Pratt & Whitney JT3D-7

Service difficulty reports · 265

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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 = 'JT3D7'
  ORDER BY difficulty_date DESC"

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SDR ARWA20030914Bleed Valve · stuckUNABLE TO OBTAIN MAX POWER INDICATION WITH NR 1 TROTTLE AT IT'S FULL FORWARD STOP POSITION. FOUND NR 1 ENGINE SURGE BLEED VALVE STUCK OPEN; REMOVED AND REPLACED NR 1 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3; OPERATIONAL CHECK NORMAL IAW MM 71-00.Sep 21, 2003 · N441J · Doug DC863F · Compressor Bleed ValveSDR ARWA20030801Bleed Valve · inoperativeCOMPRESSOR STALL NR 2 ENGINE COMMENCING THE TAKE OFF ROLL. REJECTED TAKE OFF (RTO). REMOVED AND REPLACED NR 2 PRESSURE RATIO SURGE BLEED VALVE IAW MM 75-30-3. OPERATIONAL CHECK ON RUN UP IAW MM 71-0 FOUND NORMAL.Aug 5, 2003 · N441J · Doug DC863F · Compressor Bleed ValveSDR ABXA030323Engine · overheatedDURING TAKEOFF, NR 3 ENGINE EGT WENT TO 600 DEGREES. RETARDED THROTTLE AND EGT DECREASED INTO NORMAL RANGE. OTHER INSTRUMENTS DECREASED AS WELL. SECURED ENGINE PER ABNORMAL PROCEDURES. EGT AT 600 DEGREES FOR APPROXIMATELY 15 SECONDS. NR 3 ENGINE WAS SHUTDAug 4, 2003 · N816AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA20030501Compressor · stalledNR 1 ENGINE COMPRESSOR STALLED, REDUCED POWER 1.50 EPR, N1 TACH FLUX AND MAX "O". OIL TEMP INCREASING. ENGINE SHUT DOWN 05:30Z WINDMILLING OIL PRESSURE 16 PSI. NOTE: PRELIMINARY INSPECTION REVEAL C1 BEARING FAILURE. CORRECTIVE ACTION:May 9, 2003 · N791AL · Doug DC862F · Turbine Engine Compressor SectionSDR ARWA20030404Fuel Control · malfunctionedNR 4 ENGINE HUNG START IN SKGO, SLOW TO SPOOL ON GROUND AND SLOW TO SPOOL IN FLIGHT. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL UNIT (FCU) IAW DC-8 MM 73-20-1. LEAK CHECK OK. OPERATIONAL CHECK PERFORMED IAW MM 71-00 ON RUN UP FOUND NORMAL.Apr 13, 2003 · N661AV · Doug DC863F · Fuel Control/Reciprocating EnginesSDR ARWA20030401Engine · lack of lubeAFTER T/O FROM UTP, DURING CLIMB, FE OBSERVER NR 2 OIL QUANITY INDICATOR READING 2 GALLONS & DECREASING. SWAPPED INDICATORS, NO CHANGE. FOLLOWED ABNORMAL PROCEDURES FOR FUEL DUMPING, LANDED (UTP) LESS THAN MLWG. SERVICED NR 2 ENGINE OIL WITH 9 QTS. OF OIL.Apr 3, 2003 · N8969U · Doug DC862 · Turbine Engine Oil SystemSDR ABXA030120Engine · defectiveON CLIMBOUT, THE NR 4 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 4 OIL PRESSURE NOTED TO BE 32 PSI. WHEN POWER REDUCED, OIL PRESSURE WAS 20 PSI. SHUT DOWN THE NR 4 ENGINE AT 1036Z. WINDMILLING OIL PRESSURE 8-10 PSI IN CLIMB AND CRUISE. AIRCRAFT FERMar 18, 2003 · N818AX · Doug DC863 · Engine (Turbine/Turboprop)SDR ARWA20030211Amplifier · failedSHORTLY AFTER TAKEOFF FIRE WARNING ON ENGINE NR 2. REMOVED AND REPLACED NR 2 FIRE DETECTOR AMPLIFIER. OPERATIONAL CHECK NORMAL IAW MM 26-10-0 