Pratt & Whitney JT3D-3B

Service difficulty reports · 218

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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 = '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 ARWA990307Oil Pump · failedMIA - NR 4 ENGINE OIL PRESSURE DROPPED TO 32 PSI. SHUTDOWN ENGINE AS PER ABNORMAL CHECKLIST. WINDMILL SPEEDS WERE N1, 13.5 PERCENT, N2 21 PERCENT, OIL PRESS 3 PSI. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE OIL PUMP ASSY Mar 25, 1999 · N1804 · Doug DC862 · Turbine Engine Oil SystemSDR TC8A99002Fire Warning · activatedAFTER T/O PASSING THROUGH 9,000 FEET, RECEIVED FIRE WARNING INDICATION ENGINE NR 3. ACCOMPLISHED ENGINE FIRE SEPARATION OR SERVERE DAMAGE CHECKLIST. AFTER FIRE SHUTOFF LEVER MOVED TO SELECT AGENT POSITION, FIRE INDICATIONS CEASED. COMPLETED FIRE WARNING SYSMar 4, 1999 · N182SK · Doug DC8F55 · Fire DetectionSDR ABXA9900139Engine · failedDURING CLIMB, NR 1 ENGINE CREATED LOUD BANG. N1 AND N2 RPM DROPPED BY ONE HALF, EGT WENT TO 640 DEGREES. ENGINE ANTI-ICE WAS ON. SHUT ENGINE DOWN. FIRE BOTTLES WERE NOT USED. REPLACED NR 1 ENGINE.Feb 25, 1999 · N853AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA9900021Oil Cooler · defectiveNR 3 ENGINE OIL TEMPERATURE WENT TO 150 DEGREES AFTER TAKEOFF. ENGINE WAS SHUTDOWN. REPLACED NR 3 OIL COOLER, TEMPERATURE BULB AND REGULATOR. OPS CHECKED GOOD.Jan 13, 1999 · N851AX · Doug DC861 · Engine Oil CoolerSDR ARWA990106Engine · leakingMIA - FLT 1628 - FL310, OIL QTY NR 1 ENGINE DROPPED TO .5 GALLON, OK OIL AND SUBSEQUENT ENGINE DAMAGE. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AS EPR ABNORMAL CHECKLIST. AFTER SHUTDOWN, N1 25 PERCENT, N2 40 PERCENT, OIL PRESS 21 PSI. REMOVED OIL SCREEN AND Jan 12, 1999 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)SDR CKSA99002Fuel Pump · failedDURING CRUISE FL 340, NR 1 ENG BEGAN TO LOSE PWR AS EVIDENCED BY DECREASING EPR AND RPM IND. APPLIED ENG AND SCOOP ANTI-ICE, EPR AND RPM'S CONTINUED TO DROP. AFTER 5 MIN RPM DROPPED TO APPROX 85 PERCENT N2. AS RPM DECREASED NR 1 FUEL PRESS IND DROPPED BELOWJan 1, 1999 · N813CK · Doug DC861F · Engine Fuel PumpSDR ARWA981221Fcu · failedPNX - FLT 515 - BLOCK TURNBACK, ON RIGHT RUNUP, NR 1 ENGINE DIDN'T ACCELERATE. ALL INDICATIONS REMAINED IN IDLE. INDICATION WITH SLIGHTLY FLUCTUATING EPR NEEDLE. FELT ENGINE VIBRATING AND HEARD 'KNOCKING' NOISE. IMMEDIATELY BROUGHT THROTTLE BACK TO IDLE ADec 29, 1998 · N1804 · Doug DC862 · Fuel Control/Turbine EnginesSDR TC8A98086Compressor · stalledON TAKEOFF RW 29, NR 4 ENGINE ERRONEOUS EPR INDICATION, ALL OTHER INDICATIONS NORMAL. COMPRESSOR STALL AT APPROX 60 KTS, ABORTED TAKEOFF. TAXIED TO RW 11, TAKEOFF NORMAL, SET NR 4 ENGINE POWER BY N1, WIND 110, 4 KTS. INSPECTED NR 4 ENGINE BLADES PER PW MM 72Dec 18, 1998 · N182SK · Doug DC8F55 · Turbine Engine Compressor SectionSDR TC8A98085Fuel Control · out of adjustNR 4 ENGINE WOULD NOT DEVELOPE TAKEOFF POWER, (1.87 EPR). REJECTED T/O AT 100 KTS. ADJUSTED NR 4 ENGINE FUEL CONTROL IAW DMM, CH 73-20-1. PERFORMED ENGINE RUN-UP TO T/O POWER, SYSTEM CHECKS GOOD DC8 ENGINE RUN UP MM IAW DMM 72-00.Dec 17, 1998 · N184SK · Doug DC861F · Fuel Control/Turbine EnginesSDR TC8A98084Compressor · stalledON TAKEOFF, COMPRESSOR STALL, ABORTED TAKEOFF. SUSPECT NR 4 ENGINE. CONDUCTED ENGINE RUN ON NR 4 ENGINE AND BLEED AIR CHECK WITH OPERATING FLIGHT CREW, OPS CHECK GOOD IAW MM 75-00. PERFORMED FOD CHECK OF INLET AND EXHAUST, OK. FLAG CHECK, NO FOD NOTED, FLANov 26, 1998 · N182SK · Doug DC8F55 · Turbine Engine Compressor SectionSDR ABXA9801061Transmitter · defectiveNR 3 OIL PRESSURE FLUCTUATED 35 TO 37 PSI AFTER IDLE POWER SET DURING DESCENT. PRESSURE STEADIED ABOUT 37 PSI ON LEVEL OFF AT LOW ALTITUDE. WHEN PRESSURE DROPPED TO 35 TO 34 PSI, PRECAUTIONARY SHUT DOWN WAS ACCOMPLISHED . REPLACED NR 3 ENGINE OIL FILTER AS Nov 17, 1998 · N843AX · Doug DC861 · Engine Oil PressureSDR TC8A98083Line · looseAT 90 KTS, NR 4 ENGINE COMPRESSOR STALLED, ABORTED TAKEOFF. FOUND LOOSE PNEUMATIC LINE AT INTERSTAGE BLEED VALVE. TIGHTENED LINE AND OPS CHECKED AT ALL POWER SETTINGS. FLAGGED BLEED VALVE SEVERAL TIMES, NO DEFECTS NOTED. ENGINE WAS RUN AT TAKEOFF POWER WITNov 16, 1998 · N182SK · Doug DC8F55 · Compressor Bleed ControlSDR TC8A98078Prbc · dirtyON T/O ROLL AT 110 KTS, NR 2 ENGINE COMPRESSOR STALLED, ABORTED TAKEOFF. CHECKED BRAKES PER GOM. CLEANED AND LUBED PRBC VALVE. PERFORMED FLAG CHECK IAW MM 75-30-3. PERFORMED VISUAL INSPECTION OF INTAKE EXHAUST, NO DEFECTS NOTED.Nov 7, 1998 · N181SK · Doug DC862 · Compressor Bleed ValveSDR TC8A98074Compressor · stalledTRIP# 02747. DISCREP: #2 ENGINE COMPRESSOR STALLED ON TAKEOFF ROLL. CORR ACTION: CLEANED AND LUBED PRBC VALVE, PERFORMED FLAG CHECK IAW 75-30-03. PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST, NO DEFECTS NOTED.Oct 30, 1998 · N181SK · Doug DC862 · Turbine Engine Compressor SectionSDR TC8A98075Prbc Valve · failedNR 2 ENGINE COMPRESSOR STALL ON T/O ROLL AT APPROX 60 KTS. REPLACED PRBC VALVE IAW MM 75-30-1 DUE TO FOUND STUCK. INSPECTED ENGINE, FOUND INTAKE/TAILPIPE CLEAN. BORESCOPED ENGINE IAW PW MM 72-00. RUN UP CHECK COMPLETED BY CREW. ENGINE OPERATION ALL NORMALOct 30, 1998 · N181SK · Doug DC862 · Compressor Bleed ValveSDR TC8A98076Blade · dentedCOMPRESSOR STALL NR 3 ENGINE DURING TAKEOFF ROLL, APPROXIMATELY 60 KNOTS, ANTI-ICE OFF. INSPECTED COMPRESSOR AND TURBINE IAW PW 72-0, PG 118, NO DEFECTS NOTED. INSPECTED INLET, FOUND 1 BLADE DENTED, BLENDED AND INSPECTED IAW PG 602/604.Oct 30, 1998 · N802CK · Doug DC8F54 · Turbine Engine Compressor SectionSDR TC8A98072Fire Loop · looseTRIP# 