Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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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 = 'JT8D15'
  ORDER BY difficulty_date DESC"

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SDR DHL2005746005Light · looseCABIN DOOR EMERGENCY LIGHT CAME ON AFTER T/O AND STAYED ON. RESECURED AND TESTED EMERGENCY LIGHT IAW MM CHP 33-50-01. OPS CK NORMAL AT THIS TIME.Dec 7, 2005 · N746DH · Boeing 727224 · Emergency LightingSDR AU510001874Support Fitting · crackedLT AND RT ENGINE FORWARD SUPPORT FITTING ASSEMBLIES CRACKED. LT PYLON FITTING CRACKED AT HOLE `F`. RT PYLON FITTING CRACKED AT HOLE `P`. FOUND DURING INSPECTION IAW AD/B727/151 AND BOEING SB 727-54A0010.Dec 7, 2005 · Boeing 727277 · Nacelle/Pylon, Attach FittingsSDR 05FDEA04156Floor Support · corrodedCORROSION BS 297-304, WL 208, LBL 12-14. UPPER FLANGE OF FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT BS 294-BS312 IAW SRM 51-30-2, SRM 51-10-2.Dec 6, 2005 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 05FDEA04158Floorbeam · gougedCORROSION BS 304, WL 280, LBL 14 GOUGE ON TOP FLANGE, FLOORBEAM. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-2 AND SRM 51-10-2.Dec 6, 2005 · N490FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA04159Strap · corrodedCORROSION ON TENSION STRAP BS 1070 RBL 45 WL 201. REPAIRED TENSION STRAP IAW SRM 53-10-8 FIG 6.Dec 6, 2005 · N490FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR GAIA05035OPConnector · dirtyDURING APPROACH, INITIAL GEAR EXTENSIO, NOSE GEAR INDICATOR (NOT SAFE), AFTER RECYCLE AND A SHORT DELAY INDICATION NORMAL. LANDING WAS MADE WITHOUT INCIDENT. CLEAN AND RESEATED NOSE GEAR CONNECTOR PLUGS. INSPECTED NOSE GEAR AREA. NO DEFECT NOTED. CHECKED Dec 6, 2005 · N281KH · Boeing 7272J0 · Landing Gear System WiringSDR C8GA20050024Door · openDURING CLIMBOUT OPERATION, AIRCRAFT WOULD NOT PRESSURIZE ABOVE 1.5 PSID. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND L1 ENTRY DOOR NOT FULLY CLOSED, OPEN, CYCLED AND RESET DOOR, CONFIRMED FULLY CLOSED AND LOCKED. NO DEFECTS NOTED. AIRCDec 2, 2005 · N708AA · Boeing 727223 · Passenger/Crew DoorsSDR ABXA050321Pan · crackedFORWARD LOWER CARGO DOOR PAN CRACKED AT AFT HOLD OPEN FITTING. REPAIRED CRACKED DOOR PAN IAW SSRM K05159.Dec 2, 2005 · N963AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050320Retainer · crackedCRACKS NOTED ON X-RAY INSPECTION AT CAPTAIN'S OVERHEAD WINDOW RETAINER. REMOVED AND REPLACED CRACKED DOUBLER IAW SRM 51-30-2.Dec 1, 2005 · N963AX · Doug DC941 · Flight Compartment WindowsSDR GAIA05034OPEngine · leakingDURING TAKEOFF ROLL THE COCKPIT FILLED WITH SMOKE. TAKEOFF WAS ABORTED AND THE AIRCRAFT TAXIED TO THE RAMP. INVESTIGATION FOUND OIL IN THE NR1 ENGINE BLEED SADDLE DUCTS. ENGINE REMOVED, AIRCRAFT PARKED. (K)Nov 29, 2005 · N278US · Boeing 727251 · Engine (Turbine/Turboprop)SDR ABXA050319Fitting · crackedRT FORWARD OVERWING EXIT DOOR HAD A CRACKED FITTING AT FORWARD LOWER CORNER. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING IAW SRM 57-30-5 AND 51-30-2.Nov 28, 2005 · N963AX · Doug DC941 · Emergency ExitsSDR DHL2005753003Battery · dischargedEMERGENCY EXIT LIGHTS, BATTERY LOW. REPLACED BATTERIES. EMERGENCY EXIT LITES ILLUMINATED- SERVICEABLE REF. 33-26-00, P/N 87067-001.Nov 24, 2005 · N753DH · Boeing 727223 · Emergency LightingSDR A0512001Jackscrew · failedON APPROACH, WITH FLAPS SELECTED TO 5 DEG, STAB TRIM WHEEL RAN AWAY FROM APPROX 5 UNITS NOSE UP TO 0 DEG AND BUFFETING WAS FELT IN FLT CONTROLS. AC STARTED A 2000 TO 4000 RPM RATE OF DESCENT, PILOTS TRIED TO INPUT UP ELEVATOR TO ARREST SINK RATE, THERE WAS NONov 22, 2005 · N720CK · Boeing 727200 · Flight Control SystemSDR PCSA11190501Flow Valve · defectiveON CLIMBOUT, CREW REPORTED PRESSURIZATION SYSTEM WILL NOT MAINTAIN CABIN ALTITUDE. AIRCRAFT RETURNED BACK TO DEPARTURE AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT PRESSURIZATION SYSTEM AND FOUND FLOW CONTROL AND MODULATING VALVE AT FAULT, Nov 19, 2005 · N994AJ · Boeing 727233 · Cabin Pressure Control SystemSDR CA051110002Engine · surges(CAN) AIRCRAFT EXPERIENCED NR 2 ENGINE SURGE DURING TAKEOFF ROLL. SEVERE CROSSWINDS WERE EXPERIENCED WHICH WILL CAUSE THIS ENGINE SURGE. DUE TO THE CROSSWINDS AND THEN INTERRUPTION OR DISTURBANCE OF AIRFLOW THRU THE AIR INTAKE.Nov 10, 2005 · Boeing 727247 · Turbine Engine Air Inlet SectionSDR DHL2005747001Wire · chafedNR 1 GEN FAILED ON T/O ROLL DISCONECTED CSD RTO INFO OAT 16 C PA 4300 SPEED 45 KNOTS MODERATE BREAKING A/C WEIGHT 131,400 REV. THRUST MODERATE. DEFERRED IAW MEL 24-1CAT B CONTROL NR 23128 MC INATALS KPS. TRANSFERED TO DMI GREEN SHEET. C/W SPECIAL PROCEDURNov 8, 2005 · N747DH · Boeing 727224 · Electrical Power System WiringSDR 0501599943Engine · smokeAFTER TAKEOFF FLIGHT ATTENDANTS AND PASSENGERS COMPLAINED OF SMOKE IN THE CABIN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT. MAINTENANCE REPLACED ENGINE NR 1.Nov 6, 2005 · N1308T · Doug DC931 · Engine (Turbine/Turboprop)SDR GAIA05029OPLight · inoperativeDURING A-CHECK FOUND L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT AT L1 DOOR. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K)Nov 2, 2005 · N281KH · Boeing 7272J0 · Emergency LightingSDR 05FDEA03457Floorbeam · corrodedMAIN CARGO COMP FLOORBEAM CORRODED, STA 344 FROM LBL36 TO RBL18. REMOVED, FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED FLOORBEAM REPAIR AT STA 344 FROM LBL36 TO RBL18 ALL IAW SRM 51-30-2, 51-10-2, 51-20-031-7 AND SRZ SR27-53-007.**S/D COMING**Oct 20, 2005 · N223FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 05FDEA03459Access Door · out of positionA/C TOOK OFF AND RETURNED TO GATE. FLT CREW SAID THE A/C WOULD NOT PRESSURIZE. MAIN ENTRY DOOR WAS CLOSED DOOR WAS JAMMED WOULDN'T OPEN. REMOVED DOOR SLIDE DOOR TRIM FOUND THE AFT ROLLERS WERE NOT IN THE ROLLER GUIDES OR IN THE CAMS. FOUND SOLID BULKHEAD AOct 20, 2005 · N466FE · Boeing 727200 · DoorsSDR 05FDEA03451Skin · dentedEXTERNAL FUSELAGE SKIN IS DENTED AT RT STA 495 AND STRINGER 20R. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR ON FUSELAGE EXTERNAL SKIN FROM STA 480 TO 540 FROM STRINGER 20R TO 23R ALL IAW SRM 53-30-1,53-30-2 FIG 2,53-30-3 FIG 3,51-30-2 AND 51-1Oct 19, 2005 · N265FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR TSAA0532049Brake · inoperativePILOTS OBSERVED BOTH ANTI-SKID LIGHTS CAME ON IN FLIGHT ONLY WHEN THE LANDING GEAR IS IN THE (OFF) POSITION; LANDED WITH NO DIFFICULTIES. REMOVED AND REPLACED PARKING BRAKE SHUTOFF VALVE ASSEMBLY. MAINTENANCE ALSO FOUND A BAD NR 4 TRANSDUCER AND CURRENTLY WAOct 18, 2005 · N805AL · Boeing 7372M6C · Landing Gear Brake SystemSDR 2005FA0001450Seal · wrong partINCORRECT SEAL INSTALLED ON PRE-ASB6169 FUEL NOZZLES, PT NR 809137-01, SEAL NR 814352 INSTALLED, CORRECT SEAL FOR PRE ASB6169 IS NR 775723. (K)Oct 12, 2005 · Fuel Injector NozzleSDR AU510001461Line · damaged(AUS) HYDRAULIC PIPES PNO 65-17849-61 AND PNO 65-17849-4014 RUBBING TOGETHER CAUSING ONE PIPE TO BE HOLED. LOSS OF HYDRAULIC FLUID. INVESTIGATION FOUND A FAILED `P` CLIP ON ONE OF THE PIPES WHICH ALLOWED THE PIPES TO RUB TOGETHER.(OTHER CAUSE: AGE ) (CASA# 510Oct 6, 2005 · Boeing 727277 · Hydraulic System, MainSDR DHL2005743002Switch · out of adjustAFT AIRSTAIR AMBER LIGHT ON S/O PANEL ILLUMINATES INTERMITTENTLY. ADJUSTED AFT AIRSTAIR UP SWITCH, OPS CHECK GOOD IAW M/M 52-62-01.Oct 5, 2005 · N743DH · Boeing 727225 · Entrance StairsSDR 05FDEA02600Frame · damagedPILOT HOLES NEXT TO FASTENER HOLES IN STUB FRAME BS 610 STR3L. REPAIRED FRAME PER FED-EX EA 7-5330-92328. [CLOSED]Aug 23, 2005 · N218FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA02601Frame · damagedN01449, WHILE WORKING EA 7-5330-72293B PT 2, FOUND DOUBLE HOLE IN FRAME AT 620 LBL 21 WL 302. REPAIRED DOUBLE HOLE IN FRAME, BS 620, LBL 21 PER FED-EX EA 7-5330-92327.Aug 23, 2005 · N218FE · Boeing 727200 · Fuselage Main, FrameSDR SROM200500014Skin · gougedDURING ROUTINE INSPECTION FOUND A GOUGE IN THE SKIN AT BS 1036.5, STR 8L. REPAIRED IAW MFG MESSAGE 1-115922448-4 AND SRM 53-30-3, FIG. 50. BLENDED, REMOVED DAMAGE, EDDY CURRENT INSPECTED FOR CRACKS AND INSTALLED AN EXTERNAL DOUBLER IAW MESSAGE AND SRM REFEREAug 21, 2005 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR 05FDEA02478Engine · failedDURING CLIMBOUT S/O NOTICED RT MANIFOLD DROP TO ZERO. THIS WAS FOLLOWED BY NR 3 STRUT OVERHEAT LIGHT & ACRID SMELL. FOLLOWED QRH TO NR 3 ENGINE SHUTDOWN & EMERGENCY RETURN TO ONT. 20 MIN ENGINE WINDMILLING. STRUT EXTINGUISHED AFTER ABOUT 3 MINUTES. (OPEN)Aug 16, 2005 · N241FE · Boeing 727200 · Engine (Turbine/Turboprop)SDR CA050819003Regulator · unserviceable(CAN) AIRCRAFT EXPERIENCED LOSS OF NR 1 GENERATOR SYSTEM ON APPROACH. THE FLAP INDICATION SYSTEM INDICATED A FLAP OUT OF ASYMMETRIC CONDITION CA USING THE CREW TO ABORT THE LANDING AND DECLARE AN EMERGENCY. THE AIRCRAFT LANDED SAFELY ON SECOND APPROACH AND TAXAug 16, 2005 · Boeing 727247 · AC RegulatorSDR C8GA20050018Adc · inoperativeON TAKEOFF ROLL, FO AIRSPEED INDICATION INOPERATIVE. FLAG CAME OUT AFTER STOP. CLEANED NR 2 ADC CONNECTOR PLUG AND RERACKED ADC. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Aug 15, 2005 · N899AA · Boeing 727223 · Air Data ComputerSDR DHL2005748501Vertical Beam · crackedVERTICAL BEAM AT BS1183 RBL 36.WL 240, APPROX, SHOWS CRACK AT CHORD ANGLE. STOP DRILLED CRACK IAW SRM 51-10-1,LOCATED,DRILLED AND INSTALLED REPAIR KIT P/N 65C34406-15,PO NR 531481 IAW S/B 727-53-0192 REV 1,MAY 30,1991.Aug 15, 2005 · N748DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2005748599Vertical Beam · crackedVERTICAL BEAM AT BS.1183, RBL 36, WL 240, APPROX, SHOWS CRACK AT CHORD ANGLE. STOP DRILLED CRACK IAW SRM 51-10-1,LOCATED,DRILLED AND INSTALLED REPAIR KIT P/N 65C34406-15,PO NR 531481 IAW S/B 727-53-0192 REV 1,MAY 30,1991Aug 15, 2005 · N748DH · Boeing 727225 · Fuselage Main, StructureSDR CA050815005Fan · vibration(CAN) NOTICED, FELT VIBRATION ON INITIAL CLIMB OUT BELOW 10000 FT, BROUGHT UP ENG PARAMETERS ON MFD/VIB AT 3.5/ADVSD MTC. CONTROL/VIB. INCREASED GRADUALLY TO EXCEED 4.0 THROUGH 20000 FEET. AIRCRAFT RETURNED TO DEPARTURE. ENGINE FAN BLADES WERE RE-INSTALLED. AAug 8, 2005 · Boeing 737204 · Turbine Engine Compressor SectionSDR CA050722007Tube · chafedAIRCRAFT WAS 20 MINITES OUT WHEN THE NUMBER 3 ENGINE OIL LEVEL STARTED TO DROP. THE ENGINE OIL LEVEL WAS MONITORED BY THE F/E AND THE ENGINE WAS NOT SHUT DOWN. THE AIRCRAFT LANDED SAFELY WITH NO PROBLEMS AND THE ENGINE WAS SHUT DOWN AFTER LANDING. MAINTENANCJul 22, 2005 · Boeing 727247 · Engine Oil Distribution (Airframe Furnished)SDR C7WA200500109Connector · looseAIR TURNBACK; ENGINE SHUTDOWN, NR 2 EGT FLUCTUATES AT FLIGHT LEVEL 27,000. OIL PRESSURE DROPPED TO ZERO, OIL QUANTITY FOLLOWED TO ZERO. DURING INSPECTION OF NR 2 ENGINE FOUND INLET CASE TUBE CONNECTOR ASSEMBLY LOOSE AND LEAKING. TIGHTENED LOOSE BOLTS. LEAJul 12, 2005 · N742RW · Boeing 7272M7 · Turbine Engine Oil SystemSDR 05FDEA01759Transmitter · malfunctionedON TAKEOFF WITH STANDARD EPR SET NR3 N1,N2 AND FUEL FLOW WERE LOW. AC RELEASED FOR SERVICE IAW MEL/CDL: 77-01-01 01JUL05 14:55 ORF REMOVED PT2 SENSOR FROM ENG, BLEW AIR THROUGH LINE TO INSURE NO OBSTRUCTIONS PRESENT. RE-INSTALLED SAME. DISCONNECTED NR3 Jul 1, 2005 · N465FE · Boeing 727200 · Power Indicating SystemSDR 05FDEA01767Compressor · stalledON TAKEOFF ROLL THROTTLES SMOOTHLY ADVANCED TO T/O PWR NR 2 ENGINE HAD AVERY PRONOUNCED COMPRESSOR STALL APPROX. 5-8 SEC. INTO TAKEOFF ROLL REJECTED T/O AND CLEARED RUNWAY. INSPECTED INLET AND EXHAUST NO DAMAGE NOTED. PERFORMED TAKEOFF POWER EPR TEST REF Jun 30, 2005 · N488FE · Boeing 727200 · Turbine Engine Compressor SectionSDR CA050610005Warning Light · illuminated(CAN) A/C WAS IN CRUISE WHEN THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CHECKLIST WAS ACCOMPLISHED, POWER LEVER RETARDED, AND OIL PRESSURE DECREASED WITH POWER DECREASE. LOW OIL PRESSURE LIGHT CAME ON AND ENGINE WAS SHUTDOWN. A/C CONTINUED TO DESTIJun 9, 2005 · Boeing 737204 · Turbine Engine Oil SystemSDR CA050620002Bolt · loose(CAN) ON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND AIR/GND PROX TARGET LEVER BOLT LOOSE. BOLT/NUT- P/N NAS 1303-8/BACN10JC3.May 31, 2005 · Boeing 727243 · Landing Gear Position and WarningSDR CA050602008Actuator · inoperative(CAN) ON CLIMB OUT, CREW NOTICED THAT THE NR 1 KRUGER FLAP WOULD NOT RETRACT. THE