Pratt & Whitney JT8D-217A

Service difficulty reports · 235

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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 = 'JT8D217A'
  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 GTIA050060Skin · damagedFLUSH REPAIR FS 622 LONGERON 22R-24R HAS NO FINGER DOUBLER. REMOVED TEMP REPAIR. FABRICATED PERMANENT REPAIR PARTS. TREATED AND PRIMED ON FINAL REPAIR. INSTALLED REPAIR IAW SRM. (K)Feb 18, 2005 · N804NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA050065Skin · dentedFUSELAGE SKIN DENTED AT FS 310, LONGERON 29L-28L. (D=0.5 INCH, X=0.010 INCH, D/X=50). DENT WAS FOUND TO BE LESS THAN 1.0 INCH AND REQ A CUT OUT REPAIR. FAB`D NEW SKIN SECTION, REPAIR DOUBLER, FINGER DOUBLER, FABED (4 EA) STRAPS. TREATED, PRIMED AND TOP COAFeb 18, 2005 · N804NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA050068Wedge · damagedLT WING, IB FLAP, OB T/E WEDGE HAS TEMPORARY REPAIR LOWER SIDE IB. REMOVED TEMP REPAIR, REMOVED DAMAGED AREA (2 INCH DIA) FABRICATE DOUBLER AND FILLER, TREATED, PRIMED DOUBLER AND FILLER. INSTALLED REPAIRED DOUBLER AND FILLER IAW SRM. (K)Feb 18, 2005 · N804NK · Doug DC982 · Trailing Edge FlapsSDR GTIA050069Skin · dentedDENT ON AFT CARGO DOOR AT STA 1165, 13 INCHES FROM FORWARD EDGE, 14 INCHES FROM UPPER EDGE (D=2.0, X=0.05, D/X=40). FOUND DENT TO BE COND. 1B. PERFORMED COLD WORK AREA BACK TO ORIGINAL CONTOUR. DYE PENETRANT PERFORMED FOR CRACKS. FABRICATED DOUBLER. TREATFeb 18, 2005 · N804NK · Doug DC982 · Cargo/Baggage DoorsSDR GTIA050070Door · dentedDENT ON AFT CARGO DOOR AT STA 1183, 14 INCHES FROM UPPER EDGE/ 23 INCHES FROM AFT EDGE (D=1.0, X=0.015, D/X=66.7). REMOVED AFT CARGO DOOR TO FOM DENT FOUND TO BE COND 1B. COLD WORK PERFORMED TO ORIGINAL CONTOUR. DYE PENETRANT PERFORMED FOR CRACKS. FABRICATEFeb 18, 2005 · N804NK · Doug DC982 · Cargo/Baggage DoorsSDR GTIA050057Longeron · corrodedLONGERON 28R STA 1140 HAS CORROSION AROUND FASTENERS THROUGH SKIN IN AFT PIT. REMOVED FASTENERS THROUGH SKIN AND REMOVED CORROSION. LONGERON 28R AT STA 1140 IS OUT OF LIMITS. LOCATED AND DRILLED FABED LONG SECTION AND SPLICE. TREAT AND PRIMED, INSTALLED LOFeb 17, 2005 · N804NK · Doug DC982 · Fuselage Main, Longeron/StringerSDR GTIA050048Angle · corrodedDOOR FRAME TO SKIN CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM ARE CORRODED IN AFT PIT. REMOVED CORROSION ON DOOR FRAME TO SKIN CORNER ANGLES AND DOOR JAMB. MATERIAL LOSS OUT OF LIMITS. DRILLED AND LOCATED NEW ANGLE, TREATED, PRIMED AND INSTALLED NEW Feb 16, 2005 · N804NK · Doug DC982 · Fuselage Miscellaneous StructureSDR GTIA050062Angle · crackedMID PIT DOOR INTERNAL ANGLE CRACKED AT LOWER CENTER EDGE. REMOVED INTERNAL ANGLE FROM MID CARGO DOOR LOWER CENTER EDGE. LOCATED AND DRILLED NEW INTERNAL ANGLE (FITTING), INSTALLED NEW FITTING IAW SRM. (K)Feb 16, 2005 · N804NK · Doug DC982 · Cargo/Baggage DoorsSDR GTIA050045Beam · corrodedAFT PIT LOWER DOOR