Pratt & Whitney JT3D-3B

Service difficulty reports · 218

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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 = 'JT3D3B'
  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 IXXA20121001028OBattery · inoperativeF/A EMERGENCY FLASHLIGHTS FOUND INOPERATIVE. R & R THE RT EMERGENCY FLASHLIGHT AND BATTERIES IAW MM 16.02. OPS CHECK GOOD.Oct 1, 2012 · N71CX · Doug DC862F · Emergency EquipmentSDR IXXA20120907023OEngine · stalledDURING TAKEOFF ROLL, CREW EXPERIENCED A COMPRESSOR STALL ON THE NR 3 ENGINE. TAKEOFF WAS REJECTED AT 85 KIAS AND 1.96 EPR. RETURNED BACK TO GATE. MX PERSONNEL PERFORMED A VISUAL INSPECTION OF NR 3 ENGINE, NO DEFECTS OBSERVED. ACCOMPLISHED ENGINE RUN UP TO Sep 7, 2012 · N71CX · Doug DC862F · Engine (Turbine/Turboprop)SDR IXXA10SMN068SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING UPPER SKIN CORRODED AT STA XRS 38.000 -112.000. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED NEW SKIN, REPAIR DOUBLEJun 18, 2010 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA100024OFan · odorAFTER 10 MINUTES OF RUNNING THE RT RECIRCULATION FAN , THE CREW SENSED AN ELECTRICAL/ OZONE SMELL. THE RT RECIRCULATION FAN WAS TURNED OFF, CIRCUIT BREAKER WAS PULLED AND SMELL WENT AWAY. MX REPLACED THE RT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1 ANMar 27, 2010 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA100001OBleed Valve · stuckDURING TAKEOFF ROLL AT APPROX 90 PERCENT N2 RPM THE ENG COMPRESSOR STALLED, EPR, N2 AND EGT ROLLED BACK. THE CREW ABORTED THE TAKEOFF AND RETURNED TO PARKING. MX INSPECTED THE ENG AND FOUND THE PRESSURE RATIO BLEED CONTROL VALVE, (PRBC) STICKING. PRBC WAS LUJan 14, 2010 · N71CX · Doug DC862F · Compressor Bleed ValveSDR IPXA09855748Engine · vibrationINSPECTION TYPE:N/A REPORTED SEVERE AIRCRAFT VIBRATION AND NR 2 ENGINE LOSING POWER. ENGINE SHUT DOWN AND CONTINUING ON TO ATL. R&R NR 2 ENG IAW TC 9071-1, 9071-2, 9071-3. OPS & LK CK. OK FOR SERVICEMay 5, 2009 · N803UP · Doug DC873F · Engine (Turbine/Turboprop)SDR PL92008F00000Turbine Blades · failedDURING CLIMBOUT FROM PHX NR 4 ENG EGT BEGAN TO CLIMB RAPIDLY AND NR 1 & NR 2 SPOOLED DOWN. ENG WAS SHUT DOWN FOLLOWING PUBLISHED PROCEDURES AND THE ACFT RETURNED TO PHX AND LANDED WTIHOUT INCIDENT. AFTER LANDING THE ENG WAS INSPECTED AND FOUND THAT THERE WERAug 16, 2008 · N88ZL · Boeing 707330B · Turbine SectionSDR UPS08852422Pump · malfunctionedINSPECTION TYPE:N/A AT FLT F/L 36.0 WITH BOOST OFF NR 2 ENGINE FLAMED OUT WHEN THROTTLE WAS MOVED TO IDLE. THIS WAS DURING A CONDITION FLT WITH A NEW PROCEDURE THAT THE FLT CREWS ARE FOLLOWING. A/C WAS NOT IN NORMAL FLT CONDITION WHEN THE FLAME OUT OCCURRED.Jun 3, 2008 · N894UP · Doug DC873F · Engine Fuel PumpSDR RRXA001532Frame · damagedDURING A MAINT VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT. FS 1340 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW SRM 51-1-8. PLUGGED HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED IAW EOJan 21, 2008 · N994CF · Doug DC862 · Fuselage Main, FrameSDR UPS06848715Engine · flamed outINSPECTION TYPE:N/A NR 3 ENGINE FLAMED OUT DURING CRUISE AT FL300. ALL INDICATIONS WERE NORMAL & THE ENGINE WAS RELIT AT FL250. NORMAL OPS REMAINDER OF FLT. PERFORMED T/S PER MM 71-00-00, FIG 139. NO DEFECTS NOTED AT THIS TIME.Nov 23, 2006 · N700UP · Doug DC871F · Engine (Turbine/Turboprop)SDR P5CA0501421Tire · blownAT TOP OF CLIMB, CREW REPORTED LOUD BANG FOLLOWED BY EICAS MESSAGE (GEAR DOOR) WITH AC VIBRATION AND AIR NOISE. ACCOMPLISHED MMC 14-7 CHECKLIST DOOR CLOSED, NO VIBRATION OR NOISE, SUSPECT BLOWN TIRE IN LT BODY GEAR WELL, AUTO BRAKE TEMP SENSOR NR 5 FAIL. SOFTDec 7, 2005 · N452PA · Boeing 74746NF · TireSDR ABXA050189Engine · failedLOW OIL PRESSURE LIGHT NR 2 ENGINE OIL PRESSURE DROPPED TO 30 PSI. SHUT DOWN NR 2 ENGINE DOWN AT 0350Z. ZERO OIL PRESSURE AFTER ENGINE SHUT DOWN. REMOVED AND REPLACED NR 2 ENGINE IAW JOB CARD 8090507 AND WORK PACK 600230688.Aug 17, 2005 · N813AX · Doug DC863 · Engine (Turbine/Turboprop)SDR ARWA20040907Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; DISCREPANCY: FORWARD LOWER CARGO COMPARTMENT STA 230 BETWEEN LONG. 36 AND LONG 35R, SKIN WITH CORROSION.Sep 28, 2004 · N906R · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA040210Engine · vibrationAT 2000 FEET AND LEVELING OFF, POWER ADVANCED TO MAINTAIN AIRSPEED, HAD SEVERE NR 3 ENGINE VIBRATION. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM IAD TO ILN. UPON ARRIVAL AT ILN, THE NR 3 ENGINE WAS REPLACED.Jun 17, 2004 · N847AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA030394Transmitter · defectiveNR 4 ENGINE OIL PRESSURE INDICATED + 100 PSI AT TOP OF CLIMB. SECURED ENGINE AT 0325Z, RETURNED TO 22 PSI AT 0345. REPLACED NR 4 OIL PRESSURE TRANSMITTER, NR 4 OIL PRESSURE RELIEF VALVE AND MAIN ENGINE OIL FILTER. RAN NR 4 ENGINE, OIL PRESSURE AT IDLE 41 PSOct 23, 2003 · N825AX · Doug DC863 · Engine Oil PressureSDR ABXA030330Element · missingENROUTE , NR 3 ENGINE FIRE WARNING CAME ON. ONLY OTHER INDICATION WAS HIGH OIL TEMP. CREW ELECTED TO USE RT WING OB ENGINE FIRE BOTTLE. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE NR 3 ENGINE. NO EVIDENCE OF FIRE OR FIRE DAMAGE FOUND. DURING INSPECTION, Aug 18, 2003 · N847AX · Doug DC861 · Fire DetectionSDR IXXA0300050OEngine · leakingDURING FLIGHT FROM GOOY TO EDDS NR 4 ENGINE HAD A LOW OIL PRESSURE, LOW OIL QUANTITY AND HIGH TEMPERTURE WARNING. THE ENGINE WAS SHUT DOWN AND THE CREW RETURNED AIRCRAFT TO GOOY. MAINTENANCE INSPECTION IS ON GOING. AS MORE INFORMATION BECOMES AVAILABLE IT WJul 25, 2003 · N799AL · Doug