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 AMTA200400199Engine · malfunctionedRT ENGINE SHUTDOWN ACCOMPLISHED DUE TO OIL PRESSURE AND QUANTITY ZERO, APPROX FL 300. REPLACED ENGINE IAW M57-71-04. (M)Feb 24, 2004 · N555TZ · Boeing 75733NSDR CA040227001Engine · making metal(CAN) ONCE AT LEVEL FLIGHT THE RT ENGINE OIL PRESSURE WAS NOTICE TO BE AT THE LOWER END OF THE GREEN ARC 70 PSI, THE OIL PRESSURE WAS MONITORED UNTIL IT DROPPED TO 65 PSI AND THE CREW ELECTED TO RETURN. THE PRESSURE REMAINED STABLE AT 65 PSI, UNTIL TOUCHDOWN WFeb 24, 2004 · Swrngn SA226TCSDR CA040226006Engine · making metal(CAN) ONCE AT LEVEL FLIGHT THE RT ENGINE OIL PRESSURE WAS NOTICE TO BE AT THE LOWER END OF THE GREEN ARC 70 PSI, THE OIL PRESSURE WAS MONITORED UNTIL IT DROPPED TO 65 PSI AND THE CREW ELECTED TO RETURN. THE PRESSURE REMAINED STABLE AT 65 PSI, UNTIL TOUCHDOWN WFeb 24, 2004 · Swrngn SA226TCSDR DHL2004805001Engine · malfunctionedON TAKEOFF ROLL NR 1 ENGINE ROLLED BACKED TO IDLE. CHECKED NR 1 ENGINE MAIN ENGINE CONTROL (MEC) CONTROL RODS, INSPECTED INLET & EXHAUST, CHECKED SPECIFIC GRAVITY, FOUND OK IAW CFM M/M 72-00-00. PERFORMED POWER ASSURANCE CHECK IAW JRH 13.3, FOUND OK. UNABLEFeb 24, 2004 · N805DH · Doug DC873FSDR HNAA0400012Engine · failedNR 1 ENGINE FAILED IN FLIGHT. PRIOR TO ENG NR 1 ENG OIL PRESS WARN LIGHT MOMENTARILY ILLUMINATED. WHEN ENGINE FAILED PROP DID NOT FX HAD TO USE ALT FX. AIRCRAFT WAS IN DESCENT, ENGINE AND PROP WERE IN A STABLE CONDITION. REMOVED AND REPLACED ENGINE. APPEAFeb 21, 2004 · N965HA · Dhav DHC8201SDR RYN2004F00001Engine · malfunctionedON TAKEOFF, THERE WAS A LOUD BANG AND ECAM WARNING INDICATED EGT OVERTEMP ON NR 2 ENGINE. ECAM PROCEDURES FOLLOWED AND EMERGENCY DECLARED. AIRCAFT RETURNED, AND LANDED WITHOUT INCIDENT.Feb 21, 2004 · N951LFSDR S04472025Engine · surges744 B18273, DURING FINAL APPROACH, AT ALT 4000 FT, AUTO THROTTLE WAS ENGAGED. WHEN THROTTLE ADVANCE FROM IDLE, ENG 1 SURGE AND SPOOL DOWN.C/A: REPLACE ENG 1 VSV ACT. PERFORM MAINT ACTION IAW FIM 71-00-00. CHECK NML.Feb 20, 2004 · Boeing 747400SDR C2XA04IA015Engine · flamed outDURING CLIMBOUT THROUGH 27,000 FT THE NR 2 ENGINE FAILED. ATTEMPTS WERE MADE TO RESTART THE ENGINE WITHOUT SUCCESS. THE AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT WHERE THE AFFECTED ENGINE WAS REPLACED.Feb 20, 2004 · N21129 · Emb EMB145XRSDR CA040219002Engine · stalled(CAN) NR 1 ENGINE STALL IN CRUISE. DUE TO HISTORY MTC ADVISED RETURN FOR INVESTIGATION AND FURTHER T/S. DFDR PULLED.Feb 19, 2004 · Airbus A320211SDR HEEA093676Engine · malfunctionedDURING CRUISE FLIGHT NR 2 ENGINE TORQUE DROPPED TO 10 PERCENT AND NR 1 ENGINE TORQUE ROSE TO 99 PERCENT. ROTOR RPM DECREASED TO 104 PERCENT. MAINTENANCE REPLACED THE NR 1 ENGINE ASSEMBLY.Feb 18, 2004 · N22342 · Skrsky S76ASDR MEX2004067Engine · fodFLT 106 - GDL-MEX - DURING TRANSIT CHECK TWO BLADES ON LEFT ENGINE AND NOISE SUPPRESSOR WERE DETECTED WITH DAMAGE BY FOD. THE DAMAGES WERE WITHIN LIMITS IAW MM 72-33-22. THE BLADES WERE REPAIRED IAW MM 72-33-22. THE NON ROUTINE CARD NR A0055136 WAS ISSUED TFeb 18, 2004 · N216AM · Doug DC987SDR CA040219003Engine · failed(CAN) UPON THE TRANSITIONING FROM CLIMB TO CRUISE, A LOUD BANG WAS HEARD AND SUBSEQUENT VIBRATION FELT THROUGHOUT THE AIRFRAME. ALL NR 1 ENGINE PARAMETERS IMMEDIATELY BEGAN TO DETERIORATE RAPIDLY. AT FL280, ENGINE FAILURE DRILL INITIATED AND COMPLETED. ATC AFeb 18, 2004 · Boeing 727225SDR UPS04541950Engine · bird ingestionINSPECTION TYPE: ASE, ENGINE SHUT DOWN FOR BIRD STRIKE NR 1. REPLACED LT ENGINE ASSY PER TC 5002 (RR) PAGE 1-17 & TC5001 (RR) PAGES 1-41.Feb 18, 2004 · N457UP · Boeing 75724APFSDR C2XA04IA013Engine · defectiveLCH-FLIGHT 970, THE CREW REPORTED SMOKE IN THE CABIN, THE CREW SHUT DOWN THE NR 2 ENGINE, AND DIVERTED TO LCH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIFeb 18, 2004 · N13970 · Emb EMB145SDR PCAA0402170Engine · out of rigFLIGHT 3915 SYRACUSE REPORTED THE AIRCRAFT DID NOT SLOW DOWN WHEN POWER LEVERS WERE SELECTED TO DISC. MAINTENANCE INSPECTED SYSTEMS AND RAN AND TAXIED THE AIRCRAFT, NO DEFECTS WERE NOTED. ITEM WAS THEN DEFERRED UNTIL AIRCRAFT REACHED MAINTENANCE AND ENGINE RFeb 18, 2004 · N844EX · Dhav DHC8102SDR ANCF200400003Engine · surgesRT ENGINE SURGE DURING ACCEL (AFTER SELECTING CLIMB THRUST) AT 5000 FT ENG OPERATION ABNORMAL AFTER SURGE. ENG WAS NOT SHUTDOWN. BOROSCOPE INSPECTION WAS PERFORMED IAW AMM 71-00-00/601, FIM 71-06-00, FIG 105A NEGATIVE TEST, THE ENGINE WILL BE REPLACE ON FEBRUFeb 17, 2004 · N517NA · Boeing 75728ASDR AUS20040100Engine · leaking(AUS) LT ENGINE OIL LEAK EVIDENT IN P2.5 CAVITY.Feb 14, 2004 · Dhav DHC8202SDR N401MAIsolation Mount · debondedENROUTE TO THE HOSPITAL FOR PATIENT PICKUP. STRONG 2 PER REV VIBRATION EXPERIENCED. LANDED AT PSP AIRPORT. CONTACTED MAINTENANCE FOR REPAIRS. AFTER TROUBLESHOOTING FOUND LATERAL ISOLATION MOUNT DEBONDED. REMOVED AND INSTALLED SERVICEABLE UNIT.Feb 14, 2004 · N401MA · Bell 412SDR DXTA200400242Engine · shutdownON LANDING WHILE PULLING BACK ON THE THRUST REVERSER LEVERS, NR 1 ENGINE WENT TO SHUTDOWN AND NR 1 ENGINE FIRE LIGHT ILLUMINATED. PULLED NR 1 ENGINE FIRE BOTTLE, AIRCRAFT ARRIVED AT GATE WITHOUT FURTHER INCIDENTS. ITEM IS UNDER INVESTIGATION.Feb 12, 2004 · N548QS · Braero HAWKER1000SDR QXEA200400134Engine · malfunctionedSEA FLIGHT 2045 RETURN TO FIELD FOR TORQUE SPLIT AND/OR FUEL FLOW SPLIT EN ROUTE TO PDT. ON RETURN TO SEA ON APPROACH AT 5,000 FEET CABIN AND COCKPIT FILLED WITH SMOKE. CAPTAIN DECLARED EMERGENCY BUT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE. OPERATIONFeb 12, 2004 · N347PH · Dhav DHC8202SDR 