02716. DISCREP: ON CLIMB OUT, ENGINE FIRE #3 ENGINE. PERFORMED CHECK LIST AND RETURNED TO KDAY FOR LANDING. SECURED LOOSE FIRE WARNING LOOP IN BOMB BAY AREA, OPS CHECKS NORMAL IAW MM 26-2-0.Oct 23, 1998 · N182SK · Doug DC8F55 · Fire DetectionSDR TC8A98067Engine · failedDFW-DAY. TRIP# 02617 DISCREP: #1 ENGINE LOSS OF POWER ON CLIMBOUT 240-330. ENGINE SURGING FROM CLIMB EPR TO 1.6 THEN 1.3 SHUTDOWN, ALL PARAMETERS NORMAL. FERRIED AIRCRAFT TO KMIA. CORR. ACTION: 10/28/98 REMOVED AND REPLACED #1 Oct 7, 1998 · N184SK · Doug DC861F · Engine (Turbine/Turboprop)SDR CKSA98514Wire · failedON CLIMBOUT, NUMBER 1 ENGINE FIRE WARNING SOUNDED. DURING ENGINE SHUTDOWN THE LIGHT IN THE HANDLE EXTINGUISHED. ENGINE FIRE, SEPARATION, SEVERE DAMAGE CHECKLIST ACCOMPLISHED. AGENT WAS NOT DISCHARGED. OIL PRESSURE AT SHUTDOWN 5 PSI. AIRCRAFT FUEL DUMP ACCSep 10, 1998 · N6161C · Doug DC8F55 · Fire DetectionSDR TC8A98056Switch · failedON CLIMBOUT, NR 2 ENGINE LOW OIL PRESSURE LIGHT ON. CHECK LIST COMPLETED AND LIGHT STILL ON. SHUT DOWN NR 2 ENGINE PRECAUTIONARY. CREW DEBRIEF REVEALED NO OIL PRESSURE LOSS AND NO OIL QTY LOSS. DISCOVERED OIL DIFFERENTIAL PRESSURE SWITCH LEAKING. REMOVED Sep 4, 1998 · N181SK · Doug DC862 · Engine Oil PressureSDR CKSA98508Duct · looseON CLIMBOUT APPROXIMATELY 2,000 FT, NR 1 ENGINE FIRE WARNING CAME ON. DURING POWER LEVER REDUCTION LIGHT EXTINGUISHED. PERFORMED ENGINE FIRE CHECKLIST, SHUTDOWN NR 1 ENGINE, NO FIRE BOTTLES USED. NR 1 ENGINE FIRE LIGHT TESTED OK. OIL PRESSURE 15 PSI AFTER Aug 28, 1998 · N6161C · Doug DC8F55 · Pneumatic Distribution SystemSDR TC8A98053Bleed Valve · replacedMULTIPLE COMPRESSOR STALLS ON CLIMBOUT, 6,000 FT ON NR 1 ENG. REMOVED AND REPLACED NR 1 PRBC VALVE, OPS CHECKS OK IAW 75-30-3.Aug 22, 1998 · N802CK · Doug DC8F54 · Compressor Bleed ValveSDR ARWA980908Valve · inoperativeNR 3 ENGINE AT IDLE, OIL PRESS 35 PSI, SHUT DOWN ENG, OIL PRESS LIGHT CAME ON. REMOVED AND REPLACED NR 3 ENG OIL PRESS RELIEF VALVE, OPS CHECKED NORMAL IAW 79-32-0.Jul 27, 1998 · N8968U · Doug DC862 · Turbine Engine Oil SystemSDR TC8A98041Compressor · stalledLOUD, PRONOUNCED, SUSPECTED ENGINE COMPRESSOR STALL ON RT SIDE DURING TAKEOFF PASSING 70 KIAS, ABORT INITIATED. INSPECTED NR 3 AND NR 4 ENGINES FOR DAMAGE, NONE NOTED. LUBED SURGE BLEED VALVE ON NR 3 AND NR 4 ENGINES. RAN ENGINES IAW 71-00, NO COMPRESSOR STJul 15, 1998 · N802CK · Doug DC8F54 · Turbine Engine Compressor SectionSDR TC8A98040Compressor · stalledINITIATED ABORT PASSING 80 KNOTS BECAUSE OF SUSPECTED COMPRESSOR STALL OR BLOWN TIRE. RETURNED TO THE BLOCKS, LET BRAKES COOL, INSPECTED BRAKES AND TIRES IAW M/M 32-40-1. ALSO RAN UP ALL FOUR ENGINES IAW 71-00, COULD NOT DUPLICATE COMPRESSOR STALL, ENGINE RJul 10, 1998 · N802CK · Doug DC8F54 · Turbine Engine Compressor SectionSDR