Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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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 = 'JT8D15'
  ORDER BY difficulty_date DESC"

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SDR 06FDEA0413Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT STR 4 RT BS 680. REPAIRED PER SRM 51-30-2.Jan 27, 2006 · N488FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0414Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT STR 4 RT BS 720C. REPLACED PER SRM 51-30-6.Jan 27, 2006 · N488FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0415Frame · dentedFRAME DENTED AT BS 500 BETWEEN STR 23R AND STR 24R IN THE FWD CARGO COMPARTMENT. DENTS IN FRAME AT BS 500 BETWEEN STR 23R & 24R IN FLANGE & RADIUS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS, ALODINED & PRIMED ALL WORK DONE IAW SRMJan 27, 2006 · N488FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA0416Frame · dentedAFT CARGO FRAME DENTED AT BS 1110, STR 26L. REPLACED PER SRM 51-40-3, 51-10-2, 51-30-2.Jan 27, 2006 · N488FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA0417Frame · dentedN00608 AFT CARGO FRAME DENTED AT BS 1130, STR 26R. REPAIRED PER SRM 51-40-3.Jan 27, 2006 · N488FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA0418Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT BS 720A, STR 7RT. REMOVED AND REPLACED STRINGER CLIP FOUND TO BE OUT OF LIMITS ALL WORK DONE IAW SRM 53-10-1, 51-30-2Jan 27, 2006 · N488FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0377Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 950B, STRINGER 8 RT.Jan 25, 2006 · N492FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA0373Frame · dentedFRAME DENTED B/S 660 STR 23-25 RT. REPAIRED FRAME BS 660 STR 23-25 RT IAW SRM 51-40-3.Jan 25, 2006 · N492FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA0310Wire · corrodedPDIS 262 26-12 0007718 20JAN06 AFW OPEN R LOGPAGES: 01310127 MAIN CARGO SMOKE ZONE 5 LIGHT AND MASTER FIRE WARNING LIGHTS CAME ON PASSING 5000FT IN CLIMB AND ON TOUCHDOWN. BLEW OUT LINE FROM NR 5 DETECTION UNIT LINE AFT FOR DE BRIS. NOTHING NOTICABLJan 21, 2006 · N262FE · Boeing 727200 · Fire Protection System WiringSDR 06FDEA0186Engine · failedDURING A MAX POWER T/O AT 70-80 KNOTS THERE WAS A LOUD BANG AND AIRCRAFT PULLED LEFT. PERFORMED REJECTED. NR 1 EPR - 2.18 AT FAILURE. REPLACED NR 1 ENG PER WORK CARDS 70T0001-01 AND 70T030 1-01. ALL TEST NORMAL. RELEASED FOR SERVICE. COMPLIED WITH EO 7-Jan 13, 2006 · N282FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR DHL2006572511Hinge · crackedFOUND NR 111073; MCD HINGE CRACKED FROM AFT SECTION BS 650 NDT CONFIRMED. REMOVED AND REPLACED MCD AFT HINGE SECTION P/N MS20001-16-7200 PO 9002527 IAW AEI M/M CHAPTER 25, FIG 5201B REV F DATED 01-22-2001. THIS REPAIR A CAT (A).Jan 13, 2006 · N752DH · Boeing 727223 · Electrical/Electronic Compartment DoorsSDR DHL2006572512Slat · crackedDISCREPANCY FOUND NR 111075; NR 2 SLAT RIB NR1 AT SLAT STA 234.0 IS CRACKED. REMOVED DAMAGED PART IAW SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 1 SLAT 180 DIM 16 X 5 MAT USE 7075.0 0.40 PO 9001602 IAW SRM 57-50-2 FIG NR 2 AND 51-20-1 PART TREATEDJan 13, 2006 · N752DH · Boeing 727223 · Wing StructureSDR DHL2006572510Slat · dentedFOUND NR 111042; DENT ON NR1 SLAT UPPER SURFACE WSTA 720. CUTOUT SKIN SIZE 4.6250 X 1.5 AND INNER SKINS SIZES 8.5 X 3.25 AND 8.5 X 3.5 IAW SRM 57-50-3 FIG 1 AND FIG 4 FABBED SKIN DOUBLER FROM 2024 T3 .080 SIZE 8.5 X 5.1250 PO 9002459 AND INNER SKIN FROM 2024Jan 9, 2006 · N752DH · Boeing 727223 · Leading Edge DevicesSDR 06FDEA00055Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT RT WING OB OF LANDING LIGHT WAS ACCOMPLISHED IAW SRM 57-30-4, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING, GENERAL WORKMANSHIP ANDJan 6, 2006 · N498FE · Boeing 727200 · Wing StructureSDR 06FDEA00056Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA.1323 LT SIDE BELOW PYLON TRAILING EDGE WAS ACCOMPLISHED IAW SRM 51-40-2, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKJan 6, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00057Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1325 ABOVE AIRSTAIRS CUTOUT WAS ACCOMPLISHED IAW SRM 51-40-2 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSIST OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS SPACING AND NUMBERS, GENERAL WORKMANSJan 6, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00058Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT FWD OF NR 2 ENGINE LT SIDE WAS ACCOMPLISHED IAW SRM 51-40-2, FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP Jan 6, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 0601042Floorbeam · corrodedREPAIRED MAIN CARGO CABIN TRANSVERSAL BEAM DUE TO CORROSION.Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Floor BeamSDR 06FDEA00032Repair · unknownFOUND EXISTING REPAIR AT STA 710, STR 26L WAS ACCOMPLISHED IAW ISSUED EA 7-5330-70412, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS WITH LOCATION, SHAPE, TYPE OF MATERIAL AND THICKNESS, FASTENERS SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR CLASSIFIED AJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00033Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT ST.312, STR.9L WAS ACCOMPLISHED WITH ISSUED EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, SHAPE, SIZE, TYPE OF MATERIAL AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00034Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 227, STR20L WAS ACCOMPLISHED WITH SRM 53-30-3 FIG. 13, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, TYPE, SIZE, TYPE OF MATERIAL AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP AND REPAIR IS Jan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00036Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00037Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CLAJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00038Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 344, STR 7L WAS ACCOMPLISHED IAW EO 7-5340-7-5002 PT1, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, SHAPE, SIZE, TYPE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS Jan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00039Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 2 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57- 50-3, FIG. 3, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP,Jan 5, 2006 · N498FE · Boeing 727200 · Wing StructureSDR DHL2006572509Skin · corrodedDISCREPANCY FOUND NR 110979; FWD CARGP FUSELAGE INNER SKIN AT STR 28L BS 580-600 HAS HEAVY CORROSION. CUT OUT DAMMAGED AREA OF SKIN AT STR 28L BETWEEN BS 580-600 DIM 19 INCH X 3 INCH FABBED DOUBLER 2024-T3 .100 PO 9002507 29.75 INCH X 12.0 INCH AND FILLER 20Jan 5, 2006 · N752DH · Boeing 727223 · Fuselage Main, Plate/SkinSDR DHL2006572508Actuator · crackedNR 2 SLAT ACTUATOR I/B SUPPORT MOUNT CRACKED. CORRECTIVE ACTION; REMOVED CRACKED NR 2 SLAT ACTUATOR I/B SUPPORT MOUNT IAW B727 SRM 51-30-2 FABBED DOUBLER PLATE MIL 5-5059 301 1/2 HD .100 7.4" X 3" PO 9001425 IAW S/B 727-57-0130 REV 3 DATED 4-24-03 FABBED SUPJan 4, 2006 · N752DH · Boeing 727223 · Aileron TabsSDR DHL2006572506Grommet · deterioratedDISCREPANCY FOUND NR 110899; DB COOPER VANE STOP GROMMET, LT SIDE FUSELAGE SKIN IS DETERIORATED STA 1323 ABOVE STR 26L. REMOVED VANE STOP GROMMET IAW SRM 51-30-2 FAB DOUBLER FROM 2024-T3 .063 PO 9002435 9 .3750 X 4.7500 IAW SRM 53-30-3 FIG1 TREATED AND PRIMEDJan 3, 2006 · N752DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2006752504Frame · puncturedFOUND PUNCTURE HOLE ON UPPER SEGMENT OF FRAME AT BS 480 STR 26R (FWD PIT, UNDER FLOOR SUPPORT STAP). REMOVED TRANSMISSION PANEL IN FWD BAG RT FROM 480 TO 560 FOR ACCESS IAW SRM 51-30-2 CUT OUT DAMAGED AREA SIZE 1 INCH X .5 INCH IAW SRM 51-10-1 FABBED ANGLE RJan 2, 2006 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR PCSA12300501Control Panel · unsecureCLIMBED TO CRUISE, CREW REPORTED NR 3 GEN BREAKER LIGHT CAME ON & WOULD NOT HOLD POWER, NR 2 GEN BREAKER & FIELD LIGHTS CAME ON, NO FAULT NOTED, RESET NR 2 GEN & 20 MIN LATER FAULT RETURNED NO LIGHTS. DID NOT RESET NR 2 BREAKER. DIVERTED ACFT, & LANDED WITHOUTDec 30, 2005 · N994AJ · Boeing 727233 · AC Generation SystemSDR DHL2006752501Skin · dentedDISCREPANCY FOUND NR 110587; DENT LT SIDE FUSELAGE SKIN AT STA 373 STR. 24L (MARKED). DENT IS IN AREA NOT ALLOWED IAW SRM SPECIFICATIONS. CUT OUT DAMAGED AREA DIM 3INCHES X 1INCH FABBED FILLER 2024-T3 .050 PO 9002695 3.1 INCHES X 1.3 INCHES AND DOUBLER 2024-Dec 29, 2005 · N752DH · Boeing 727223 · Fuselage Main, Plate/SkinSDR DHL2006752503Spar · corrodedDISCREPANCY FOUND NR 110621; RT/WING AT WS 170 APPRX L/E CAVITY FRONT SPAR LWR CHORD HAS CORROSION. REMOVED CORR ON RT/WING LWR SPAR AT WS 170 ORIGINAL THICKNESS .413 MAT REMOVED .109 MATL REMAINING IS .304 AND IS OUT OF LIMITS IAW SRM 57-10-1 FIG2 FABBED DDec 29, 2005 · N752DH · Boeing 727223 · Wing SparSDR 05FDEA04408Flap Track · corrodedN0108, CORROSION ON UPPER SURFACE OF NR 6 FLAP TRACK AROUND BOTH AFT MOUNT BOLT HOLES AND CNT OB MOUNT BOLT HOLE. COMING REPLACED NR 6 FLAP TRACK IAW WC27X5708-03Dec 22, 2005 · N490FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA04389Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1140, STR 20L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG.1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP OF THE INSTALLADec 21, 2005 · N274FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR ABXA050381Cable · brokenAFTER TAKEOFF AT GEAR RETRACTION, LOUD NOISE AND SEVERE VIBRATION FROM THE NOSE GEAR AREA WAS FELT. RECYCLED THE LANDING GEAR AND A LOUD BANG WAS HEARD. RETURNED TO THE AIRPORT AND MADE A NORMAL LANDING WITH ALL THE CORRECT INDICATIONS. FOUND THE NOSE GEAR DODec 21, 2005 · N954AX · Doug DC941 · Landing Gear Door Retract SectionSDR 05FDEA04365Structure · damagedCHORD DAMAGED AND RUB STRIP MISSING ON LWR EDGE BELOW NR 2 ENGINE BS 1352.Dec 16, 2005 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR SPAA0500078Battery Pack · dischargedSCHEDULED MAINTENANCE VISIT, FWD DOOR AREA CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW B737MM 33-51-02. OPERATIONAL CHECK NORMAL.Dec 16, 2005 · N712S · Boeing 7372Y5 · Emergency LightingSDR DHL2005747003Connector · looseAFTER FLAPS WERE RETRACTED TO 0 THE AMBER LE FLAPS LIGHT ILLUMINATED ON FWD PANEL SO PANEL READ NR5 LE FLAP IN TRANSIT ABNORMAL PROCEDURE COMPLETE PROBLEM REMAINED. FOUND CONNECTOR LOOSE FOR SWITCH CLEANED, RESECURED SWITCH CONNECTOR PLUG RAN FLAPS OPS CK NMLDec 16, 2005 · N747DH · Boeing 727224 · Leading Edge Slat Control SystemSDR GAIA05037OPDownlock Switch · inoperativeDURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. VISUAL INSPECTION THROUGH