Pratt & Whitney JT3D-7

Service difficulty reports · 265

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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 engine_model_key = 'JT3D7'
  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 ABXA000518Bleed Valve · malfunctionedAT CRUISE, FL 330 ENGINE A/I ON NR 3 ENGINE STARTED TO COMPRESSURE STALL. TURNED IGNITION ON, ENGINE STOPPED STALLING. AFTER FIVE MINUTES, CREW TURNED IGNITION OFF. THE ENGINE STARTED STALLING AGAIN. THE CREW SECURED THE NUMBER THREE ENGINE. CREW REPORTED THATDec 1, 2000 · N813AX · Doug DC863 · Compressor Bleed ValveSDR ABXA000468Engine · failedRIGHT ENGINE FAILED ON CLIMBOUT. NO FIRE INDICATION. RETURNED TO ICT. REPLACED RIGHT ENGINE.Oct 10, 2000 · N981AX · Doug DC932 · Engine (Turbine/Turboprop)SDR ABXA000430Engine · seizedNR 1 ENGINE SEIZED ON CLIMBOUT. NOTED EGT 800 DEGREES C, OIL QTY ZERO. REPLACED NR 1 ENGINE IAW JOB CARD 8090507.Sep 22, 2000 · N801AX · Doug DC862 · Engine (Turbine/Turboprop)SDR ARAWA000901Fuel Control · malfunctionedON APPROACH TO SKCL, NR 4 ENGINE FAILED. PERFORMED EMERGENCY PROCEDURES AS PER FINE AIR PROCEDURES. LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL IAW MM 73-22-00. REMOVED AND REPLACED NR 4 ENGINE DRIVEN FUEL PUMP IAW MM 73-01-01. Sep 16, 2000 · N426FB · Doug DC8F54 · Fuel Control/Reciprocating EnginesSDR RRXA001051Engine · malfunctionedAT FL 290 NR 4 ENG COMPRESSOR STALLED. INSURED ENG HAD POSITIVE FUEL FLOW AND IGNITION. EGT STARTED TO RISE TOWARD CAUTION ZONE, THEN ENGINE WAS SHUT DOWN. EGT CONTINUED TO RISE TO ABOVE RED LINE BEFORE COOLING. MAX EGT WAS 600 DEG FOR A SEC OR SO. REMOVEAug 22, 2000 · N950R · Doug DC863 · Engine (Turbine/Turboprop)SDR ABXA00373Pressure Switch · malfunctionedAFTER LEVEL-OFF AT FL 350, NR 4 ENGINE OIL PRESSURE LIGHT STARTED FLICKERING WITH SHORT PERIODS OF BEING ON STEADY. RETARDED NR 4 THROTTLE AND LOW PRESSURE LIGHT REMAINED ONSTEADY. SHUT NR 4 ENGINE DOWN. REPLACED OIL DIFFERENTIAL PRESSURE SWITCH. OPS CHECKAug 9, 2000 · N826AX · Doug DC863 · Engine Oil PressureSDR RRXA000235Engine · malfunctionedON TAKEOFF AT KBRO (TEMP 23C, FIELD ELE 23 FT, ANTI-ICE OFF, MAX PWR, 1.87 EPR) NR 1 ENG EGT EXCEEDED 600 CELSIUS (APPROX 610 CELSIUS FOR 5 SECONDS) AFTER LIFT OFF. POWER HAD TO BE REDUCED TO 1.70 EPR TO MAINTAIN EGT WITHIN LIMITS. SHUT ENG DOWN AS PER GOM Apr 15, 2000 · N797AL · Doug DC863 · Engine (Turbine/Turboprop)SDR ARWA000401Engine · malfunctionedMIA - FLT 517 - NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY DROPPED TO .5 GALLON. A PRECAUTIONARY ENGINE SHUTDOWN WAS PERFORMED. OIL PRESSURE WAS DECREASING AND OIL TEMP WAS INCREASING. MAX TEMP WAS 125 CELSIUS AND LOWEST OIL PRESSURE WAS 37Apr 6, 2000 · N1804 · Doug DC862 · Turbine