AND ENGINE RUN UP IAW MM 71-00.Feb 27, 2003 · N784AL · Doug DC863F · Fire DetectionSDR ABXA030074Engine · failedNR 4 ENGINE SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND OIL PRESSURE, AT 1100Z WINDMILLING, OIL PRESSURE 3 PSI, N2 30 PERCENT. REMOVED AND REPLACED THE NR 4 ENGINE IAW DC-8 MM AND ABX WORK PACK 600166755.Feb 18, 2003 · N828AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA030067Transmitter · failedDURING CLIMBOUT, WHEN NR 1 ENGINE ANTI-ICE WAS TURNED OFF, NR 1 ENGINE COMPRESSOR STALLED ACCOMPANIED BY NR 1 OIL PRESSURE WENT TO 100 PSI AND OIL QUANTITY FLUCTUATED +/-2 GALLONS. SECURED ENGINE. ENGINE WINDMILLED ABOVE 25 PERCENT FOR 45 MINUTES. FOUND NR 1 Feb 11, 2003 · N811AX · Doug DC863F · Engine Oil PressureSDR ARWA20030111Bleed Valve · failedON TAKE-OFF UNABLE TO ATTAIN MAXIMUM POWERN ON NR 2 ENGINE WITH THROTTLE FIRE WALL EPR 1.36 N1 98 N2 95 FIREWALL POWER. AIRCRAFT ABORTED TAKE-OFF AIRCRAFT RETURNED TO BLOCK. REMOVED AND REPLACED SURGE BLEED VALVE IAW MM 75-30-3. PERFORMED OPERATIONS CHECK AJan 31, 2003 · N784AL · Doug DC863F · Compressor Bleed ValveSDR ARWA20030106Packing · leakingINFLIGHT OIL QUANTITY GRADUALLY DROPPED TO ZERO, SUBSEQUENTLY OIL PRESSURE FLUCTUATED BETWEEN 45 36 PSI. OIL PRESSURE LIGHT ON, PERFORMED IN FLIGHT NR 3 ENGINE SHUTDOWN AS PER ABNORMAL WIND MILL OIL PRESSURE 10 PSI. DECLARED EMERGENCY. PERFORMED FUEL DUMP PRJan 28, 2003 · N784AL · Doug DC863F · Engine Oil QuantitySDR ARWA20030105Line · leakingNR 2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO FLUCTUATING OIL PRESSURE AND INTERMITTENT PRESSURE WARNING LIGHT AT 1555Z WINDMILLING OIL PRESSURE 15-25 PSI. INSPECTED NR 2 ENGINE, FOUND RIGID LINE BETWEEN MAIN OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH DAMAGED (LJan 25, 2003 · N441J · Doug DC863F · Engine Oil Distribution (Airframe Furnished)SDR ARWA20021202Engine · malfunctionedPRECAUTIONARY NR 4 ENGINE SHUTDOWN; OIL QUANTITY LOW. TIME: 0605Z, N1: 37 PERCENT. OIL PRESSURE 0-10 PSI. ACCOMPLISHED INFLIGHT ENGINE SHUTDOWN CHECKLIST. REMOVED AND REPLACED NR 4 ENGINE IAW ARROW AIR TASK CARD DC8 UN-003 AND MASTER TALLY UNDER W/O 601627Dec 5, 2002 · N8969U · Doug DC862 · Engine (Turbine/Turboprop)SDR ARWA20021004Engine · malfunctionedDURING CRUISE NR 3 ENGINE IDLE PRESS. LIGHT ILLUMINATED. OIL PRESS. 25 PSI, QTY, 1 GALLON. TEMP 135 DEGREES. ENGINE SHUT DOWN AT 1421Z. WINDMILLING OIL PRESSURE ZERO. REMOVED ENGINE, AND REPLACE WITH SERVICEABLE ENGINE. FUNCTIONAL TEST AND GROUND RUN-Oct 12, 2002 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)SDR ARWA20021003Indicator · stickingON TAKEOFF ROLL OUT OF MIAMI, FIRST OFFICERS AIRSPEED INDICATOR STUCK AT 70 KNOTS. CAPTAINS INDICATOR 95 KNOTS. ABORTED TAKEOFF, RETURNED TO RAMP FOR CORRECTIVE ACTION. REMOVED & REPLACE WITH NEW PART, FIRST OFFICERS AIRSPEED INDICATOR. ALL WORK ACCOMPLISHOct 8, 2002 · N906R · Doug DC863F · Airspeed/Mach IndicatorSDR ABXA020153Engine · malfunctionedNR 4 ENGINE LOW OIL PRESSURE LIGHT CAME ON ACCOMPANIED BY AN OIL PRESSURE FLUCTUATION AND QUANTITY DECREASING. ENGINE WAS SECURED AND OIL PRESSURE WAS BELOW 5 PSI WITH ENGINE WINDMILLING AT 30 PERCENT N2 FOR REMAINED OF FLIGHT. REPLACED THE NR 4 ENGINE. RUNSep 3, 2002 · N814AX · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA20020902Bleed ValveLOG PAGE # 112879. DISCREPANCY: DURING TAXI NOTICED # 3 ENGINE COMPRESSOR STALLING ACCELERATION OF ENGINE. CORRECTIVE ACTION: REMOVED AND REPLACED # 3 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3. OPERATIONS CHECKED OK; RUNUP FOUND NORMAL IAW DC-8 MM 71-00Sep 3, 2002 · N1804 · Doug DC862 · Compressor Bleed ValveSDR ARWA20020811Bleed Valve · malfunctionedWHILE SPOOLING ENGINES FOR TAKEOFF, NR 3 ENGINE MADE A LOUD NOISE AT 1.1 EPR 80 PERCENT N2 BLEEDS OFF. REMOVED AND REPLACED PRESSURE RATIO BLEED CONTROL IAW DC-8 MM 75-30-0. CHECKED ENGINE RUN UP NORMAL IAW 71-00.Aug 31, 2002 · N661AV · Doug DC863F · Compressor Bleed ValveSDR ARWA20020809Oil System · lack of lubeNR 3 ENGINE OIL QUANTITY INDICATING ZERO; WITH OIL PRESSURE FLUCTUATING AND LOW OIL PRESSURE, LIGHT ILLUMINATED. PERFORMED IN-FLIGHT ENGINE SHUTDOWN AT 1920Z. NOTE WINDMILLING OIL PRESSURE 20 PSI TURNED ON START LEVER AT 2020Z AS PER AFM. SERVICED NR 3 ENGIAug 28, 2002 · N441J · Doug DC863F · Turbine Engine Oil SystemSDR ARWA20020803Engine · power lossAFTER BRAKE RELEASE, LOST PARTIAL POWER ON NR 4 ENGINE. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED NR 4 ENGINE, OPS CHECK AND LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.Aug 13, 2002 · N441J · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA020003Pump · sheared#2 engine driven fuel pump was inop. Found spline shaft sheared on #2 engine driven fuel pump. Replaced pump IAW 73-10-2. Ops and leak checked good IAW 71-00.Jun 24, 2002 · N812AX · Doug DC863F · Engine Fuel PumpSDR ARWA20020601B-Nut · looseABORTED TAKEOFF DUE TO NR 4 ENGINE WOULD NOT GO TO MAX POWER. FOUND COMPRESSOR BLEED ACTUATOR TO CONTROL CLOSED TUBE B-NUT LOOSE; TIGHTENED B-NUT IAW MM 75-30-2; PERFORMED FLAG CHECK ENGINE RUN UP OPS CHECKED NORMAL IAW MM 75-30-3 AND 71-00 MAX TAKEOFF POWER Jun 14, 2002 · N441J · Doug DC863F · Compressor Bleed ControlSDR ARWA20020509Mount · brokenDURING A-CHECK AT MIA THE FOLLOWING WAS FOUND, NR 4 ENGINE AFT MOUNT BROKEN. REPLACED FORWARD LT, FORWARD RT AND AFT ENGINE MOUNT ASSEMBLY IAW MM 71-20-2. AFT MOUNT SENT OUT FOR ANALYSIS.May 29, 2002 · N661AV · Doug DC863F · Engine Mount SectionSDR ARWA20020508Engine · malfunctionedAFTER TAKEOFF, CLIMBING THROUGH 12 THOUSAND OIL QUANTITY CAME DOWN TO 2 GALLONS, FOLLOWED BY OIL PRESSURE LIGHT. PERFORMED ABNORMAL CHECK LIST NR 4 ENGINE OFF (SHUTDOWN). CAME BACK TO SAN SALVADOR WITHOUT ANY MORE ABNORMALITIES. PREPARED