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 UALA2013020400616Engine · surgesNR 2 ENGINE SILENT SURGE. PERFORMED TESTS IAW MM 71-00-00 P5XX, FIM 71-05 TASK 815 STEP B(1), MM 71-00-00 P5XX, FIM 71-08 TASK 828.1.2, & MM 71-00-00 P5XX. ALL TESTS PASSED. NO ENG SURGES NOTED. ACCOMPLISHED EG 7673, EG7 674 AND EG 7675, NO PROBLEMS FOSDR CA130212021Engine · power loss(CAN) DURING CRUISE ON REVENUE FLIGHT, THE PILOTS NOTED A SUDDEN POWER ROLLBACK. THE ACFT YAWED TO THE RT. THE CREW REPORTED A LOW OIL PRESSURE WARNING FOLLOWED BY A LOW FUEL PRESSURE. THEY ELECTED TO SHUTDOWN THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING SDR CA130212014Engine · unknown(CAN) THE NR 1 ENGINE SUFFERED AN IFSD AFTER A LOUD NOISE. AN UNEVENTFUL LANDING WAS MADE. THE GROUND INSPECTIONS FOUND THE PROPELLER WAS SEIZED.SDR CA130206002Engine · failed(CAN) ON THE CLIMBOUT AT APPROXIMATELY 7000 FT, THE ACFT EXPERIENCED A SUDDEN RT ENGINE FAILURE. NEITHER FILGHT CREW HAD NOTICED ANY INDICATION OF AN ONCOMING ENGINE PROBLEM PRIOR TO A SUDDEN LOUD POPPING NOISE AND THE ACFT YAWING TO THE RT. THEY INSTANTLY ISDR CA130822004Engine · power loss(CAN) AFTER CUSTOMER VISIT, IT WAS JUST REPORTED TO ENGINE MFG THAT THE ACFT SUSTAINED A POWER ROLLBACK IN CRUISE. AFTER COMPLETING EMERGENCY CHECKLIST, PILOT ATTEMPTED TO RESTORE POWER USING THE EMERGENCY POWER LEVER. THE POWER WAS RESTORED AND ACFT CONTINUSDR SIMA20130131011Engine · bird ingestionFOR FLIGHT 3582 THE CREW REPORTED THAT ON TAKEOFF AFTER V1 MANY SUSPECTED BIRD STRIKES. THE SMELL ENTERED THE CABIN OF COOKED BIRD. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED THOROUGH INSPECTION OF A/C IAW EMB WORKCARD 05-200-07 BIRD STRIKE INSPECTIONSDR CA130201001Engine · failed(CAN) DURING POST-PROCESS TEST, THE ENGINE EXPERIENCED AN INTERNAL FAILURE IN THE TEST CELL.SDR UHLA2013013000023Engine · odorSTRONG ODOR SEEMS TO BE ASSOCIATED WITH NR 1 BLEED, NOTICED AFTER TAKEOFF UNTIL NR 1 BLEED WAS DESELECTED. REMOVED AND REPLACED ENGINE.SDR CA130212010Engine · overtemp(CAN) PILOT REPORTED INTER TURBINE TEMPERATURE, ITT INDICATION UP TO 806 DEGREES. FOLLOWED BY VIBRATIONS ON THE CONDITION LEVER AND BURNING ODOR IN THE CABIN. ACFT SAFELY RETURNED TO AIRPORT. TROUBLESHOOTING ONGOING.SDR UALA2013013000553Engine · surgesLEFT ENGINE SURGES. NOTICEABLE ENGINE VIBRATION DESCENDING THRU FL180. LEFT ENGINE VIBRATION 2.4, RIGHT ENGINE VIBRATION .5. REPLACED LT ENGINE.SDR QMLA2013012913017Engine · contaminatedNORMAL DEPARTURE, AT APPROX 400' AGL; ABOUT 5 MINUTES AFTER TAKEOFF, OPENED VALVE FOR THE WINDSHIELD DEMIST. AT 500 FT AGL AND BEGAN A TURN FOR