Engine Oil SystemSDR RRXA000182Engine · leakingDURING CLIMBOUT, NOTED NR 1 ENGINE LOW OIL PRESS LIGHT ILLUMINATED. NR 1 OIL PRESS 20 PSI AND DROPPING, OIL TEMP DECREASING, NR 1 OIL QUANTITY 1.5 GAL AND DECREASING EVEN AFTER ENGINE WAS SHUTDOWN. PERFORMED INFLIGHT ENGINE SHUTDOWN AND QRH PROCEDURES INITIAFeb 2, 2000 · N997CF · Doug DC862F · Engine (Turbine/Turboprop)SDR ABXA000007Fcu · malfunctionedNR 4 ENGINE SLOW ON ACCELERATION TO TAKEOFF POWER. ABORTED TAKEOFF. REPLACED NR 4 ENGINE FUEL CONTROL UNIT IAW DC8 MM 73-20-1. LEAK AND OPS CHECK GOOD.Jan 13, 2000 · N817AX · Doug DC863 · Fuel Control/Turbine EnginesSDR ABXA9900805Connector · contaminatedWHEN THROTTLE WAS RETARDED FOR DESCENT, NR 1 LOW OIL PRESSURE LIGHT CAME ON. THROTTLE WAS PULLED BACK TO IDLE, LOW OIL PRESSURE LIGHT STAYED ON. OIL PRESSURE WAS 41 PSI, TEMP 75 DEGREES AND QUANTITY WAS 4.2 GALLONS. SHUT ENGINE DOWN IAW ABNORMAL PROCEDURES.Nov 22, 1999 · N828AX · Doug DC863 · Engine Oil PressureSDR ABXA9900717Fuel Control · malfunctionNR 2 ENGINE FLAMED-OUT AT FL330, FUEL PRESSURE WENT TO ZERO. OIL PRESSURE LIGHT ILLUMINATED. SECURED ENGINE. OIL QUANTITY WAS 3.2 GALLONS. OIL PRESSURE WAS 25 PSI. ENGINE MOTORED FOR APPROXIMATELY 2 HOURS AND 40 MINUTES. REPLACED NR 2 FUEL CONTROL IAW DCSep 15, 1999 · N817AX · Doug DC863 · Fuel Control/Turbine EnginesSDR ABXA9900642Connector · unsecuredNR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO ILLUMINATION OF OIL PRESSURE LIGHT, OIL TEMPERATURE ERRATIC, THEN OFF SCALE HIGH AND NR 2 GENERATOR FAIL LIGHT ILLUMINATION. AFTER ENGINE SECURED, OIL PRESSURE REMAINED AT 20 PSI. FOUND CANNON PLUG AT NR 2 ENGINE PYLON Aug 12, 1999 · N824AX · Doug DC863 · Engine Oil PressureSDR ABXA9900635Engine · defectiveDURING CRUISE, NR 4 OIL QUANTITY DROPPED TO ZERO, OIL PRESSURE FLUCTUATED 20-45 PSI. ENGINE WAS SHUT DOWN. AFTER SHUTDOWN, OIL PRESSURE MAINTAINED 0-5 PSI. ENGINE WINDMILLED FOR 48 MINUTES. REPLACED NR 4 ENGINE IAW ABX WORK CARD 8090501, DC8 A AND B.Aug 6, 1999 · N815AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA9900606Engine · defectiveNR 1 ENGINE LOST OIL PRESSURE AFTER DEPARTURE. NO OIL QUANTITY, HIGH OIL TEMP, PRESSURE 20 PSI. SECURED NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE.Jul 26, 1999 · N816AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA990602Engine · failedSJU - FLT 601 - CLIMBING-OUT THROUGH 16000 FT AT 1302Z, NR 4 ENGINE LOUD BANG ALL PARAMETERS ERRATIC. COMPLETED APPROPRIATE CHECK LISTS. DUMPED FUEL TO MAX LANDING WEIGHT. RETURNED TO TJSJ WITHOUT INCIDENT. CUASE OF FAILURE CONTINUES. REMOVAL AND REPLACEMEJun 22, 1999 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)SDR IXXA9900007Turbine · failedEN ROUTE FROM PKWA TO PHIK DURING CLIMB, A LOUD NOISE WAS HEARD FROM THE NUMBER TWO ENGINE, ACCOMPANIED BY INCREASING ENGINE GAS TEMPERATURE AND A DECLINE IN OIL PRESSURE. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND CONTINUED TO PHIK FApr 20, 1999 · N728PL · Doug DC862 · Turbine SectionSDR ABXA9900303Switch · defectiveDURING DESCENT INTO ONT, WITH POWER REDUCED TO IDLE, NR 1 ENG LOW OIL PRESS LIGHT ILLUMINATED. OIL PRESS IND 42 PSI. SHUT NR 1 ENGINE DOWN, OIL PRESS WAS 7 PSI DURING DESCENT AND APPROACH FOR 8 MINUTES. INSPECTED MAIN OIL FILTER, NO CONTAMINATION FOUND. CHApr 19, 1999 · N828AX · Doug DC863F · Engine Oil PressureSDR RRXA99190Compressor · stalledAT ROTATION EXPERIENCED COMPRESSOR STALLS NR 4 ENG. RETARTED ENGINE, 30 SECONDS LATER ENGINE FAILED. NO FIRE, PERFORMED EMERGENCY FIRE AND DAMAGE SHUT DOWN. REMOVED AND REPLACED NR 4 ENG IAW EWA MEL 77. OPS CKS LEAK, CKS GOOD.Mar 29, 1999 · N964R · Doug DC863 · Turbine Engine Compressor SectionSDR ABXA9900228Switch · defectiveNR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED DURING CRUISE. OIL PRESSURE GAUGE READ 50 PSI. REDUCED POWER, NO HELP. SECURED ENGINE IAW DC8, OPS MANUAL. REPLACED NR 1 ENGINE OIL LOW PRESSURE SWITCH AND MAIN ENGINE OIL FILTER. LEAK AND OPS CHECKED GOOD.Mar 18, 1999 · N817AX · Doug DC863 · Engine Oil PressureSDR ABXA9900188Engine · failedON APPROACH TO ILN, NR 1 ENGINE OIL PRESSURE DROPPED TO 28 PSI. SECURED NR 1 ENGINE. FOUND OIL FILTER CONTAMINATED WITH METAL. REPLACED NR 1 ENGINE.Mar 10, 1999 · N812AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA9900140Compressor · stalledNR 4 ENGINE COMPRESSOR STALLED WHEN REDUCING POWER FROM CLIMB TO CRUISE. ENGINE OIL QUANTITY DROPPED RAPIDLY FROM 3.1 TO 1.6 GALLONS. SHUT ENGINE DOWN. REPLACED NR 4 ENGINE IAW ABX JOB CARD J-8090507. OPS AND LEAK CHECKED GOOD.Feb 24, 1999 · N819AX · Doug DC863F · Turbine Engine Compressor SectionSDR ARWA981219Gear Box · leakingMIA - FLT 941 - DURING CLIMB, FL 210, NR 4 ENGINE OIL PRESSURE DROPPED TO 35 PSI, PULLED POWER LEVEL BACK TO A LOWER POWER SETTING AND PRESSURE DROPPED TO 30 PSI OIL PRESSURE, LIGHT ILLUMINATED PULLED POWER LEVEL BACK TO IDLE, PRESSURE DROPPED DOWN TO 20 PSI ODec 23, 1998 · N8968U · Doug DC862 · Turbine Engine Reduction GearSDR ARWA981214Fcu · malfunctionedKDEN - FLT 2801 - NR 3 ENGINE HUNG START, FAILS TO ACCELERATE PAST IDLE RPM, ANTI-ICE ON OR OFF. REMOVED AND REPLACED NR 3 ENGINE FUEL CONTROL UNIT PER MM 73-20-00. PERFORMED ENGINE RUN UP IAW ARROW AIR DC-8 MM JC 6527. ALL PARAMETERS NORMAL.Dec 22, 1998 · N661AV · Doug DC863F · Fuel Control/Turbine EnginesSDR ARWA981209Line · looseCOMPRESSOR STALL NR 3 ENGINE, ABORTED TAKEOFF AT 90 KTS. FOUND LOOSE SENSE LINE AT SURGE BLEED VALVE. SECURED LINE AND OPS CHECKED NO LEAKS IAW MM 75-30-00.Dec 18, 1998 · N661AV · Doug