Pratt & Whitney JT8D-17A

Service difficulty reports · 362

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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 = 'JT8D17A'
  ORDER BY difficulty_date DESC"

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SDR DHL2006770505Stringer · corrodedFORWARD CARGO COMPARTMENT, BS 660, STR 28L, CORROSION ON STR 28L. REMOVED CORROSION AT STR, MATERIAL LOSS IS .022, ORIGINAL MATERIAL THICKNESS .063 AND MATERIAL REMAINING .041. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG.1. CUT OUT DAMAGED APPOX 16 INCHES. Sep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770510Frame · dentedFORWARD CARGO COMPARTMENT BS 680, STR 26R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG.1. FABRICATED DOUBLER IAW SRM 53-10-2 FIG.3 AND 51-40-3 FIG.1. HEAT TREATED DOUBLER IAW ENGINEERING REPORT NR 2-37153-801 REV.IR. INSTALLED REPAIR PARTS Sep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006770506Frame · dentedFORWARD CARGO COMPARTMENT, BS 720C, STR 26R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA SIZE 1.50 INCH BY 1.50 INCH IAW SRM 51-40-3 FIG 1. FAB DOUBLER WITH 7075-0, .071, SIZE 15 INCHES BY 4 INCHES, PO NR 9003817 IAW SRM 53-10-2 FIG.3 AND 51-40-3 FIG.1. HEAT TSep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006770511Stringer · corrodedDISCREPANCY: FORWARD CARGO COMPARTMENT, BS 660, STR 28L, CORROSION ON STR 28L. REMOVED CORROSION AT STR, MATERIAL LOSS IS .022, ORIGINAL MATERIAL THICKNESS .063 AND MATERIAL REMAINING .041. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG.1. CUT OUT DAMAGED Sep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770501Attach Angle · crackedASTAR NR 111384: LT IB MID FLAP T/E LOWER STRUCTURE, WBL 70 TO 134 IS CRACKED FOUR PLACES IN CUT OUTS. CUT OUT DAMAGED AREA IAW SRM 51-30-2 AND 51-40-3, FIG.1. FAB NEW FROM AC 1003-100046-7075-T6, SIZE 68.75 INCH PO NR 6295115 AND ONE SPLICE WITH AC 1003-100Sep 28, 2006 · N770AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006770515Floorbeam · corrodedLOWER LOBE AND WALKWAY BEAM LT SIDE, BS 294, CORROSION ON CHORD. REMOVED, FAB AND REPLACED CORRODED STIFFENER FROM P/N BAC 1505-29222, PO NR 9003865, IAW SRM 51-30-2, 51-30-5, 53-10-2 FIG 1 AND 51-20-1 FIG2. CUT OUT DAMAGED WEB AND FAB DOUBLER FROM 2024-0, .Sep 28, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Floor BeamSDR DHL2006770509Stringer Splice · corrodedNR 111153, PILLOWING RT FUSELAGE SKIN BETWEEN STA.1110 AND STA.1130, STR.30. CUT OUT DAMAGED AREA APPOX 2.75 INCH IAW SRM 53-10-3 FIG.1. FAB REPAIR SPLICE FROM P/N BAC 1498-131, PO NR 9003866 AND FILLER FROM P/N BAC1498-131, PO NR 9003866, APPOX 2.75 INCH IAWSep 26, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770516Skin · dentedAFT AIRSTAIRS SKIN , BS 1263, STR 26R, DENT CLUSTER. EVALUATED DENTS, RATIOS ARE A: .30 AND Y: .008 A/Y: 37.5, A: .50, Y: .016, A/Y: 31.3, DENTS ARE WITHIN ALLOWABLE LIMITS IAW SRM 52-00-2 AND 53-10-1 FIG 1. ONE DENT FOUND OUT OF LIMITS, DIM., A: .70 , Y: .Sep 26, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR CA060829004Bearing · seized(CAN) AIRCRAFT ENCOUNTERED INTERMITTENT REPEAT SNAGS FOR STIFF ELEVATOR MOVEMENT. FINAL RECTIFICATION CAME ON AUGUST 5 2006 WHEN THE