A DOWNWIND DEPARTURE, AN ODOR WAS BECOMING OBVIOUS. IN LESS THAN ONE MINUTE, FUMES BECAME OBNOXIOUS. COULD SEE SSDR CA130212004Bearing · failed(CAN) THE CREW REPORTED ODOR IN THE CABIN. THE ON GROUND BORESCOPE INSPECTION REVEALED TRACE OF OIL IN THE NR 5 BEARING AREA. THE AIRLINE WILL REPLACE THE ENGINE.SDR CA130212003Engine · failed(CAN) DURING CLIMBING THRU 18000`, THE ANTI-ICE TURNED OFF. THE CREW HEARD A LOUD NOISE FOLLOWED BY MULTIPLE NOISES WITH VIBRATION AND A MOMENTARY ODOR OF SMOKE THRU THE ENVIRONMENTAL SYS. THE CREW NOTICED THE LT ENGINE ITT WAS IN THE RED. THE CREW DECLARED SDR UALA2013012900548Engine · surgesNR 1 ENGINE SILENT SURGE CHECKS. ECM DETECTED A 'SILENT' SURGE AT OR NEAR TOP OF DESCENT AT LOW POWER ON FLT 959-28. ECM DOES NOT SHOW ANY PARAMETER SHIFTS BEFORE THE SURGE. THIS IS THE SECOND SURGE WITHIN A WEEK.SDR 2013FA0000060Engine · failedIN NORMAL CRUISE AT 3,000 FT MSL, THE LT ENGINE LOST COMPLETE POWER AND SUBSEQUENTLY BEGAN TO NTS (NEGATIVE THRUST SENSING). THE ENGINE WAS INDENTIFIED, VERIFIED AND FEATHERED IAW EMERGENCY CHECKLIST PROCEDURES.SDR MASA2013012752392Engine · dirtyFOUL ODOR DURING TAKEOFF AT FULL THRUST. PERFORMED ENGINE WATER WASH. RAN ENGINE FOR PERFORMANCE, ODOR AND OIL CONSUMPTION. NO FAULTS NOTED, ALL PARAMETERS WITHIN LIMITS.SDR UALA2013012800491Liner · damagedACOUSTIC MATERIAL MISSING FROM NR 2 ENGINE. FOUND MATERIAL MISSING FROM THE ATTRITION LINER 5 O'CLOCK POSITION APPROX 1 INCH DIAMETER. CLEARED LOOSE MATERIAL. REPAIRED NR 2 ENG ATTRITION LINER AT 5 O'CLOCK POSITION.SDR SIMA20130127006Engine · failedFLIGHT 3917. DURING CRUISE ALTITUDE FL 360, NR 2 ENGINE ITT ON EICAS SPIKED TWICE, AND TEMP AS HIGH AS 1015 DEGREES. WITH THE SPIKES TWO SEPARATE VIBRATIONS WERE FELT. NR 2 ENGINE THEN HAD AN UN-COMMANDED SHUTDOWN. OIL SHOWED TO BE 4 QUARTS. AT DEPARTURSDR DXTA2013012805263Engine · shutdownCLIMBING THRU 18,000' AND JUST TURNED ANTI-ICE OFF, WE HEARD A LOUD BANG FOLLOWED BY MULTIPLE BANGS, WITH VIBRATION AND A MOMENTARY SMELL OF SMOKE THRU THE ENVIROMENTAL SYS. LEFT ENG ITT WAS IN THE RED WITH NO OTHER ENG PARAMETERS NOTED TO BE IN THE RED. WE SSDR FDEA201301270199Line · cloggedENGINE FAIL WARNING ILLUMINATED ON GLARESHIELD ON TAKEOFF, NR 1 ENG N1 DID NOT ACCELERATE PAST 87 PERCENT. ENG DID NOT FAIL. DISCONNECTED NR 1 ENG CDP LINE. BLEW LINE CLEAR, FOUND MINOR DEBRIS IN LINE. CAPPED LINE AND PRESSURE CHECKED FOR LEAKS, NONE FOUSDR REXA2013012700199Engine · fireON FLIGHT 3629 (CLT TO MEM) STARTED ENGINE NR 2 SECOND. DURING START WE GOT THE "HOT" ICON AND STOPPED START. AIRCRAFT BEHIND US INDICATED THAT FLAMES WERE COMING