NR 4 ENGINE FOR FERMay 25, 2002 · N345JW · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA20020503Garlock Seal · leakingNR 4 ENGINE OIL QUANTITY 3/4 OF A GALLON. PERFORMED INFLIGHT SHUT DOWN ABNORMAL. OIL PRESS WINDMILLING 20 PSI. SERVICED ENGINE OIL IAW DC-8 MM 12-20-1 AND PERFORMED ENGINE RUN-UP; FOUND OIL LEAK AT MAIN FUEL PUMP DRAIN. REMOVED AND REPLACED MAIN FUEL PUMP May 8, 2002 · N810BN · Doug DC862 · Turbine Engine Oil SystemSDR ARWA20020305Engine · malfunctionedWITH THROTTLE SET FOR MAX TAKEOFF NR 4 ENGINE GOT UP TO 1.70 EPR, N1-100, N2-100, AND THROTTLE FULL FORWARD. TAKEOFF ABORTED AND RETURNED TO THE RAMP.Mar 6, 2002 · N441J · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA20020207Compressor · stalledUPON COMMENCING T/O ROLL NR 2 ENGINE COMPRESSOR STALLED SPEED NIL WIND CALM. AIRCRAFT RETURNED TO THE RAMP. PERFORMED VISUAL INSPECTION OF NR 2 ENGINE IN ACCORDANCE WITH 71-00, OPS CHECKED FOUND NORMAL ON GROUND RUN UP.Feb 26, 2002 · N1808E · Doug DC862 · Turbine Engine Compressor SectionSDR ABXA010707Fuel Control · failedDURING DESCENT, THE NR 4 ENGINE FAILED TO ACCELERATE. EPR, EGT, RPM AND F/F DECAYED. OIL PRESSURE WAS NORMAL (WINDMILLING). PERFORMED CHECKLIST - NO HELP. DURING LEVEL OFF WITH INCREASED AIRSPEED - NEGATIVE RELIGHT. PERFORMED ENGINE SHUTDOWN ACTIONS CHECKFeb 8, 2002 · N811AX · Doug DC863F · Fuel Control/Turbine EnginesSDR ARWA20020108Diffuser · damagedNR 4 ENGINE SHUT DOWN IN FLIGHT DUE TO FIRE WARNING, POST FLIGHT INSPECTION FOUND 4 INCH HOLE BURNED IN DIFFUSER CASE. AIRCRAFT FERRY FLIGHT TO SINGAPORE. REMOVED AND REPLACED NR 4 ENGINE. PERFORMED ENGINE RUN. ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERJan 6, 2002 · N8968U · Doug DC862 · Turbine Engine Compressor SectionSDR ARWA20020105ValveLOG PAGE 108167. DISCREPANCY:ON ATART UP WHEN # 2 ENGINE THROTTLE IS ADVANCED ENGINE SURGES AND VIBRATES. WHEN REVERSE IS SELECTED TR TRANSLATES AND BUCKET DEPLOYS BUT ENGINE DOES NOT ACCELERATE IN REVERSE. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENGINE SURJan 5, 2002 · N1808E · Doug DC862 · Compressor Bleed ValveSDR ARWA20011212Bleed Valve · lack of lubeNR 3 ENGINE COMPRESSOR STALL AT BRAKE RELEASE MAX POWER 1.89 EPR RETURN TO RAMP FOR CKV & FOR NOTE 13 DEGREE CELSIUS ENGINE ANTI ICE OFF AND NO WIND. LUBED SURGE BLEED VALVE IAW MM 75-30-3, SYSTEM OPS CKD NORMAL IAW MM 71-00 ENGINE RUN. AIRCRAFT RETURNED TO Dec 23, 2001 · N802BN · Doug DC862 · Compressor Bleed ValveSDR ARWA20011206Engine · failedAPPROX 200 MILES OUT OF BAHRAIN AT FL 330 NR 4 ENGINE COMPRESSOR STALLED IN CLEAR WEATHER, FOLLOWED BY DROP IN EPR FROM 1.65 TO 1.15. ALL OTHER PARAMETERS NORMAL, ABOVE 85 PERCENT N2 ENGINE SURGES. AIRCRAFT LANDED WITHOUT INCIDENTS. POST FLIGHT INSPECTION RDec 12, 2001 · N661AV · Doug DC863F · Engine (Turbine/Turboprop)SDR ARWA20011205EngineLOG PAGE 101856. DISCREPANCY: ON