TC8A98038Engine · malfunctionedABORTED T/O AT IAH DUE TO HIGH EGT ON ENGINE NR 2, 1.85 EPR, EGT GOES 555 REDLINE AND CONTINUE TO CLIMB, SHUT DOWN ENGINE, TAXI BACK. ENGINE NR 2 EXCEEDS MAX EGT LIMITS. TO CLARIFY, NO LIMITS WERE EXCEEDED BUT APPEARED IT WOULD HAVE IF THROTTLE WAS NOT RETARJul 2, 1998 · N184SK · Doug DC861F · Engine (Turbine/Turboprop)SDR TC8A98036Oil Tank · looseON CLIMB-OUT AT APPROX 10000 FEET, NR 3 ENGINE FIRE WARNING BELL AND LIGHTS. PERFORMED ENGINE SHUTDOWN. FOUND MIDDLE STRAP ON ENGINE OIL TANK LOOSE AND IN CONTACT WITH LT FAN DOOR FIRE WARNING LOOP. SECURED CLAMP, PERFORMED ENGINE RUN-UP AND FIRE WARNING TEJun 25, 1998 · N802CK · Doug DC8F54 · Engine Oil Storage (Airframe Furnished)SDR ABXA9800536Indication · malfunctionNR 1 ENGINE WAS SHUTDOWN DURING FLIGHT DUE TO DECREASING OIL QUANTITY. INSPECTED OIL QUANTITY INDICATION WIRING, DRAINED AND REFILLED OIL TANK WITH KNOWN QUANTITY OF OIL, BAGGED ENGINE DRAIN LINES AND RAN ENGINE AT 75 PERCENT FOR 5 MINUTES. NO LEAKS OR DEFECJun 14, 1998 · N817AX · Doug DC863 · Engine Oil QuantitySDR ABXA9800479Engine · failedDURING CRUISE FLIGHT AT FL 280, MACH.82, A SUDDEN VIBRATION WAS FELT. NR 2 ENGINE INDICATED; EGT 540, N2 80 PERCENT, OIL TEMP 125 DEG. OIL QUANTITY WAS ZERO AND EPR WAS 1.0. NR 2 ENGINE WAS SHUTDOWN AND EMERG CHECKLIST WAS ACCOMPLISHED. ENGINE WINDMILLED Jun 2, 1998 · N845AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA9800470Engine · failedLOST OIL PRESSURE AND QUANTITY DURING FLIGHT. ENGINE WAS SHUT DOWN. OIL PRESSURE WAS 3 PSI DURING WINDMILLING. REMOVED AND REPLACED NR 2 ENGINE.May 27, 1998 · N849AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA9800451Relief Valve · defectiveAFTER TAKEOFF NR 2 ENGINE OIL QUANTITY DROPPED FROM 9.1 GAL TO 4 GAL AND WAS DECREASING. SHUT NR 2 ENGINE DOWN. ENGINE WINDMILLED FOR ONE HOUR. OIL PRESSURE STAYED AT 35 PSI UNTIL THE LAST 15-20 MINUTES THEN DROPPED TO 11-15. REPLACED OIL PRESSURE RELIEF VMay 13, 1998 · N851AX · Doug DC861 · Engine Oil Distribution (Airframe Furnished)SDR ABXA9800443Switch · defectiveNR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ON CLIMBOUT. OIL QUANTITY, TEMPERATURE AND PRESSURE WERE NORMAL. PERFORMED ABNORMAL PROCEDURE. LIGHT REMAINED ON. PRECAUTIONARY ENGINE SHUTDOWN. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. OPS CHECKED NORMMay 3, 1998 · N853AX · Doug DC861 · Engine Oil PressureSDR TC8A98020Cover Plate · loosePRECAUTIONARY SHUTDOWN NR 3 ENGINE ON SHORT FINAL. OIL PRESSURE STARTED FLUCTUATING BETWEEN 45 PSI AND YELLOW ARC. SHUT IT DOWN WHEN ITWENT BELOW THE RED LINE. REMOVED, INSPECTED AND REPLACED OIL FILTER PER MM 79-20-7, NO METAL FOUND IN FILTER, LEAK CHECKS Apr 30, 1998 · N184SK · Doug DC861F · Turbine Engine Accessory DriveSDR RRXA98082Engine · failedNR 4 ENG LOUD BANG, HEAVY