OUT OF RIGHT ENGINE. (ITT REACH AT 550 DEG). NO ITT EXCEEDANCE HISTORY RECORDED IN MDC. PERFSDR DALA13005840996Engine · failedCREW RETURNED THE ACFT WITH THE NR 2 ENGINE SHUTDOWN. WHILE CLIMBING THRU 12,000 FEET, THE CREW HEARD A SMALL BANG FOLLOWED BY A LOUDER BANG AND THEN SHORTLY THEREAFTER NOTICED N1 AND N2 HAD ROLLED BACK AND THE EGT CLIMBED TO 800 DEG. THE FLIGHT CREW COMPLIEDSDR AALA20130126001Blade · damagedLAX - INFLIGHT SNA-DFW. CREW REPORTED MULTIPLE BIRD STRIKES ON TAKEOFF. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FIVE DAMAGED BLADES ON RIGHT ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION.SDR REXA2013012600201Engine · vibrationON FLIGHT 3938 (DTW TO ORF) SHORTLY AFTER DEPARTURE CREW LOST THE RIGHT ENGINE. IN FLIGHT SHUTDOWN OCCURRED ON NUMBER 2 ENGINE DUE TO SUSPECTED ENGINE DAMAGE. OCCURRED UPON PASSING 11000 MSL LOUD VIBRATION NOISE AND ITT IN THE RED. CREW DECLARED AN EMERGENCSDR UALA2013012900528Engine · oil consumptionEXCESSIVE OIL CONSUMPTION FOR THE NR 2 ENGINE . REPLACED THE FUEL COOLED OIL COOLER IAW AMM AND THE FCOC BYPASS VALVE IAW AMM. REMOVED AND REPLACED FUEL OIL HEAT EXCHANGER AND BYPASS VALVE.SDR CA130212002Engine · shutdown(CAN) THE ACFT DEPARTED AND WHEN REACHING 200 FT ENGINE NR 2 SHUTDOWN. THE PILOT COMPLETED A SINGLE ENGINE FIRST PHASE CLIMB AND THEN RE-STARTED ENGINE NR 2 WITHOUT PROBLEMS. AFTER 20 MINUTES OF FLIGHT THE RT ANALOG TORQUE INDICATOR WAS SHOWING ZERO AND REMAISDR CA130212001Engine · power loss(CAN) "DURING REPOSITIONING FLIGHT AFTER MAINTENANCE (NO MAINTENANCE DONE ON THE ENGINE, ABOUT 1.5 HR INTO THE FLIGHT THE ENGINE NR 2 TORQUE AND FUEL FLOW GRADUALLY DROPPED SLOWLY. THE PILOT TRIED MANUAL ECU BUT NO EFFECT. THE ENGINE WAS SHUTDOWN AND THE ACFTSDR CA130318005Engine · flamed out(CAN) BEFORE T/O, AFTER 10 MIN AT IDLE, THE ENGINE FLAMED OUT WITHOUT ANY PILOT INPUT. EXTENSIVE TROUBLESHOOTING COULD NOT DUPLICATE THE PROBLEM. A FERRY FLIGHT WAS MADE TO BRING THE ACFT TO WHERE FURTHER TROUBLESHOOTING WAS TO BE PERFORMED.SDR CA130128014Engine · vibration(CAN) IT WAS REPORTED THERE WAS LIGHT VIBRATION ON THE NR 1 ENGINE. TROUBLESHOOTING FOUND A FUEL LEAK AT THE FUEL FLOW DIVIDER VALVE DRAIN AT ANY POWER SETTING CONDITIONS. THE LEAK RATE WAS 200ML OF FUEL AFTER A 5 MINUTES RUN AT IDLE, LOW POWER FEATHER.SDR CA130128013Oil System · fluctuates(CAN) THE CREW REPORTED AN OIL PRESSURE FLUCTUATION FOLLOWED BY A MASTER WARNING. THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND TO DIVERT THE ACFT.SDR CA130128015Engine · power loss(CAN) ON SHORT FINAL, PILOT REPORTED PROPELLER RPM DROPS TO 320-350 