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 CHQA200500126Engine · unserviceableAFTER STARTING DESCENT OUT OF 16,000 FT, HEAT-TYPE ODOR NOTED SHORTLY AFTER MAKING INITIAL POWER REDUCTION. ODOR SUBSIDED AND ATTRIBUTED TO OCCASIONAL PACK SMELL. SOP UNTIL AFTER PASSING APPROX 400 AGL. A/C CONFIGURED AND SET FOR NORMAL VMC ILS. NR 1 ENGINE SDR 2005UALA00647Engine · overheatedRETURNED TO THE FIELD DUE TO HIGH OIL TEMPERATURE ON NR 2 ENGINE. REPLACED FUEL/OIL COOLER BYPASS VALVE SOLENOID. TESTED OK AFTER REPLACEMENT.SDR CA050725014Engine · making metal(CAN) THE ENGINE WAS REPORTED TO EMIT A NOISE ACCOMPANIED BY A CHIP DETECTOR INDICATION. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED MAGNETIC DEBRIS IN THE ENGINE. P&WC WILL INVESTIGATE SDR CA050725018Engine · failedTHE ENGINE LOST TORQUE AND OIL PRESSURE DURING A SPRAYING RUN (AT 50 FT ALTITUDE). THE PILOT FEATHERED THE PROPELLER AND COMPLETED A FORCED LANDING WITH RESULTANT AIRFRAME AND PROPELLER DAMAGE. PWC WILL MONITOR INVESTIGATION OF THE INCIDENT TO ESTABLISH ROOTSDR 2005UALA00641Valve · malfunctionedRECEIVED ECAM AND A FIRE ALARM FOR ENG NR 1. SHUT DOWN ENGINE. NR 1 ENGINE PRESSURE REGULATING VALVE FOR LEAKAGE AROUND SPINDLE SHAFT.SDR XN0A1245Engine · failedENGINE NR 2 WOULD NOT START. REMOVED AND REPLACED NR 2 ENGINE, OPS CK GOOD REF MM 74-11. (ORIG/CLOSED)SDR DL76L050353Engine · odorON CLIMBOUT CABIN CREW REPORTED SMOKE DETECTORS SOUNDING. PERFORMED TASK 21-00-21-102-030 NOTHING ABNORMAL FOUND. INSPECT APU BLEED VALVE APU BLEED DUCT RT LT FLOW CONTROL VALVES INSPECTED CABIN INTERIOR NO ODOR. RAN BOTH ENGINES AT HIGH POWER SETTING 1.3 SDR DLM88050352Engine · making metalRIGHT ENGINE OIL STRAINER CLOG MSG. REPLACED ENGINE FOR METAL IN STRAINER.SDR DXTA200500823Engine · vibrationENG NR 1 SHUTDOWN INFLIGHT DUE TO ENGINE VIBRATION, BUZZING AND A STRONG ODOR OF SMOKE. REMOVED NR 1 ENGINE P/N TFE731-5BR-IH S/N P-107672 WITH TOTAL TIME 3052.8 AND TOTAL CYCLES 2099. INSTALLED SERVICEABLE ENGINE P/N TFE731-5BR-IH S/N P-107777 WITH TOTAL TISDR SWAA051963Engine · power lossNR 1 ENGINE WOULD NOT DEVELOP FULL POWER ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR CA050725009Engine · power loss(CAN) DURING FIRE-FIGHTING OPERATIONS, THE AIRCRAFT FLEW THROUGH A COLUMN OF SMOKE AND THE ENGINE REPORTEDLY LOST POWER. THE AIRCRAFT MADE AN EMERGENCY LANDING AND WAS SUBSEQUENTLY CONSUMED BY FIRE. PWC WILL MONITOR THE INVESTIGATION AND ADVISE OF ROOT CAUSESDR CA050725008Engine · flamed out(CAN) DURING CRUISE IN SEVERE RAIN STORMS, THE ENGINE FLAMED OUT. THE AUTOMATIC RE-LIGHT SYSTEM SUCCESSFULLY RESTARTED THE ENGINE WITHIN 12 SECONDS. POST FLIGHT GROUND CHECKS FOUND NO ANOMALIES AND THE AIRCRAFT RETURNED TO SERVICE.SDR GUU2005F00031Engine · failedLOUD BANG FROM NR 2 ENGINE UPON INITIAL POWER ADVANCEMENT, ABORTED TAKEOFF. NR 2 ENGINE FIRE T-HANDLE, BLEW BOTTLE. EVACUATED PASSENGERS. DETERMINED RT POWER SECTION TO BE SEIZED. EVIDENCE OF DEBRIS DAMAGE TO INSIDE OF EXHAUST STACKS. INVESTIGATION IN PROSDR MASA200500518Mfc · failedNR 1 ENGINE