JAMB BEAM CORRODED AND HAS BARE METAL. REMOVED CORROSION, FABRICATED REPAIR IAW SRM. OK TO TREAT, PRIME AND TOPCOAT REPAIR. LOCATED AND DRILLED 2 DOOR STOP FITTINGS AND INSTALLED DOOR JAMB BEAM REPAIR. (K)Feb 15, 2005 · N804NK · Doug DC982 · Fuselage Main, StructureSDR GTIA050054Skin · crackedFUSELAGE EXTERIOR STA 1485 CANT. LT LOWER SKIN CRACKED. CUT OUT DAMAGED AREA 2 INCH X 4.8 INCH AT STA 1485. FABED FINGER DOUBLER, TREATED AND PRIMED. INSTALLED REPAIR ON LT LOWER SKIN, STA 1485 CANT IAW SRM. (K)Feb 15, 2005 · N804NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA050063Angle · corrodedDOOR FRAME TO SKIN CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM ARE CORRODED IN AFT PIT. REMOVED CORROSION ON DOOR FRAME SKIN, CORNER ANGLES STA 1155 AND 1212 AT DOOR JAMB BEAM. CORNER ANGLE IS OUT OF LIMITS STA 1212 AND LOCATED NEW ANGLE, INSTALLED ANGFeb 15, 2005 · N804NK · Doug DC982 · Fuselage Miscellaneous StructureSDR GTIA050066Skin · damagedRT WING OB FLAP MID FIXED VANE DAMAGED. REMOVED DAMAGED SKIN AND CORE TO OB FLAP VANE, FABRICATED REPAIR DOUBLER AND HONEYCOMB CORE. TREATED METAL, BONDED CORE AND DOUBLER. INSTALLED REPAIRED CORE AND SKIN IAW SRM. (K)Feb 15, 2005 · N804NK · Doug DC982 · Trailing Edge FlapsSDR GTIA050067Skin · dented(1EA) MINOR DENT ON MID CARGO DOOR EXTERNAL SKIN AT LOWER L/R MARKED. DENT MEASURE IS OUT OF LIMITS CONDITION. 2(D=0.25, X=0.75). REMOVED CARGO DOOR FOR FOM, APPLIED DYE PENETRANT FOR CRACKS. FABED (3 SHIMS) AND REPAIR DOUBLER. TREATED SKIN, SHIMS AND DOUFeb 14, 2005 · N804NK · Doug DC982 · Cargo/Baggage DoorsSDR GTIA050007Engine · malfunctionedTAKEOFF ROLL A/T ENGAGED AT APPROX 40 KNOTS, THROTTLES AT FLEX POWER FELT SOMETHING LIKE A BLOWN TIRE, RT ENGINE SLIGHT YAW, ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE. (M)Jan 11, 2005 · N804NK · Doug DC982 · Engine (Turbine/Turboprop)SDR GTIA040853Smoke Detector · inactiveLP NR 273191-1; RT LAV SMOKE DETECTOR DID NOT ACTIVATE WHEN PAX WAS SMOKING IN AIRCRAFT LAV. OPS TESTED SMOKE DETECTOR, NO FAULTS WERE NOTED.Nov 25, 2004 · N804NK · Doug DC982 · Smoke DetectionSDR GTIA040847Skin · crackedLP NR 0167013; LT MAIN GEAR DOOR SKIN CRACKED ABOVE AND BELOW SKIN PLATE. UNSCHEDULED CHANGE OF AIRCRAFT EN ROUTE. PERFORMED REPAIR AND INSTALLED DOUBLER.Nov 16, 2004 · N804NK · Doug DC982 · Landing Gear DoorsSDR GTIA040852Stud · backed outLP NR 0126074-1; LT OIL PRESSURE LOW LIGHT CAME ON WITH OIL QUANTITY DROPPING AND OIL PRESSURE DROPPING, SHUT DOWN NR 1 ENGINE. FOUND 2 FWD MOUNTING STUDS FOR OIL FILTER CAP LOOSE AND BACKED OUT, INSTALLED HELICOIL THREADED INSERTS AND RE-INSTALLED STUDS, NO Nov 12, 2004 · N817NK · Doug DC982 · Turbine Engine Oil SystemSDR GTIA040840Engine · bird ingestionLP NR 0252843; MULTIPLE BIRD STRIKES ON APPROACH TO LGA, NR 2 LT EGT HIGH. REMOVED AND REPLACED NR 2 ENGINE.Nov 3, 2004 · N821NK · Doug DC982 · Engine (Turbine/Turboprop)SDR GTIA040825Gyro · inaccurateHEADING LIGHT ON IN FLIGHT 6 FT-8 FT OFF. REPLACED NR 1 DG AND SWITCHING UNIT.Oct 20, 2004 · N821NK · Doug DC982 · Directional Gyro and Indicating SystemSDR GTIA040818Retract Cylinder · out of adjustAFTER TAKEOFF, RT MAIN GEAR RED LIGHT REMAINED ON WITH GEAR HANDLE UP. FOLLOWED PROCEDURE IN QRH AND CONSULTED WITH MECHANIC CONTROL. CONTINUED TO DESTINATION AT REDUCED SPEED IAW QRH. ON DESCENT IN TPA AT 10,000 PRIOR TO EXTENDING LANDING GEAR, RED LIGHT WOct 17, 2004 · N817NK · Doug DC982 · Landing Gear Retraction/Extension SystemSDR P9RA20040046Power Supply · inoperativeAIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHTS INOPERATIVE AT ROW 26. REMOVED AND REPLACED POWER SUPPLY IAW MM.Oct 12, 2004 · N14816 · Doug DC982 · Emergency LightingSDR P9RA20040047Power Supply · inoperativeAIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHT AT ROW 28 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW MM.Oct 12, 2004 · N14816 · Doug DC982 · Emergency LightingSDR GTIA040813Cable · misinstalledONE TAILCONE CABLE NOT INSTALLED IN BLOCK. (TAILCONE LIGHT WAS ILLUMINATED). ROUTED AND INSTALLED CABLE IAW MM 53-53-02.Oct 11, 2004 · N815NK · Doug DC983 · Fuselage Main, Bulkhead Fuselage wiringSDR GTIA040811Cable · misroutedR1 SLIDE INFLATION CABLE NOT ROUTED THROUGH GROMMET TAB. RE-ROUTED CABLE.Oct 11, 2004 · N817NK · Doug DC982 · Escape SlideSDR GTIA040810Handle · defectiveAIL SLIDE MANUAL DEPLOY HANDLE (RED STRAP) NOT ROUTED THROUGH DEPLOYMENT LANYARD RELEASE. UPON ATTEMPTING TO REROUTE TAIL SLIDE MANUAL DEPLOY HANDLE FOUND SLIDE COMING APART. REMOVED AND REPLACED SLIDE PACK.Oct 11, 2004 · N817NK · Doug DC982 · Escape SlideSDR ASMF200410005Modulator · leakingDURING LT ENGINE STARTING CAPTAIN REPORTED LT HYDRAULIC SYSTEM LEAKAGE AND PRESSURE DROP TO ZERO. DURING REVISION THE TECHNICAL PERSONNEL DETECTED THAT THE LEAK WAS FROM A LINE OF THE MAIN FILTERS MODULE. LINE WAS TIGHTENED AND HYDRAULIC FLUID RECHARGED. TESTSOct 7, 2004 · N1003Y · Doug DC982 · Hydraulic System, MainSDR GTIA040801Engine · shutdownINFLIGHT SHUTDOWN, EMERGENCY AIR RETURN. RT OIL TEMP HIGH IN CLIMB, SHUTDOWN ENGINE AT 165 DEGREES. REMOVED AND REPLACED NR 2 ENGINE IAW MM. LEAK CHECK OK.Oct 6, 2004 · N810NK · Doug DC981 · Engine (Turbine/Turboprop)SDR GTIA040795Latch · out of rigMAIN ENTRANCE DOOR WILL NOT LOCK. FOUND L1 DOOR INTERLOCK MECHANISM HANGING UP. LUBED SAME. ADJUSTED/RIGGED DOOR, HOLD OPEN LATCH WAS OUT OF RIG/ADJ.Oct 1, 2004 · N808NK · Doug DC983 · Passenger/Crew DoorsSDR ASMF200409007Link · jammedCAPTAIN REPORTED THAT AFTER TAKEOFF, NOSE LANDING GEAR NOT RETRACTED, LIGHT ON, ABNORMAL PROCEDURE PERFORMED. AIRCRAFT SENT TO THE HANGAR AND NOSE LANDING GEAR OPERATIONAL TEST WAS PERFORMED. NOSE LANDING GEAR LINK WAS JAMMED DURING RETRACTION, THEREFORE NOSSep 19, 2004 · N505MD · Doug DC982 · Landing Gear Retraction/Extension SystemSDR ASMF200409005Actuator · failedAIRCRAFT RETURNED OF FLIGHT, NOSE LANDING GEAR DOOR WAS OPENED AND STRONG NOISE WAS HEARED BY CREW. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE LANDING GEAR DOOR ACTUATORS WERE REPLACED IAW MM 32-22-01, TEST CORRECT.Sep 13, 2004 · N501AM · Doug DC982 · Landing Gear Door ActuatorSDR GTIA040780Engine · vibrationFLT 197 - LGA - LEFT ENGINE UNUSUAL NOISE AND VIBRATION ON CRUISE POWER CHECK (L) HYD PUMP OFF PACK (L) OFF AND NOT CHANGES. REMOVED AND REPLACED NR 1 ENGINE. (M)Sep 11, 2004 · N810NK · Doug DC981 · Engine (Turbine/Turboprop)SDR ASMF200408022Thermocouple · damagedDURING OVERNIGHT SERVICE WAS DETECTED RT ENGINE WITH HIGH EGT INDICATION. EGT INDICATION WAS CHECKED IAW MM 77-21-00 AND THERMOCOUPLE NR 4 WAS DETECTED WITH DAMAGE, IT WAS REPLACED IAW MM 77-21-03. PT2 AND PT7 WERE CHECKED AND NO LEAKS WERE DETECTED, TRIMMINGAug 26, 2004 · N1003Y · Doug DC982 · Engine EGT/TIT Indicating SystemSDR CALA0400616Flange · crackedINSPECTION FOUND A 3 INCH CRACK IN THE AFT CARGO DOOR FORWARD LOWER STOP FLANGE. REPAIRED IAW ECRA 5232-01047.Aug 25, 2004 · N18835 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0400607Slat Track · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 10 AUX TRACK SLAT CAN XOS 380.229. THE NR 10 AUX TRACK SLAT, CAN WAS REMOVED AND REPLACED IAW SRM 51-30-0 AND 51-20-0.Aug 20, 2004 · N819NY · Doug DC982 · Leading Edge DevicesSDR CALA0400609Release Cable · out of rigTHE TAILCONE PULL CHECK FROM THE INTERIOR RELEASE HANDLE, FAILED. THE CABLES WERE ADJUSTED IAW MM 53-53-00.Aug 20, 2004 · N18835 · Doug DC982 · Aerodynamic FairingsSDR GTIA040734Guide Vane · crackedDTW - NR 1 ENGINE IGV HAS A HAIRLINE CRACK ON THE VANE ATTACHMENT WELD AT THE 3:30 POSITION APPROX 2.750 INCH LONG. REMOVED AND REPLACED IGV. (M)Aug 18, 2004 · N803NK · Doug DC982 · Turbine Engine Air Inlet SectionSDR GTIA040735Engine · leakingPOSSIBLE FUEL LEAK ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE. (M)Aug 17, 2004 · N803NK · Doug DC982 · Engine (Turbine/Turboprop)SDR ASMF200408013Compensator · failedCAPTAIN REPORTED DIFFERENCE BETWEEN LT AND RT FUEL INDICATORS. DURING COMPENSATORS TEST WAS DETECTED THAT THE RIGHT TANK HAD 2500 LBS, LT TANK HAD 2600 LBS AND CENTRAL TANK HAD 3000 LBS. FUEL WAS TRANSFERRED FORM PRINCIPAL TANKS TO CENTRAL TANK AND BOTH TANKS Aug 14, 2004 · N505MD · Doug DC982 · Fuel Quantity SensorSDR ASMF200408011Regulator · openCAPTAIN REPORTED THAT AT FL 330 FLOWS LIGHT TURNED ON DUE TO PRESSURIZATION FAILURE PERFORMING AN ABNORMAL AND EMERGENCY PROCEDURE. ANTI-ICE WAS APPLIED TO ENGINES AND WINGS BUT LIGHT CONTINUE AND CABIN ALTITUDE LIGHT TURNED ON, PRESSURIZATION WAS CONTROLLED Aug 12, 2004 · N505MD · Doug DC982 · Pressure Regulator/Outflow ValveSDR GTIA040731Engine · failedFOUND RIGHT ENGINE FAILED AT 800 FEET DURING CLIMB-OUT FROM RSW. REPLACED NR 2 ENGINE. (M)Aug 12, 2004 · N803NK · Doug DC982 · Engine (Turbine/Turboprop)SDR ASMF200408010Relay · malfunctionedAIRCRAFT