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 EIA2004035Engine · stalledNR 4 ENGINE STALLED AT FL 370, INFLIGHT START ACCOMPLISHED AT FL 210, ALL INDICATIONS NORMAL.SDR ASMF200405011Engine · malfunctionedAIRCRAFT SUSPENDED TAKE OFF AND RETURNED TO PLATFORM, LOW POWER ON RT ENGINE. INLET AND OUTLET OF RT ENGINE WERE CHECKED, ALL CORRECT. FUEL CONTROL UNIT WAS REPLACED AND PT2, PT7 AND OIL FILTER WERE CHECKED. TRIM TO BOTH ENGINES WAS PERFORMED AND EGT REACHED 6SDR 2004F00424Engine · stalledON DESCENT INTO MEMPHIS, TN, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LEFT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (M)SDR COMA0460310Engine · overtempFLIGHT 5678 LT ENGINE ITT OVERTEMP DURING T/O. REPLACED LT ENGINE.SDR FF62004F00000Magnetic Seal · galledSEAL LEAKING AFTER 200 HOURS. SEAL WAS GALLED.SDR AMTA200400526Engine · vibrationNR 2 ENGINE EXPERIENCED A SUDDEN INCREASE IN VIBRATION FROM .8 TO 2.5 WITH A SELECTED. WARNING LIGHT WAS ON. SELECTED B DID NOT HELP SHUTDOWN ENGINE AT 1350Z ENGIEN CONTINUED TO WINDMILL AT APPROX 14 PERCENT N1 PLUS MADE OIL PRESS B2 + C2 ATM'S RUN CONTINUOUSDR 010461Engine · surgesFLT 4563 FROM PIT TO AVP, 10 MINUTES INTO THE FLIGHT, AIRCREW FELT NR 1 ENGINE SURGE. AIRCREW REDUCED POWER TO 25 PERCENT AND THE ENGINE STEADIED ITSELF. AIRCRAFT RETURNED TO THE GATE.SDR 109050504Engine · smokeAFTER LANDING AT A REMOTE FIRE STATION TO PICK UP A PATIENT, THE CREW CHIEF NOTICED HEAVY WHITE SMOKE COMING FROM THE NR 1 ENGINE EXHAUST. THE AIRCRAFT WAS SHUT DOWN AND REMAINED ON SIGHT OVERNIGHT. THE FOLLOWING DAY MAINTENANCE CONFIRMED THE PROBLEM AND THE ESDR C2XA04CL048Engine · malfunctionedCLE FLIGHT NR 2843 THE CREW REPORTED THE NR 1 ENGINE SHUT DOWN IN FLIGHT. THE SHUT DOWN WAS UNCOMMANDED. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.SDR UIEA200400089Engine · malfunctionedPRIOR TO TAKEOFF, DUE TO ANTI-ICE ON, STAT 'C' RUN AT 60 PERCENT. N1 WAS NORMAL. WITH BRAKE RELEASE, TAKEOFF THRUST SET, ROLLING DOWN RUNWAY 13, ASI BELOW 60 KNOTS, NR 3 ENGINE HAD 'BACKFIRED WITH A LOUD NOISE', WITH REDUCTION IN N1 RPM OF ABOUT 10-15 PERCENSDR DLM90040391Engine · malfunctionedACS REPORTED TAIL PIPE FIRE NR 2 ENGINE AFTER ENGINE SHUTDOWN. REPLACED ENGINE.SDR LKL2004F00000Engine · failedAIRCRAFT WAS IN CRUISE FLIGHT AT 26,000 FT WHEN PILOT HEARD A BANG FROM THE LT ENGINE. THE LT ENGINE CAME TO A STOP AND THE PILOT PERFORMED A SINGLE ENGINE LANDING WITH OUT INCIDENT. INITIAL OBSERVATION BY THE PILOT SHOWED METAL FLAKES IN THE EXHAUST AND OILSDR MASA200400237Fuel Control · inoperativeCREW REPORTED RT ENGINE FAILED IN FLIGHT. THE ENGINE SHUTDOWN UNCOMMANDED INFLT. MX CHANGED THE RT FCU. OPS CHECK GOODSDR UPS04542310Engine · flamed outLT ENG FLAMED OUT ON FINAL APPROACH. DURING APPROACH RECEIVED L GEN EICAS