DC863F · Compressor Bleed ControlSDR ARWA981207Bleed Valve · malfunctionedAFTER ROTATION WITH ANTI-ICE ON, NR 4 ENGINE HAD A COMPRESSOR STALL. ALL PARAMETERS FOR REMAINDER OF FLIGHT NORMAL. REMOVED AND REPLACED NR 4 ENGINE SURGE BLEED VALVE, RT AND LT, IGV ANTI-ICE VALVE, GROUND OPERATION CHECK NORMAL IAW M/M 75-20-3, 75-10-5 AND Dec 11, 1998 · N661AV · Doug DC863F · Compressor Bleed ValveSDR ARWA981208Igv · inopNR 2 ENGINE WITH CLIMB POWER SET, WHEN TURNING OFF ENGINE ANTI-ICE OFF HAD A COMPRESSOR STALL. ALL PARAMETERS FOR REMAINDER OF FLIGHT NORMAL. REMOVED AND REPLACED BOTH IGV/ AIR PRESSURE REGULATOR (ANTI-ICE), GROUND OPERATION CHECKED NORMAL IAW M/M 75-10-2 ANDec 11, 1998 · N661AV · Doug DC863F · Turbine Engine Compressor SectionSDR ARWA981129Engine · failedSHUT DOWN NR 4 ENGINE AT 21:48 DUE TO LOSS OF OIL QUANTITY. WINDMILLING OIL PRESS, 2 TO 5 PSI. INSPECTED MAIN OIL FILTER AND FOUND CONTAMINATED. PREPARED ENGINE FOR FERRY FLIGHT IAW GMM PAGE 6-3-1 TO 6-3-5, TO MIAMI FOR ENGINE CHANGE.Nov 23, 1998 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA980911Fitting · looseTUS - SHUTDOWN NR 4 ENGINE S/N 671443 AT 1345Z DUE TO STEADY OIL PRESS LIGHT AND INDICATED PRESS LESS THAN 35 PSI. WINDMILLING PRESS AT 18 PSI. TIGHTENED LOOS SWIVEL FITTING AT NR 6 BEARING INLET. ENGINE RUN UP. NO LEAKS NOTED. (M)Sep 22, 1998 · N802BN · Doug DC862 · Turbine Engine Oil SystemSDR TC8A98059Prbc Line · looseNR 2 ENGINE WOULD NOT ACCELERATE. CONTINUOUS COMPRESSOR STALL WHEN THROTTLE WAS PUSHED PAST IDLE. CHECKED PRBC SENSE LINES AND FOUND 1 LOOSE. SECURED LOOSE SENSE LINES IAW M/M 75-30-2. CREW RAN UP ENGINE AND OPS CHECK OF THE PRBC VALVE GOOD.Sep 20, 1998 · N183SK · Doug DC862F · Compressor Bleed ControlSDR ARWA980909Fan Blades · bentON PREFLIGHT FOUND BENT FAN BLADES NR 4 ENGINE. BLENDED 5 BLADES PER JT3D M/M (P/W) 72-00-00 BORESCOPE C/W, NO DEFECTS NOTED AT THIS TIME IAW M/M 72-00-00.Sep 17, 1998 · N1808E · Doug DC862 · Turbine Engine Compressor SectionSDR TC8A98055Engine · surgedDURING T/O ROLL 90 KNTS, NR 4 ENGINE SURGED, FOLLOWED BY EXTREMELY HIGH EGT 700 DEGREES. ABORTED TAKEOFF AND SHUTDOWN NR 4 ENGINE.Sep 1, 1998 · N183SK · Doug DC862F · Engine (Turbine/Turboprop)SDR ARWA9807133Gear Box · leakingBLD - FLT 505 - AFTER TAKEOFF OF BDL CREW PHONE LOST OIL QTY NR 2 ENGINE SHUT DOWN A/C DIVERTED TO MIAMI. AFTER LANDING, NR 2 ENGINE WAS OIL SERVICE, MOTORIZED. FOUND GEAR BOX LEAKING. ENGINE WILL BE REPLACED. (M)Jul 30, 1998 · N345JW · Doug DC863 · Turbine Engine Reduction GearSDR CKSA98493Fire Loop · out of adjustENGINE FIRE INDICATION NR 1, BOTTLE NR 1 DISCHARGED, HANDLE LIGHT REMAINED ILLUMINATED, BOTTLE NR 2 DISCHARGED, LIGHT REMAINED ILLUMINATED, ON POST FLIGHT, NO VISABLE INDICATION OF FIRE. REMOVED