Pratt & Whitney JT8D-219

Service difficulty reports · 1,944

Newest first. General aviation reporting is voluntary.

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 = '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 WX0A2016032873114Sense Line · rupturedDURING THE CLIMB, NOTICEABLE SPLIT IN THE EPR AS THEY CLIMBED ABOVE FL 250. AT CRUISE AT FL 330 THERE WAS A .25 SPLIT IN THE EPR WITH THE N1 MATCHED. THE EPR WAS LOWER ON THE NR 1 ENG WITH THE N1S MATCHED. WITH THE EPRS MATCHED THERE WAS A 9% DIFFERENCE IN Mar 27, 2016 · N419NV · Doug DC983 · Fuel Controlling SystemSDR WX0A2016032873113Fuel Control · faultyRIGHT ENG WAS SURGING WHILE CLIMBING TO FL 330. ALL ENG INDICATIONS WERE FLUCTUATING, FF +- 200 N1 UP TO 10 EPR 1.90 2.02. VIDEO WAS EMAILED TO MTC CONTROL SHOWING FLUCTUATIONS. THROTTLES WERE STATIONARY DURING FLUCTUATIONS. LT ENG WAS FLUCTUATING TOO, BUTMar 26, 2016 · N887GA · Doug DC983 · Fuel Control/Turbine EnginesSDR WX0A2016032873110Engine · overspeedON APPROACH AT 6000 MSL, AUTO-THROTTLE COMMANDED FULL POWER & DISCONNECTED, RESULTING IN BOTH ENGS OVER SPEED. AIRSPEED WAS 170 KTAS EPR 2.10-2.12 N1 APROX 105% & FLASHING LESS THAN ONE SECOND.Mar 22, 2016 · N421NV · Doug DC983 · Engine (Turbine/Turboprop)SDR AALA20160309004Engine · failedRIGHT ENG LOST OIL PRESS & QUANTITY DURING DESCENT. ENG SHUTDOWN. AN EMER WAS DECLARED. ENG WIND MILLED ABOUT 5 MINUTES. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENG TIME WAS ABOUT 10 MINUTES. R & R RT ENG IAW MCM 71-91-99. THE ACFT WAS Mar 9, 2016 · N9620D · Doug DC983 · Engine (Turbine/Turboprop)SDR AALA20160310001Engine · failedTHE INBD CREW REPORTED ODOR & HAZE IN THE CABIN, CAUSING EYES TO WATER & WAS DIFFICULT TO BREATHE. ACCOMPLISHED SIC 21-96-01 & FOUND LT ENG TO BE THE SOURCE OF THE ODOR. R & R THE LT ENG IAW SIC 71-91-99 & BOW. LEAK CHECK & OPERATIONS CHECKED GOOD. ACCOMPLMar 8, 2016 · N966TW · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2016030773099Engine · failedDURING THE TAKEOFF THE CREW NOTED A LOUD BANG FOLLOWED BY ALL PARAMETERS FLASHING ON THE RT ENG. FIRST OFFICER CALLED THE ABORT AT 100 KTS AFTER SEEING ALL OIL QTY GONE & DASHES ON THE N1. THERE WAS SMOKE IN THE CABIN AT THE TIME OF THE EVENT. THE CREW DECLMar 5, 2016 · N403NV · Doug MD88 · Engine (Turbine/Turboprop)SDR WX0A2016030173094Engine · failedON TAKEOFF ROLL AT ABOUT 20 KIAS AT 1.86 EPR LT ENG BEGAN TO COMPRESSOR STALL. R & R NR 1 ENG IAW WO 289702 OPERATIONS, LEAK CHECK & TRIM CHECKED OK. REFER TO TC 71-080-003, TC 71-070-001, M739 FOR INDIVIDUAL SIGN OFFS. RECORDS TRACKING ENTRY.Feb 28, 2016 · N405NV · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2016030173096Moisture Trap · unsecureRIGHT ENG SLOW TO SPOOL ON TAKEOFF & INFLIGHT RT ENG LAGS. 7 - 10 SECONDS BEHIND RT ON TAKEOFF. IN AIR LAGS