2 INTAKE AND EXHAUST WITH NO DAMAGESDR EVAS91003Blade · damagedDURING TAKE OFF, NR 3 ENGINE HIGH EGT & HPC STALL. REPLACED NR 3 ENGINE, ON GROUND FOUND SEVERAL BLADES & STAGE NR 6 SEVERE DAMAGE OF COMPRESSOR.SDR CG8A20020001Pump · shearedFlt 707 from DEN to TOL. During cruise level at FL 330 #3 engine flame out. Oil pressure and quantity as well as N1 and N2 were normal. Descended to two engine cruise altitude and conducted engine failure shutdown checklist and all indications were normal, attSDR C2XA02IA001Engine · leakingIAH- FLIGHT NUMBER 3792 THE CREW NOTED SMOKE IN THE CABIN AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, PERFORMED A OPERATIONAL AND LEAK CHECK. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVSDR MALA020102Engine · seizedON TAKEOFF OF FLIGHT 3410 CREW HEARD A LOUD BAND FROM NR 3 ENGINE AND REPORTED THE NR 3 ENGINE FROZE UP, NO OTHER PARAMETER INDICATIONS WERE IDENTIFIED. CONTINUED TO DTW AND DECLARED EMERGENCY AND LANDED WITH NO PROBLEMS. COMPLETED TASK CARD THREE ENGINE FERSDR CA020121005Engine · failed(CAN) ENGINE SHUT DOWN. WHILE IN CRUISE NR 1 ENGINE SURGED FOLLOWED BY GRADUAL INCREASE IN EGT AND FUEL FLOW. SHORTLY AFTER, ENGINE FILTER CLOG MESSAGE DISPLAYED AND THEN ENGINE LOW OIL PRESSURE.FOUND EVIDENCE OF NR 4 BEARING FAILURE. REPLACED ENGINE.RESULT SDR 0104809988Engine · stalledDURING CLIMBOUT THE RIGHT ENGINE EXPERIENCED A STALL WITH ASSOCIATED VIBRATION AND POWER LOSS. CREW SHUTDOWN THE RIGHT ENGINE AND RETURNED TO DTW. ENGINE OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE.SDR ASOA01303Carbon Seal · leakingFLT 4698 - WHILE CLIMBING THROUGH FL270 FROM ATL-SWF, THE CAPTAIN REPORTED RECEIVING A RIGHT ENGINE OIL PRESSURE MESSAGE FOLLOWED BY AN AURAL WARNING. THE OIL PRESSURE WAS FLUCTUATING BETWEEN 30 AND 49 PSI. THE CAPTAIN SECURED THE RIGHT ENGINE AND RETURNED TSDR DL757011983Engine · leakingAFT LAV SMOKE DETECTOR WENT OFF ON T/O FLT CREW NOTICE SMELL ASSOC WITH AC PACK. FOUND OIL LEAKING FROM NR 1 ENG 2.5 BLEED VLV PORT AT T/O POWER. REPLACED ENGINE.SDR AUS20011389Fairing · separated(AUS) NR 1 ENGINE RT TRANSFER DRIVE FAIRING SEPARATED. LT TRANSFER DRIVE FAIRING DAMAGED AND ONLY PARTIALLY ATTACHED. PART NUMBERS OF FAIRINGS; UL23537 AND PNO UL23538. DAMAGE WAS FOUND ON SHAFTS AND PLUMBING IN THE AREA OF THE TRANSFER DRIVE AND THE INA.SDR COMA0260016Engine · faultyFLIGHT 5959 L/H ENGINE HIGH OIL TEMP AND LOW OIL PRESSURE I.F.S.D.REPLACED L/H ENGINESDR CHQ00080Engine · making metalNR 2 ENGINE ABNORMAL VIBRATION. FOUND CHIPS ON ALL CHIP DETECTOR. REPLACED ENGINE ON AIRCRAFT.SDR AT0100244Engine · failedFOUND NR 1 ENGINE LOST OIL QUANTITY. OIL TEMPERATURE WENT UP AND OIL PRESSURE WENT DOWN. ENGINE WAS SHUT DOWN, ENGINE TURNED FOR 25-30 MINUTES AT LESS THAN 10 PSI. REMOVED AND REPLACED THE NR 1 ENGINE IAW DC9 72-00.SDR UPS01437379Engine · flamed outINSPECTION TYPE:N/A PILOT REPORT NR 1 AND NR 2 ENGINE FLAME-OUT. INGN FUEL AND OIL SYS CK PER MM AND ENGINEERING OPRN NORMAL.SDR DLM88011967Engine · smokeON T/O CREW OF ANOTHER AIRCRAFT OBSERVED SMOKE (WHITE AT RST CHANGING TO DARK SMOKE) COMING OUT OF TAIL ON LEFT ENGINE DURING T/O ROLL AND CLIMBOUT. ALL COCKPIT INDICATIONS INDICATE NORMAL. PERFORMED VISUAL INSP OF INLET/ EXHAUST AND ENGINE EXTERIOR COMPONENTSDR 01FDEA01099Engine · faultyON CLIMBOUT NR 1 LOW OIL PRESS LIGHT ILLUM. ENG SHUTDOWN. REMOVED AND REPLACED NR 1 ENG PER W/C 70T0001-01.SDR CA020110001Engine · failed(CAN) ON TAKEOFF ROLL, AFTER N1 SELECTED ON MCP, ENGINE ACCELERATE NORMALLY TO 50 PERCENT AT 50 PERCENT ENGINE DID NOT ACCELERATE ANY FURTHER. ALL PARAMATERS NORMAL FOR BOTH ENGINES. AN AIRFRAME VIBRATION COULD BE FELT AT 25 - 50 PERCENT ON LT ENGINE. TASDR P2EA2001M0016Engine · malfunctionedON SCHEDULED PUSHBACK FOR FLIGHT 400 PILOT REPORTED THAT NR 2 ENGINE WOULD NOT START. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. NR 2 ENGINE OPERATIONAL CHECKED IAW MM 71-09-100.SDR UPS01837369Engine · flamed outINSPECTION TYPE:N/A EXPERIENCED IN FLIGHT FLAME-OUT NR 2 ENG DURING CRUISE. FLAME-OUT OCCURRED APPROX 1 MINUTE AFTER NR 2 X-FEED LEVER PLACED DOWN/OPEN. ALL MAIN BOOST PUMPS ON 1, 3 AND 4 FILL VALVES OPEN. NR 2 TANK 1000 LBS HEAVIER THAN 1, 3 + 4. PERFORMESDR UPS01837364Engine · flamed outINSPECTION TYPE:N/A NR 2 ENG FLAMEOUT ON DESCENT ANTI-ICE 'ON' ING OVERRIDE FLT 15000 - 16000 FT. T/S PER 71-00-00 CFM MANUAL, COMPLIED WITH ALL STEPS FOR ENG FLAME-OUT PER MM 71-00-00 PG 101, 102 & 103. NO DEFECTS NOTED.SDR AUS20011345Engine · overtemp(AUS) NR 1 ENGINE OVERTEMP. LIMITED INFORMATION PROVIDED.SDR CA011221002Engine · malfunctioned(CAN) ON TAKE OFF ACCELERATING THROUGH 60 KTS TME A/C YAWED TO PORT AND THE PORT ENGINE TORQUE WAS SEEN TO DROP. THE ENGINE WAS SHUT DOWN AND THE TAKE OFF ABORTED. AT PRESENT THE INCIDENT IS SUBJECT TO A FULL ENGINEERING INVESTIGATION. FURTHER DETAILS WILLSDR ARWA20011206Engine · failedAPPROX 200 MILES OUT OF BAHRAIN AT FL 330 NR 4 ENGINE COMPRESSOR STALLED IN CLEAR WEATHER, FOLLOWED BY DROP IN EPR FROM 1.65 TO 1.15. ALL OTHER PARAMETERS NORMAL, ABOVE 85 PERCENT N2 ENGINE SURGES. AIRCRAFT LANDED WITHOUT INCIDENTS. POST FLIGHT INSPECTION RSDR IXXA0100076OEngine · leakingEN ROUTE FROM JFK TO BDL. WHEN LEFT AIR CONDITION PACK WAS TURNED ON SMOKE WAS EMITTING FROM THE VENTS. THE FLIGHT CREW SECURED THE PACK AND THE SMOKE SUBSIDED. THE FLIGHT CREW THEN NOTICE A DECLINE IN THE NUMBER ONE ENGINE OIL QUANTITY AND OIL PRESSURE REMSDR CHQ00063Engine · fluctuatesABORTED TAKEOFF FOR LT ENGINE TORQUE FLUX. GROUND RAN A/C, NO DEFECTS NOTED.SDR SABA011071Helicoil · strippedFLIGHT 5042, AS AIRCRAFT WAS PASSING THROUGH 9500 FT, THE LT ENGINE LOST ENGINE OIL PRESSURE, TORQUE AND