Pratt & Whitney JT8D-219

Service difficulty reports · 1,944

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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 = 'JT8D219'
  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 ASMF200709008Strut · leakingAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AFTER TAKEOFF, THE NOSE LANDING GEAR RED LIGHT STAYED ON. MAINTENANCE PERSONNEL PERFORMED THE NOSE GEAR STRUT SERVICE IAW MM 32-21-02 AND THE EXTENSION AND RETRACTION TEST IAW MM 32-30-00, ALL CORRECT. AS A PRECAUTIOSep 23, 2007 · N158PL · Doug MD88 · Nose/Tail Landing Gear Strut/AxleSDR ASMF200709003Powerplant · overspeedCAPTAIN REPORTED WINDSHEAR DURING APPROACH AND ATS DISCONNECTED, SPEED DECREASED, SO AUTOTHOTTLES WERE SET TO THE MAXIMUM POWER. AT PLATFORM, MAINTENANCE PERSONNEL DOWNLOAD THE ENGINES INFORMATION FROM THE MINIQAR DETECTING THAT THE RT ENGINE HAD VALUES OF N1Sep 5, 2007 · N803ML · Doug DC987 · Auto Throttle SystemSDR MWEA070187Pressure Switch · malfunctionedOIL STRAINER CLOGGING LIGHT CAME ON, OIL TEMPERATURE WENT TO 120 THEN DECREASED OIL PRESSURE AT 45 EPR. REMOVED AND REPLACED OIL DIFFERENTIAL PRESSURE SWITCH.Aug 22, 2007 · N601ME · Doug MD88 · Engine Oil PressureSDR ASMF200708003Shutoff Valve · leakingAIRCRAFT RETURN TO PLATFORM DURING TAXI, CREW SELECTED SLATS EXTEND AND THE HYDRAULIC QUANTITY LIGHT TURNED ON. MAINTENANCE DETECTED HYDRAULIC LEAK IN RT SYSTEM AND QUANTITY ZERO, SO THE SYSTEM WAS SERVICED AND HYDRAULIC PRESSURE WAS APPLIED AND THE LEAK WAS Aug 12, 2007 · N214AM · Doug DC987 · Hydraulic System, MainSDR DLM88071052Pump · failedAT ALT 230 CLEAN CONFIG LEFT HYD SYSTEM PRESSURE WENT TO ZERO. RAN CHECKLIST AND PER PROCEDURES REGAINED LEFT SYS PRESSURE AFTER TURNING ON AUX AND TRANS PUMPS. REPLACED LT ENGINE HYD PUMP, CASE DRAIN AND IN LINE PRESS FILTERS. RAN ENGINE CKS OK. LEAK CK OAug 9, 2007 · N900DE · Doug MD88 · Hydraulic Pump (Electric/Engine), MainSDR DLM88071041Line · leakingNUMBER 2 ENGINE HYDRAULIC PRESSURE LINE LEAK AND CAUSE TO LOSE MOST OF THE HYDRAULIC FLUID. REPLACED FLEX LINE FROM NR 2 ENGINE TO PYLON LEAK CHECKS NORMAL.Aug 7, 2007 · N944DL · Doug MD88 · Hydraulic System, MainSDR ASMF200708001Plate · brokenCAPTAIN REPORTED THAT DURING CRUISE THE AILERON GOT STUCK WHEN THE COMPENSATOR KNOB IS TURNED TO THE RT SIDE. DURING CHECK, A SCREW WAS DAMAGED AND PLATE SPIRAL DRIVE BROKEN. THEY WERE REPLACED AND TRIM WAS PERFORMED TO CONTROL MECHANISM IAW MM 27-10-07, TESTEAug 2, 2007 · N754RA · Doug DC987 · Aileron Control SystemSDR DLM88070969Engine · failedFLIGHTCREW REPORTED THAT EN ROUTE TO ATL LEFT ENGINE OIL FILTER CLOGGED MESSAGE ILLUMINATED ON OAP FOLLOWED BY THE LOSS OF OIL PRESSURE AND OIL QTY. FLIGHTCREW SHUT DOWN ENGINE AND DIVERTED TO STL. REPLACED NR 1 ENG PER TRANS 9T102.Jul 30, 2007 · N966DL · Doug MD88 · Engine (Turbine/Turboprop)SDR AALA20071342Engine · oil consumptionORD INFLIGHT T1817/24JUL - OIL PRESSURE LIGHT ILLUMINATED ACCOMPANIED BY INDICATION OF QUANTITY DECREASE TO ZERO. CREW SHUT DOWN ENGINE AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. REPLACED NUMBER ONE ENGINE ON 23 JUL 2007Jul 24, 2007 · N931TW · Doug DC983 · Engine (Turbine/Turboprop)SDR ASMF200707014Door · damagedDURING TRANSIT CHECK, AIRCRAFT WAS HIT IN THE FORWARD SERVICE DOOR BY A CATERING SERVICE TRUCK. MAINTENANCE PERSONNEL REPLACED THE DOOR IAW MM 52-41-00, PRESSURIZATION TEST WAS CORRECT.Jul 19, 2007 · N205AM · Doug DC987 · Galley DoorsSDR ASMF200707013Valve · unserviceableDURING TRANSIT CHECK A FUEL SPILLAGE OCCURRED AT PLATFORM. SPILLAGE STARTED WHEN THE AIRCRAFT WAS BEING REFUELED AND FUEL WAS TRANSFERRED FROM CENTRAL TANK TO LT TANK. MAINTENANCE PERSONNEL REPLACE THE LT FUEL FILL VALVE IAW MM 28-20-02 AND PERFORMED AN INDICAJul 16, 2007 · N583MD · Doug DC983 · Aircraft Fuel Distribution SystemSDR ASMF200707010Skin · crackedDURING TRANSIT CHECK, THE AIRCRAFT WAS HIT BY A GATEWAY PROMOTING A CRACK OF 3 INCHES LONG IN FUSELAGE SKIN LOCATED AT STA 271, BETWEEN LONGERONS 17 AND 18 LEFT SIDE. THE NON ROUTINE CARD A0116633 WAS ISSUED, TO REPAIR DAMAGE. REPAIR DETAILS WILL BE SENT AS A Jul 14, 2007 · N169PL · Doug MD88 · Fuselage Main, Plate/SkinSDR ASMF200707004Stabilizer · crackedDURING THE INSPECTION OF THE HORIZONTAL STABILIZER REAR SPAR UPPER CAPS, REQUIRED BY THE AD 2007-10-04, DETECTED A CRACK OF (2) INCHES LONG AT STATION XH = 6.5. THE REPAIR IS IN PROCESS, DETAILED INFORMATION WILL BE SUBMITTED IN A SUPPLEMENT AS SOON AS ITS COJul 5, 2007 · N583MD · Doug MD83 · Horizontal Stabilizer, Spar/RibSDR ASMF200707005Switch · failedAIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN REPORTED THAT THE LT INLET FUEL LOW PRESSURE AND MASTER CAUTION LIGHTS TURNED ON. REPORT WAS DEFERRED IAW MEL 73-3. DURING OVERNIGHT CHECK AT MEX, MAINTENANCE PERSONNEL REPLACED THE LOW FUEL PRESSURE CAUTION SWITCH Jul 5, 2007 · N214AM · Doug DC987 · Fuel Controlling SystemSDR DLM88070847Engine · unknownNR 2 ENGINE ROLLED BACK ON LEVEL OUT AT 4000 FT ON APPROACH. OIL PRESS WENT TO ZERO. ENGINE WAS MANUALLY SHUT DOWN. REPLACED NR 2 ENG OIL FILTER, NO METAL FOUND CHECKED CHIP DETECTOR NO METAL FOUND NEEDS LEAK CK REMOVED FUEL CONTROL P M/M. REPLACED FUEL PUJul 3, 2007 · N905DE · Doug MD88 · Engine (Turbine/Turboprop)SDR ASMF200707002A/C Pack · leakingAIR TURNED BACK DUE TO HIGH TEMPERATURE IN TAIL CONE, LIGHT TURNED ON AND RT ENGINE WITH LOW ACCELERATION. MAINTENANCE CORRECTED PNEUMATIC LEAKS IN THE LT AND RT AIR-CONDITIONED SYSTEMS IAW MM 36-20-02 AND MPCM 21-10-00; ADDITIONALLY, THE ACCELERATION CAMS ANJul 1, 2007 · N214AM · Doug DC987 · Air Distribution SystemSDR ASMF200706006Turbine Blades · crackedDURING LT ENGINE BOROSCOPIC INSPECTION WAS DETECTED A FIRST STAGE TURBINE BLADE WITH A CRACK OF 0.500 