SHUT DOWN IN FLIGHT BY IT SELF. MX REPLACED FUEL PUMP WITH NO FIX AND FINALLY REPLACED THE MFC AND OPS CK'D NORMAL.SDR XN0A1243Engine · malfunctionedON TAKEOFF NR 1 ENGINE EGT EXCEED LIMITS, ABORTED TAKEOFF AT APPROXIMATELY 120KTS.SDR 2005UALA00612Engine · surgesRETURNED TO IAD DUE TO NR 1 ENGINE COMPRESSOR STALL. SURGE ON POWER REDUCTION AT 5500 MSL. EPR = 1.128. TWO ADDITIONAL SURGES AT EPR < 1.128. NOT GROUP-3 SURGE. TEST-21 NOT REQUIRED. IAD HPC BSI: OK. IAD REPLACED: 2.9 BLEED SOLENOID & RELAY, HP BLEED CONSDR XN0A1242Engine · overtempDURING TAKEOFF NR 1 ENGINE EGT EXCEED LIMIT. RED EGT LIGHT ON, LESS THAN 100KTS. PER A300 MM 72-00-00 INSPECTED ENG INLET & EXHAUST, PERFORMED BOROSCOPE INSPECTION ON STAGE. 1 & 2 HPT BLADES, INSPECTED EGT INDICATION SYSTEM AS PER A300 MM 77-21-00. NO DEFESDR CA050725016Engine · vibrationTHE ENGINE WAS REPORTED TO EMIT FLAMES ACCOMPANIED BY VIBRATION AND LOUD NOISES. AN EMERGENCY LANDING WAS PERFORMED ON A DIRT ROAD. P&WC WILL INVESTIGATE THE EVENT TO ESTABLISH ROOT CAUSE.SDR 05052Engine · fireAFTER INITIATING CLIMB THRUST AT 1,000 FT, NR 3 ENGINE FIRE LIGHT ILLUMINATED WITH ACCOMPANYING FIRE WARNING BELL AND BOTH MASTER WARNING LIGHTS. ENGINE FIRE CHECKLILST, FUEL JETTISON CHECKLIST AND NR 2 GENERATOR INOPERATIVE CHECKLIST ACCOMPLISHED IAW WITH QRSDR CA050704007Engine · damaged(CAN) ON LEVELING FROM CLIMB, THE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCAFT DIVERTED. POST-FLIGHT INSPECTION REVEALED THE ENGINE OIL FILTER TO BE BLOCKED BY CARBON PARTICLES. PWC WILL MONITOR INVESTIGATISDR 2005000008Duct · rupturedNR 2 ENGINE ON T/O LOST POWER FROM 111.5 PERCENT TO 92.1 PERCENT ENGINE FAIL LIGHT CAME ON ABORTED T/O DUE TO LOSS OF N1 POWER. INSPECTED NR 2 ENGINE FOUND 14TH STAGE HIGH PRESSURE DUCT RUPTURED. REMOVED AND REPLACED PER MM 75-20 PERFORMED HIGH POWER RUN PERSDR SWAA051935Engine · overtempDIVERSION, NR 2 ENGINE OVERTEMP AT 500 FT AGL, 970 DEGREES INDICATED WITH RED LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR CA050725005Engine · power loss(CAN) THE ENGINE REPORTEDLY LOST POWER DURING TAKEOFF WITH SUBSEQUENT DAMAGE TO THE AIRCRAFT. THE ENGINE HAD BEEN CONVERTED FROM A PT6A-15AG TO A PT6A-34AG UNDER AIRFORCE TURBINE SERVICES STC SE7677SW. P&WC WILL MONITOR INVESTIGATION OF THE INCIDENT AND WILLSDR CALA0500212Engine · malfunctionedLOUD THUMP HEARD AFTER T/O. ALL ENG IND`S NORMAL THROUGH CLIMB-OUT TO 10,000 FT. PASSING 10,000 FT SEVERAL SUCCESSIVE THUMPS WITH NO ABNORMAL ENG IND`S. A/C RETURNED WITH NORMAL LANDING. ENG SHUTDOWN AFTER LANDING. L-1 AND L-2 DOOR SLIDES DEPLOYED & PAX`S EVSDR EIA2005132Engine · failedFL 340 IN CRUISE, NO TURBULENCE LOUD BANG WITH YAW TO RIGHT ENG NR 4 N1, N2 EGT PARAMETERS INDICATION EXCEEDENCES (RED) ENGINE FLAMED OUT. SECURED ENG. NO FIRE WARNING. METAL IN TAILPIPE REMOVED AND REPLACED NR 4 ENGINE IAW F7201/9724001.SDR 2005UALA00739Engine · stalledNR 1 ENG STALL ON TAKEOFF ROLL.SDR ASMF200506031Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE WITH N2 OUT OF LIMITS AFTER STARTED AT 46 PERCENT. THE