PORT INDICATED DOWN AND LOCKED. LANDING AND TAXI IN UNEVENTFUL. CLEANED AND RESEATED DOWNLOCK SWITCH AND (DOWNLOCKDec 15, 2005 · N281KH · Boeing 7272J0 · Landing Gear Position and WarningSDR PCSA12150501Outflow Valve · stuckFLIGHT 731 AFTER DEPARTURE, DURING CLIMB THRU 6000 FT. CREW REPORTED CABIN PRESSURIZATION STARTED CLIMBING AT AN EXCESSIVE RATE AND COULD NOT MAINTAIN CABIN PRESSURIZATION. THE CREW REPORTED THE OUTFLOW VALVE WAS FULLY CLOSED, IT APPEARED THAT THE RT PACK WAS Dec 15, 2005 · N495AJ · Boeing 727233 · Cabin Pressure ControllerSDR GAIA05038OPPin · missingEXCESSIVE NOSE WHEEL SHIMMY ON LANDING. THE AIRCRAFT WAS TOWED OFF THE RUNWAY. INSPECTION REVEALED THAT THE NOSE GEAR TORQUE LINK QUICK DISCONNECT WAS MISSING. THE AIRCRAFT WAS INSPECTED FOR DAMAGE AND THE TORQUE LINK PIN WAS REPLACED. AIRCRAFT WAS RETURNEDec 14, 2005 · N279US · Boeing 727251 · Nose/Tail Landing GearSDR AU510001519Door Frame · crackedNR 3 CARGO DOOR LOWER FORWARD FRAME RADIUS AND `T` FRAME CRACKED THROUGH THREE FASTENER HOLES. FOUND DURING INSPECTION IAW SB 727-52-0149.Dec 12, 2005 · Boeing 727277 · Fuselage Main, StructureSDR AU510001526Wheel · crackedMAIN WHEEL INNER HUB CRACKED APPROXIMATELY 35MM (1.377IN) BELOW THE MATING FACE AND EXTENDING THROUGH TO THE OUTSIDE OF THE HUB AT THE TIE BOLT HOLE SEAT RADIUS. CRACK LENGTH 18MM (0.708IN). CRACK IS LOCATED OUTSIDE OF AREAS LAID DOWN IN THE MAINTENANCE MANUDec 12, 2005 · Boeing 727277 · Wheel/Ski/FloatSDR AU510001646Hinge Pin · cracked(AUS) LT HORIZONTAL STABILIZER OUTER HINGE PIN CRACKED IN AREA OF THREAD ROOT ADJACENT TO SPLIT PIN HOLES. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW SB727-55A0090R1 PART 4 AND AD/B727/173.(AD/SB DESC: AD/B727/173, SB727-55A0090R1 ) (CASA# 510001646)Dec 12, 2005 · Boeing 727277 · Horizontal Stabilizer Miscellaneous StructureSDR AU510001660Skin · crackedFUSELAGE SKIN LAP JOINTS CRACKED. JOINTS WERE LOCATED AT STRINGER 4R BETWEEN BS 480 AND BS 720B AND AT STRINGER 26L BETWEEN STN 560 AND STN 580. FOUND DURING MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION IAW AD/B727/160 AND SB727-53AO222.Dec 12, 2005 · Boeing 727277 · Fuselage Main, Plate/SkinSDR AU510001954Compressor · misrepairedNR 3 ENGINE FIRST STAGE COMPRESSOR BLADE BLENDED BEYOND LIMITS IN MAINTENANCE MANUAL. RECORDS GAVE NO INDICATION OF BLEND REPAIR BEING CARRIED OUT.Dec 12, 2005 · Boeing 727277 · Turbine Engine Compressor SectionSDR AU510001985Spar · crackedLT ELEVATOR REAR SPAR CRACKED. FOUND DURING INSPECTION IAW AD/B727/100.Dec 12, 2005 · Boeing 727277 · Elevator, Spar/RibSDR AU510002077Guide Vane · fractured(AUS) NR 1 ENGINE FIRST STAGE NOZZLE GUIDE VANE (NGV) BURNED THROUGH. NGV WAS LOCATED ADJACENT TO NR 9 COMBUSTION CHAMBER. SUSPECT CAUSED BY CRACKING ON THE LEADING EDGE ALLOWING HOT AIR TO PENETRATE THE NGV. FOUND DURING INSPECTION OF THE COMBUSTION CHAMBERDec 12, 2005 · Boeing 727277 · Turbine SectionSDR PIDA20050199Control Panel · inoperativeFIRST OFFICER'S COURSE WINDOW MIDDLE DIGIT SKIPS PAST THE NR 1 ON THE MODE CONTROL PANEL. REPLACED MODE CONTROL PANEL AND OPS NORMAL IAW MM 22-11-341.Dec 10, 2005 · N251TR · Boeing 737228 · Autopilot SystemSDR PCSA12070501Compressor · stalledFLIGHT 723 DEPARTED MIA AND CLIMBED TO 34,000 FT CRUISE ALTITUDE, CREW REPORTED NUMBER 2 ENG COMPRESSOR STALLED, POWER WAS REDUCED AND NR 2 ENG CONTINUED TO COMPRESSOR STALL. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN, ALL FLIGHT CONDITIONS WERE NORMADec 7, 2005 · N199AJ · Boeing 7272F9 · Turbine Engine Compressor Section
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