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.

SDR 05FDEA02228Service difficultyNR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACKS ON FWD DOLLY MOUNTS AT APPROX 8 O'CLOCK. FPI IAW NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 SPM. STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND PER AAug 3, 2005 · N671FE · Airbus A300F4605RSDR 05FDEA02227Service difficultyNR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACK ON AFT DOLLY MOUNT AT APPROX 8 O'CLOCK POSITION. FPI IAW NTM 51-91-00 CRACK CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 OF SPM. STOP DRILLS ACCEPTABLE PER EA 6-7223-82106-NAug 3, 2005 · N671FE · Airbus A300F4605RSDR 05FDEA02226Powerplant · crackedW/O 29493, NR N00177, ENGINE NR 1 AT FORWARD INBOARD LOWER HOIST POINT, THE FLANGE IS CRACKED AT IT'S BASE. FPI IAWM NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 PER GESPM STOP DRILL ACCEPTABLE PER EAAug 3, 2005 · N671FE · Airbus A300F4605RSDR UPS05845033Engine · shutdownNR 4 ENG SHUT DOWN IN FLT DUE TO OVER TEMP AND LOUD THUD. FROM LP 427064 ITEM 1 AND LP 427065 ITEM 3: PERFORMED THRUST LEVER STATIC TRIM IAW AMM 71-00-00 PG 595.23 TEST 9A. PERFORMED PART POWER TRIM AND INCREASED BY 10 CLICKS. PERFORMED ENG HIGH PWR RUN-UP.Aug 3, 2005 · N813UP · Doug DC873FSDR EVC2005F00000Engine · failedENGINE CAUTION WARNING CHIP DETECTOR LIGHT ILLUMINATED IN FLIGHT. CHIP DETECTOR WAS REMOVED AND NO SIGNIFICANT CHIP WAS FOUND. REINSERTED CHIP PLUG AND RAN AIRCRAFT LIGHT ILLUMINATED AGAIN. MAINTENANCE FOUND EXTENSIVE METAL ON BOTH UPPER AND LOWER ENGINE CHAug 2, 2005 · N59AE · Bell 206L1SDR COMA0560424Engine · overtempFLIGHT 5807- LT ENGINE HIGH ITT. SHUDDER AND VIBE IN AIRFRAME. REPLACED ENGINE.Aug 2, 2005 · N442CA · Cndair CL6002B19SDR HALA0500801Engine · malfunctionedLT ENGINE PARAMETERS STARTED TO FLUCTUATE APPROX 7000 FT ON CLIMBOUT. WENT FROM CLB1 TO MCT PWR, IGN SYMBOL CAME ON. FMS PAGE CHANGED TO CONFIRM ENG OUT ALL FLUCTUATIONS WERE SMALL AND DID NOT SHUTDOWN ENGINE. ACCOMPLISHED FIM 73-22, TASK 807 EEC, INPUTS FRAug 2, 2005 · N486HA · Boeing 717200SDR EVCA105166Engine · making metalENGINE CAUTION WARNING CHIP DETECTOR LIGHT ILLUMINATED IN FLIGHT. CHIP DETECTOR WAS REMOVED AND NO SIGNIFIGANT CHIP WAS FOUND. REINSERTED CHIP PLUG AND RAN AIRCRAFT LIGHT ILLUMINATED AGAIN. MINTENANCE FOUND EXTENSIVE METAL ON BOTH UPPER AND LOWER ENGINE CHIPAug 2, 2005 · N59AE · Bell 206L1SDR CA050808004Engine · making metal(CAN) LOSS OF ENGINE OIL PRESSURE OBSERVED IN CRUISE. ENGINE WAS SHUTDOWN AND UNEVENTFUL SINGLE ENGINE LANDING PERFORMED. GROUND EXAMINATION SHOWED A QUANTITY OF METAL CHIPS ON THE RGB CHIP DETECTOR. ENGINE IS EN-ROUTE TO MFG FOR TEAR-DOWN INVESTIGATION. MFGAug 1, 2005SDR VNAA0508002Sensor · failedNR 2 ENGINE N1 STARTED FLUCTUATING +/-10% WHILE CLIMBING THROUGH 21,000 FT. THE AIRCRAFT RETURNED