ENOUGH TO CREATE YAW BY LT ENG SPOOLING UP FASTER. PERFORMED TROUBLESHOOTING FOR SLOW ACCELERATION IAW AMM 72-00-04. FOUND FWD MOISTURE TRAP IMPROPEFeb 28, 2016 · N419NV · Doug DC983 · Fuel Controlling SystemSDR DALA2016012700662Isolator · corrodedCORROSION ON INNER SURFACE OF HOUSING BOLTS ON RT ENGINE AFT VIBRATION ISOLATOR. ON RT ENGINE AFT VIBRATION ISOLATOR WAS CLEANED AND CORROSION WAS FOUND. DUE TO CORROSION REPLACED AND INSTALLED IAW AMM 71-20-02-201 AND PS 900-1-2-1, NR 01.Jan 26, 2016 · N990DL · Doug MD88 · Engine Mount SectionSDR AALA20160121009Moisture Trap · contaminatedAIRCRAFT WAS GNDED. RT ENG WOULD NOT REACH TAKEOFF POWER. TAKE OFF ABORTED AT APPROX 100 KNOTS. CLEANED & PURGED THE RT ENG PT7 MANIFOLD MOISTURE TRAP. R & R THE RT ENG EPR TRANSMITTER IAW AMM 77-11-02. OPERATIONAL & LEAK CHECKED GOOD. ACCOMPLISHED MCM CJan 21, 2016 · N967TW · Doug DC983 · Engine Pressure Ratio (EPR)SDR AALA20160103002Battery Pack · dischargedAIRCRAFT WAS NOT GNDED. DURING TAXI FROM HANGAR 2 TO HANGAR 1, TAXI CREW REPORTED THAT THE CEILING EMER EXIT LIGHT OVER THE OVERWING EMER EXIT WILL NOT EXTINGUISH. R & R EMER LIGHT BATTERY PACK B5-104. OPERATIONAL CHECKED NORMAL IAW AMM 33-53-00.Jan 3, 2016 · N9626F · Doug DC983 · Emergency LightingSDR WX0A2016010473061Engine · failedFLIGHT 145 WAS AT CRUISE AT FL330. THEY HEARD A BANG & FELT A SHUDDER IN THE ACFT. THEY WATCHED THE RT ENG INDICATIONS ROLL BACK AS THE ENG SHUTDOWN & RT ENG EGT MAXED OUT AT 800 DEGREES. DECLARED AN EMER & STARTED A DESCENT WITHIN LESS THAN A MINUTE OF THEJan 2, 2016 · N875GA · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2015123173057Engine · failedACFT HAD A SUDDEN ENG FAILURE AT CRUISE AT FL320. AN EMER WAS DECLARED, THE ENG WAS SECURED & THE CREW LANDED. THE PAXS DID NOT BRACE. THIS ACFT WAS ABOUT 500 POUNDS OVERWEIGHT FOR THE LANDING. THE RT ENG SPOOLED DOWN WITHOUT ANY WARNING. THE ONLY OTHER CDec 31, 2015 · N405NV · Doug DC983 · Engine (Turbine/Turboprop)SDR DALA2016010100017Engine · malfunctionedFAS IN AFT CABIN REPORTED POPS FROM LT ENGINE AT TAKEOFF POWER. REPLACED NR 1 ENGINE IAW 88-7110-9-0010.Dec 30, 2015 · N942DL · Doug MD88 · Engine (Turbine/Turboprop)SDR DALA2015123007757Hub · damagedNR 1 AND NR 2 ENGINE N1'S WENT TO 103 PERCENT FOR 7 SECS. DURING LOW ALTITUDE GO AROUND. REPLACED NR 2 ENGINE HUB IAW SPC 03-7201-9-0016. REPLACED NR 1 ENGINE HUB IAW SPC 03-7201-9-0016.Dec 29, 2015 · N970DL · Doug MD88 · Turbine Engine Air Inlet SectionSDR WX0A2015121800046Oil System · leakingAFTER TAKEOFF. LAVATORY SMOKE ANNUNCIATOR ILLUMINATED FOR FWD LAVATORY DURING QRH CHECKLIST, ANNUNCIATOR EXTINGUISHED. IN COCKPIT ODOR OF EVAPORATING OIL NOTED. TROUBLESHOOTING ACCOMPLISHED ON LP 610870 & 610871, LT ENG REPLACED IAW WO 279553. ENG RUNS ACCODec 15, 2015 · N403NV · Doug MD88 · Turbine Engine Oil SystemSDR AALA20151119013Pressure Switch · failedLEFT ENG OIL STRAINER LIGHT FLICKERED, THEN CAME ON CONTINUOUSLY AFTER TAKEOFF. THE LT ENG WAS BROUGHT BACK TO IDLE. OIL PRESS, TEMP, & QTY NORMAL. EMER WAS DECLARED & FLIGHT RETURNED WITHOUT FURTHER INCIDENT. LT ENG WAS SHUT DOWN ON TAXI IN. ACFT REMOVEDNov 19, 2015 · N483A · Doug DC982 · Engine Oil PressureSDR AALA20151118002Tube · blownRETURNED, RT ENG FIRE HANDLE ILLUMINATED ALONG WITH AURAL WARNING ON CLIMB OUT. AN EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. FOUND ANTI-ICE TUBE ON TOP OF RT ENG BLOWN. REPLACED RT ENG ANTI-ICE DUCT Nov 17, 2015 · N9617R · Doug DC983 · Engine Anti-Icing SystemSDR AALA20151116007Start Valve · faultyFLIGHT DIVERTED, RT ENG START VLV LIGHT ILLUMINATED IN FLIGHT. CREW SHUTDOWN RT ENG. SINGLE ENG TIME WAS 15 MINUTES. AN EMER LANDING WAS DECLARED. LANDING UNEVENTFUL. THE ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED MCM PROCEDURES ON MEL 80-01, DEFERRED RNov 16, 2015 · N9617R · Doug DC983 · Engine Start Valves/ControlsSDR WX0A2015111172992Sense Line · disconnectedDURING CLIMB, WE HAD A FULL THROTTLE SPLIT WITH THE THROTTLE UP. TURNED ON ANTI-ICE & THE RT EPR & N1 DROPPED SIGNIFICANTLY. WE ACCOMPLISHED QRH 72.10 FOR, EPR ERRATIC. WE CONTINUED CLIMB WITH ANTI-ICE ON, EPR LT 1.98, RT .98, LT NI 90, RT 90, EGT LT 490, RNov 10, 2015 · N410NV · Doug DC983 · Fuel Controlling SystemSDR AALA20151110012Compressor · stalledAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. NR 2 ENG EXPERIENCED COMPRESSOR STALLS IN FLIGHT. POWER REDUCED TO IDLE FOR DESCENT & LANDING. ENG NOT SHUT DOWN. R & R NR 2 ENG IAW MCM 71-91-99. PERFORMED OPERATIONAL CHECK OF NR 2 Nov 10, 2015 · N9401W · Doug DC983 · Turbine Engine Compressor SectionSDR WX0A2015110872990Oil Cooler · leakingAT CRUISE NORMAL INDICATIONS, FELT A THUD & THE AP KICKED OFF. CAPT HAND FLEW THE ACFT FOR A FEW MINS & TURNED THE AP BACK ON. 10 MINUTES LATER, THE 40 PSI OIL PRESS LIGHT WAS ON FOR THE RT ENG. STARTED, QRH 72.14, BEFORE FINISHING NOTICED THE RT ENG OIL PRNov 5, 2015 · N418NV · Doug DC983 · Engine Oil CoolerSDR AALA20151021017Bleed Valve · malfunctionedRETURNED, ACCOUNT LT ENG COMPRESSOR STALL ON CLIMB OUT. EMER LANDING WAS DECLARED, UNEVENTFUL LANDING. ACFT REMOVED FROM SERVICE. REPLACED LT ENG PRBC IAW MM 75-31-01. ENG OPERATIONS CHECKED NORMAL.Oct 21, 2015 · N9401W · Doug DC983 · Compressor Bleed ValveSDR WX0A2015011273062Engine · failedDURING TAKEOFF ROLL, HEARD LOUD BANGING NOISE, RT ENG WITH STRONG VIBRATION & ACFT SHUDDER. ABORTED TAKEOFF AT 110 - 120 KTS. IT WAS REPORTED THAT THE RT ENG WAS SMOKING, PULLED FIRE HANDLE & BLEW ONE BOTTLE. NO EMER DECLARED & PAXS WERE NOT EVACUATED USINGOct 11, 2015 · N408NV · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2015101272932Cowling · crackedNUMBER 2 ENG, LOWER FWD COWL DISBONDED & CRACKED. REPLACED FWD LOWER NR 2 ENG COWL IAW AMM 71-10-03-2-1.Oct 8, 2015 · N401NV · Doug MD88 · Engine Cowling SystemSDR 2WAA20150930001Engine · failedRIGHT ENGINE FAILURE AFTER TAKEOFF. EVENT HAPPENED ABOUT 1000 FT. ENGINE MADE A LOUD BANG, SUSPECTED CATASTROPHIC FAILURE. THRUST LOST IMMEDIATELY. R & R RT ENGINE. ACCOMPLISHED LEAK CHECK AND RUN-UP, NO LEAKS NOTED. CHECKED NORMAL IAW T/C 71-900-01-01 ANSep 30, 2015 · N802WA · Doug DC983 · Engine (Turbine/Turboprop)SDR AALA20150922009Switch · faultyAFTER TAKEOFF, CLIMBING THROUGH 15,000 FT, RECEIVED RT ENG OIL FILTER CLOG INDICATION. ALL ENG PARAMETERS WERE NORMAL. IAW QRH, ENG WAS RETARDED TO IDLE FOR LANDING. EMER DECLARED, RETURNED & LANDED UNEVENTFULLY. ACFT WAS REMOVED FROM SERVICE. RT ENG STRASep 22, 2015 · N9617R · Doug DC983 · Engine Oil TemperatureSDR WX0A2015092472884Engine · malfunctionedDURING CLIMB OUT IN CALM CLEAR AIR, FELT A HEAVY VIBRATION THROUGHOUT THE ENTIRE ACFT, IT ONLY LASTED A FEW SECONDS. R & R NR 2 ENG IAW TC 71-080-003. ACFT OK FOR SERVICE.Sep 19, 2015 · N423NV · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2015092872896Engine · making metalRIGHT OIL STRAINER CLOGGING ANNUNCIATORS ILLUMINATED IN FLIGHT. FOLLOWED QRH 72.16, DIVERTED IAW QRH INSTRUCTION. FOUND METAL IN THE OIL, REPLACED NR 2 ENG IAW TC 71-080-003. REF LOG PAGE 576743.Sep 19, 2015 · N423NV · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2015091472857Seal · leakingNUMBER 2 ENG OIL QTY DROPPED FROM 13QTS TO 9QTS IN FLIGHT. FOUND STARTER DRIVE OIL SEAL LEAKING. R & R STARTER DRIVE OIL SEAL IAW AMM 72-61-59. LEAK CHECKED GOOD. ALSO SEE LG PG 495225.Sep 10, 2015 · N408NV · Doug DC983 · Turbine Engine Oil SystemSDR DALA2015090105376Flange · crackedFOUND A CRACK ON FLANGE J1 AT RT ENGINE 6 RT SIDE POSITION. THE ENGINE WAS REPLACED.Aug 31, 2015 · N910DL · Doug MD88 · Turbine Engine Compressor SectionSDR WX0A2015082472824Engine · overtempCLIMBING OUT OF 16,000 FEET THE CREW NOTICED THAT THEY HAD AN INDICATION OF OIL TEMP HIGH ON THE NR 1 ENG. THE OIL TEMP WAS 145 & THE FUEL TEMP WAS 99. THE AUTO FUEL HEAT SYS WAS ON, BUT HEAT WAS NOT BEING APPLIED AT THE TIME. THE CREW DID THE QRH PROCEDUREAug 17, 2015 · N403NV · Doug MD88 · Engine (Turbine/Turboprop)SDR WX0A2015081672808Pressure Switch · faultyDURING CLIMB, LT INLET PRESS LOW LIGHT FLICKERED SEVERAL TIMES. AFTER LEVELING OFF, IT CONTINUED TO FLICKER & LT MAIN TANK FEED DOWN TO 8300. IAW QRH TURNED OFF LT MAIN TANK PUMP & LT MAIN TANK QTY STILL DECREASED TO 8200, LIGHT CONTINUED TO FLICKER, TURNED Aug 14, 2015 · N881GA · Doug DC983 · Fuel Pressure SensorSDR WX0A2015081172786Bolt · looseOIL QTY DECREASED FROM 9 QTS TO 5 QTS DURING CLIMB. PERFORMED EQRH 72.15. OIL STABILIZED AT 5 QTS LANDED