ADVANCING THROTTLE FOR TAKE OFF #4 ENGINE HUNG, CARRIED OUT ABNORMAL PROCEDURE FOR ENGINE HUNG WITH THRUST LEVER IN REVERSE ENGINE STARTED TO ACCELERATE. CANCELED REVERSE THRUST ENGINE CONTINUED TO ACCELERATE WITH THROTTLE CLOSDec 11, 2001 · N1804 · Doug DC862 · Engine Fuel and ControlSDR ARWA0010902EngineLOG PAGE 106168. DISCREPANCY: ON CLIMB OUT OF KMIA NBR-3 ENG OIL PRESS LIGHT CAME ON AND OIL PRESS ERRATIC. PERFORMED PRECAUTIONARY SHUT DOWN. TOTAL WINDMILLING TIME 25 MIN. LANDING WT 240.0 LBS ENG SHUT DOWN AT 0536Z.AIRCRAFT LANDED WITHOUT INCIDENT. CORRECTISep 18, 2001 · N810BN · Doug DC862 · Engine Oil PressureSDR ARWA0010811Compressor · stalledNR 4 ENGINE SHUT DOWN DUE TO COMPRESSOR STALL. AIRCRAFT RETURNED TO SAL AND LANDED WITHOUT INCIDENT. C1 HARD TO ROTATE BY HAND. PREPARE NR 4 ENGINE FOR FERRY FLIGHT ONE ENGINE INOPERATIVE IAW ARROW AIR GMM 6-3-1 THRU 6-3-5. LOG PAGE 105029 ITEM 12 M, REMOVED Aug 30, 2001 · N661AV · Doug DC863F · Turbine Engine Compressor SectionSDR ARWA0010803SealLOG PAGE 53334. DISCREPANCY: ON FINAL APPROACH SHUT DOWN #3 ENGINE DUE TO RAPID DROP IN OIL QUANTITY AND PRESSURE. CORRECTIVE ACTION: REMOVED HOUSING AND SEAL FROM FUEL BOOST PUMP DRIVE ON # 3 ENGINE GEAR BOX. INSTALLED SEAL (SEAL P/N 730376) AND HOUSING Aug 7, 2001 · N802BN · Doug DC862 · Engine Oil System (Airframe Furnished)SDR ARWA0010802Wire · burnedAFT T/O NR 3 ENG T/R LT ILLUM, NR 3 ENG ANTI-ICE VLV LT CAME ON. NR 3 ENG OIL PRESS LT CAME ON, NR 3 ENGINE OIL PRESS GAUGE READ ZERO. FOLLOWED ABNORM CKLIST FOR OIL PRESS LIGHT, INFLIGHT SHUTDOWN. ON APPR NR 3 ENG ANTI-ICE VLV CB TRIPPED, GRD COOLING & BLOAug 2, 2001 · N6661A · Doug DC863F · Engine Thrust ReverserSDR ARWA0010720Bolt · shearedDURING FL 350 AND AS CRUISE ALTITUDE, THE NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND THE EGT BECAME ERRATIC. PERFORM CHECKLIST, SHUT DOWN ENGINE AT 0819Z, OIL PRESSURE READING 45 PSI. ON LANDING SMELLED BURNING SMELL IN COCKPIT. LANDED WITHOUT INCIDENT.Jul 28, 2001 · N8968U · Doug DC862 · Engine Anti-Icing SystemSDR ARWAA0010718Pin · brokenON DEPARTURE TAKEOFF OUT OF MIAMI, GEAR NOT LATCHED LIGHT ILLUMINATES WITH GEAR IN UP POSITION. ABNORMAL CHECKLIST PERFORMED. LANDED WITHOUT INCIDENT. OVERWEIGHT LANDING WEIGHT INSPECTION COMPLETED. UPON INSPECTION OF THE AIRCRAFT, THE RIGHT HAND MAIN GEARJul 22, 2001 · N345JW · Doug DC863 · Landing Gear ActuatorSDR ARWA0010605Engine · malfunctionedDURING TAKEOFF ROLL LOSS POWER ON NR 1 ENGINE. ABORTED TAKEOFF AT 70 KNOTS. REFERRED TO PERFORMANCE MANUAL BRAKE ENERGY CHART OK TO TAXI. CHECKED ALL TANK CROSSFEED VALVES AND SELECTOR VALVES FOR OPERATION FOUND NORMAL IAW MM 28-22-2,3. INSPECTED FUEL FILTJun 19, 2001 · N810BN · Doug DC862 · Engine (Turbine/Turboprop)SDR ARWA74100Compressor · stalledTAKEOFF ROLL WAS ABORTED AT 65 KNOTS DUE TO COMPRESSOR STALL ON NR 3 ENGINE. PERFORMED TEST OF COMPRESSOR