TO PHL WHERE MAINTENANCE REMOVED AND REPLACED THE T2C COMPRESSOR INLET TEMPERATURE SENSOR IAW CRJ200 AMM 73-21-09-000(400)-801. ALL GROUND OPERATIONAL CHECKS WEAug 1, 2005 · N230PS · Cndair CL6002B19SDR 2005UALA00746Engine · contaminatedRETURNED TO FIELD UNDER AMBER ALERT DUE TO FUMES IN THE COCKPIT. ODOR DISSAPATED DURING RETURN TO GATE. THE DETERGENT WASH OF THE ENGINES IS THE SORCE OF THE ODOR. PER MM 72-05-99 PAGE 701, ENGINE NEEDS HIGH POWER RUN AFTER WASH TO REMOVE ANY DETERGENT RESIDUAug 1, 2005 · N595UA · Boeing 757222SDR HNAA0500073Garlock Seal · leakingMASTER WARNING LIGHT AND NR 2 ENGINE OIL PRESSURE WARNING LIGHT FLICKERED ONCE EVERY 35 SECONDS TO A MINUTE. OIL PRESSURE FLUCTUATED BETWEEN 40 AND 55 PSI. PERFORMED ABNORMAL CHECKLIST. WITH P/L AT F/I AND C/L AT MIN OIL PRESSURE STABILIZED AT 55 PSI. REMOAug 1, 2005 · N808EX · Dhav DHC8102SDR GTIA050222Engine · failed1500 FT ON CLIMB-OUT LOUD BANG, NR 2 ENGINE FAILURE, ROLLBACK. ENGINE FAILURE CHECKLIST COMPLETED, OVERWEIGHT LANDING PERFORMED. REMOVED AND REPLACED NR 2 ENGINE, OPS AND LEAK CHECK GOOD. (M)Jul 31, 2005 · N802NK · Doug DC983SDR CA050824001Engine · flamed out(CAN) ON CLIMB FOLLOWING A WATER DROP, THE ENGINE FLAMED OUT AND THE PROPELLER AUTO-FEATHERED. THE MECHANICAL FUEL CONTROL UNIT AND FUEL PUMP WERE SUBSEQUENTLY REPLACED. PWC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Jul 31, 2005SDR AALA20050485Engine · fodCCS INFLIGHT T1522/31JUL - LEFT ENGINE INGESTED LARGE VULTURE AND ENGINE EXHAUST GAS TEMPERATURE WAS 934 C. ENGINE SHUTDOWN. FOUND THREE FAN BLADES DAMAGED. AIRCRAFT OUT OF SERVICE.Jul 31, 2005 · N605AA · Boeing 757223SDR WRLA2005139Engine · flamed outON ROLLOUT, NR 2 ENGINE FLAMED OUT, ENGINE WAS IN REVERSE THRUST. PERFORMED T/S AS PER FIM 71-01-02. ALL CHECKS OK PERFORMED EXTENDED DURATION ENGINE RUN IN FWD AND REVERSE THRUST CONDITIONS. ENGINE RUNS ALL NORMAL.Jul 31, 2005 · N801DE · Doug MD11SDR SF20050730Engine · overtempFLT NR 7531 FROM CRW TO IAD, ON TAKEOFF ROLL, NR 1 ENGINE OVERTEMP. TEMP REACHED 933 FOR APPROX 2 SECONDS. AIRCREW REJECTED TAKEOFF AND RETURNED TO GATE.Jul 30, 2005 · N14XS · Saab SF340ASDR 2005FA0001087Engine · damagedAIRCRAFT PROCEEDED WITH A NORMAL TAKEOFF IN VFR CONDITIONS. FOLLOWING ROTATION, AND AT APPROXIMATELY 50 TO 100 FT AGL, THE RT ENGINE LOST POWER, THE PILOT LEVELED OFF. THE AC WOULD NOT MAINTAIN ALTITUDE, PILOT CHOSE TO LAND IMMEDIATELY, WITH ADEQUATE RUNWAYJul 30, 2005 · N432FA · Beech 200BEECHSDR CA050809002Engine · failed(CAN) AC WAS IN CRUISE, RT ENG WAS INDICATING NML, ENG SEEMED TO STUMBLE, COME BACK TO NML, THEN IMMEDIATELY FAILED. TEMP GAUGE FOR ENG RAPIDLY EXCEEDED 1000 DEGREES C, RPM DROPPED TOWARDS 0, TORQUE JUMPED THEN DROPPED TOWARDS 0. CAPT PULLED THROTTLE BACK, FJul 28, 2005 · Braero HS7482ASDR 05FDEA02128Engine · fireNR 1 ENG FIRE ON GROUND-LOUD BANG, FOLLOWED