Pratt & Whitney JT8D-1

Service difficulty reports · 195

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 = 'JT8D1'
  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 GTIA040418Stop Fitting · corrodedFWD CARGO DOOR FUSELAGE SIDE, DOOR STOP CORRODED/ FROZEN. REMOVE DOOR STOP. INSTALLED NEW DOOR STOP.Mar 19, 2004 · N817NK · Doug DC982 · Fuselage Main, StructureSDR GTIA040454Cable · disengagedEVACUATION SLIDE COVER AT TAILCONE SECURITY CABLE LT SIDE DISENGAUGED. RESECURED LT SECURITY CABLE.Mar 14, 2004 · N817NK · Doug DC982 · Escape SlideSDR GTIA040455Panel · corrodedLT L/E WING PANEL NR 1165C EXFOLIATED CORROSION AROUND FASTENER HOLES. FABRICATED NEW PANEL.Mar 11, 2004 · N817NK · Doug DC982 · Wing, Plate/SkinSDR GTIA040458Longeron · corrodedAFT PIT 1099 STR 29R CORRODED. REMOVED LONGERON 29R FROM STA 1136 TO 1003. FABRICATED NEW LONGERON SECTIONS FROM STA 1003 TO 1068.875 AND FROM STA 1068 TO STA 1136. FABRICATED LONGERON SPLICE. INSTALLED LONG 29R AND SPLICE FROM STA 1003-1136.Mar 10, 2004 · N817NK · Doug DC982 · Fuselage Main, Longeron/StringerSDR GTIA040290Doubler · crackedAFT CARGO DOOR LATCH CUT OUT HOLE IS DEFORMED AND REPAIR DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER.Mar 9, 2004 · N817NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA040460Skin · damaged12 INCH X 10 INCH CLASS II EXTERNAL REPAIR AT FS 249 BETWEEN LONGERON 17C AND 18L. REMOVED EXISTING EXTERNAL REPAIR. CUT OUT DAMAGED AREA 13.5 INCHES X 14 INCHES. FABRICATED NEW REPAIR PARTS EXTERNAL SKIN, FINGER DOUBLER, 03 EA DOUBLERS. INSTALLED NEW REPAMar 8, 2004 · N817NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA040461Skin · dentedDENT AT FS 58.75 BELOW RT CUSP LINE. REMOVED DAMAGED AREA 10.2500 X 16.5000. FABRICATED FILLER, DOUBLER, AND PLATE EA 5330-0410. INSTALLED REPAIR PARTS.Mar 8, 2004 · N817NK · Doug DC982 · Fuselage Main, Plate/SkinSDR MEX203546Tire · debondedAFTER LANDING WAS LISTED AN STRONG NOISE IN THE MAIN LANDING GEAR. DURING REVISION OF THE MENTIONED AREA WERE FOUND SEVERAL DAMAGES IN THE NEARBY AREA OF THE LEFT MLG CAUSED BY A TREAD SEPARATION. AC WAS CARRIED TO THE HANGAR TO REPAIR THE FOLLOWING AFFECTEDDec 4, 2003 · N205AM · Doug DC987 · TireSDR 03FDEA01670Floor Support · corrodedCORROSION ON LONGITUDINAL BEAM AT STA 760 TO 850 LBL 29 WL 208. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208, AND INSTALLED NEW LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208. ALL WORK DONE PER SRM 5Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01674Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C STRINGER 7 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, 7RH IAW SRM 51-30-2 & 51-30-5Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01675Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C, STRINGER 5 RT. REPLACED CLIP. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 5RH IAW SRM 51-30-2 & 51-30-5Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01676Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 950C, STRINGER 9 LT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 9 LT IAW SRM 51-30-2Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01677Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950D, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950D, STRINGER 6 RT IAW SRM 51-30-2.Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01678Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950B, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950B, STRINGER 6 RT IAW SRM 51-30-2 & 51-30-5.Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01679Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C, STRINGER 4 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 4 RT IAW SRM 51-30-2 & 51-30-5Oct 1, 2003 · N469FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01615Floorbeam · corrodedCORROSION ON BS 1070 FLOORBEAM LBL 45 - RBL 50.Sep 24, 2003 · N469FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01617Skin · corrodedCORROSION ON INTERNAL STRAP BS 683 BELOW STR 26 LT . REMOVED CORROSION ON INTERNAL STRAP BS 683 BELOW STR 26 LT OF A AREA 2 X 2 X .005 OF ORIGINAL .063 MATERIAL. FOUND IN LIMITS I.A.W. BOEING SRM 53-30-1. WORK DONE IAW BOEING 727 SRM 53-10-1, BOEINGSep 24, 2003 · N469FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01616Floorbeam · corrodedCORROSION BS 950F FLOORBEAM LWR CHORD NUTPLATE HOLES LBL 45 - RBL 45 WL 200. REPAIRED IAW SRM 53-10-8Sep 24, 2003 · N469FE · Boeing 727200 · Fuselage Main, Floor BeamSDR RYN2004F00022Line · chafedON CLIMB OUT, LOST HYDRAULIC A-SYSTEM. ACCOMPLISHED APPROPRIATE CHECK LIST AND MANUALLY EXTENDED THE LANDING GEAR. EMERGENCY DECLARED AND AIRCRAFT RETURNED. AIRCRAFT LANDED MDT WITHOUT INCIDENT. REPLACED NR 2 ENGINE HYDRAULIC PUMP FLEX PRESSURE LINE. LEAKAug 14, 2003 · N7638U · Boeing 727222 · Hydraulic System, MainSDR DL73S030630Insulation · out of positionSMOKE SMELL IN AFT CABIN. FOUND INSULATION TOUCHING APU BLEED DUCT CAUSING SMELL. REPOSITIONED INSUL. FWD APU AIR TO MCO AND PLAC AS PRECAUTION.Jul 12, 2003 · N329DL · Boeing 737232 · Passenger Compartment EquipmentSDR MEX2003271Suppressor · damagedAIRCRAFT AIR TURN BACK DUE TO ENGINE 2 FAILURE DURING INITIAL CLIMB, REACHING 660 DEGREE C OF EGT EMERGENCY PROCEDURE WAS PERFORMED. DURING REVISION THE EXHAUST CONE, SUPPRESSOR AND TURBINE FAN WITH DAMAGE. ENGINE NR 2 WAS REPLACED IAW MM, OPERATIONAL TEST Jul 7, 2003 · N583MD · Doug DC983 · Engine Noise SuppressorSDR GTIA030221Light · inoperativeEMERGENCY OVERHEAD LIGHTS INOPERATIVE IN PAX CABIN AISLE NR 3,7,10,12,14,18,22,25,29. TROUBLESHOT AND REPAIRED EMERGENCY OVERHEAD LIGHTS.Mar 16, 2003 · N809NK · Doug DC983 · Emergency LightingSDR GTIA030142Floor Panel · crackedAFT PIT CRACKED FLOOR WEB AT FS1289-1309 LONG 18R. FAB DOUBLER. INSTALLED DOUBLER.Mar 12, 2003 · N809NK · Doug DC983 · Fuselage Floor PanelSDR GTIA030180Floor Support · damagedFORWARD CABIN STA 160 TO STA 200 LBL 44 FLOOR SUPPORT HAS GOUGED/ DAMAGED CORRODED. FABRICATED NEW FLOOR SUPPORT.Mar 2, 2003 · N809NK · Doug DC983 · Fuselage Miscellaneous StructureSDR GTIA030145Floorboard · corrodedFORWARD CABIN STA 200 TO 160 LBL 44 TO 53 INCHES (9 X 40) FLOOR