RETURNED TO PLATFORM, (SIF) LIGHT TURNED ON. SYSTEM WAS CHECKED AND RELAY R2-58 WAS DETECTED ON FLIGHT POSITION AFFECTING LT STALL COMPUTER. RELAY WAS REPLACED IAW MM 32-62-00 AND TESTED IAW MM 34-19-00, ALL CORRECT.Aug 9, 2004 · N831LF · Doug MD83 · Stall Warning SystemSDR ASMF200408003Control Valve · damagedCAPTAIN REPORTED, DURING CLIMB "LT REVERSE ACCUMULATOR" LIGHT TURNED ON AND LT HYDRAULIC QUANTITY DOWN AT 4 QUARTERS. LT REVERSE VALVE WAS CHECKED AND LEAK ON PRESSURE LINE WAS DETECTED, NIPPLE WAS TIGHTENED AND HYDRAULIC PRESSURE WAS APPLIED AND LEAK CONTINUEAug 3, 2004 · N1003Y · Doug DC982 · Engine Thrust ReverserSDR GTIA040334Accoustic Liner · damagedDTW - FOUND ACCOUSTIC LINE DAMAGE AT 12 O'CLOCK POSITION ON NR 1 ENGINE REAR FAN CASE SECTION. REMOVED AND REPLACED NR 1 ENGINE. (M)Apr 23, 2004 · N803NK · Doug DC982 · Engine Air Intake SystemSDR GTIA040011Engine · flamed outRT ENG FLAMED-OUT, AIR RETURN AT 800 TO 1000 MLS RT ENG EPR DROPPED BELOW 1.2 EPR, ARTS FIRED BASES X-TERED TO LT GENERATORS ACCOMPLISHED QRH ITEMS PULLED CVR C/B. PERFORMED ENG HI-POWER TRIM CHECKRUN ENG OPS CK NORM. R & R NR 2 ENG FUEL CONT, OPS CK GOOD. Jan 15, 2004 · N812NK · Doug DC982 · Engine (Turbine/Turboprop)SDR MEX2003548Oil Filter · cloggedAC RETURNED THIRTY MINUTES AFTER TAKEOFF, THE (RT OIL STRAINER CLOGGING) LIGHT CAME ON. CAPTAIN INFORMED THAT THE ENGINE WAS NOT TURNED OFF AND IT WAS PUT AT FLIGHT IDLE POWER. AT PLATFORM THE MAIN FILTER ASSY AND THE CHIP DETECTORS WERE INSPECTED, THE FILTEDec 10, 2003 · N158PL · Doug MD88 · Turbine Engine Oil SystemSDR GTIA030995Engine · failedFOUND ENGINE HAS LEAK AT N1 TACH GENERATORS. ENGINE FAILED BORESCOPE INSPECTION ENGINE TO BE SENT OSV FOR REPAIR. (M)Nov 18, 2003 · N818NK · Doug DC981 · Engine (Turbine/Turboprop)SDR AALA20031285Engine · malfunctionedIAD T646/14 EN ROUTE MIA-YYZ AIRCRAFT LOST OIL PRESSURE AND QUANTITY IN NUMBER ONE ENGINE. LANDED AT IAD WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSEDNov 15, 2003 · N228AA · Doug DC982 · Engine (Turbine/Turboprop)SDR GTIA030876Engine · failedRIGHT ENGINE FAILURE AT 80 KTS. REMOVED AND REPLACED NR 2 ENGINE. (M)Oct 31, 2003 · N811NK · Doug DC981 · Engine (Turbine/Turboprop)SDR AALA20030827Fuel Control · failedEWR - FLT 1005 - LGA-TPA - DURING CLIMB-OUT AT ABOUT 16,000 FEET RIGHT ENGINE SHUT DOWN WITH NO INDICATION OF VIBRATION OR DAMAGE. AIRCRAFT DIVERTED TO EWR AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATIAug 2, 2003 · N262AA · Doug DC982 · Fuel Controlling SystemSDR ASAA0380519Engine · failedLAX - A LOUD BANG AND VIBRATION FROM RT ENGINE CLIMB AT FL24500 OUT OF LAX. SUSPECT COMPRESSOR STALL. DECLARED EMERGENCY AND RETURNED TO LAX. ENGINE WAS REPLACED. SUBSEQUENT ENGINE TEARDOWN REVEALED A COMPLETE FAILURE OF THE T-3 AND T-4 STAGES, AND THIS FAJul 1, 2003 · N953AS · Doug DC982 · Engine (Turbine/Turboprop)
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