BY SMOKE, FOLLOWED BY NR 1 ENGINE FIRE WARNING ENGINE FIRE AND SEVERE QRH COMPLIED WITH AS WELL AS ALL APPLICABLE CHECKLISTS. NR 1 FIRE BOTTLE FIRED, NR 1 PACK ON-TEMP 38C GOOD FIRE TEST. REMOVED AND REPLACED NR 1 EJul 28, 2005 · N397FE · Doug DC1010SDR 7272005N234CAEngine · bird ingestionON TAKEOFF FROM NR 1 ENGINE INGESTED A BIRD. THIS OCCURRED AFTER V1. JUST AFTER ROTATION THE NR1 ENGINE QUIT. IT WAS RESTARTED AND THE AIRCRAFT CLIMBED TO THE ASSIGNED ALTITUDE. THE CREW NOTIFIED THE TOWER AND RETURNED TO DEPARTURE. (K)Jul 27, 2005 · N234CA · Amd FALCONSDR CA050727001Engine · failedDURING TAKEOFF ROLL, ENG NR 2 FAILED. TAKEOFF REJECTED. RAISED, ENGINE CHANGE IN PROGRESS (YOW).Jul 27, 2005SDR MWEA050073Engine · odorREAR CABIN BEGAN TO FILL WITH SOME HAZE AND RIGHT SMOKE DETECTOR WENT OFF. REMOVED AND REPLACED RIGHT ENGINE.Jul 27, 2005 · N809ME · Doug DC982SDR DL75K050403Engine · making metalLEFT ENGINE FAILED ON TAKEOFF ROLL, ABORTED T/O. REPLACED ENGINE.Jul 26, 2005 · N650DL · Boeing 757232SDR ASMF200507022Hose · damagedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF WHEN LEFT ENGINE WAS STARTED, IT DID NOT REACH THE MINIMUM IDLE VALUES. DURING TAXING, ENGINE WAS ACCELERATED TO 80% OF RPM AND IT ONLY REACHED EPR 1.00, N1 18 PERCENT, N2 43 PERCENT, EGT 520 AND FF 400 KGPM. TJul 26, 2005 · N204AM · Doug DC987SDR SF20050726Engine · malfunctionedFLT 7539 IAD-DAY STARTED NR 1 ENGINE NORMALLY, AFTER TURNING ON NR 1 GENERATOR, LT ITT INCREASED TO 1068, MOTORED NR 1 ENGINE DOWN & SHUTOFF NR 1 GENERATOR.Jul 26, 2005 · N121CQ · Saab SF340ASDR ASMF200507019Engine · failedCAPTAIN REPORTED THAT DURING LEFT ENGINE STARTING AND SHUT OFF, VIBRATION WAS FELT IN THE HOLE AIRCRAFT. THE LEFT ENGINE VIBRATION ABSORBERS, BARS AND ACCESSORIES WERE INSPECTED, BEING ALL CORRECT. THE LEFT ENGINE WAS STARTED DETECTING VIBRATION. THE UVC WAS DJul 25, 2005 · N583MD · Doug DC983SDR CA050728010Engine · shutdownTHE ENGINE EXPERIENCED A POWER LOSS IN CRUISE. THE POWER SECTION WAS SHUT DOWN IN FLIGHT. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Jul 24, 2005 · Bell 212SDR COMA0560407Engine · failedFLIGHT 5378- ENROUTE OKC-CVG RECEIVED A ZERO PSI OIL PRESSURE WARNING ON THE LEFT ENGINE. CREW DECLARED AN EMERGENCY, DIVERTED TO TUL AND LANDED WITHOUT INCIDENT.Jul 24, 2005 · N916CA · Cndair CL6002B19SDR AALA20050460Engine · making metalDFW INFLIGHT T563/23JUL - ON CLIMB-OUT APPROXIMATELY 1400 FEET RIGHT ENGINE LOW OIL PRESSURE LIGHT ON. RIGHT OIL QUANTITY NORMAL. RIGHT OIL TEMPERATURE DECREASING. REDUCED POWER ON RIGHT ENGINE TO IDLE. APROXIMATELY 5 MINUTES LATER INCREASED POWER ON RIGHTJul 23, 2005 · N430AA · Doug DC982SDR CHQA200500132Engine · failedFL350, THRUST SET TO CLIMB, NR 1 ITT YELLOW RANGE AT APPROX 903-904 CELSIUS. POWER RETARDED & ITT REDUCED TO GREEN. ITT REMAINED 80-90 DEGREES HOTTER THAN NR 2 