RPM. NO RESPONSE FROM THE POWER LEVER OR CONDITION LEVER. DURING THE ON GROUND TROUBLESHOOTING, THE REDUCTION GEARBOX CHIP DETECTOR WAS REMOVED AND METAL DEBRIS AND PIECES WERE FOUND. THE PSDR ASAA2013012293723Engine · damagedNR 2 ENGINE TREND DATA SHOWS A SUDDEN SHIFT IN EGT (TAKEOFF AND CRUISE), FUEL FLOW AND DELTA CORE SPEED. CORE SPEED AND EGT ARE CURRENTLY WITH ETOPS LIMITS. NR 2 ENGINE VBV GUIDE PAD UNDER NR 9 FAN DUCT PANEL IS DISBONDED. (REF AMM 75-32-00-200-801-F00) ACFT SDR CA130128009Engine · power loss(CAN) ABORTED TAKEOFF DUE TO LOW POWER ON RT ENGINE DURING TAXING, UNABLE TO REACH HIGH POWER, ONLY 53 PERCENT REACHED. THIS WAS THE FIRST REVENUE FLIGHT FOLLOWING LT ENGINE REPLACEMENT. TROUBLESHOOTING ONGOING.SDR CA130128010Engine · inoperative(CAN) UNABLE TO START THE ENGINE DURING A REVENUE FLIGHT. TROUBLESHOOTING IS ONGOING. INSPECTION OF FUEL FILTER FOR DEBRIS AND REPLACEMENT OF FMU AND FDV IN PROGRESS.SDR ASAA2013012093724Actuator · faultedWHILE PERFORMING TASK CARD 78273000, INTERROGATED FMC CDU FOR ENGINE FAULTS. THE NR 1 ENGINE SHOWS FAULT 75-10391 THE VSV POSITION SIGNAL IS OUT OF RANGE. THIS IS A 450 HOUR, LONG TIME FAULT.SDR CA130128008Engine · power loss(CAN) DURING SCHEDULED PASSENGER FLIGHT WHILE IN MODERATE ICING CONDITIONS AN IFSD OCCURRED ON LT ENGINE. THE EVENT DURATION WAS 8-10 SECONDS. THE SHP DROPPED FROM 1700 TO 1. TORQUE DROPPED FROM 66 PERCENT TO 0 PERCENT. NH DROPPED FROM 95 PERCENT TO 75 PERCESDR UALA2013011800313Engine · seizedLEFT ENG SEIZED BANG ON CLIMB OUT AT 9,000 FT, ENGINE SHUT DOWN. RETURNED TO FIELD. CREW REPORTED LOW OIL PRESSURE ON LEFT ENGINE IN FLIGHT. REPLACED NR 1 ENGINE PER MM 71-00 -02 PAGE 401.SDR JJBA20130118011Engine · power lossON FINAL APPROACH, WHEN THE POWER LEVER WENT TO FLIGHT IDLE THE NR 2 ENGINE GAVE 20 PERCENT TORQUE. MX CREW RAN THE ENGINES AND DID NOT OBSERVE THE PROBLEM. ALL OPS CHECKED SATISFACTORY. THE ACFT WAS RETURNED TO SERVICE.SDR ASOA20130118237Engine · smokeACFT WAS LEAVING AIRPORT WHEN CREW WERE ALLERTED TO SMOKE AND FUMES. ACFT RETURN TO BLOCK AND WAS FERRIED TO WHERE MX R & R THE NR 1 ENGINE IAW TASKCARD 6271001. COMPLIED WITH THE AIR CONDITIONING DUCTS CLEANING TASK IAW AMM 21-20-00-100-805-A, STEP K 1 THRUSDR CA131104016Bearing · lack of lube(CAN) DURING THE APPROACH TO AIRPORT, THE PILOT NOTICED A LIGHT VIBRATION ON THE LT ENGINE FOLLOWED BY HEAVY SMOKE IN THE EXHAUST. THE PILOT REDUCED POWER TO FLIGHT IDLE AND PERFORMED AN UNEVENTFUL LANDING. THE ENGINE WAS REMOVED. THE DISASSEMBLY REPORT CONCSDR UALA2013011700309Accelerometer · faultedNR 2 ENGINE HIGH VIB FELT IN AIRFRAME OR