RPM. ENGINE WAS SHUTDOWN BY THE AIRCREW. AIRCRAFT RETURNED TO CHARLESTON WITH NO OTHER PROBLEMS. INFLIGHT EMERGENCY WAS DECLARED AND EMERGENCY PROCEDURES WSDR CA020121010Compressor · failed(CAN) ENGINE SENT FOR INVESTIGATION & REPAIR AFTER OPERATOR REPORTED THAT ENGINE HAD SUSTAINED FOD TO COMPRESSOR SECTION. ENGINE HAD EXTENSIVE DAMAGE. DAMAGE ORIGINATED FROM 1ST STAGE COMPRESSOR STATOR & DISK SPACER WHICH HAD LOST PIECES OF INNER RIM & CONTINSDR RAIA00112003Engine · flamed out5482-STL-DURING TAXI LEFT ENGINE FLAMED OUT. MAINTENANCE TROUBLESHOT, ADJUSTED LEFT ENGINE DECELERATION SCHEDULE, AND PERFORMED OPERATIONAL CHECK PER J41 MM 72-00-00.SDR HEEA077387Engine · malfunctionedENGINE WOULD NOT START.SDR ANCF200100022Engine · malfunctionedAFTER TAKEOFF, LT ENGINE WAS REDUCED DUE TO IMPENDING HIGH EGT (576°C), THE BEHAVIOR OF THE LEFT ENGINE WAS NORMAL UNTIL CLIMBING, THROUGH APPROXIMATELY FL 280, A STRONG STALL NOISE WAS FELT WITH AIRCRAFT YAWING. LT ENGINE EPR WAS DECREASED AND EGT ROSE UP. SDR CA020114009Engine · failed(CAN) ENGINE WAS SENT TO ATI FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED THAT ENGINE HAD BEEN SHUT DOWN IN FLIGHT. THE OPERATOR REPORTED THAT DURING THE APPROACH THE PILOT HAD NOTICED THE TURBINE INTERSTAGE TEMPERATURE HAD INCREASED TO 950 DEGREESSDR UPS01237343Engine · failedINSPECTION TYPE:N/A NR 1 ENGINE FAILURE - NOSE COWL AND BULLET DAMAGED. RETURNED TO LAN. REMOVED AND REPLACED NR 1 ENGINE PER UPS TC 1201 S/N OFF P687435B, ON 6 87439.SDR JIK2001F00000Bearing · failedENGINE INFLIGHT SHUTDOWN AS A RESULT OF TOWER SHAFT FRACTURE. FRACTURE CAUSED BY THRUST BEARING FAILURE. BEARING FAILURE MADE AND THE TOTAL TIME NOT YET DETERMINED.SDR CHQ00044Engine · overtempLEFT ENGINE OVERTEMP DURING TAKEOFF ROLL WITH CTOT ON.SDR CHQ00043Engine · overtempLEFT ENGINE OVERTEMP DURING TAKEOFF ROLL, ABORTED TAKEOFF.SDR UPS01837333Engine · flamed outINSPECTION TYPE:N/A AT FL370 NR 3 ENG BEGAN TO ROLLBACK SLOWLY. NO RESPONSE TO THROTTLE. TURNED OFF PMC, NO HELP. ATTEMPTED RESTART AT FL330, NO RESTART. ATTEMPTED 2ND RESTART AT 17000 FT, NORMAL START. PERFORMED FUEL LINE NEGATIVE PRESSURE CHECK IAW MM 2SDR SIMA200132602Carbon Seal · failedABI - FLT 9305 - RETURN TO FIELD ABI, SMOKE IN LAVATORY, EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED O-RING AND ZERO CARBON SEAL ON RT ENGINE. (M)SDR CA020104018Seal · leaking(CAN) APPROX. 1 HOUR AFTER TAKE OFF, NR 3 OIL QUANTITY INDICATED AMBER, NR 3 OIL PRESSURE WENT INTO RED (6PSI) ACCOMPANIED BY ECAM ADVISING TO SHUT DOWN ENGINE. AIRCRAFT RETURNED TO VANCOUVER. FOUND NR 3 ENGINE STARTER DRIVE SEAL LEAKING. SEAL REPLACED AND GRSDR 2001F00724Engine · malfunctionedAUG - DURING TAKEOFF ROLL, RIGHT OIL PRESS LIGHT CAME ON. ABORTED TAKEOFF. TAXI BACK TO GATE, OIL PRESS GAUGE READ BETWEEN 30-50 PSI. REMOVED AND REPLACED RIGHT