BLEED VALVE IAW MM 75-30-3, FOUND NORMAL. CHECKED ON ENGINE RUN UP IAW MM 71-00, FOUND NORMAL OPERATION NO COMPRESSOR STALL NOTED.Apr 26, 2001 · N345JW · Doug DC863 · Turbine Engine Compressor SectionSDR ARWA0010406Bleed ValveLog Page 54673. Discrepancy: Take Off roll was aborted at 65 Knots due to compressor stall on #3 engine. Corrective Action: Performed test of compressor bleed valve IAW MM 75-30-3 found normal. Checked on engine run up IAW MM 71-00 found normal operation no coApr 26, 2001 · N345JW · Doug DC863 · Compressor Bleed ControlSDR ABXA010357Case · crackedNR 4 ENGINE INLET GUIDE VANE CASE HAD NUMEROUS CRACKS AT WELDS. WELDED CRACKS ON INLET CASE IAW P&W OVERHAUL MANUAL 72-21-1.Apr 18, 2001 · N828AX · Doug DC863 · Turbine Engine Air Inlet SectionSDR ARWA0010307O-Ring · leakingAT TOP OF DESCENT NR 3 ENGINE OIL PRESSURE GAUGE FLICKERS FULL SCALE HIGH AND LOW AND NR 3 ENGINE OIL PRESSURE LIGHT FLICKERS ON AND OFF. ALL OTHER ENGINE PARAMETERS NORMAL. PRECAUTIONARY ENGINE SHUTDOWN. ON INSPECTION OF ENGINE, FOUND TOWER SHAFT SEAL LEAKMar 20, 2001 · N810BN · Doug DC862 · Turbine Engine Accessory DriveSDR ARWA0010201Oil Cooler · damagedRETURNED TO MKJP SHORTLY AFTER THE TAKEOFF DUE TO HIGH OIL TEMP NR 1 ENGINE. PRECAUTIONARY ENGINE SHUTDOWN AT 22:28Z TEMP 142 DEGREES, FOLLOW BY ABNORMAL CHECK LIST OIL PRESSURE WAS 47 PSL. WINDMILLING OIL PRESSURE 8 PSI. REMOVED AND REPLACED NR 1 ENGINE FUFeb 3, 2001 · N8968U · Doug DC862 · Engine Fuel/Oil CoolerSDR ARWA0010103Bleed Valve · dirtyAT THE BEGINNING OF TAKEOFF ROLL NR 2 ENGINE HAD COMPRESSOR STALL. ENGINE PARAMETER WERE TAKEOFF, EPR WAS 1.88; DROPPED TO 1.75 N2 AND RECOVERED, FUEL FLOW DMI AND EGT WAS NORMAL. PERFORMED VISUAL CHECK AIR BLEED VALVE, CLEANED AND LUBRICATED IAW M/M 75-30-Jan 28, 2001 · N1808E · Doug DC862 · Compressor Bleed ValveSDR RRXA001091Compressor · stalledON CLIMBOUT WITH ENGINE ANTI-ICE ON NR 3 ENG COMPRESSOR STALLED, OIL PRESSURE WAS 59 PSI. DURING B-CHECK INSP FOUND PRBC LOCKED UP. REMOVED AND REPLACED PRBC IAW 75-30-3. BORESCOPE NR 3 ENG IAW DC-8 MM 72-00 431453082, PRBC CHECKS GOOD, NO COMPR STALL ON ENDec 12, 2000 · N950R · Doug DC863F · Turbine Engine Compressor SectionSDR ABXA000528Seal · cutTWENTY MINUTES AFTER TAKEOFF FROM EWR, THE NR 3 ENGINE OIL PRESSURE FLUCTUATED AND OIL QUANTITY DROPPED TO APPROX. ZERO GALLONS. THE CREW SHUT THE ENGINE DOWN IN FLIGHT, IAW ABX PROCEDURES. MAINTENANCE INSPECTED AND FOUND THE NR 3 FRONT ACCESSORY HOUSING O-RINDec 11, 2000 · N815AX · Doug DC863F · Turbine Engine Oil SystemSDR ABXA000521Engine · seizedON TAKEOFF FROM PHL, THE NUMBER TWO ENGINE SIEZED. THE CREW SECURED THE ENGINE AND CONTINUED TO ILN. ILN MAINTENANCE INSPECTED AND REPLACED THE NUMBER TWO ENGINE IAW ABX JOBCARD 8090507.Dec 7, 2000 · N816AX · Doug DC863F · Engine (Turbine/Turboprop)
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