INCH IN TIP. ENGINE WAS REPLACED IAW MM 71-00-02 AND OPERATIONALLY TESTED IAW MM 71-00-01, ALL CORRECT.Jun 28, 2007 · N803ML · Doug DC987 · Turbine SectionSDR ASMF200706005Fuel Control · failedCAPTAIN REPORTED THAT AFTER LT ENGINE WAS STARTED, THE EGT INCREASED UNTIL 475 DEGREES (C) WITH N2 IN 47 PERCENT, SO ABNORMAL PROCEDURE (SLOW ENGINE(S) ACCELERATION ON GROUND) WAS PERFORMED CONTINUING THE FAILURE. MAINTENANCE PERSONNEL SERVICED AND TESTED THJun 25, 2007 · N162PL · Doug MD88 · Fuel Control/Turbine EnginesSDR ASMF200706003Apu · failedCAPTAIN REPORTED SMOKE ON AFT LAVATORIES. AT PLATFORM, MAINTENANCE PERSONNEL PERFORMED A TURBINE COOLING SYSTEM CHECK, DETERMINING TO REPLACE THE WATER SEPARATOR OF LT AIR CONDITIONING SYSTEM IAW MM 21-20-01; SO AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNJun 11, 2007 · N838AM · Doug DC983 · APU Core EngineSDR AALA20071068Strainer · cloggedATL INFLIGHT T2441/09JUN - UPON DESCENT NUMBER ONE ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. SHUT DOWN NUMBER ONE ENGINE. LANDED ATL WITHOUT INCIDENT AND TAXIED TO GATE UNDER OWN POWER. FOUND CARBON IN FILTER AT SECOND FILTER CHANGE. REPLACED LEFT HAJun 9, 2007 · N972TW · Doug DC983 · Turbine Engine Oil SystemSDR DLM88070703Engine · leakingATB - SMOKE IN THE CABIN ON TAKEOFF/CLIMB. POWER REDUCED. SMOKE/ODOR DISSIPATED. POWER REAPPLIED, SMOKE/ODOR RETURNED ALONG WITH AFT SMOKE DETECTOR SOUNDING. CROSSFEED VALVES CLOSED. NR 2 ENG REPLACED ON TRANS 9T102.Jun 8, 2007 · N937DL · Doug MD88 · Engine (Turbine/Turboprop)SDR ANCF200700013Engine · damagedAT TO ABOUT 11000 FT, A BIRD IMPACT OCCURRED ON THE LEFT ENGINE, PARAMETER DROP 1.4 EPR THEN ALL PARAMETERS CAME BACK TO NORMAL. IN ACCORDANCE WITH EWO 83-72-7309 LT ENGINE WAS REPLACED IAW AMM 71-00-00 PAGE 501 WAS PERFORMED ADJUSTMENT/TEST AND CONDITIONS ARJun 2, 2007 · N583AN · Doug MD83 · Engine (Turbine/Turboprop)SDR DLM88070622Csd · inoperativeON T/O OUT OF MIA, RT ENGINE CSD OIL TEMP HIGH AND RT GENERATOR FAILED, STARTED APU AND COVERED RT BUSS AND THEN GOT APU GEN FAILED 3 MINUTES LATER. FOUND RT CSD OVER SERVICED AND METAL ON CSD CHIP DETECTOR. REMOVED AND REPLACED NR 2 CSD/GEN/AND CSD OIL COOMay 29, 2007 · N967DL · Doug MD88 · Alternator-Generator DriveSDR ASMF200705007Transceiver · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO THE WEATHER RADAR FAILED IN FLIGHT. MAINTENANCE PERSONNEL REPLACED THE RADAR TRANSCEIVER IAW MM 34-41-04 TESTED CORRECT.May 19, 2007 · N754RA · Doug DC987 · Weather Radar SystemSDR ASMF20070505Valve · failedDURING TRANSIT CHECK CAPTAIN REPORTED PRESSURIZATION FAILURE, AT 25000 FEET FLOW AND CABIN ALT LIGHTS TURNED ON. DURING MAINTENANCE CHECK AUTOMATIC CABIN PRESSURE CONTROL SYSTEMS WERE INOPERATIVE. SYSTEMS WERE DEFERRED IAW MEL 21-24 AND AIRCRAFT WAS DISPATCHEDMay 10, 2007 · N158PL · Doug MD88 · Air Distribution SystemSDR DLM88070487Mount · corrodedRT PYLON FRONT SPAR ENGINE MOUNT FITTING LOWER HOLE HAD CORROSION IN THE BORE AND SURROUNDING FORWARD FACE. REPAIRED PER ER/A 461312-14.May 7, 2007 · N944DL · Doug MD88 · Engine Mount SectionSDR ASMF200705004Line · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO SMOKE ODOR IN PASSENGERS CABIN. A HYDRAULIC LEAK WAS DETECTED IN THE APU INLET DUCT. THE HYDRAULIC LEAK WAS REPAIRED AND WATER SEPARATORS WERE REPLACED IAW MM 21-20-02, TESTED CORRECT. DURING BOARDING, THE HYDRAULIC ODOR WAMay 6, 2007 · N169PL · Doug MD88 · Hydraulic System, MainSDR ASMF200705003Line · leakingDURING TRANSIT CHECK, A LOW HYDRAULIC LEVEL WAS DETECTED IN THE LT SYSTEM WITH AN INDICATION OF 6 QUARTERS. DURING MAINTENANCE INSPECTION, THE LEAK WAS CONFIRMED IN THE LT MAIN WHEEL WELL, SO AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, HYDRAULIMay 4, 2007 · N169PL · Doug MD88 · Hydraulic System, MainSDR DLM88070467Turbine · failedON CLIMBOUT THROUGH 7000 FT LEFT ENG HAD A LOUD BANG, STALL EGT CLIMBED THROUGH 770 DEGREES. OIL PRESSURE INDICATED ZERO ENGINE STOPPED RUNNING- CREW COMPLETED ENGINE SEVERE DAMAGE SHUTDOWN CHECKLIST. AFTER ARRIVAL OIL QTY APPEARED NORMAL, MTC CONFIRMED REAMay 4, 2007 · N998DL · Doug MD88 · Turbine SectionSDR ASMF200705002Csd · failedAIRCRAFT RETURNED TO PLATFORM, RT GENERATOR OUT OF LINE AFTER ENGINES START. DURING MAINTENANCE CHECK, THE RT GCU WAS RESEATED, BUT THE FAILURE CONTINUED. THE REPORT WAS DEFERRED IAW MEL 24-1-1 CAT B. DURING OVERNIGHT CHECK, THE RT CSD, GENERATOR AND HEAT EXCHMay 3, 2007 · N158PL · Doug MD88 · Alternator-Generator DriveSDR ASMF200705001Line · looseAIRCRAFT RETURNED TO PLATFORM, THE LT HYDRAULIC HIGH TEMP LIGHT TURNED ON AND DURING TAXI, THE HYDRAULIC QUANTITY VARIATION 17 - 7 QUARTERS. DURING MAINTENANCE CHECK, THE LT HYDRAULIC SYSTEM QUANTITY WAS CHECKED AND DETECTED WITH LOW LEVEL. THE LT HYDRAULIC REMay 1, 2007 · N169PL · Doug MD88 · Hydraulic System, MainSDR ASMF200704016Controller · malfunctionedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING, CAPTAIN REPORTED LOSS OF CABIN PRESSURE CONTROL AT 32000 FEET; EMERGENCY DESCENT PROCEDURE WAS PERFORMED AND OXYGEN MASKS WERE ACTIVATED. DURING MAINTENANCE CHECK, RT AUGMENTATION VALVE LINES WERE REPAIRED IAW MM 20-1Apr 30, 2007 · N161PL · Doug MD88 · Cabin Pressure ControllerSDR DLM88070348Engine · leakingNR 2 ENGINE IFSD DUE TO LOSS OF OIL QTY AND PRESSURE. REPLACED NR 2 ENGINE PER TRANS 9T102.Apr 22, 2007 · N992DL · Doug MD88 · Engine (Turbine/Turboprop)SDR AALA20070725Blade · damagedEWR INFLIGHT T1179/21APR DURING CLIMB LEFT ENGINE COMPRESSOR STALLED AT 600 FEET ABOVE GROUND LEVEL. POSSIBLE BIRD STRIKE. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. ENGINE SHUT DOWN FOR TAXI. REPLACED NUMBER ONE ENGINE ON 20 APR 2007 AT EWR DUE TO BLADEApr 21, 2007 · N598AA · Doug DC983 · Turbine Engine Compressor SectionSDR ASMD200704013Augment Valve · failedRT PNEUMATIC SYSTEM FAILED DURING CLIMB, SO RT PNEUMATIC CABIN DEPRESSURIZED AND PASSENGERS OXYGEN MASKS WERE ACTIVATED. CAPTAIN PERFORMED ABNORMAL PROCEDURE DESCENDING AT 25,000 FEET. DURING MAINTENANCE CHECK, THE OXYGEN MASKS AND 25 OXYGEN GENERATORS WERE DEApr 19, 2007 · N168PL · Doug MD88 · Pneumatic Distribution SystemSDR AALA20070712Compressor · stalledORD INFLIGHT T1877/18APR AFTER TAKE OFF LEFT HAND ENGINE COMPRESSOR STALLED. THROTTLE RETARDED AND INDICATIONS NORMAL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. METAL DEBRIS FOUND IN LEFT HAND ENGINE EXHAUST. REPLACED LEFT HAND ENGINE ON 19 APR 2007 AApr 18, 2007 · N975TW · Doug DC983 · Turbine Engine Compressor SectionSDR ASMF200704012Engine · unknownAIRCRAFT REJECTED TAKEOFF DUE TO LT ENGINE DID NOT ACCELERATE. THE PARAMETERS WERE: LT ENGINE WITH EPR 1.40 AND RT ENGINE WITH EPR 1.86 AND T/O FLX TEMP 50. DURING MAINTENANCE CHECK, THE ACCELERATION CHAMBER AND MOISTURE TRAMP SERVICES WERE PERFORMED IAW MM 7Apr 17, 2007 · N583MD · Doug DC983 · Engine (Turbine/Turboprop)SDR ASMF200704011Pressure Valve · failedAIRCRAFT RETURNED, DUE TO HIGH OIL PRESSURE (57 PSI) AND TEMPERATURE (157 DEGREES C) INDICATIONS OF RT ENGINE WERE SHOWN. DURING MAINTENANCE CHECK, A BOROSCOPIC INSPECTION WAS PERFORMED AND CHIP DETECTOR WAS CHECKED, ALL CORRECT. AS PRECAUTIONARY ACTION OIL, FApr 13, 2007 · N754RA · Doug DC987 · Engine Oil Distribution (Airframe Furnished)SDR ASMF200704009Cooling Turbine · contaminatedAIRCRAFT RETURNED TO PLATFORM DUE TO SMOKE DETECTORS ALARMS OF AFT LAVATORIES WERE ACTIVATED BEFORE TAKE-OFF. DURING MAINTENANCE INSPECTION, IT WAS DETECTED OIL CONTAMINATION IN DUCTS OF COOLING TURBINE, WATER SEPARATOR AND PRIMARY AND SECONDARY HEAT EXCHANGERApr 12, 2007 · N162PL · Doug MD88 · Cabin Cooling SystemSDR 070094Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK, MAINTENANCE INSPECTION, MAINTENANCE REPORTED THAT THE CEILING EMERGENCY LIGHTS BETWEEN FUSELAGE STATIONS 1133 AND 1171 WOULD NOT TEST. FURTHER REPORT THE REMOVAL AND INSTALLATION OF AN EMERGENCY LIGHT POWER SUPPLY BATApr 11, 2007 · N876GA · Doug DC983 · Emergency LightingSDR 070095Lamp · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK, MAINTENANCE INSPECTION, REPORTED THAT THE EMERGENCY EGRESS PATH LIGHTING AT SEAT ROW 16 WOULD NOT TEST. FURTHER REPORT THE REMOVAL AND REPLACEMENT OF 2 (TWO) LAMPS AT ROW 16. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMApr 11, 2007 · N948MA · Doug DC987 · Emergency LightingSDR ASMF200704008Fan · stuckCAPTAIN REPORTED BURNING ODOR WAS DETECTED ON CABIN CREW, SO AIRCRAFT WAS SENT TO THE HANGAR AND DURING INSPECTION INSTRUMENTS FAN WAS DETECTED STUCK AND WITH BURNED ODOR. FAN WAS REPLACED AND TESTED IAW MM 21-50-01, ALL CORRECT. AS A PRECAUTIONARY ACTION, AIRApr 11, 2007 · N161PL · Doug MD88 · Air Distribution