FOLLOWED BY LT BUS FAIL, THEN 18 PSI & RED OIL PRESSURE INDICATION. PERFORMED IN FLIGHT SHUTDOWN LT ENGINE. INSP WIRE CLAMPS D1380 NO DMG NOTED, INSP ENG CHIP DET, DET CLEAN. INS P ISDR AALA20040497Engine · failedABQ INFLIGHT T1508 ON TAKE OFF ON ROTATION HEARD A LOUD BANG FROM RIGHT ENGINE ACCOMPANIED BY POWER LOSS AND AIRCRAFT YAW. RETURNED FOR LANDING. NUMBER 1 AND NUMBER 2 HAD ROTATION OIL PRESSURE ALSO IN GREEN. RETURNED TO ABQ AND LANDED OVERWEIGHT WITHOUT INCIDESDR C2XA04TY074Engine · malfunctionedTYS - FLIGHT 2110 PERFORMED AIR RETURN DUE TO ABNORMAL SMELL FROM NR 2 PACK. A/C WAS RELEASED IAW MEL 21-51-00/2 CAT-C CONTROL 041491 TO TYS WHERE MAINT REMOVED AND REPLACED THE NR 2 ENG IAW ROLL ROYCE MM 72-00-00. ALL WORK WAS ACCOMPLISHED WITH LEAK, VIBES SDR 2004UALA00406Seal · failedNR 1 ENGINE N1 VIBRATIONS. 6TH STAGE TURBINE AIRSEAL FAILURE REF: PW4074/77 IPC (PN 51A346) 72-53-00 FIGURE 7, ITEM 70A. A 4-INCH AXIAL BY 6-INCH CIRCUMFERENTIAL PIECE OF THE SEAL HAD BROKEN OUT & WAS MISSING. THE REMAINDER OF THE LPT SUFFERED HEAVY DOWNSTREASDR CA040427012Engine · failed(CAN) IN CRUISE FLIGHT THE PILOT HEARD A BANG AND THE RT ENGINE STOPPED TURNING. THE PROP WAS FEATHERED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. AFTER LANDING, THE PROPELLER COULD NOT BE TURNED BY HAND.SDR GTIA040447Engine · failedAIR RETURN, NR 1 ENGINE FAILED AFTER TAKEOFF AT 1000 AGL-FLEX PWR T/O AT 1000 AGL. WE HAD AN ABRUPT BANG AND VIBRATION AND NR 1 ENGINE ROLLED BACK. ENGINE WINDMILLED N1 30 PERCENT TILL LAND-EGT WAS OK. DID NOT NOTICE OIL PRESSURE. DID NOT TRY TO RESTART ENSDR C2XA04CL042Engine · failedCMH FLIGHT NR 2699 THE CREW REPORTED THE NR 2 ENGINE EXCEEDED 950 DEGREES ON CLIMBOUT. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. THE CREW ALSO REPORTED A SMOKE SMELL. MAINTENANCE REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOODSDR C2XA04SH253Engine · damagedSHV - FLIGHT 2806 FROM IAH TO MEM CREW REPORTED LOW OIL QUANTITY AND HIGH OIL TEMPERATURE 25 MINUTES AFTER TAKEOFF AT CRUISE ALTITUDE. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT DIVERTED TO SHV WHERE IT LANDED WITHOUT INCIDENT. SDR DL764040374Engine · shutdownAT 2000 FEET RIGHT ENG ROLLED BACK HAD HIGH FUEL FLOW AND HIGH VIBS ENG NOT RESPONDING TO THROTTLE INPUTS. AFTER LANDING ENG SHUTDOWN DUE HIGH VIBS. METAL FOUND IN TAILPIPE. REPLACED ENGINE.SDR MWEA040066Engine · inoperativeRT ENGINE POWER LOSS AND VIBRATION ON TAKEOFF ROLL. N1, N2, AND EGT APPEARED NORMAL. EPR WOULD ACCELERATE ABOVE IDLE ON TAXI BACK. REMOVED AND REPLACED RT ENGINE.SDR 04017Engine · failedAT 100 FT AFTER TAKEOFF THE NR 2 ENGINE FAILED.SDR DHL2004760002Engine · shutdownPERFORMED HUNG START PROCEDURES FOR THE NR 1 ENGINE DUE TO AFTER N2 WENT TO 40 PERCENT THE FUEL FLOW WENT TO 0 AND THE ENGINE SHUTDOWN. 