DC862 · Engine (Turbine/Turboprop)SDR UPS03840898Fitting · crackedINSPECTION TYPE: C3, AFT PIT BETWEEN STA 1260 AND STA 1280 STR 31L CRACKED REMOVED CRACKED LONGERON SPLICE IAW SRM 51-1-20D. REC'D, LOCATED AND DRILLED NEW SPLICE IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 5 1-1-20DJun 2, 2003 · N851UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03840900Doubler · crackedINSPECTION TYPE: C3, L2 DOOR UPPER FWD CORNER SHOWS CRACK INDICATION WITH XRAY INSPECTION. REMOVED CRACKED INTERNAL SKIN DOUBLER AND PARTIALLY REMOVED WEB TO FOM. FAB NEW INTERNAL SKIN SPLICE DOULBER IAW DWG NR 4751734 AND PRIMED IAW DC8 SMR 51-1-8, THEN IJun 2, 2003 · N851UP · Doug DC873F · Passenger/Crew DoorsSDR UPS03840901Longeron · crackedINSPECTION TYPE: C3, AFT PIT BETWEEN STA 1260 AND STA 1280 STR 36 CRACKED REMOVED CRACKED LONG 36 FS 1270-1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 36 FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0.Jun 2, 2003 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR ABXA030146Pressure Switch · defectiveAT FL 330, RAT -15, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED WITH 51 PSI AND OIL TEMP. OF 110 DEG. DURING IDLE, TEMP WAS 115 DEGREES, RPESSURE OF 48 PSI. OIL PRESSURE LIGHT FLICKERED AT IDLE. PERFORMED ENGINE SECURING PROCEDURE. NR 3 ENGINE N2 40 PERCENT ANDMay 19, 2003 · N819AX · Doug DC863F · Engine Oil PressureSDR ARWA20021002Engine · failedDURING CRUISE AT 280, NR 1 ENGINE ANTI-ICE LIGHT ON. NR 2 ERATIC FOLLOWED BY COMPRESSOR STALL. COULD NOT GET POWER OUT OF ENGINE. AT FL 280 UNABLE TO CLOSE 2N ANTI-ICE VALVE NO NR 1 ENGINE STARTED BACKFIRING AND REDUCED POWER TO PREVENT IT UNTIL POWER COMPLEOct 7, 2002 · N30UA · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA020225Pressure Switch · faultyNR 4 LOW OIL PRESSURE LIGHT CAME ON. THROTTLED BACK BUT LIGHT STAYED ON. SECURED THE NR 4 ENGINE. ALSO THE NR 3 LOW OIL PRESSURE LIGHT CAME ON. THROTTLED BACK AND LIGHT WENT OUT, BUT ILLUMINATED INTERMITTENTLY. AIRCRAFT DIVERTED TO LOUISVILLE. REPLACED TOct 1, 2002 · N814AX · Doug DC863F · Engine Oil PressureSDR ABXA020081Indicator · defectiveNR 1 ENGINE OIL TEMP WENT TO 150 DEG CELSIUS FOR APPROXIMATELY 20 MINUTES. SECURED THE NR 1 ENGINE. ALL OTHER INDICATIONS WERE NORMAL. REPLACED THE NR 1 ENGINE OIL TEMP BULB IAW DC-8 AMM 79-34-01-2 AND THE NR 1 ENGINE OIL TEMP GAUGE IAW DC-8 AMM 31-00-00-2.Aug 19, 2002 · N847AX · Doug DC861 · Engine Oil TemperatureSDR ABXA020002Switch · defective# 1 engine low oil pressure light on in flight. Oil pressure was 46 psi. Engine was shut down at 0905 Z. Windmilling oil pressure on secured engine was 12 psi for 19 minutes. Replaced low pressure switch IAW DC-8 MM 79-30. Ran # 1 engine, no leaks noted. EngiJun 24, 2002 · N849AX · Doug DC861 · Engine Oil PressureSDR