FanSDR ASMF200704006Oil System · emptyAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MID DUE TO CAPTAIN REPORTED RT CSD FAILED; APU DID NOT START AND BATTERIES CHARGER CIRCUIT BREAKER POPPED OUT. AT MID TECHNICAL PERSONNEL REPLACED CSD AND GENERATOR, TESTED CORRECT IAW MM 2-10-01 AND 24-20-01. BATTApr 10, 2007 · N161PL · Doug MD88 · DC Generating SystemSDR 070093Indicator · malfunctionedFLIGHT 591, THE FLIGHT CREW REPORTED THAT AFTER RETRACTING THE GEAR, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE NLG INDICATOR PIN (MECHANICAL) INDICATED NOSE GEAR UP. CYCLED GEAR AND RED UNSAFE LIGHT EXTINGUISHED AND DID NOT REOCCUR FOR THE REMAIApr 9, 2007 · N864GA · Doug DC983 · Landing Gear Position and WarningSDR ASMF200704003Vor System · failedDURING TRANSIT CHECK, THE VOR NR 2 FLAG WAS SHOWN ON BOTH PFD'S, RADIO ALTIMETER NR 1 AND EFIS PANEL TEST FAILED IN BOTH SIDES. TECH PERSONNEL REPLACED VHF NAV NR 2 AND RADIO ALTIMETER NR 1 IAW MM 34-32-02 AND 34-42-03 RESPECTIVELY, TESTED CORRECT. BOTH EFISApr 9, 2007 · N158PL · Doug MD88 · Localizer/VOR SystemSDR ASMF200704001Computer · failedAIRCRAFT RETURNED TO PLATFORM DUE TO WHEN SELECTING FLAPS TO 19.5 DEGREES FOR TAKE-OFF, SLATS DISAGREE LIGHT REMAINED ON. AFTER MAINTENANCE INSPECTION, RT STALL WARNING COMPUTER WAS REPLACED IAW 34-19-02 AND TESTED IAW MM 27-81-00, ALL CORRECT.Apr 4, 2007 · N838AM · Doug DC983 · Stall Warning SystemSDR AALA20070597Turbine Blades · damagedTUL INFLIGHT - DURING CLIMB FELT STRONG VIBRATION FOLLOWED BY TAIL COMPARTMENT OVER TEMPERATURE INDICATION. PRESSURIZATION WAS HARD TO CONTROL. LANDED TUL WITHOUT INCIDENT. FOUND DAMAGE TO FOURTH STAGE LOW PRESSURE TURBINE BLADES. REPLACED NUMBER TWO ENGINApr 3, 2007 · N975TW · Doug DC983 · Turbine SectionSDR DLM88070277Generator · malfunctionedAT 1000 FT AGL BOTH ENG GENERATORS WERE PROVIDING INTERMIT POWER. BOTH SIDES PFD AND ND WERE FLASHING ON AND OFF WITH THE PWR CYLING. THIS WAS HAPPENING EVERY 1-2 SECS. CAPTS SIDE SWITCHED TO STBY PWR TO REGAIN INST. THE F/O SIDE CONTINUED TO FLICKER AFTERMar 31, 2007 · N992DL · Doug MD88 · AC Generation SystemSDR ASMF200703007Unknown · unknownAIRCRAFT REJECTED TAKEOFF AT 75 KNOTS DUE TO LT ENGINE REACHED ONLY 1.6 EPR WHILE RT ENGINE REACHED 2.04 EPR WITH N1 100 PERCENT, SO AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL CHECKED ENGINE INLET/OUTLET, CONTROLS, PT2 AND PT7 LINES AND MANIFOLMar 27, 2007 · N803ML · Doug DC987 · Engine (Turbine/Turboprop)SDR ASMF200703008Engine · overspeedAIRCRAFT REJECTED TAKEOFF AT 77 KNOTS DUE TO LT ENGINE REACHED ONLY 1.6 EPR WITH N1 104 PERCENT. AIRCRAFT WAS SENT TO THE HANGAR AND ENGINE WAS REMOVED AND SENT TO THE SHOP. THE NRC A0111096 WAS ISSUED TO CHECK ENGINE PT2 AND PT7 LINES AND MANIFOLD BY LEAKS IMar 27, 2007 · N803ML · Doug DC987 · Engine (Turbine/Turboprop)
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