2ND ATTEMPT SUCCESSFUL EXCEPT THE FUEL FLOW INITIALLY WENT TO 1700 THEN DROPPED TO NORMAL START PARAMETERS. RAN NR 1 ENGINESDR C2XA04CL041Engine · failedCLE FLIGHT NR 2162 THE CREW REPORTED NR 1 ENGINE HIGH VIBRATION ON DESCENT AND AFTER LANDING REPORTED LOW OIL PRESSURE. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.SDR MALA040343Engine · overtempLEFT ENGINE OVER TEMPED INFLIGHT. CLIMBING THROUGH 8000 FT LEFT ENG FAILED APPEARED TO HAVE COMPRESSOR STALL. TORQUE WAS LESS THAN 10 PERCENT ITT WAS 1200-1300C (QRH COMPLETE WITH SHUTDOWN ENG) AIR RETURN TO MSP. REMOVED AND REPLACED ENG IAW JC 7100-301. PSDR UPS04442243Engine · flamed outDURING CRUISE NR 2 ENG FLAMED OUT AT 37K DURING CROSSFEED FROM NR 3 TANK. OIL PRESS REMAINED 10PSI, N1 25 PERCENT, N2 28 PERCENT ENG WAS SHUTDOWN FOR APPROX 25MIN. CREW ATTEMPTED RESTART AT 33K PER QRH - NO JOY, CREW COMPLETED ENG SEVERE DAMAGE CHECKLIST. CSDR 2004UALA00370Engine · malfunctionedDIVERTED DUE TO LOSS OF LT ENGINE POWER. ENGINE HUNG DURING ACCELERATION. TSI WAS 10 HRS. FOUND PCB 3.5, PTT2 TOTAL AIR TEMP AND PIR INTERSTAGE RETURN PSI TUBE FROM TT2 SENSOR LOOSE. ALL WERE SECURED AND SAFETIED.SDR COMA0470032Engine · overheatedFLIGHT 5711 DURING TAKEOFF ROLL AT 80 KNOTS NR 2 ENGINE ITT REACHED 906C DEGREES, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE.SDR C2XA04CL038Engine · failedTHE CREW REPORTED NR 1 ENGINE VIBRATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO DAYTON AND LANDED. AFTER LANDING THE NR 1 ENGINE HAD A SMALL FIRE OUT THE BACK OF THE ENGINE. THE FIRE WAS EXTINGUISHED AND NO OTHER INCIDENT OCCURRED. MAINTENANCE REPLACED THE NSDR CA040419004Engine · failed(CAN) DEPARTING, WHILE CRUISING AT 31 000 FT, LOUD BANG COMING FROM LT ENGINE WITH DECREASING EPR , INCREASING EGT UP TO 575 C. DID NOT HAVE A RE-LIGHT WITH IGNITER ON INCREASING POWER WAS NOT RESPONDING, SO WE TREATED THAT AS A SEVERE DAMAGE OR SEPARATION SDR UPS04642147Engine · flamed outINSPECTION TYPE: ETOP, RT ENGINE FLAMED OUT WHEN POWER WAS REDUCED FOR LANDING. OBVIOUSLY NO RE-START ATTEMPTED. NO ENG PARAMETER EXCEEDENCE OBSERVED. REPLACED RIGHT ENG PER TC 6002 & TC 6001 OP'S CHECK SATISFIED.SDR 2004UALA00358Nose Cowl · damagedRETURN TO FIELD DUE TO A BIRD STRIKE TO THE NR 2 ENGINE. A BIRD STRIKE CAUSED ENGINE VIBRATION AND REDUCED POWER. REPLACED NR 2 ENGINE AND NOSE COWL.SDR AUS20040308Engine · surges(AUS) NR 2 ENGINE POWER SURGE. DURING GROUND RUN TORQUE BLED OFF. INVESTIGATION FAILED TO FIND ANY CAUSE AND THE ENGINE WAS REMOVED.SDR MASA200400201Engine · malfunctionedCREW REPORTED NR 2 ENGINE ITT 84 DEG HIGHER THAN THE NR 1 ENGINE. MX PERFORMED AN ENG COMP WASH AND PWR ASSURANCE CHECKS. MX BORESCOPED NR 2 ENGINE AND REJECTED IT. MX REPLACED NR 2 ENGINE. OP CHECKS GOOD.SDR DLM88040341Engine · fireON