ENGINE WAS ADJUSTED IN LOW RPM'S IAW MM 71-00-00, PARAMETERS WERE BETWEEN LIMITS (N2 :54 PERCENT AND EGT: 440), TESTED CORRECT.SDR CA050704009Engine · malfunctioned(CAN) DURING CLIMB, THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUT TO REDUCE POWER. THIS WAS ACCOMPANIED BY AN ELECTRONIC ENGINE CONTROL (EEC) REVERSION. THE FLIGHT WAS DIVERTED AND THE ENGINE WAS SHUT DOWN ON FINAL APPROACH. P&WC WILL INVESTIGATE THE EVENTSDR 05FDEA01744Engine · bird ingestionRTO AT 120 KIAS DUE TO LOUD BANG,VIBRATION,AND PULL TO THE RIGHT. F/O SAW AT LEAST TWO BIRDS MOMENTARILY BEFORE EVENT. MAX POWER DUE WET RUNWAY WINDS CALM. VIBRATION CEASED WHEN NR 2 ENGINE SHUTDOWN ON RUNWAY. REMOVED AND INSTALLED NR 2 ENG, NOSE COWL, RT SDR A6WA200540224Engine · flamed outRIGHT ENGINE FLAMED OUT ON LANDING ROLL, WHILE ATTEMPTING TO USE REVERSE THRUST. CHECKED RIGGING, ADJUSTED TO TOP OF LIMITS, CHECKED ATR, RIGGED, SET IDLE SPEED, PERFORMED POWER ASSURANCE ATR, N1 DISABLE TO ACCEL/DECEL IAW CRJ AMM CHP 71, 76, 78. (M)SDR 05FDEA01707Engine · failedAFTER TAKEOFF AT SMF NR 1 ENG RPM ROLLED BACK TO 42 PERCENT EGT TO 992 AN HAD SEVERE VIBRATION. SHUTDOWN NR 1 IAW QRH. NOTE HAD NO FIRE WARNING IND. 1 FIRE BOTTLE USED- GND WITNESS OBS FLAMES FROM CENTER OF ENG. EXHAUST REMOVED AND REPLACED #1 ENG NR 1 FIRSDR CHQA200500125Engine · smokeONE MINUTE AFTER TAKEOFF, F/A REPORTED LAV SMOKE ALARM ACTIVATED, SMOKE PRESENT IN REAR OF CABIN. EMERGENCY DECLARED & VECTORED BACK FOR VISUAL INTO CMH. RAN QRH FOR LAV SMOKE AND FOLLOWED PROCEDURE. THE AIRCRAFT WAS CONFIGURED FOR AN OVERWEIGHT LANDING ANDSDR 06262005Engine · overtempON TAKEOFF, RT ENGINE HAD AN ITT OF 907 WITH TAKEOFF POWER ON BOTH ENGINES AT 88 PERCENT WHILE CLIMBING TO POWER.SDR 06252005Engine · failedRIGHT ENGINE FAILED INFLIGHT.SDR CHQA200500123Engine · unserviceableDURING POST ENGINE CHANGE HIGH POWER RUN, LAV SMOKE OCCURRED ON EICAS AFTER ABOUT 1.5 MINUTES AT 88 PERCENT N2. ENGINE REPLACED DUE TO PREVIOUSLY INSTALLED ENGINE CAUSING LAV SMOKE ON EICAS AND SMOKE IN COCKPIT AND CABIN. SEE SDR CHQA200500122 FOR DETAILS. SDR CA050629006Engine · making metal(CAN) DURING CRUISE THE ENGINE EXPERIENCED AN UNCOMMANDED TORQUE REDUCTION. THE AIRCRAFT CONTINUED TO DESTINATION WHERE GROUND INSPECTION REVEALED DEBRIS ON BOTH ENGINE CHIP DETECTORS. A SUBSEQUENT START ATTEMPT PRODUCED UNUSUAL ENGINE NOISES. MFG WILL MONISDR P5CA0501376Engine · failedAFTER TAKEOFF, NR 1 ENGINE FELT LARGE BANG ALONG WITH EGT OFF SCALE HIGH. SHUT DOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE MM 71-00-02.SDR CA050628002Engine · shutdown(CAN) A LOSS OF OIL PRESSURE WAS NOTED BY THE FLIGHT CREW WHO ELECTED TO SHUT THE ENGINE DOWN ONCE THE OIL PRESSURE APPROACHED LOWER LIMITS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED FINE BLACK PARTICLES, CARBON IN THE OIL AND DETERMINED TSDR 05FDEA01677Torque Ring · crackedNR 3 ENG, RIGHT FORWARD FRAME UPPER TORQUE RING CRACKED APPROXIMATELY 5 INCHES IN LENGTH. THRUST REVERSER REMOVED AND INSTALLED AS PER WORK CARD 78T3003-R AND WORK CARD 78T3903-R FOR WORK DETAILS. THRUST REVERSER ADJUSTMENT AND OPERATION CHECK CARRIED OSDR CHQA200500122Engine · smokeDURING CLIMB-OUT, LAV SMOKE MESSAGE APPEARED ON EICAS AND BURNING ODOR NOTED IN COCKPIT. F/A REPORTED DETECTING BURNING OIL ODOR IN CABIN AS WELL. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO FIELD WITHOUT EVENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE SDR CA050629005Engine · making metalDURING TAKEOFF AN UNCOMMANDED PROPELLER FEATHER OCCURRED. NORMAL POWER WAS RESTORED AFTER PULLING THE PROPELLER SYSTEM CIRCUIT BREAKER AND THE AIRCRAFT DIVERTED TO AN AUXILIARY AIRFIELD. THE ENGINE CHIP DETECTOR WARNING SUBSEQUENTLY ANNUNCIATED FOLLOWED BY USDR MALA050498Engine · vibrationCREW SHUT DOWN NR 3 ENGINE DUE TO ENGINE VIBRATION. NO EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT.SDR SFO2005F00003Heat Shield · failedINSP, A LOUD SCRAPING NOISE WAS HEARD WHEN FAN WAS TURNED. BORESCOPE OF TURBINE SEC., AFTER EXHAUST DUCT WAS REMOVED, NR 4 BRG HSG HEAT SHIELD WAS FOUND BROKEN, TWISTED, IN 3 SEPARATE PIECES, WAS RUBBING ON AFT FACE OF NR 3 LOW PRESSURE TURBINE DISC. DISC WASDR WRNA200500016Engine · damagedVERY LOUD RUMBLE ON TAKE OFF. UPON LANDING, NR 2 ENGINE WAS FOUND TO HAVE COILS MISSING FROM LT SIDE. RT SIDE DAMAGED, ALONG WITH VARIOUS OTHER AREAS OF DAMAGE TO DUCT WORK, FIRE SEAL, AND HYD RACEWAY. ALL ITEMS WERE REPAIRED/REPLACED IAW MM 72-11-02,75-24-SDR DXTA200500792Engine · malfunctionedON TAKEOFF WITH THROTTLE IN THE T/O DETENT, THE LT ENGINE ITT EXCEEDED 720 DEG CELSIUS WITHIN 10 SECS. THE LT ITT INDICTED 724 DEG CELSIUS AND WAS STILL SLOWLY INCREASING. LT THROTTLE REDUCED TO CLIMB. DETENT AND ITT INDICATION IMMEDIATLY DECREASED BELOW 720SDR CA050621015Engine · shutdown(CAN) DURING CRUISE, ENGINE OIL PRESSURE WAS OBSERVED TO FLUCTUATE AND SUBSEQUENTLY DECREASE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED INTERNAL OIL LEAKAGE. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE, ONCE ESTABLISHESDR SWAA051823Engine · failedINFLIGHT SHUTDOWN/DECLARED EMERGENCY/DIVERSION. NR 2 ENGINE FAILED AT 34,000 FT, LOUD BANG TWICE & LOSS OF THRUST. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR GTIA050194Engine · failedFLT 304 - DURING CLIMB-OUT, LEFT ENGINE EGT BEGAN TO CLIMB JUST BELOW MAX TEMP, REDUCED POWER TO MAINTAIN MAX TEMP. FLIGHT ATTENDANT REPORTED LOUD NOISE FROM LEFT ENGINE AND RETURNED TO MCO, AIRCRAFT TAIL SWAP WITH 832. REMOVED AND REPLACED LEFT ENGINE, OPS SDR ASMF200506020Engine · vibrationCAPTAIN REPORTED VIBRATION IN RT ENGINE DURING CRUISE. ACFT SENT TO HANGAR AND WAS CHECKED BY CONDITION AND TESTS PERFORMED IAW MM 72-00-00. ALL CORRECT. RT ENGINE WAS ACCELERATED UNTIL TAKEOFF POWER AND MAXIMUM VIBRATION REGISTERED 0.5, MAXIMUM VIBRATIONSDR CA050621017Engine · leaking(CAN) DURING TAKEOFF CLIMB, SMOKE WAS OBSERVED IN THE CABIN AND FLIGHTDECK. THE CREW DECLARED AN EMERGENCY AND RETURNED TO POINT-OF-DEPARTURE WITH ENGINE BLEEDS SELECTED (OFF). SUBSEQUENT INSPECTION REVEALED ENGINE INTERNAL OIL LEAKAGE. MFG WILL INVESTIGATE
Back to JASC 7200