WITH 4 QTS. FOUND LOOSE BOLTS IAW ON NR 4 BEARING OIL BREATHER TUBE ATTACH POINT UPSTREAM. SECURED BOLTS IAW AMM 79-20-02-2-0 10 B. LEAK CHECKED GOOD Aug 8, 2015 · N406NV · Doug DC983 · Engine Oil Distribution (Airframe Furnished)SDR WX0A2015081172784Engine · overtempRIGHT ENG EGT ON TAKEOFF WAS 635 C FOR 20 SECONDS, OAT 41 C, EPR 1.93. R & R RT ENG IAW TASK CARD 71-080-003. OPERATIONS & LEAK CHECKED GOOD.Aug 4, 2015 · N422NV · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2015080372779Engine · vibrationAT CRUISE 31 ENGINE VIBRATION OCCURRED & IFSD WAS CONDUCTED. FLIGHT CREW REPORTED A RUBBER ODOR & SUSPECTED THE AUTO THROTTLE CLUTCHES. AFTER AUTO THROTTLES WERE TURNED OFF, THE ODOR DISSIPATED, BUT THE NR 1 ENG BEGAN TO VIBRATE HEAVILY. THE ENGINE WAS SHUTAug 3, 2015 · N874GA · Doug DC983 · Engine (Turbine/Turboprop)SDR 2WAA20150801001Engine · bird ingestionBIRD STRIKE, NORMAL INDICATIONS. DURING CRUISE LEFT ENGINE FLUCTUATIONS. PRECAUTIONARY SHUTDOWN. REMOVED NR 1 ENG SN 709818 IAW WAA TC 71-900-01-01. INSTALLED NR 1 ENG SN 717360 IAW WAA TC 71-900-01-01. LEAK CHECK GOOD PENDING OPERATIONS CHECK. TRIM & RUNAug 1, 2015 · N802WA · Doug DC983 · Engine (Turbine/Turboprop)SDR AALA20150727008Oil Cooler · faultyAT LEVEL OFF, DURING CLIMB LT CSD OIL PRESSURE LOW LIGHT ILLUMINATED ACCOMPANIED BY HIGH CSD TEMP INDICATION. DIVERTED, AND LANDING UNEVENTFUL. APU PREVIOUSLY PLACARDED OUT OF SERVICE. R & R LT CSD IAW AMM 24-10-01 & LT CSD OIL COOLER IAW AMM 24-10-03. PEJul 23, 2015 · N965TW · Doug DC983 · Alternator-Generator DriveSDR 2WAA20150709001Structure · damagedBIRD STRIKE ON T/O, LOSS OF AIRSPEED ON RT SIDE INTERMITTENT ON LT SIDE AIRSPEED. FOUND EVIDENCE OF BIRD STRIKE AT RADOME, PITOT TUBES, WING L/E. INSPECTED AND CLEANED AREAS IAW AMM 12-22-01. NO DENTS OR DEFECTS NOTED. OVERWEIGHT LANDING, OVER BY 200 LBS. AJul 9, 2015 · N804WA · Doug DC983 · Standard Practices/StructuresSDR WX0A2015070672714Line · defectiveDURING DECENT, THROUGH ABOUT 20,000 FEET POWER AT IDLE, RT OIL PRESS LOW CAME ON THE OAP NR 2 ENG OIL PRESS INDICATED 34 PSI, OIL QTY INDICATED 0. COMPLIED WITH QRH 72.14. OIL PRESS CONTINUED TO DECREASE TO 18 PAI AT TIME SHUTDOWN WITH AN OIL TEMP OF 114. CJun 30, 2015 · N425NV · Doug DC983 · Engine Oil Indicating SystemSDR WX0A2015061972669Engine · overtempON TAKEOFF NR 1 ENG OVER TEMP, 632 EGT FOR 25 SECONDS EPR 1.91 OAT 42C N1 92 N2 95 MAX POWER PACK ON. REF WO 00259024. R & R LT ENG. ACFT OK FOR SERVICE.Jun 15, 2015 · N886GA · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2015081272792Engine · overtempON TAKEOFF LT ENG EGT 636 FOR APPROX 9 SEC N1 94% N2 97 & EPR 1.98 OAT 34C OIL TEMP WENT TO 136 DEGREE. DURING THE TAKEOFF ROLL THE CREW NOTED THE EGT ON THE LT ENG WENT TO 636 C FOR 9 SECONDS. THIS ACFT WAS ALREADY ON THE MTO PROGRAM & AT THIS TEMP IT WILL Jun 12, 2015 · N886GA · Doug DC983 · Engine (Turbine/Turboprop)SDR DALA2015061103670Compressor · stalledTHE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AFTER TAKEOFF. THE NR 1 ENGINE WAS SHUTDOWN AND AN AIR TURNBACK WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 ENGINE AND THE ACFT HAS RETURNED TO SERVICE.Jun 10, 2015 · N918DE · Doug MD88 · Turbine Engine Compressor SectionSDR AALA20150609001Probe · obstructedDURING TAKEOFF, RT ENG WOULD NOT MAKE TAKEOFF POWER. MAXIMUM EPR WAS 1.73. TAKEOFF ABORTED AT LESS THAN 60 KNOTS. REMOVED DEBRIS FROM LT ENG PT 2 PROBED. PERFORMED ENG RUNS AT ALL POWER SETTINGS IAW AMM 71-00-00. SYS CHECKED NORMAL.Jun 8, 2015 · N967TW · Doug DC983 · Engine Pressure Ratio (EPR)SDR AALA20150605014Fuel Control · faultedDURING TAKEOFF, LT ENGINE EPR INDICATION WAS ERRATIC. TAKEOFF ABORTED AT APPROXIMATELY 70 KNOTS. R & R FUEL FLOW CONTROL IAW CARD 73-91-99 & ENG FUEL PUMP IAW CARD 73-94-03. ACCOMPLISHED ENG PARAMETERS CHECK IAW CARD 71-91-20. SYS CHECKED NORMAL.Jun 5, 2015 · N9404V · Doug DC983 · Engine Pressure Ratio (EPR)SDR WX0A2015061072643Fuel Control · malfunctionedDURING DECENT, IDLE POWER, RT ENG HAS HIGHER POWER SETTING THAN LT. PARAMETERS AT 15,000 DESCENDING, RT EPR 1.113 N1 61% EGT 323 N2 78% FF 2110 & LT EPR 0.93 N1 41% EGT 295 N2 67% FF 910. R & R RT ENG FUEL CONTROL IAW MM 73-20-01. OPERATIONS & LEAK CHECKED Jun 5, 2015 · N875GA · Doug DC983 · Fuel Control/Turbine EnginesSDR AALA20150518012Engine · fodDURING CLIMB, FLIGHT CREW REPORTED HOT PLASTIC, VARNISH ODOR & SMOKE IN COCKPIT. TURNED OFF RECIRCULATION FAN & SMOKE DISSIPATED. ATTEMPTED PACK BURNOUT PROCEDURE IAW AMM 21-20-02-201 DURING WHICH BLACK SMOKE & SPARKS WERE OBSERVED EXITING NR 1 ENGINE TAIL CMay 18, 2015 · N966TW · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2015051172581Inlet Bullet · dentedLEFT ENG INLET BULLET HAS TWO SMALL DENTS. R & R LT ENG INLET BULLET. NO DEFECTS NOTED IAW MM 71-10-02.May 9, 2015 · N414NV · Doug MD88 · Turbine Engine Air Inlet SectionSDR WX0A2015051172585Engine · malfunctionedNUMBER 1 ENG DISPLAYED LOW OIL PRESS & ZERO OIL QTY. WE SHUT NR 1 ENG DOWN AS INSTRUCTED BY CHECKLIST. WE LANDED WITH NO OTHER FAILURES. CRUISE POWER SETTING ALTITUDE 32000, OIL QTY 0, 20 PSI TO 0, AFTER 10 - 15 MIN 0 PSI INDICATED, APPROX 20 - 30 MIN TT. May 7, 2015 · N873GA · Doug DC983 · Engine (Turbine/Turboprop)SDR WX0A2015050872568Unknown · vibrationAFTER TAKEOFF, FLIGHT ATTENDANT 2 & 4 REPORTED A RUBBER ODOR, BUT DISSIPATED. APPROX 40 MINUTES INTO FLIGHT, FLIGHT ATTENDANTS REPORTED EXCESSIVE NOISE & VIBRATION FROM ROW 33 & PROGRESSED AFT. ENG PARAMETERS WERE NOTED ON TREND AFTER AUTO-THROTTLES WERE TURApr 30, 2015 · N405NV · Doug DC983 · Fuselage Structure (General)
Back to Pratt & Whitney JT8D-219