REFERENCED BEARING AND RETAINER WERE REPLACED. REFERENCED BEARING WAS FOUND SEIZED. CURRENT MAINTENANCE PROGRAM WAS REVIEWEAug 5, 2006 · Boeing 737217 · Elevator Control SystemSDR ASAA0610820Battery Pack · dischargedAFTER RECON TO ALL SEATS L1 AND R1 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS.Jul 27, 2006 · N746AS · Boeing 7372X6C · Emergency LightingSDR DHL2006765002Engine · malfunctionedON ENG START - START WAS NORMAL. ENG ACCELERATED TO 30 PERCENT N1, 520 EGT 52 PERCENT N2. GRD PERSONNEL REPORTED ENG SMOKING & ENG FLAMED-OUT. ENG FAILURE CHECKLIST COMPLETE. FLOW CHART COMPLETE. INSP INLET & EXHAUST - NO DAMAGE NOTED. OPENED COWLING & IJun 27, 2006 · N765AT · Boeing 727264 · Engine (Turbine/Turboprop)SDR 2006FA0000588Cap · inoperativeAFTER COMPLETING 2 FLIGHTS, (A) HYDRAULIC SYSTEM BECAME INOPERATIVE. A LARGE AMOUNT OF FLUID WAS NOTED ON THE GROUND UNDER THE LT WHEEL. UPON FURTHER INVESTIGATION IT WAS NOTED THAT THE RT (A) SYSTEM MODULE CHECK VALVE INSTALLATION CAP HAD SHEARED IN THE MODJun 7, 2006 · N736BP · Boeing 737205 · Hydraulic System, MainSDR CA060314003Unknown · multiple failWHILE CLIMBING THROUGH 15000 FT, THE FOLLOWING WAS ENCOUNTERED: CABIN EMERGENCY LIGHTS FLASHING. THRUST REVERSER ISOLATION VALVE OPEN ILLUMINATED. NOSE GEAR UNSAFE INDICATION (GEAR RETRACTED). DFDR ILLUMINATED. CARGO OVERHEAT/DETECTION FAULT. APU FAILED TOMar 12, 2006 · Boeing 737* · Standard Practices/StructuresSDR DHL2005760006Switch · out of adjustWHEN PUTTING LANDING GEAR LEVER FROM UP TO OFF. IT CAUSED THE RT GEAR DOOR LIGHT TO ILLUMINATE ON S.O. PANEL. PERFORMED ABNORMAL PROCEDURE. LT GEAR HANDLE IN UP POSITION FOR LIGHT TO STAY OUT. CLEANED SWITCH PERFORMED ADJ AND TEST IAW MM REF 32-62-11 GRD OP CDec 8, 2005 · N760AT · Boeing 7272B7 · Landing Gear Position and WarningSDR DHL2005783007Connector · dirtyAFTER TAKEOFF, GEAR HANDLE TO OFF, DOORS LIGHT ON FWD PANEL AND RT DOOR LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, RESTORED NORMAL OPERATIONS. CLEANED AND RESEATED CONNECTOR ON RT MLG DOOR SWITCH AND OPS CHECKED GOOD IAW MM 32-62-11.Dec 7, 2005 · N783DH · Boeing 727227 · Landing Gear System WiringSDR ASAA0510352Skin Panel · corrodedCORROSION ON INTERNAL SURFACE OF SKIN PANEL BETWEEN KEEL BEAMS AT BSTA 618 TO 635. REPLACED PANEL WITH FABRICATED REPAIR PART IAW ERO AND EA. (K)Nov 29, 2005 · N746AS · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR ASAA0510351Attach Angle · cracked2 EA CRACKS FOUND AT STOP FITTING FASTENER HOLES AT BS 348.2, S16L. REPLACED INTERCOSTAL ATTACH ANGLE AND WEB FLANGE IAW EA. (K)Nov 28, 2005 · N746AS · Boeing 7372X6C · Fuselage Main, Attach FittingsSDR CA051128009Flex Line · kinked(CAN) THE SUBJECT AIRCRAFT HAD INTERMITTENT HISTORY ASSOCIATED WITH NOSE GEAR EXTENSION/RETRACTION ANOAMLIES. DURING A RECENT HEAVY CHECK THIS ISSUE WAS FURTHER INVESTIGATED.THE TEFLON LINED HYDRAULIC FLEX LINE WAS FOUND TO HAVE KINKED.IT IS BELIEVED THAT THISNov 22, 2005 · Boeing 737275C · Hydraulic System, MainSDR 05FDEA03458Floorbeam · corrodedFLOORBEAM HAS SEVERAL CORRODED FASTENERS NUT PLATES AND SURFACE UNDER NUT PLATES. BS 1166 FROM RBL 27 TO OB END. REMOVED CORRODED NUT PLATES IAW SRM 51-31-2 REMOVED CORROSION IAW SRM51-10-6,CHECKED LIMITS . ORIGINAL MATERIAL: .125 AFTER REWORK: .118 WITH IOct 20, 2005 · N213FE · Boeing 727200 · Fuselage Main, Floor BeamSDR ASAA0510289Floorbeam · corrodedBSTA 927.0 RT WL 155 AND RBL 8.0, FLOOR SUPPORT RAIL EXFOLIATION CORROSION UNDER ANCHOR NUT. REPAIRED FLOOR SUPPORT RAIL AT BSTA 927.0 AT WL155 AND RBL 8.0 IAW SRM. (K)Sep 9, 2005 · N745AS · Boeing 737298C · Fuselage Main, Floor BeamSDR SROM200500012Floor Support · damagedDURING 24 MONTH INSPECTION FOUND DAMAGE TO CARGO FLOOR SUPPORT STRUCTURE AT STA 797 STR 8R. ALLOWABLE DAMAGE .090 IAW SRM 63-10-1 FIG 5, DAMAGE - .340. REPAIRED DAMAGE IAW SRM 53-10-5, FIG 6.Aug 2, 2005 · N736BP · Boeing 737205 · Fuselage Miscellaneous StructureSDR SROM200500011Skin · gougedDURING 24 MONTH INSPECTION FOUND GOUGE IN SKIN AT STA 910, STR 16 TO BE OUT OF LIMITS DUE TO SKIN THICKNESS AFTER BLENDING. REPAIRED GOUGE IN SKIN AT STA 910, STR 16 IAW B737 SRM 53-30-3 FIG. 18.Jul 29, 2005 · N736BP · Boeing 737205 · Fuselage Main, Plate/SkinSDR CA050706008Line · leakingLOSS OF A SYSTEM HYDRAULICS. RECTIFICATION INVESTIGATION FOUND THE NUMBER 2 ENGINE THRUST REVERSER HYDRAULIC RETURN LINE HAD FAILED CAUSING THE LOSS OF A SYSTEM FLUID, PART NUMBER B432E0562C. UPON DELIBERATION WITH FLIGHT OPERATIONS, IT WAS DECIDED TO DISPATJul 5, 2005 · Boeing 737275C · Hydraulic System, MainSDR CA050420004Engine · failed(CAN) CLIMBING THROUGH APPROX 17,000' AT 320 KIAS, WITHOUT WARNING, A BANG WHICH CAUSED ACFT TO SHUDDER FOLLOWED BY VIBRATION & A HOWLING NOISE NR 2 ENG VIBRATION INDICATOR READING IN EXCESS OF 2 UNITS, EGT & OIL TEMP STARTED TO RISE, & ALSO A DROP IN EPR. ACApr 17, 2005 · Boeing 737275C · Engine (Turbine/Turboprop)SDR CA050405013Cable · malfunctioned(CAN) PILOT REPORTED THAT THE STEERING TILLER AND THE RUDDER PEDALS DO NOT CENTER WHEN RELEASED, AND THE TILLER STICKS ON HARD TURNS. MAINTENANCE FOUND THE STEERING CABLE TURN BARREL ID TAG HAD SLIPPED FROM THE TURN BARREL, THEREBY RESTRICTING FREE MOVEMENT OMar 28, 2005 · Boeing 737275C · Landing Gear Steering SystemSDR ASAA0540166Skin · dentedPAE - NR 6 SLAT TRAILING EDGE HAS A DENT. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM, REPAIR 21. (K)Mar 10, 2005 · N764AS · Boeing 7374Q8 · Leading Edge DevicesSDR BJNA05021Engine · failedNR 2 ENGINE FAILED ON THE BEGINNING OF TAKEOFF ROLL, 1.6 EPR HARD COMPRESSOR STALL AND ROLL DOWN. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. ENGINE TOTAL TIME 550207, TOTAL CYCLES 52176. SINCE Feb 11, 2005 · N344TM · Boeing 737282 · Engine (Turbine/Turboprop)SDR DHL2005760005Engine · flamed outENGINE NR 1 FLAMED OUT AFTER 30 SEC OF IDLE. ATTEMPTED 2ND START PER MX CONTROL, NO LIGHT OFF, NO FUEL FLOW. PERFORMED ABNORMAL PROCEDURE PER AOM. ATTEMPTED ANOTHER START WITHOUT ANY PROBLEM. ENGINE IDLES NORMALLY. RESET FIRE HANDLE AND ATTEMPTED RESTART.Feb 4, 2005 · N760AT · Boeing 7272B7 · Engine (Turbine/Turboprop)SDR BJNA050103Line · leakingNR 1 ENGINE LOST ENGINE OIL QUANTITY AND ILLUMINATED THE LOW OIL PRESSURE LIGHT. ENGINE WAS SHUTDOWN AND WIND MILLED APPROX 20 MIN. INSPECTION FOUND THE ENGINE GEARBOX P-5 PORT THREADS STRIPPED AND THE PORTS BANJO FITTING FOR THE OIL PRESSURE SWITCH LINE LEAJan 26, 2005 · N344TM · Boeing 737282 · Turbine Engine Oil SystemSDR BJNA041201Battery Pack · dischargedDURING A PREFLIGHT WALK AROUND INSPECTION THE NR 1 OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT BATTERY PACK IAW MM. EMERGENCY EXIT LIGHTS NO OPERATE NORMALLY. (K)Dec 15, 2004 · N344TM · Boeing 737282 · Emergency LightingSDR ASAA0410663Skin · damagedPAE, D-CHECK: DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR ASAA0410667Web · corrodedPAE, D-CHECK: CORROSION ON UNDERSIDE AT WEB. REPLACED WEB.