2005UALA00159Engine · fluctuatesDIVERTED TO HNL DUE TO NR 2 ENGINE POWER FLUCTUATION. AS A PRECAUTIONARY MEASURE BOROSCOPED ENGINE TO CHECK COMPRESSOR HEALTH, RECHECKED CHIP DETECTORS AND OIL FILTER. ALSO REPLACED 10TH STAGE CHECK VALVE.Feb 11, 2004 · N547UA · Boeing 757222SDR DHL2004782006Engine · malfunctionedAT FL310 DURING CRUISE A LOUD HUM ACCOMPANIED BY A VIBRATION OCCURRED ON ENGINE NR 3. PERFORMED ABNORMAL IN-FLIGHT ENGINE SHUTDOWN PROCEDURE PER 727 AOM. REMOVED AND REPLACED NR 3 ENGINE ASSEMBLY IAW ASTAR B-727 MTM 71.1. OPS CHECKED GOOD, OK FOR SERVICE.Feb 11, 2004 · N782DH · Boeing 727227SDR 00131Engine · flamed outPILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL 370. WILL UPDATE THIS SDR AFTER MAINTENANCE. LT ENGINE REMOVED FOR HSI INSPECTION NO ABNORMAL WEAR REPORTED, PERFORMANCE RUN COMPLETED, ENGINE AND AIRCRAFT RETURN TO SERVICE.Feb 10, 2004 · N888TW · Lear 24DSDR AALA20040220Engine · contaminatedMIA INFLIGHT T/1901/10 ON CLIMBOUT NR 2 OIL QUANTITY BEGINS TO DECREASE. AT 20000 FEET OIL QUANTITY WAS AT ZERO AND OIL TEMPERATURE WENT UP TO 154. OIL PRESSURE FLUCTUATED BETWEEN 30 PSI AND 50 PSI. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. AFTER LANDIFeb 10, 2004 · N90070 · Airbus A300B4605RSDR BAQA092608Case Half · crackedPLASTIC MISSING/CRACKED BEYOND LIMITS. UNIT ORIGINAL EQUIPMENT OFF OF ENG.. REPLACED WITH SERVICABLE UNIT. 02/26/2004Feb 9, 2004 · N912KY · Aerosp AS355F2SDR DL76L040141Engine · stalledNR 2 ENG STALLED ON TAKEOFF ROLL 110 KNOTS, RT ENG SURGE DET ON EICAS ENG EXCT RECORD 660 FOR 12 SEC. REPLACED NR 2 ENG S/N 723843 PER TRANS 1T149.Feb 8, 2004 · N181DN · Boeing 767332SDR UPS04841817Engine · flamed outNR 1 ENGINE FLAMED OUT AT TOP OF DESCENT WHEN POWER REDUCED. ENGINE READINGS WERE NORMAL W/ WINDMILLING RPM OF 22 PERCENT N2. RESTART AT FL 200 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GEN. INSP CK FLT IDLE, SPECIFIC GRAVITY SETTING. MAGNETIC CHIP DETECTORS Feb 4, 2004 · N880UP · Doug DC873FSDR 04FDEA00304Engine · malfunctionedDURING CLIMBOUT IN VMC NR 2 ENG (LOUD NOISE) FROM TAIL AREA. NEXT HIGH EGT (RED) AND VIBRATION. REF QRH SHUT NR 2 ENG DOWN. LANDED RPLL. CREW DEBRIEF AT CLIMBOUT 19,000 FT ENCOUNTERED LOUD NOISE FROM TAIL AREA AND VIBRATION, PERFORMED WALK-AROUND INSPECTIOFeb 3, 2004 · N620FE · Doug MD11SDR UPS04841813Engine · flamed outUPON THROTTLE REDUCTION TO IDLE FOR DESCENT FROM FL 370 M .80, NR 1 ENGINE FLAMED OUT. ENG READINGS WERE NORMAL WITH WINDMILLING RPM OF 22 PERCENT N2. RESTART AT FL300 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GENERAL INSP, CK FLT IDLE, SPECIFIC GRAVITY SETTFeb 3, 2004 · N880UP · Doug DC873FSDR PCAA0402162Engine · odorFLIGHT 3884, SYRACUSE TO PHILADELPHIA, HAD TO DIVERT TO AVOCA DUE TO ODOR IN THE CABIN AND COCKPIT. MAINTENANCE INVESTIGATED AND