PNL SOFT/ MUSHY CORRODED INSERTS. FABBED NEW CABIN FLOORBOARD, STA 200-160 LBL 53.Feb 21, 2003 · N809NK · Doug DC983 · Fuselage Floor PanelSDR GTIA030146Floor Panel · damagedFWD CABIN STA 180 TO 160 LBR 8 INCHES TO 44 INCHES (20X36) FLOOR PANEL SOFT/ MUCHEY DAMAGED DETERIORATED CORR. INSERTS. FABRICATED NEW PANEL.Feb 21, 2003 · N809NK · Doug DC983 · Fuselage Floor PanelSDR GTIA030147Panel · deterioratedFORWARD CABIN STA 200 TO ST 256 LBL 44 INCHES (21X56) FLOOR PANEL SOFT/ MUSHEY, DETERIORATED CORR. INSERTS.Feb 21, 2003 · N809NK · Doug DC983 · Fuselage Main, Plate/SkinSDR GTIA030148Floor Panel · deterioratedFORWARD CABIN STA 200 TO 256 FLOOR PANEL SOFT/ MUSHEY DETERIORATED, CORR. INSERTS, LBR 22 TO LBR 44 (21X56). FABRICATED NEW PANEL.Feb 21, 2003 · N809NK · Doug DC983 · Fuselage Floor PanelSDR GTIA030144Shear Tie · crackedAFT CARGO FS 1250 SHEAR TIE CRACKED STR 28R. REMOVED CRACKED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED REPAIR PARTS.Feb 20, 2003 · N809NK · Doug DC983 · Fuselage Main, StructureSDR GTIA030143Fitting · corrodedAFT CARGO FS 1336 STR 28R END FITTING CORRODED. REMOVED STR 28R END FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED STRINGER 28R END FITTING.Feb 19, 2003 · N809NK · Doug DC983 · Fuselage Main, StructureSDR 03FDEA00074Position Switch · faultyINFLIGHT, NO NOSE GEAR DOWN INDICATION. (GREEN LIGHTS). REPLACED BOTH BULBS NO EFFECT. CYCLED GEAR, TESTED BULBS, DID NOT WORK, REPLACED BOTH BULBS, AGAIN A VERY WEAK LIGHT, GOOD INDICATION, WENT TO BRIGHT, WORKED. BACK TO DIM AND WAS INTERMITTENT, LANDIJan 25, 2003 · N188FE · Boeing 727100 · Landing Gear Position and WarningSDR 03FDEA00008Skin · corrodedCORROSION UNDER EDGE OF RIGHT RAM AIR DOOR ACTUATOR PANEL. CORROSION OUT OF LIMITS, REPAIRED IAW EA 7-5330-68147.Jan 8, 2003 · N489FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00007Frame · dentedDENT IN FRAME, BS 950C STR 26L. REPAIR FRAME IAW SRM.Jan 8, 2003 · N489FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00010Skin · dentedOIL CAN DENT IN SKIN AT BS 211, RBL 23, WL 182. REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR IAW SRM 53-30-3.Jan 8, 2003 · N489FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00009Skin · dentedOIL CAN DENT IN SKIN AT BS 190, RBL 22, WL 182. REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR IAW SRM 53-30-3.Jan 8, 2003 · N489FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR RYN2003F00002Splice · crackedAT B CHECK, CRACK FOUND AT FUSELAGE INTERIOR FLOOR SPLICE PLATE TO LOWER SILL BEAM, BS 640.Jan 3, 2003 · N7638U · Boeing 727222 · Fuselage Miscellaneous StructureSDR RYN2003F00001Frame · crackedAT B CHECK, CRACK FOUND ON FORWARD AND AFT SIDES OF FUSELAGE INTERIOR, LT FRAME AT BS 680 ATTACHMENT TO SKIN LOWER SILL BEAM.Dec 27, 2002 · N7638U · Boeing 727222 · Fuselage Main, FrameSDR RYN2003F00003Floorbeam · crackedAT B CHECK, CRACK FOUND IN FUSELAGE INTERIOR AT FLOORBEAM LOWER CHORD ANGLE BS295, LBBL30.Dec 27, 2002 · N7638U · Boeing 727222 · Fuselage Main, Floor BeamSDR RYN2003F00004Skin · crackedDURING B CHECK, FOUND SKIN