CREW LEFT THE FLAPS IN THE DOWN POSITION AND RETURNED TO BASE. MAINTENANCE REPLACED THE NR 1 KRUGER FLAP ACTUATOR AND THE A/C WAS RETURNED TO SERVICE.May 31, 2005 · Boeing 727223 · Leading Edge Slat ActuatorSDR DL73S050276Actuator · stickingNR 2 ENGINE THRUST REVERSER UNLOCKED LIGHT ON DURING TAKEOFF ROLL. CLEANED LOWER ACTUATOR FOR STICKING.May 17, 2005 · N316DL · Boeing 737232 · Engine Thrust ReverserSDR CA050517005Valve · leaking(CAN) ON APPROACH, AFTER GEAR EXTENSION (A) SYSTEM HYDRAULIC FLUID WAS FOUND DROPPING. A NORMAL LANDING WAS ACCOMPLISHED BUT THE AIRCRAFT HAD TO BE TOWED OFF THE TAXI WAY DUE TO HYDRAULIC LOSS CAUSING THE STEERING SYSTEM TO BE INOP. AT THE RAMP MAINTENANCE TROMay 17, 2005 · Boeing 727247 · Hydraulic System, MainSDR DL73S050372Engine · bird ingestionSUSPECT BIRD INGESTION ON TAKEOFF FELT SMALL SHUDDER AND HEARD SOUND FOLLOWED BY FOUL ODOR. ENGINE PARAMETERS NORMAL. PERFORMED MTC INSPECTION PER MM 05-51-201-201. PS 3 FILTER NR 1 ENG CLEAN. RAN ENGINE TO T/O PWR ALL PARAMETERS NORMAL. NO ODORS IN A/C. May 17, 2005 · N321DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR C8GA20050013Compressor · stalledFLT 711 FROM DEN TO TOL, ON CLIMB FROM DEN, NR 1 ENGINE COMPRESSOR STALLED. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. AFTER RETURN TO BLOCKS, WITH ENGINE OPERATING AT 1.40 EPR, ENGINE COMPRESSOR STALLED AGAIN. PERFORMED BORESCOPE INSPECTION AND May 12, 2005 · N899AA · Boeing 727223 · Turbine Engine Compressor SectionSDR CA050502005Control Unit · malfunctionedA/C 743 WAS IN CRUISE WHEN 'B' SYSTEM LOW QUANTITY LIGHT CAME ON FOLLOWED BY GAUGE GOING TO ZERO. 'B' SYSTEM LOW PRESSURE LIGHTS ILLUMINATED, BOTH 'B' PUMPS SELECTED OFF. OVERHEAT LIGHTS DID NOT ILLUMINATE. A/C WAS EN ROUTE TO YEG, ATC WS ADVISED AND EMERGEApr 26, 2005 · Boeing 737204 · Hydraulic System, MainSDR CA050426003Valve · fouled(CAN) AFTER DEPARTING, THE CREW OBSERVED AN INDICATION OF ANTI-ICE SELECT FAILURE ON NR1 ENGINE. THE CREW RETURNED TO DEPARTURE, WHERE MAINTENANCE FOUND INTERNAL PARTS FROM THE THERMOSTATIC VALVE FOR THE NR1 LT NOSE COWL ANTI-ICE HAD FOULED THE ANTI-ICE VALVE.Apr 20, 2005 · Boeing 727233 · Antenna/Radome Anti-Ice/De-Ice SystemSDR FX7A200500005Shaft · shearedENGINE FLAME OUT NR 1 DURING CRUISE. UPON TROUBLESHOOTING, MAINTENANCE FOUND THE NR 1 ENGINE FUEL PUMP SHAFT SHEARED, REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP AS PER MAINTENANCE MANUAL REFERENCE 73-11-1, PERFORMED OPS/LEAK CHECK.Apr 15, 2005 · N79749 · Boeing 727224 · Engine Fuel and ControlSDR AU510001965Engine · bird ingestionNR 1 ENGINE BIRDSTRIKE. INVESTIGATION FOUND THE REMAINS OF THREE FLYING FOXES. THOROUGH INSPECTION OF THE ENGINE FOUND NO OBVIOUS DEFECTS. A WATER WASH WAS CARRIED OUT AND THE AIRCRAFT RELEASED TO SERVICE.Apr 10, 2005 · Boeing 727277 · Engine (Turbine/Turboprop)SDR AU510001545Duct · brokenNR 2 ENGINE INLET ANTI-ICE DUCT FLANGE COUPLING LIP FRACTURED AND SEPARATED. EVIDENCE OF A PRE-EXISTING CRACK.Apr 7, 2005 · Boeing 727277 · Air Intake Anti/De-Ice System
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