REMOVED AND REPLACED THE AIR CYCLE MACHINE AND THE NR 2 AIR SWITCHING VALVE. PROBLEM STILL EXISTED. AIRCRAFT WAS FERRIED TO MIDDFeb 2, 2004 · N844EX · Dhav DHC8102SDR 187531Engine · malfunctionedDURING CRUISE THE CREW SET THE RIGHT ENGINE POWER AT 80 PERCENT TQ. THE CREW HEARD A LOUD BANG, FELT A SLIGHT YAW AND NOTICED THAT THE RIGHT TQ HAD DROPPED TO APPROX 70 PERCENT. THE CREW ADJUSTED THE TQ AND THEN HEARD MULTIPLE BANGS ALONG WITH A DROP IN RIGHFeb 1, 2004 · N158SD · Saab SF340ASDR CA040205004Engine · failed(CAN) AFTER TAKE OFF, 2000 ASL, NR 2 LOUD BANG FOLLOWED BY ENGINE STOPPAGE, MAYDAY DECLARED, ENGINE SECURED AND QRH DRILLS ACTIONED. RADAR VECTORED SINGLE ENGINE APPROACH AND LANDING. FIRE SERVICE ESCORTED ON LANDING, PAX OFFLOADED ON STAND. THE ENGINE WAS REPJan 31, 2004 · Cndair CL6002C10SDR CHQA000433Engine · failedDURING CLIMBOUT OF LGA AT 10,000 FT CREW HEARD A POP WITH IMMEDIATE LOSS OF THRUST ON NUMBER 2 ENG. EICAS INDICATED A SPOOL DOWN WITH RAPIDLY RISING ITT. BROUGHT THRUST LEVER TO IDLE AS ITT REACHED 1050 DEGREES. ITT REDUCED AND ENGINE WAS SHUT DOWN. NO OTHER AJan 31, 2004 · N290 · Emb EMB145LRSDR AUS20040055Engine · failed(AUS) RT ENGINE FAILED TO START. FURTHER INVESTIGATION FOUND N2 SHAFT NOT BEING DRIVEN BY N2 GEARBOX. INVESTIGATION IS CONTINUING.Jan 28, 2004 · Boeing 767338SDR DXTA200400232Engine · flamed outWHILE DESCENDING THROUGH FL 310 WITH THE RIGHT POWER LEVER AT FLIGHT IDLE, THE BOOST PUMP CAME ON AND OIL PRESSURE DROPPED TO ZERO, GENERATOR WENT OFF-LINE. THE RIGHT ENGINE FLAMED OUT, IT THEN AUTO RELIT AT FL 290. REMOVED AND REPLACED THE RT ENGINE IAW CESSJan 28, 2004 · N804QS · Cessna 560CESSNASDR CA040130003Retainer · collapsed(CAN) THE HOT SECTION WAS GIVEN A SCHEDULED HOT SECTION INSPECTION. FOUR CT SHROUD SEGMENTS HAD SHIFTED SLIGHTLY. THE RETAINING RING HAD COME OUT OF THE GROOVE. THIS PROBLEM HAS BEEN DOCUMENTED ON OTHER ENGINES. PWA HAS ISSUED P/N 3110741-02 RETAINING RING ON Jan 26, 2004 · Cessna 208BSDR MASA200400045Engine · hot startCREW REPORTED LEFT ENGINE HOT START. MX DRY MOTORED AND THAN STARTED THE ENG. OP CHECKS GOOD. NO PARTS USEDJan 25, 2004 · N17217 · Cndair CL6002B19SDR HEEA093483Engine · failedWHILE IN CRUISE FLIGHT HEARD A BUMP, THE AIRCRAFT YAWED, NR 1 ENGINE OUT LIGHT CAME ON, MAST CAUTION LIGHT CAME ON, ENGINE CHIP LIGHT CAME ON, AND ALL GAUGES WENT TO ZERO ON THE NR 1 ENGINE. CONTINUED FLIGHT AND LANDED AT AIRPORT.Jan 25, 2004 · N761PH · Skrsky S76ASDR HNAA0400007Engine · surgesAFTER AUTOFEATHER WAS SELECTED IT DID NOT INITIALLY ARM DURING TAKEOFF ROLL. WHEN IT DID ARM, IT CAUSED NR 2 ENGINE TO SURGE UNCOMMANDED. GROUND RAN AIRCRAFT AND PERFORMED AUTOFEATHER AND STATIC TEST WITH NO DEFECTS NOTED. PERFORMED POWER RUN AND CONFIRMED Jan 25, 2004 · N343EN · Dhav DHC8311SDR CA040205008Engine · flamed out(CAN) WHILE TAXIING AND TURNING ONTO THE RUNWAY, THE LT ENGINE POWER LEVER WAS ADVANCED TO FACILITATE THE TURN. AS THE THRUST LEVER WAS ADVANCED, THE LT ENGINE SUFFERED A ROLL BACK AND FLAME-OUT. THE AIRCRAFT WAS TAXIED CLEAR OF THE RUNWAY AND A FAULT ANALYSISJan 22, 2004 · Cessna 560XLSDR CA040120005Engine · flamed out(CAN) ON TAXI OUT LT ENGINE FLAMED OUT, WITH OIL ODOR IN THE CABIN. RETURNED TO GATE, AIRCRAFT CHANGED, ENGINE REPLACED IAW 71-00-02 CONF.Jan 20, 2004 · Boeing 76735HSDR 54140APlenum · crackedFOUND CRACKED AT DRAIN.Jan 19, 2004 · Jetair JETSTM4101SDR 54140Plenum · crackedFOUND CRACKED AT THE PRIMARY FUEL NOZZLE BOSS.Jan 19, 2004 · Lear 31SDR A6WA200440008Engine · vibrationNR 1 ENGINE INDICATES VIB YELLOW CAUTION ON TAKEOFF ROLL BELOW 60 KNOTS. ABORTED TAKEOFF, NO VIBRATION FELT. REVIEWED HISTORY, PERFORMED TWO SEPARATE ENGINE POWER RUNS, NO VIBRATION NOTED. FAN BLADE INSPECTED, NO DISCREPANCIES. TAKEOFF WAS PERFORMED IN SEVJan 17, 2004 · N422AW · Cndair CL6002B19SDR DL757040057Engine · making metalRT ENGINE IFSD FOR LOW OIL PSI. AFTER SHUTDOWN RT ENGINE OIL PSI FLUCTUATED 0-3 PSI. FOUND METAL ON CHIP DETECTORS. REPLACED ENGINE.Jan 17, 2004 · N631DL · Boeing 757232SDR ALG2004F00002Engine · failedENGINE START WAS NORMAL BROUGHT THE AIRCRAFT TO A 3 FT HOVER ALL ENGINE INDICATIONS NORMAL, AT THIS TIME THE PILOT HEARD A SLIGHT BANG FROM THE REAR OF THE AIRCRAFT FOLLOWED BY A LOUD GRINDING WHINE AND A HIGH FREQUENCY VIBRATION IN AIRFRAME. AC BEGAN A SLIGHJan 16, 2004 · N206SL · Bell 206L1SDR 002171Engine · malfunctionedON 01-16-2004, AT APPROX 1125 (UTC), FLT 4633, BGM-PIT, CREW HAD RETURNED TO GATE. THE LEFT ENGINE WOULD NOT LIGHT OFF. THERE WAS NO FUEL FLOW INDICATION ON THE LEFT ENGINE.Jan 16, 2004 · N146SD · Saab SF340ASDR GTIA040011Engine · flamed outRT ENG FLAMED-OUT, AIR RETURN AT 800 TO 1000 MLS RT ENG EPR DROPPED BELOW 1.2 EPR, ARTS FIRED BASES X-TERED TO LT GENERATORS ACCOMPLISHED QRH ITEMS PULLED CVR C/B. PERFORMED ENG HI-POWER TRIM CHECKRUN ENG OPS CK NORM. R & R NR 2 ENG FUEL CONT, OPS CK GOOD. Jan 15, 2004 · N812NK · Doug DC982SDR MALA040117Engine · failedLT ENG FAILED INFLIGHT. ONE STAGE 1 TURBINE BLADE SEPARATED FROM DISK BELOW BLADE PLATFORM, BLADE IMPALED IN STAGE 1 SHROUD. STAGE 1 ROTOR CONTINUED TO ROTATE, REMAINING 33 STAGE 1 TURBINE BLADES MACHINED OFF BY IMPALED BLADE. DEBRIS FROM 34 STAGE 1 TURBINEJan 14, 2004 · N420XJ · Saab 340BSDR 04014308Engine · malfunctionedDURING CRUISE OF FLT 7711 CREW REPORTED LOW ENGINE OIL PRESSURE AND SHUTDOWN THE LEFT ENGINE. FLIGHT SAFELY RETURNED TO FIELD AND PASSENGERS DEPLANED NORMALLY. THE ENGINE AND ENGINE HYDRAULIC PUMP WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORJan 14, 2004 · N308UE · Jetair JETSTM4101
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