THROTTLE. PERFORMED FAN LUBE AS PER 72-31-99 VIBE GOOD AT THIS TIME. ACP CK OF INLET & EXHAUST INCLUDING FAN BLADES FOR DAMAGE & MIDSPAN SHROUDS FOR SHINGLING. CHECKED VIBE PICKUP AT 1 O'CLOCK ON FAN CASE 'A' FLANGE FOSDR UALA2013011800321Strut · crackedINSPECTION FOUND ONE INCH CRACK AFTER STRESS RELIEF AND FPI, WELDED STRUT IAW 72-54-01 RU02 REPAIR C.SDR IPXA3M76771Engine · leakingEMERGENCY DECLARED -CREW EXPERIENCED LOSS OF OIL PRESSURE ON NR 3 ENGINE. PERFORMED A PRECAUTIONARY SHUTDOWN, DIVERTED. LANDED SAFELY WITHOUT INCIDENT. R & R NR 3 ENG IAW TC 9101. OPS CHECKED GOOD.SDR A8OA201301160002Valve · inoperative20 MINUTES IN FLIGHT, IN A CLIMB RT ENGINE EXPERIENCED HIGH OIL TEMP WARNING. CREW INITIATED RT ENGINE SHUTDOWN PROCEDURES. R & R RT ENGINE THERMOSTATIC VALVE IAW ENGINE MM 79-20-03. PERFORMED GROUND RUN, ALL INDICATIONS NORMAL. NO LEAKS NOTED. PN, OFF 3036SDR 39LA2013011500013Sensor · dirtyON CLIMB OUT, ABOUT 8 MILES FROM DPRATURE, RT ENGINE STARTED TO SURGE BETWEEN 95 -60 PERCENT TORQUE, AND 650- 250 EGT. RETURNED TO DEPARTURE. AS ACFT LEVELED OFF AND STARTED TO DESCEND THE ENGINE RAN NORMALLY. NO OTHER ABNORMALITIES WERE NOTED AND LANDINGSDR CA130128005Engine · unknown(CAN) EVENT SIMILAR TO VQ-BLL AND VQ-BLC. UNCOMMANDED POWER CHANGE IN HOTEL MODE, PROP BRAKE CAN NOT RETAIN PROPELLER. ALL THE EVENTS HAPPENED AT LOW OAT (AROUND -20 DEGREE C.SDR CA130116002Engine · making metal(CAN) DURING CRUISE NR 1 ENGINE OIL PRESSURE WAS LOSS, THE ENGINE WAS SHUTDOWN, THE FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO A NEARBY AIRPORT. DURING TROUBLESHOOTING, A SIGNIFICANT AMOUNT OF METAL PARTICLES WERE FOUND ON THE TURBO MACHINERY CHIP DETESDR ASMF201303003Bolt · looseDURING CLIMB, RT ENGINE VIBRATION REACHED 3.7 UNITS AND DURING CRUISE THE VIBRATION WAS STABILIZED IN 1.5 UNITS. AIRCRAFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A TRIM BALANCE IAW MM 71-00-00 TASK 71-00-00-700-847-G01, DETECTING 2 RT ENGINE FAN WEISDR 2013FA0000047Engine · flamed outON APPROACH, AT 4000 FT, THROTTLE SETTING ABOUT 55 PERCENT, NR 1 ENGINE FLAMMED OUT, APPROACH WAS CONTINUED. THERE WAS 261.5 HRS SINCE O/H ON ENGINE. UNABLE TO DUPLICATE PROBLEM. ACFT HAS MADE SEVERAL TAKEOFF AND LANDINGS SINCE THIS INCIDENT WITH NO FURTHERSDR A8OA201301140001Engine · overheated10 MINUTES AFTER DEPARTURE EXPERIENCE NR 2 ENGINE OVER OIL TEMP. CREW REDUCED POWER ON NR 2 ENGINE, OIL OVER TEMP OCCURRED AGAIN, CREW THEN INITIATED AND COMPLETED PRECAUTIONARY ENGINE SHUTDOWN. REMOVED AND INSPECTED ENGINE OIL FILTER WITH NO DEFECTS NOTED, RE
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