ENG ITT, A HIGHER FUEL FLOW OBSERVED, & VIBRATIONS ON HP SPOOL OF NR 1 NOTABLY HIGHER (STILL WITHINJul 23, 2005 · N561RP · Emb EMB145LRSDR DXTA200500854Engine · power lossDURING POWER UP FOR TAKEOFF RIGHT ENGINE WOULD NOT MAKE TAKEOFF POWER. PUSHED RIGHT POWER LEVER TO STOP ONLY GOT 96.0 PERCENT N1, NEEDED 96.7 PERCENT N1 FOR TAKEOFF. RAN A/C FOR POWER OF THE DAY RUN COMPUTED P.O.D FOR 94.9 ENG MADE POWER. PUSHED THROTTLE TOJul 23, 2005 · N344QS · Cessna 560CESSNASDR HEEA107351Engine · malfunctionedIN CRUISE, NR 1 ENGINE NR AND NG AND MGT WENT HIGH, TORQUE AND NP SHOWED ZERO, REDUCED NR 1 THROTTLE AND PERFORMED CHECKLIST AND SHUT ENGINE DOWN. ROTOR RPM WENT TO 107 FOR 10 SECONDS. INSPECTED ENGINE AND REPLACED YELLOW ENGINE HARNESS AND ECU.Jul 22, 2005 · N3897N · Bell 214STSDR GTIA050217Engine · overheatedSJU - LEFT ENGINE OIL GREATER THAN 170 ON CLIMB-OUT. SHUT ENGINE DOWN PER QRH AND RETURNED TO SJU. REMOVED AND REPLACED NR 1 ENGINE IAW MM 71-00-00 AND W/C 00191. (M)Jul 22, 2005 · N828NK · Doug MD83SDR AALA20050463Engine · stalledON TAKEOFF NUMBER ONE ENGINE COMPRESSOR STALLED. RETUNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 22, 2005 · N7082A · Airbus A300B4605RSDR CED2006F00023Engine · malfunctionedON TAKEOFF ROLL, THE NR 2 ENGINE WOULD NEVER PRODUCE TAKEOFF . THE CREW ABORTED TAKEOFF ROLL AND EXITED THE RUNWAY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. ALL ENGINE PARAMETERS WERE WITHIN NORMAL LIMITATIONS. (K)Jul 21, 2005 · N238CA · Lear 25SDR DL764050388Engine · failedDURING APPROACH, THROTTLES WERE PLACED AT IDLE FOR A SPEED REDUCTION. WHEN THROTTLES WERE ADVANCED HEARD A NOISE, RIGHT ENGINE STARTED TO SLOWLY ROLL BACK, SHUT DOWN ENG PER QRH. REPLACED NR 2 ENGINE.Jul 21, 2005 · N836MH · Boeing 767432ERSDR AALA20050457Engine · stalledBOS INFLIGHT T509/21JUL - AFTER TAKEOFF, RIGHT ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS. CREW SHUT DOWN ENGINE AND RETURNED TO BOS AND LANDED WITHOUT INCIDENT. FLIGHT DATA RECORDER REVEALED ENGINE EXHAUST GAS TEMPERATURE EXCEEDED 667C. REPLACED NUMBER Jul 21, 2005 · N402A · Doug DC982SDR CA050824007Engine · malfunctioned(CAN) IN CRUISE, THE ENGINE EXHIBITED AN UNCOMMANDED INCREASE IN ITT. ENGINE POWER WAS REDUCED TO IDLE AND THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. PWC WILL MONITOR INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE, ONCE DETERMINED.Jul 20, 2005 · Cessna 208BSDR CA050726002Engine · failed(CAN) DAMAGE OCCURRED TO PLATING OF FWD SEALING DIAMETER OF BETA CNTRL OIL TRANSFER SLEEVE. DIAMETER INDICATED BOND OF PLATING TO PARENT MATERIAL OF SLEEVE WAS STILL GOOD, WAS SCORING FROM FOD. EXTRUSION OF PLATE FWD FROM DIAMETER, INDICATION PIECES HAD SEPARJul 20, 2005SDR BB05055Engine · failedPVD FLT 208 EN-ROUTE, CLT TO PVD - DURING THE FLIGHT, THE LAVATORY SMOKE DETECTORS ALARMED FOR SMOKE, AND THEN