VIBRATION, DECAYING N1, N2 AND INCREASING EGT, ACCOMPANIED BY VIOLENT YAW TO THE RIGHT. HEAVY VIBRATION FELT WITH THROTTLE ADVANCEMENT. PREPARED AIRCRAFT FOR THREE ENGINE FERRY, INSPECTED AIRCRAFT AND FOUND IT SAFE FOR THE FLIGHT INApr 28, 1998 · N991CF · Doug DC8F54 · Engine (Turbine/Turboprop)SDR CKSA98265Fire Loop · chafedUPON INITIAL DESCENT NR 2 ENGINE FIRE WARNING CAME ON. COMPANY PROCEDURES FOLLOWED AND ENGINE WAS SECURED. FOUND WIRE CHAFFING AT RT FWD MAIN WIRE BUNDLE AT 3 O'CLOCK POSITION. WHEN MOVING BUNDLE, FIRE WARNING WOULD GO ON AND OFF DEPENDING ON THE POSITION OApr 21, 1998 · N809CK · Doug DC8F55 · Fire DetectionSDR CKSA98263Tr Actuator · failedDURING DESCENT, NR 2 ENGINE FIRE WARNING CAME ON. PROCEDURES FOLLOWED IAW AIA FOM. ENGINE SHUTDOWN AND NR 2 BOTTLE FIRED. NR 2 BOTTLE PRESS LOW LIGHT DID NOT COME ON NR 1 BOTTLE FIRED AND PRESS LOW LIGHT CAME ON. FOUND T/R ACTUATOR LEAKING BADLY WHICH CAUSApr 18, 1998 · N809CK · Doug DC8F55 · Engine Thrust ReverserSDR TC8A98019Prbc Valve · dirtyNR 2 ENGINECOMPRESSOR STALL DURING TAKEOFF, REJECTED TAKEOFF AT 95 KTS. INSPECTED, CLEANED AND LUBED NR 2 PRBC VALVE. PERFORMED HIGH POWER RUN IAW 71-00.Apr 17, 1998 · N181SK · Doug DC862 · Compressor Bleed ValveSDR CKSA98261Engine · fireNR 2 ENG FIRE WARNING CAME ON DURING DESCENT. AFTER SHUTDOWN LIGHT WENT OUT, THEN CAME BACK ON WITH BELL SEVERAL MINUTES LATER. DISCHARGED ONE FIRE BOTTLE, LIGHT REMAINED ON. FIRED REMAINING BOTTLE, LIGHT REMAINED ON UNTIL AFTER LANDING THEN WENT OUT. REMOApr 16, 1998 · N809CK · Doug DC8F55 · Engine (Turbine/Turboprop)SDR TC8A98017Compressor · stalledREJECTED TAKEOFF AT 80 KNOTS DUE TO COMPRESSOR STALL NR 2 ENGINE. MAX THRUST WAS USED, 1.90 EPR. INSPECTED INLET AREA, EXHAUST AREA AND INNER STAGE BLEED VALVE, NO DEFECTS NOTED. RUN-UP ENGINES, ACCOMPLISHED BY CAPTAIN, BLEED VALVES OFF, BLEED VALVES ON ANDMar 28, 1998 · N181SK · Doug DC862 · Turbine Engine Compressor SectionSDR TC8A98016Compressor · stalledABORTEDTAKEOFF DUE TO LOUD NOISE. RAN ENGINES 1, 2, 3, 4 WITH ANTI-ICE AND BLEED VALVES ON, BLEED VALVE OPS CHECKED NORMAL IAW MIP CHPT 2 71-00.Mar 25, 1998 · N181SK · Doug DC862 · Turbine Engine Compressor SectionSDR TC8A98015Compressor · stalledNR 2 ENGINE COMPRESSOR STALL ON TAKEOFF ROLL, ENGINE ANTI-ICE WAS ON, TEMP 0 CELCIUS. PERFORMED VISUAL INSPECTION OF ENGINE INLET AND EXHAUST, INSPECTED INTERSTAGE BLEED VALVE, NO DEFECTED NOTED. PERFORMED ENGINE RUN-UP WITH ANTI-ICE ON AND BLEED AIR ON AT MMar 24, 1998 · N181SK · Doug DC862 · Turbine Engine Compressor SectionSDR TC8A98014Compressor · stalledABORTED TAKEOFF DUE TO LOUD NOISE LEFT SIDE OF AIRCRAFT. CHECKED TIRES, LANDING GEAR, FUSELAGE AND ALL 4 ENGINES FOR DAMAGE, NO DAMAGE NOTED. RAN ALL 4 ENGINES TO T/O POWER, NO COMPRESSOR STALL NOTED.Mar 20, 1998 · N181SK · Doug DC862 · Turbine Engine Compressor SectionSDR ABXA9800125Regulator · malfunctionNR 2 ENGINE OIL TEMPERATURE WENT TO 153 DEG DURING CLIMB. REDUCED POWER TO IDLE, BUT TEMPERATURE REMAINED THE SAME. SHUT DOWN NR 2 ENGINE. REPLACED NR 2 ENGINE OIL TEMPERATURE REGULATOR AND NR 2 OIL STRAINER. OPS CHECKED GOOD IAW DC8 MM.Feb 23, 1998 · N843AX · Doug DC861 · Engine Oil TemperatureSDR CKSA98012Fire Loop · chaffingNR 2 ENG FIRE LIGHT ILLUMINATES INTERMITTENTLY INFLIGHT ACCOMPANIED BY BELL, SYSTEM CHECKS OK. FOUND FIRE LOOP CHAFING. REPOSITIONED RUBBER GROMMET, CLEANED CANNON PLUG AND LEAK CHECKED BLEED SYSTEM. OPS CHECKS GOOD IAW DC8 MM 26-2-0.Feb 12, 1998 · N807CK · Doug DC855 · Fire DetectionSDR TC8A98007Oil Syst · reqd serviceSHUTDOWN NR 3 ENGINE AT 1130Z IN FLIGHT DUE TO LOW OIL PRESSURE INDICATION AND LOW OIL PRESSURE LIGHT. WINDMILLING OIL PRESSURE 10 PSI. ADDED 5 QTS TO FILL OIL TANK TO FULL. INSPECTED OIL FILTER, FOUND IT CLOGGED AND BYPASSED. CLEANED FILTER IAW PWA MANUALFeb 3, 1998 · N182SK · Doug DC8F55 · Turbine Engine Oil SystemSDR TC8A98002Compressor · stalledNR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF, ABORTED TAKEOFF. INSPECTED ENGINE IAW 72-00, PERFORM GROUND RUN IAW TCA MIP VOL 2, OPS CHECK NORMAL, NO STALLS NOTED.Jan 21, 1998 · N184SK · Doug DC861F · Turbine Engine Compressor SectionSDR ABXA9800034Filter · defectiveDURING DESCENT WITH THROTTLE AT IDLE, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WITH AN OIL PRESSURE READING OF 25 PSI. SECURED NR 2 ENGINE. WINDMILLING OIL PRESS 7 PSI, N2-23 PERCENT, N1-14 PERCENT, EGT-70 DEG, AND EPR-1.00. REPLACED MAIN OIL FILTER Jan 18, 1998 · N826AX · Doug DC863F · Turbine Engine Oil SystemSDR CKSA98001Wire · brokenNR 2 OIL LIGHT LOW PRESS CAME ON, T/R AND T/R DOOR LIGHT CAME ON, GEN FAIL LIGHT CAME ON, OIL PRESS THEN DROPPED AS DID OIL QUANTITY. COMPLETED NR 2 ENGINE SHUTDOWN. LATER AT TOD NR 2 ENGINE FIRE WARNING LIGHT (1/2 SYSTEM) CAME ON, FIRED BOTTLE. REPAIRED WIJan 14, 1998 · N806CK · Doug DC8F54 · Engine Oil PressureSDR ABXA9800014Fire Loop · disconnectedDURING CRUISE, ENG FIRE WARNING MASTER LIGHT AND BELL ACTIVATED MOMENTARILY. UNABLE TO DETERMINE WHICH ENGINE CAUSED PROBLEM. FUEL FLOW ON NR 3 ENGINE INCREASED APPROXIMATELY 700 PPH. SHUT DOWN NR 3 ENGINE, WITH ENGINE WINDMILLING, N1 WAS 26.5 PERCENT, N2 WJan 8, 1998 · N804AX · Doug DC862 · Fire DetectionSDR TC8A97054Fuel Control · failedATTEMPTED T/O, HOWEVER NR 3 ENGINE N1 WOULD NOT SPOOL UP TO T/O POWER, ENGINE COMPRESSOR STALL POPPING WAS NOTED. N2 WAS 80 PERCENT, N1 HUNG AT 48 PERCENT. FOUND N1 INDICATOR STICKS, REPLACED N1 INDICATOR PER MM 77-12-0, OPS CHECKS OK. FOUND ENGINE WOULD NODec 14, 1997 · N182SK · Doug DC8F55 · Fuel Control/Turbine Engines
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