ARWA20020603Bleed Valve · seizedENGINE NR 4 UNABLE TO SPOOL TO MAX POWER DURING TAKEOFF. REMOVED AND REPLACED ENGINE BLEED VALVE IAW MM 75-30-3; OPERATIONS CHECKED NORMAL IAW MM 71-00.Jun 19, 2002 · N29UA · Doug DC861 · Compressor Bleed ValveSDR ARWA20020313Oil System · fluctuatesAT 1140Z NR 2 ENGINE SHUTDOWN DUE FLUCTUATING OIL PRESSURE GAUGE AND LIGHT AND OIL QTY READING ZERO, NOTE OIL TEMP READING NORMAL 75 DEG. REMOVED AND REPLACED ENGINE. FUNCTIONAL TEST COMPLETED AND FOUND SATISFACTORY. ACFT RETURNED TO SERVICE. ENGINE (S/N 6Mar 27, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil SystemSDR ARWA20020315Clutch · failedNR 2 ENGINE SHUTDOWN DUE FLUCTUATING OIL PRESSURE GAUGE AND LIGHT AND OIL QTY READING ZERO, NOTE OIL TEMP READING NORMAL 75 DEG. REMOVED AND REPLACED ENGINE. FUNCTIONAL TEST COMPLETED AND FOUND SATISFACTORY. ACFT RETURNED TO SERVICE. ENGINE SENT TO REPAIR Mar 27, 2002 · N426FB · Doug DC85F54 · Alternator-Generator DriveSDR ARWA20020304Housing · damagedDURING CLIMBOUT THROUGH 16,000 FEET; NR 2 ENGINE OIL PRESSURE GAUGE BEGAN FLUCTUATING AT 180, AND NR 2 OIL PRESSURE LIGHT BEGAN FLICKERING, THEN WENT STEADY. ACCOMPLISHED APPROPRIATE ABNORMAL CHECKLISTS AND SHUTDOWN ENGINE AT 22:15 ENGINE OIL PRESSURE WINDMILMar 6, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil SystemSDR ARWA20020302Relief Valve · faultyDURING CLIMBOUT THROUGH 15,000 FT, NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING, NR 2 OIL PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED APPROPRIATE CHECK LISTS AND SHUT DOWN ENGINE AT 00:15Z, OIL WINDMILLED AT 12 PSI. AIRCRAFT RETURNED TO PTY AND LANDED UNEVENTFUL.Mar 5, 2002 · N426FB · Doug DC85F54 · Turbine Engine Oil SystemSDR ARWA20011215Line · leakingNR 3 ENGINE LOSS OF OIL QUANTITY OSCILLATING OIL PRESS AND OIL PRESS WARNING ON AND OFF. SHUT DOWN NR 3 ENGINE AS PER ABNORMAL CHECKLIST OIL PRESS 15 PSI, 1 HOUR WINDMILLING. AIRCRAFT RETURNED TO KMIA UNEVENTFUL. INSPECTED ENGINE AND FOUND ENGINE OIL COOLERDec 28, 2001 · N426FB · Doug DC85F54 · Engine Oil Distribution (Airframe Furnished)SDR ARWA20011124Blade · failedON TAKE OFF MIAMI A LOUD BANG FOLLOWED BY HIGH VIBRATION ON NR 2 ENGINE REJECTED THE TAKE OFF ROLL. FOUND C2 BLADE FAILURE. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK NORMAL.Dec 1, 2001 · N426FB · Doug DC85F54 · Turbine Engine Compressor SectionSDR ARWA0010717Filter · cloggedDURING FLIGHT AT LEVEL 31.0 NR 3 ENGINE FLAMED OUT, RESTARTED ENGINE FOLLOWING ABNORMAL CHECK LIST PROCEDURES. REMOVED AND REPLACED FUEL FILTERS OF NR 3 FUEL TEMPERATURE REGULATOR IAW MM 73-11-1, NO LEAKS NOTED. OPERATIONAL CHECK ON RUN UP IAW MM 71-00, FOUNJul 11, 2001 · N30UA · Doug DC861 · Engine Fuel DistributionSDR ABXA000363Wire · brokenDURING CLIMBOUT, NR 4 ENGINE OIL TEMPERATURE WENT TO 155 DEGREES. PERFORMED ABNORMAL CHECKLIST. TEMPERATURE DID NOT CHANGE. SHUT NR 4 ENGINE DOWN. OIL TEMPERATURE REMAINED AT 155 DEGREES FOR ENTIRE FLIGHT. FOUND GROUND WIRE E-355 BROKEN AT GROUND LUG 941.Aug 3, 2000 · N845AX · Doug DC861 · Engine Oil System WiringSDR IXXA0000026Compressor · damagedEN ROUTE FROM JON TO HIK, DURING CRUISE THE NUMBER TWO ENGINE EXPERINCED A COMPRESSOR STALL FOLLOWED BY PARTIAL POWER REDUCION. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANJul 11, 2000 · N799AL · Doug DC862 · Turbine Engine Compressor SectionSDR ABXA000296Relief Valve · failedWITH THROTTLE AT IDLE NR 3 ENG OIL PRESSURE LIGHT CAME ON WITH PRESSURE INDICATING 32 PSI. POWER BROUGHT BACK UP TO 80 PERCENT N2 OIL PRESSURE WENT TO 55 PSI. THEN DROPPED TO 50 PSI WITH NO CHANGE IN THROTTLE SETTING. THROTTLE BROUGHT BACK TO IDLE PRESSURE Jun 7, 2000 · N822AX · Doug DC863 · Turbine Engine Oil SystemSDR ABXA000295Relief Valve · malfunctionedBELOW 68 PERCENT N2, NR 3 ENGINE LOW OIL PRESSURE LIGHT CAME ON. WOULD NOT GO ABOVE 35 PSIUNTIL 68 PERCENT N2. ENGINE WAS SHUT DOWN AT 10,000 FT, HAD POSITIVE OIL PRESSURE THROUGHOUTAPPROACH AND LANDING. REPLACED NR 3 OIL STRAINER AND REBUILT NR 3 OIL PRESSJun 6, 2000 · N822AX · Doug DC863 · Engine Oil PressureSDR ABXA000184Engine · failedNR 3 ENGINE LOST OIL PRESSURE IN CRUISE. SHUT ENGINE DOWN. ENGINE WINDMILLED FOR APPROX 1 HOUR AND 13 MIN. DIVERTED TO DEN. FOUND LARGE AMOUNT OF OIL IN TAILPIPE AND ON TURBINE BLADES NR THREE ENGINE. FERRIED AIRCRAFT TO ILN AND REPLACED NR 3 ENGINE.Apr 4, 2000 · N824AX · Doug DC863 · Engine (Turbine/Turboprop)SDR RRXA000001Bullet · damagedNR 3 ENG COMP STALLED VIOLENTLY AND REPEATEDLY ON CLIMB-OUT. NR 1 ENG COMP STALLED REPEATEDLY ON CLIMB-OUT. INSP NR 3 EMG INLET AND EXH FOR DAMAGE. NONE NOTED ENG RUNUP. PERFORMED MANIFOLD DECAY, INTERSTAGE BLEED SCHEDULE, HIGH STAGE BLEED AND REG CHKS. IJan 12, 2000 · N990CF · Doug DC862 · Turbine Engine Compressor SectionSDR CA000118046Tube · worn(CAN) DURING FLIGHT CREW ACTIVATED GEARDOWN AND FLAPS DOWN FOR TEST, NOTHING MOVED, FE NOTICED HYD RESEVOIR WAS EMPTY, EMER DECLARED, LG MANUALLY LOWERED AND AUX PUMP USED FOR LANDING. HYD RETURN LINE ON NO 2 ENG UNDER LH WING SAIL BOAT FARING HAD A HOLE IN THDec 21, 1999 · Boeing 720023B · Hydraulic System, MainSDR ABXA9900776Engine · low powerDURING FUNCTIONAL CHECK FLIGHT (FCF), ON INITIAL LEVEL-OFF, WHEN POWER WAS REDUCED TO IDLE, NR 3 ENGINE N1 WAS LOWER THAN OTHER ENGINES. WHEN THROTTLES WERE ADVANCED, NR 3 ENGINE DID NOT ACCELERATE. LOW OIL PRESSURE LIGHT ILLUMINATED. INDICATED OIL PRESSURNov 9, 1999 · N801AX · Doug DC862 · Engine (Turbine/Turboprop)SDR ABXA9900754Generator · defectiveFAULT ON NR 4 GENERATOR. UNABLE TO RESET IAW ABNORMAL CHECKLIST. SECURED ENGINE, MAINTAINED POSITIVE ENGINE OIL PRESSURE. INSPECTED MAIN OIL