SHUT OFF. AFTER LANDING, THE GROUND CREWS NOTED AN OIL ODOR IN THE JETWAY OF THE TERMINAL. MAINTENANCE NOTED THAT THERE WAS AN OIL MIST IN THE INJul 20, 2005 · N608AU · Boeing 757225SDR AWXA200500836Eec · malfunctionedNR 1 ENG STALLED. CREW RETURNED TO LAS WITHOUT INCIDENT. ENG BORESCOPED & FERRIED BACK TO PHX. MX R & R NR 1 ENG 7TH STAGE BLEED VALVE, 7A & 7C BLEED VALVE, & 7C BLEED VALVE SOLENOID. LUBED VSV ON NR 1 ENG & R & R NR 1 EEC. PERFORMED POWER RUNS IAW TASK CJul 19, 2005 · N802AW · Airbus A319132SDR AALA20050453Engine · stalledPHX INFLIGHT T436/18JUL PASSING 5000 FT ON DEPARTURE EXPERIENCED SINGLE LOUD BAND AND FAILURE OF LT ENGINE. RETURNED TO PHX AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)Jul 18, 2005 · N432AA · Doug DC982SDR DL757050373Engine · making metalFL380 LEVEL FLT .79 MACH RT ENGINE CHUGGED AND RT OIL TEMP ROSE TO 166 THROTTLED BACK OIL TEMP RECOVERED EICAS MSG RT OIL FILTER APPROX 5 MINUTES LATER ENGINE CONTINUALLY CHUGGED SHUT IT DOWN. NO METAL FOUND IN TAILPIPE. ALL CHIP DETECTORS HAVE METAL STATUS Jul 17, 2005 · N616DL · Boeing 757232SDR SF20050717Engine · shutdownFLT 7574 FROM BGM TO IAD, 7-17-2005. ON CLIMBOUT, AIRCRAFT HAD AN UNCOMMANDED REDUCTION IN NR 1 PROP'S RPM. AIRCREW FOLLOWED QRH AND PUT INTO TORQUE MOTOR LOCKOUT. THE REDUCTION CONTINUED. AIRCREW CONTINUED TO FOLLOW QRH AND SHUT THE ENGINE DOWN AND RETURNED TJul 17, 2005 · N43SZ · Saab SF340ASDR UPS05444898Engine · failedNR 3 ENGINE FAILED. REPLACED NR 3 ENGINE IAW TASK CARD 5000, 5016. OPS CHECK GOOD.Jul 14, 2005 · N521UP · Boeing 747212BSDR ASOA05598Engine · malfunctionedDURING CLIMB OUT, AT APPROXIMATELY 12,000 FEET THE CREW RECEIVED A (RT ENGINE OIL PRESSURE) WARNING WITH THE OIL TEMPERATURE INCREASING TO 153 DEGREES CENTIGRADE AND THE OIL PRESSURE FLUCTUATING BETWEEN 24-36 PSI. QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DEJul 13, 2005 · N871AS · Cndair CL6002B19SDR A6WA200540241Engine · odorINFLIGHT DETECTED OILY ODOR AFTER BLEED AIR CHANGE OVER FROM APU TO ENGINE AIR IN COCKPIT. FERRIED FOR ENGINE NR 1 CHANGE. (K) REMOVED AND REPLACED COALESCER SOCKS IN LEFT AND RIGHT WATER SEPARATORS, NO FURTHER ODOR NOTED. (M)Jul 13, 2005 · N457AW · Cndair CL6002B19SDR QXEA200501103Warning Light · illuminatedNR 1 AND NR 2 ENGINE MANUAL CAUTION LIGHTS ILLUMINATED. MAINTENANCE RESET CIRCUIT BREAKER FOR BETA LOCKOUT. CAUTION WENT AWAY. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Jul 13, 2005 · N374PH · Dhav DHC8202SDR C2XA05IA086Bevel Gear · failedFLIGHT 2543 - EN ROUTE TO IAH THE CREW REPORTED THAT THE NR 1 ENGINE SHUT DOWN UNCOMMANDED DURING DESCENT AROUND 14,000 FT. ENGINE 1 OUT, MESSAGE WAS DISPLAYED ON THE EICAS SCREEN ALONG WITH SHED BUS 1 AND 2. THE CREW ATTEMPTED TO AIR START THE ENGINE BUT WAJul 12, 2005 · N17159 · Emb EMB145XR
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