ENGINE LEAK AND OPS CHECK GOOD. (M)SDR MALA010780Engine · failedDURING FLIGHT 3445, NR 2 ENGINE FAILED AFTER TAKEOFF. ENGINE SHUTDOWN, AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECKS GOOD P/N ON & OFF 2-003-040-15, S/N OFF P07700, S/N ON LF07588.SDR USAASB01317Engine · failedMIA-BWI - FLT 2738 - DURING CRUISE, THE FLIGHT CREW HEARD A LOUD BANG AND THE AIRCRAFT YAWED. THE RIGHT ENGINE N1 AND N2 DIMINISHED AND THE EGT CLIMBED ABOVE THE RED LINE. THE ENGINE SPOOLED DOWN AS THE CREW INITIATED SHUTDOWN PROCEDURES. A PASSENGER REPORTSDR 2001F00706Engine · failedMIA-BWI - FLT 2738 - DURING CRUISE, THE FLIGHT CREW HEARD A LOUD BANG AND THE AIRCRAFT YAWED. THE RIGHT ENGINE N1 AND N2 DIMINISHED AND THE EGT CLIMBED ABOVE THE RED LINE. THE ENGINE SPOOLED DOWN AS THE CREW INITIATED SHUTDOWN PROCEDURES. A PASSENGER REPORTSDR ARWA20011117Engine · making metalAT CRUISE 33,000; NR 3 ENGINE OIL PRESSURE DROPPED TO 30 PSI - MOVED THROTTLE TO IDLE, OIL PRESSURE REDUCED TO 20 PSI; COMPLETED ENGINE SHUTDOWN PROCEDURE AT 23:45 ZULU. OIL QUANTITY IS OK. INSPECTION REVEALED METAL IN OIL SYSTEM. ACCOMPLISHED NR 3 ENGINE CSDR CA020709002Engine · vibration(CAN) VIBRATION INDICATION ON NR 1 ENGINE, 3.0 UNITS ON CHANNEL A AND B. THE ENGINE WAS SHUT DOWN IAW THE SOP. MAINTENANCE REMOVED THE LP FAN BLADES , CLEANED AND REINSTALLED THEM IAW AMM 72-31-05. THE TEST NR 11, VIBRATION SURVEY WAS C/OUT AND FOUND TO BE WITSDR CA011127015Engine · failed(CAN) ENROUTE FROM VANCOUVER TO JAPAN, THE FLIGHT EXPERIENCED A POWER LOSS ON NR 3 ENGINE. ROLL BACK TO 77 PERCENT THEN AUTO RE LIGHT OCCURRED RAPIDLY. LATER ON INTO THE FLIGHT, THE FLIGHT CREW HAD THE ENGINE LOW PRESSURE MESSAGE AND ON APPROACH TO NARITA, THSDR 01EVA006Engine · unserviceable1.AIRCRAFT LOW SPEED T/O ABORTED (ABOUT 95 KTS) DUE TO "ENG FAIL" LT ON WITH "BAN" SOUD HEARD. AFTER ABORT ACTION COMPLETED. "ENG FAIL" RED LT WENT OFF. 2.GND VISUAL INSPETED NO. ENG EXHAUST SLEEVE, FOUND METAL CHIP AROUND INNER SURFACE, AND METAL CHIPS FOUND SDR CA020114008Engine · failed(CAN) ENGINE WAS UNABLE TO ACHIEVE THE RATED POWER WITHIN THE SPECIFIED TEMPERATURE LIMITS. THE OPERATOR DECIDED TO PERFORM AN HSI AND REMOVED THE HOT SECTION COMPONENTS FOR SHIPMENT TO ATLANTIC TURBINES FACILITY IN ATLANTA. AT THIS POINT IT WAS NOTED THAT THSDR ERAA077294Engine · making metalENGINE IS MAKING METAL, BOTH PLUGS. FC-OP GEARSHAFT DAMAGED PN 6896437 ACTION TAKEN: INSTALLED NEW GEARSHAFT & COMPLIED WITH CEB-A-1386 TQ METER GEAR INSPECTION .SDR GN42002F00000Seal · failedHOLE IN HPT FWD AIR SEAL, BOLT SHEARED FLUSH AT ROTOR DISC TO ROTOR FWD SEAL ATTACH FLANGE RELEASING SELF LOCKING NUT AND ENGAGED SECT OF BOLT SHANK. INSP REVEALED TIP CRACKING, MISSING MATERIAL TO MOST OF BLADES. LEADING EDGE/CONCAVE SIDE HOLES WERE PRESENT
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