CRACKED AT FUSELAGE INTERIOR, LT SIDE, BS 480, FRAME TO LOWER SILL BEAM FROM TIE TO FUSELAGE.Dec 27, 2002 · N7638U · Boeing 727222 · Fuselage Main, Plate/SkinSDR 02FDEA00971Stringer · crackedLOWER FUSELAGE, STRINGER 21R, IS CRACKED AT STA 400. REMOVED DAMAGED SECTION OF STRINGER FROM STATION 390-410 AND REPLACED IAW SRM.Dec 26, 2002 · N189FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 02FDEA00974Skin · dentedDENTS IN SKIN, BS 660 - 670, S22R. REPAIRED DENTS IN SKIN IAW SRM.Dec 26, 2002 · N489FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 02FDEA00975Skin · damagedFUSELAGE SKIN DAMAGED AT BS 1050, STR 19R, JUST BELOW THE LAP. REPAIRED SKIN IAW SRM.Dec 26, 2002 · N489FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR ABXA030012Frame · crackedLEFT MAIN FRAME, STA 699, HAD CRACK IN FORWARD FLANGE FROM POINT J TO POINT G. REPAIRED LEFT MAIN FRAME IAW EA 53400100-001-1.Dec 19, 2002 · N937AX · Doug DC931 · Fuselage Main, FrameSDR ABXA030009Skin · delaminatedRIGHT CONTROL TAB DELAMINATED IN NUMEROUS PLACES UPPER SKIN. REPLACED RIGHT ELEVATOR CONTROL TAB IAW DC-9 MM 27-30-03-2-0000.Dec 18, 2002 · N937AX · Doug DC931 · Elevator, Tab StructureSDR ABXA030010Skin · delaminatedRIGHT GEAR TAB DELAMINATED IN NUMEROUS PLACES UPPER SURFACE. REPLACED RIGHT GEARED TAB IAW DC-9 MM 27-30-04-2-0001.Dec 18, 2002 · N937AX · Doug DC931 · Elevator, Tab StructureSDR ABXA030011Skin · delaminatedLEFT CONTROL TAB DELAMINATED UPPER SURFACE IN NUMEROUS PLACES. REPLACED LEFT ELEVATOR CONTROL TAB IAW DC-9 MM 27-30-03-2-0001.Dec 18, 2002 · N937AX · Doug DC931 · Elevator, Tab StructureSDR 0204119995Strut · flatAFTER TAKEOFF WHEN GEAR WAS RETRACTED LOUD VIBRATION IN NOSE GEAR AREA. NO UNSAFE INDICATIONS ON GEAR. EXTENDED GEAR AND VIBRATION STOPPED. FLIGHT RETURNED AND LANDED WITHOUT INCIDENT. UPON RETURN TO GATE FOUND RIGHT NOSE GEAR DOOR OPEN. NOSE GEAR STRUT FDec 16, 2002 · N8978E · Doug DC931 · Nose/Tail Landing Gear Strut/AxleSDR 0204139931Switch · inoperativeON CLIMBOUT ALL THREE (GEAR UNSAFE) LIGHTS ILLUMINATED. ALL OTHER INDICATIONS NORMAL. ON GEAR EXTENSION GOT ALL GREEN LIGHTS ILLUMINATED AND (GEAR UNSAFE) LIGHT EXTINGUISHED. ALL OTHER INDICATIONS NORMAL. FLIGHT LANDED WITHOUT INCIDENT. REPLACED SWITCH ASSEMBLDec 14, 2002 · N90S · Doug DC931 · Landing Gear Position and WarningSDR 02FDEA00944Downlock Switch · inoperativeDURING LANDING GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. NO DOWN, GREEN LIGHT. NOTE: MANUAL GEAR EXTENSION PROCEDURE COMPLETED EMERGENCY, DECLARED WITH ATC. TROUBLESHOT LANDING GEAR POSITION INDICATING SYSTEM IAW M.M. FOUND FAULTY NOSE LANDING Dec 13, 2002 · N114FE · Boeing 72724C · Landing Gear Position and WarningSDR 02FDEA00942Duct · blownAFTER TAKEOFF NR 3 ENGINE HAD FIRE INDICATOR, IAW FLIGHT MANUAL QRM SHUTDOWN ENGINE, FIRELIGHT EXTINGUISHED BY ITSELF AND TESTED GOOD. NO ABNORMAL ENGINE INDICATIONS WERE NOTED. AFTER ENGINE SHUTDOWN WINDMILLED FOR APPROXIMATELY 10 MIN. NR 3 OIL PRESS APPRDec 11, 2002 · N188FE · Boeing 727222 · Engine Cranking
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