TAXI OUT ANOTHER AIRCRAFT REPORTED SMOKE AND OR FIRE ON NR 2 ENGINE. REPLACED ENGINE.SDR 2004UALA00357Engine · vibrationREPORTS OF VIBRATION NR 2 ENGINE. DUE TO REPORTS OF ENGINE VIBRATION THE ENGINE WAS BOROSCOPED, CHIP DETECTORS INSPECTED AND INLET AND EXHAUST CHECKED. NO DEFECTS NOTED. THE ENGINE THEN HAD A TRIM BALANCE AND RETURNED TO SERVICE.SDR GLBA20030611Engine · overtempLT ENGINE TEMP LIMITED AT TAKE OFF, PREFORMED GROUND RUN ALL PARAMETERS WITHIN LIMITSSDR CA040412006Engine · bird ingestion(CAN) FAULT: HIT 2 GEESE ON T/O HIGH SPEED REJECTED RETURNED TO GATE. FOUND EVIDENCE OF BIRD INGESTION AT NR 1 ENG. SEVERAL DAMAGED BLADES, A/C ROUTED TO HANGAR FOR ENGINE BOROSCOPE.SDR AUS20040454Engine · overheated(AUS) RT ENGINE OVERTEMPED ON START. ENGINE REMOVED.SDR AUS20040268Engine · overtorqued(AUS) RT ENGINE OVERTORQUED TO 155 PERCENT.SDR 2004UALA00327Engine · malfunctionedRETURNED TO FIELD DUE TO NR 2 ENGINE POWER PROBLEM. DOWNLOAD FROM FLIGHT DATA RECORDER (FDR) FOUND POWER LOSS ON THE NR 1 ENGINE. FOUND NR 1 POSITION SPAR VALVE WIRING W802-002-18 & W802-005-20 SHORTED TOGETHER UNDER CLAMP, 65 INCHES FROM CONNECTOR D5162P ANDSDR SWAA041010Engine · faultyAIR TURNBACK, DECLARED EMERGENCY, ON TAKEOFF NR 1 ENGINE EGT FELL TO 350 DEGREES, AIRBORNE AT 800 FEET NR 1 ENGINE VIBRATION METER MAXED OUT AT 5 UNITS WITH AIRFRAME VIBRATION. NR 1 ENGINE WAS PUT IN IDLE POSITION AND VIBRATION STOPPED, EGT STILL LOW. REMOVESDR DL757040316Engine · failedENGINE FAILURE ON LEFT ENGINE WITH T/O POWER SET, BOTH FIRE BOTTLES DISCHARGED INTO ENGINE MAX EGT 762 DEG FOR 3.06 MINUTES. REPLACED ENGINE.SDR SWAA041009Engine · failedABORTED TAKEOFF, NR 1 ENGINE FAILED ON TAKEOFF ROLL. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR DL73S040314Engine · malfunctionedABORTED T/O DCA DUE TO NR 2 ENG EPR HUNG AT 1.6, N1, N2, EGT, FF LOWER THAN NR 1. CLEARED RUNWAY, RAN ENG TO FULL POWER OK. SUSPECT CROSSWIND FOR THE LEFT AFFECTED NR 2. DID STATIC RUNUP PRIOR TO 2ND T/O, NR 2 SLOWER TO ACCEL TO T/O THAN NR 1, BUT DID REACHSDR AMTA200400394Engine · surgesLEFT ENGINE SURGES AT TAKEOFF POWER NOTED SURGE IN EPR AND N1. ACCOMPLISHED TEST 13 PER AMM CHAPTER 71-00-00-5 UNLATCHED EEC, FLUCTUATION STOPPED. INSPECTED PF RAKES FOUND NR 2 HEAD ON OUTBOARD RAKE BROKEN SEE 1405/658 FOR ACCOMPLISHMENT OF TEMP REPAIR. (M)SDR CHQA000474Engine · odorAFTER ROTATION OUT OF IND, STARTED TO SMELL FUMES. THERE WAS NO EVIDENCE OF SMOKE IN THE CABIN BUT THE F/A REPORTED THE ODOR WAS STRONGER IN THE FRONT. DECISION WAS MADE TO RETURN TO IND. THE ODOR DID START TO DISSIPATE DURING LANDED. MAINTENANCE CHECKED TSDR P5CA0401068Engine · malfunctionedNR 1 ENGINE UNABLE TO MAKE TAKEOFF POWER. REMOVED AND REPLACED NR 1 ENGINE IAW 71-00-11 AND MM 71-00-02. ENGINE RUN NORMAL.
Back to JASC 7200