FILTER, FOUND NO CONTAMINATION. CHECKED OIL QUANTITY, RAN ALL ENGINES, ENGINE RUN WAS NORMAL. CHECKED AIRCRAFT WIRIOct 28, 1999 · N808AX · Doug DC862 · AC Generator-AlternatorSDR 2000ZZZX472Fcu · inoperativeDURING SHORT FINAL, NR 3 ENGINE FLAMEOUT; FUEL ON NR 3 TANK WAS 5800; SUSPECT FCU MALFUNCTION. CHANGED AND TESTED FCU UNIT IAW PW MM 72-0. (X)Oct 21, 1999 · N7046H · Doug DC8F54 · Fuel Control/Turbine EnginesSDR CKSA99072Sequence Valve · failedON CLIMB HAD FIRE WARNING ON NR 3 ENGINE. PERFORMED FIRE SEVERE DAMAGE OR SEPARATION CHECKLIST. ENGINE SECURED AT 2324Z, HAD GOOD OIL PRESS (15 PSI) FUEL DUMP COMPLETED. FOUND NR 3 THRUST REVERSER SEQUENCE VALVE LEAKING HOT AIR ON FIRE SENSOR. REMOVED AND Aug 20, 1999 · N6161M · Doug DC8F55 · Engine Thrust ReverserSDR ABXA9900628Engine · defectiveDURING CLIMB, NR 4 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 35-50 PSI. OIL QUANTITY DROPPED TO .4 GALLONS. OIL TEMPERATURE WAS 125 DEGREES C. SHUT NR 4 ENGINE DOWN. AFTER SHUT DOWN, OIL PRESSURE FLUCTUATED BETWEEN 15-20 PSI. REPLACED NR 4 ENGINE IAW ABX WORAug 3, 1999 · N852AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA9900380Valve · malfunctionedNR 4 ENGINE WAS SHUT DOWN DUE TO OIL QUANTITY GOING TO 0 AND OIL PRESS FLUCTUATING. AT SHUTDOWN OIL PRESS WAS 15 PSI, THEN WENT TO 0. CLEANED AND INSPECTED NR 4 ENGINE OIL FILTER AND OIL SCAVENGE FILTER. NO METAL CONTAMINATION FOUND. REPLACED NR 4 ENGINE OMay 20, 1999 · N852AX · Doug DC861 · Engine Oil PressureSDR TC8A99015Fuel Control · malfunctionedTRIP NR 03295 LATI-EINN, NR 1 ENGINE FLAMEOUT AT 22:05 Z, ON DESCENT. ENGINE FLAMEOUT CHECKLIST COMPLETED, 35 PERCENT N2, OIL PRESSURE 20 PSI AND 25 PERCENT N1. PROCEEDED IN FLIGHT START JT3D CHECKLIST, NO RESPONSE. REMOVED AND REPLACED FUEL CONTROL IAW MM Apr 24, 1999 · N184SK · Doug DC861F · Fuel Control/Turbine EnginesSDR TC8A99013P & D Valve · failedNR 1 ENGINE FLAME-OUT AFTER ENGINE START. FUEL FLOW INDICATOR SHOWING FLUCTUATION OF 1,000 +/- 500 PSI. FUEL PRESSURE ENGINE DRIVEN PUMP. NORMAL RANGE - FUEL PRESSURE INDICATION FUEL PUMP TANK PRESSURE/FEED. REMOVED AND REPLACED P & D VALVE AND FUEL FILTERApr 17, 1999 · N184SK · Doug DC861F · Fuel Controlling SystemSDR TC8A99012Fire Loop · malfunctionedCLIMBOUT FROM KBRO, NR 3 ENGINE FIRE WARNING ON. COMPLETED CHECKLIST, SHUT DOWN NR 3 ENGINE. REMOVED AND REPLACED AFT PYLON FIRE LOOP, OPS CHECK GOOD ON GROUND RUN IAW DC8 MM 26-2-1.Apr 4, 1999 · N182SK · Doug DC8F55 · Fire DetectionSDR TC8A99010Duct · leakingON CLIMBOUT FROM KBRO, NR 3 ENGINE FIRE WARNING ON. COMPLETED CHECKLIST AND SHUTDOWN NR 3 ENGINE. REPAIRED AIR LEAK IN REVERSER AREA, OPS CHECK GOOD ON GROUND RUN IAW MM 78-00 AND 75-00.Apr 1, 1999 · N182SK · Doug DC8F55 · Pneumatic Distribution System
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