AND REPLACED NR 1 ENGINE FIRE LOOP AS PER MM 26-10-1 GROUND GOODJul 30, 1998 · N815CK · Doug DC863F · Fire DetectionSDR ABXA9800638Relief Valve · malfunctionNR 4 ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED ON DESCENT. OIL PRESSURE READ 30 PSI. THROTTLE WAS IN IDLE. SHUT DOWN NR 4 ENGINE. WINDMILLING OIL PRESSURE WAS 3 PSI. REPLACED OIL PRESSURE RELIEF VALVE IAW PRATT AND WHITNEY MM 72-00 AND ADJUSTED OIL PRESSJul 26, 1998 · N821AX · Doug DC863 · Engine Oil PressureSDR ABXA9800590Transmitter · cloggedDURING CRUISE, NR 3 ENGINE OIL PRESSURE WENT TO 100 PSI. SECURED NR 3 ENGINE. REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER AND OIL FILTER IAW DC8 MM 79-30-00.Jun 30, 1998 · N813AX · Doug DC863 · Engine Oil PressureSDR ARWA980602Fuel Contl Unit · failedAIR TURNBACK, AFTER DEPARTURE NR 3 ENGINE UNSPOOLED AND WHEN POWER LEVER WAS ADVANCED ENGINE WOULD NOT ACCELERATE. RETURNED TO TUS WITHOUT INCIDENT. INSPECTED ENGINE INLET, TAILPIPE, OIL AND FUEL FILTERS. NO DEFECTS NOTED. REMOVED AND REPLACED FCU, MAIN OIJun 6, 1998 · N1804 · Doug DC862 · Fuel Control/Turbine EnginesSDR TC8A98025Anti-Ice Duct · brokenFIRE WARNING NR 2 ON CLIMBOUT. REMOVED AND REPLACED BROKEN ANTI-ICE DUCT IAW MM 75-10-3 AND REPAIRED CRACK ON DIFFUSER IAW MM 72-00.May 14, 1998 · N183SK · Doug DC862F · Airfoil Anti/De-ice SystemSDR ABXA9800452Transmitter · defectiveIN CLIMB WITH MCT SET, NR 1 ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 37 PSI WITH FLUCTUATION OF PLUS AND MINUS, MINUS 7 PSI. WHEN THROTTLE MOVED TO IDLE, OIL PRESSURE DROPPED TO 33 PSI. ENGINE SHUT DOWN. ENGINE WINDMILLED FOR APPROX 3.4 HRS WITH OIL PREMay 13, 1998 · N824AX · Doug DC863 · Engine Oil PressureSDR TC8A98024Fire Loop · inoperativeTRIP NR 01807, FIRE WARNING NR 2 ENGINE ON CLIMB. NR 2 ENGINE FIRE DETECTION SYSTEM CHECKED IAW M/M 26-00. FOUND UPPER FIRE LOOP INOP. UPPER FIRE LOOP REPLACED AND TESTED IAW 26-10-1, FOUND IN NORMAL CONDITION.May 13, 1998 · N183SK · Doug DC862F · Fire DetectionSDR ABXA9800432Loop · defectiveFIRE WARNING ON NR 4 ENGINE. SECURED ENGINE AND DISCHARGED FIRE BOTTLE. MASTER FIRE WARNING CAME ON MOMENTARILY WITH NO LIGHT IN ANY LEVER OR ON FLIGHT ENGINEER PANEL. TESTED EACH ENGINE FIRE WARNING SYSTEM, NR 4 ENGINE WOULD NOT TEST. MASTER WARNING FLASHEApr 28, 1998 · N812AX · Doug DC862 · Fire DetectionSDR CKSA98202Fire Warning · illuminatedTEN MINUTES AFTER TAKEOFF, NR 2 ENGINE FIRE WARNING ILLUMINATED, SHUTDOWN ENGINE ACCOMPLISHED CHECKLIST. BOTH BOTTLES EXTINGUISHED. PERFORMED NR 2 ENGINE INSPECTION, NO DEFECTS NOTED AND RAN ENGINE FOR 30 MINUTES, 5 AT MAX POWER. OPS CHECK NORMAL IAW MM 72-Mar 21, 1998 · N781AL · Doug DC863 · Fire DetectionSDR ABXA9800110Fire Loop · defectiveNR 4 ENGINE FIRE WARNING BELL SOUNDED