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAAWeb · corrodedPAE, D-CHECK: CORROSION ON LAV WEB. REPLACED WEB.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410665Seat Track · corrodedPAE, D-CHECK: CORROSION ON LWR SURFACE OF SEAT TRACK. REPLACED SEAT TRACK.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0410669Web · crackedPAE, D-CHECK: AFT CARGO DOOR UPLATCH WEB IS CRACKED. REPLACED.Nov 30, 2004 · N746AS · Boeing 7372X6C · Cargo/Baggage DoorsSDR ASAA0410670Web · corrodedPAE, D-CHECK: CORROSION IN AFT CARGO WEB. REPLACED WEBNov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410666Seat Track · damagedPAE, D-CHECK: CROWN TOOTH DAMAGED ON SEAT TRACK. REPLACED SEAT TRACK.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0410668Web · corrodedPAE, D-CHECK: CORROSION ON LAV WEB. REPLACED WEB.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410672Seat Track · misinstalledPAE, D-CHECK: SEAT TRACK REQUIRES REPLACEMENT DUE TO FASTENER EDGE MARGIN. REPLACED SEAT TRACK.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0410673Seat Track · corrodedPAE, D-CHECK: CORROSION ON SEAT TRACK. REPLACED SEAT TRACK.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0410674Seat Track · misdrilledPAE, D-CHECK: SEAT TRACK HAS MISDRILLED HOLES. REPLACED SEAT TRACK.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0410675Web · gougedPAE, D-CHECK: AFT CARGO DOOR AFT CUTOUT CLOSURE WEB BETWEEN STRINGERS IS GOUGED. REPLACED WEB.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410676Seat Track · corrodedPAE, D-CHECK: CORROSION ON SEAT TRACK. REPLACED SEAT TRACK.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0410677Intercostal · corrodedPAE, D-CHECK: CORROSION ON INTERCOSTAL. REPLACED INTERCOSTAL.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410678Crease Beam · crackedPAE, D-CHECK: CREASE BEAM WEB IS CRACKED. REPLACED CREASE BEAM WEB.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Main, StructureSDR ASAA0410679Angle · corrodedPAE, D-CHECK: CORROSION ON WEB IB ANGLE BELOW CAPT NR 2 WINDOW. REPLACED WEB IB ANGLE.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410680Angle · corrodedPAE, D-CHECK: CORROSION ON WEB ANGLE. FABRICATED AND REPLACED WEB IB ANGLE.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410683Angle · corrodedPAE, D-CHECK: CORROSION ON WEB ANGLE. REPLACED WEB ANGLE.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410685Web · corrodedPAE, D-CHECK: CORROSION ON AFT LAV FLOOR WEB. REPAIRED WEB (K)Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR ASAA0410682Intercostal · corrodedPAE, D-CHECK: CORROSION ON AFT CARGO INTERCOSTAL. REPLACED INTERCOSTAL.Nov 30, 2004 · N746AS · Boeing 7372X6C · Fuselage Miscellaneous Structure
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