INTERMITTENTLY. ALL FOUR ENGINES WERE TESTED. NR 4 WOULD NOT TEST. NR 4 ENGINE WAS SECURED. CSD WAS DISCONNECTED AND NR 4 FIRE BOTTLE WAS DISCHARGED. NR 4 ENGINE FIRE LOOP ELEMENT WAS FOUND TO BE DEFECTIVE. REPLACED Feb 17, 1998 · N812AX · Doug DC863F · Fire DetectionSDR RRXA98014Compressor · stalledNR 1 ENGINE COMPRESSOR STALLS, SHUTDOWN IN-FLIGHT PER EWA PROCEEDURES. COMPLIED WITH FORM SP003, FOUND 2 BENT BLADES, BLENDED BLADES. FOUND TO BE WITH IN LIMITS PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-0. NR 1 ENGINE OPS CKS GOOD AT ALL POWER SETTINGS.Feb 6, 1998 · N998CF · Doug DC862F · Turbine Engine Compressor SectionSDR TC8A98008Engine · stalledBEFORE T/O, PUSHING THE THROTTLES FOR STATIC T/O, NR 1 ENGINE STALLED. TAXIED BACK TO THE RAMP. FOUND TWO SMALL PIECES OF BUSHES IN THE INTAKE. REMOVED, CLEANED, VISUALLY INSPECTED AND RAN UP THE ENGINE AT T/O POWER, FOUND OK.Feb 6, 1998 · N183SK · Doug DC862F · Engine (Turbine/Turboprop)SDR ARWA980201Engine · failedCHECK NR 2 ENGINE FOR VIBRATIONS NR 2 THROTTLE AND START LEVEL HARD IN CRUISE. ACCOMPLISHED R/B 8269 REMOVED AND REPLACED NR 2 ENGINE IAW ARROW AIR J/C 6519 AND J/C 6528, OPERATIONS AND LEAK CHECKED NORMAL ON RUN UP, IAW J/C 6527.Feb 2, 1998 · N1804 · Doug DC862 · Engine (Turbine/Turboprop)SDR CKSA97585Engine · flamed outNR 1 ENGINE FLAMED OUT FL330 IN CRUISE. RESTARTED AFTER PERFORMING ENGINE FAILURE CHECK LIST. BOOST PUMP ON - 2800 LBS NR 1 MAIN TANK. CHECKED NR 1 TANK FOR OBSTRUCTIONS, NO DEFECTS NOTED. CHECKED RIGGING OF NR 1 ENGINE FUEL SHUTOFF VALVE IAW DC8 MM 28-22-Dec 6, 1997 · N781AL · Doug DC863 · Engine (Turbine/Turboprop)SDR CKSA97572Engine · flamed outAT 4,000 FT NR 4 ENG FLAMEOUT SUCCESSFULLY RESTARTED. ON GROUND DURING TAXI IN ENG WOULD NOT ACCELERATE NORMALLY. FUEL TEMP WAS READING 34 DEGREES. SUSPECT FUEL ICING, ENGINE IDLES AT 55 PERCNET N2. REPLACED NR 4 ENG FUEL PUMP IAW 73-10-2 LEAK CHECKS GOOD Nov 18, 1997 · N815CK · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA971003Engine · failedDURING CRUISE, NR 1 OIL PRESS LIGHT FLASHED INTERMITTENTLY, OIL PRESS OSCILATED BETWEEN 25-48 PSI, OIL TEMP ROSE TO 125 C, OIL QUANTITY INDICATED 2 GALS, N1 N2 READ NORMAL. PERFORMED PRECAUTION BY SHUT DOWN AS PER ABNORMAL IN FLIGHT ENG SHUT DOWN. REMOVED ANOct 11, 1997 · N441J · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA9701454Oil Press Vlv · defectiveDURING DESCENT, NR 4 ENGINE OIL PRESSURE DROPPED TO 32 PSI AND LOW OIL PRESSURE LIGHT CAME ON, QTY AND TEMP WERE OK. SECURED NR 4 ENGINE. REPLACED OIL PRESSURE RELIEF VALVE SEAT AND SPRINGS IAW DC8 MM CH 80. RAN ENGINE, OPS CHECK AND LEAK CHECKED GOOD IAW DSep 5, 1997 · N815AX · Doug DC863 · Engine Oil Pressure
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