N663GT

Service difficulty reports · 245

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N663GT' AND registry_match = 'registration'
  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 UIEA2019081535081Start Valve · malfunctionedSTART VALVE NOT FULLY OPEN DURING ENG RUN TEST, LT ENGINE. REPLACED THE LT ENG START VALVE IAW AMM 80-11-02-004-001 & AMM 80-11-02-004-017.Aug 12, 2019 · N663GT · Boeing 767324 · Engine Start Valves/ControlsSDR UIEA201908153075Filter · dirtySTARTER VALVE PNEUMATIC FILTER CLEAN AND REINSTALL(<P>PFM ESN 707422 STARTER VALVE FILTER CLEAN IAW AMM 80-11-04-002-001 & AMM 80-11-04-112-019.</P>)Aug 12, 2019 · N663GT · Boeing 767324 · Engine Start Valves/ControlsSDR UIEA2019081535110Coupling · looseFOUND ENG (SN: 707425) PNEUMATIC DUCT COUPLING LOOSE AND WITH NO SAFETY WIRE. TOTAL OF 3 LOCATIONS, NEAR FUEL MANIFOLD.(<P>REMOVED ENG (SN 707425) 14TH PNEUMATIC DUCT IAW AMM 70-52-00-912-001 REV. 127. PERFORMED ENG 14TH PNEUMATIC REPAIR AND TEST COMPLETED IAWAug 12, 2019 · N663GT · Boeing 767324 · Pneumatic Distribution SystemSDR UIEA2019081535098Valve · malfunctionedFOUND RT FAMV ALWAYS IN REGULATOR DURING ENG RUN. REMOVED AND REPLACED THE RT ENG FAN AIR VALVE IAW AMM 36-11-16-004-001 REV. 127. PERFORMED RT ENG FAN AIR VALVE OPERATIONAL TEST IAW AMM 36-11-16-404-015 REV. 127, OPS TEST NORMAL. CONDITION CHECKED SATISFACTAug 12, 2019 · N663GT · Boeing 767324 · Pneumatic Distribution SystemSDR UIEA2019081535097Warning Message · false activationIDG FILTER, CHECK OIL FILTER PRESSURE INDICATOR POSITION.(<P>PERFORMED OIL FILTER PRESSURE INDICATOR POSITION CHECK IAW 24-11-01-246-211 REV. 127. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. </P>)Aug 12, 2019 · N663GT · Boeing 767324 · AC Generator-AlternatorSDR UIEA2019081535095Warning Message · false activationSTARTER CHIP DETECTOR, PERFORM A VISUAL INSPECTION. PERFORMED STARTER CHIP DETECTOR INSPECTION IAW AMM 80-11-01-206-014-H00 REV. 127, RESULTS CHECK NORMAL FOR ENG SN: 707425.</P>)Aug 12, 2019 · N663GT · Boeing 767324 · Engine StarterSDR UIEA2019081505193Support Channel · corrodedSUPPORT CHANNEL, BULK CARGO COMPARTMENT, BS 1415 - 1540, BL 0 CORRODED. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV. 110. INSTALLED NEW SUPPORT CHANNEL WITH FASTENERS IAW SRM 51-40-02-0G-0, DWG 146T5002 SH 2 REV F, DWG 657T5102 SH 6 REV A, DWG 146T5002 SHAug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081545166Module · corrodedFOUND GROUND MODULE GD04170B LOCATED AT BS 590, WL127, LBL 60 CORRODED. REMOVED CORRODED GROUND MODULE IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW GROUND MODULE IAW SRM 51-40-02-0G-0 REV.110. REMOVED & REINSTALLED GD04170B GROUND MODULE PINS IAW SWPM 20-90-11Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Structure (General)SDR UIEA2019081545165Block · corrodedFOUND GROUND BLOCK OF GD00202 LOCATED AT STA 547, WL 123, LBL 55 FOUND CORRODED. REMOVED CORRODED GROUND BLOCK IAW SRM 51-04-02-0G-0 REV 110. INSTALLED NEW GROUND BLOCK ON REPAIR ANGLE IAW EI T2019A53M-2632 REV.2. REMOVED & RE-INSTALLED GD00202 GROUND MODUAug 12, 2019 · N663GT · Boeing 767324 · Fuselage Structure (General)SDR UIEA2019081545164Support Angle · corrodedCORROSION - SUPPORT ANGLE, FWD CGO FLOOR STRUCTURE STA 632 TO STA 610, RBL 31. REMOVEDDAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PART IAW SRM 51-40-02-0G-0 REV.110 AND DWG 143T5012 SH 3 REV G.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081535108Support Channel · corrodedCORROSION - SUPPORT CHANNEL, BULK CARGO COMPARTMENT STA 1415 TO STA 1540, LBL 7.9. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0, REV 110. INSTALLED NEW SUPPORT CHANNEL WITH FASTENERS IAW SRM 51-40-02-0G-0, REV. 110, AND DWG 146T5002, SH 1, REV E.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081535107Bracket · corrodedBRACKET, AFT CGO COMPARTMENT AT STA 1263, BETWEEN LBL 6.5 AND LBL 22.5 CORRODED. REPLACED THE BRACKET WITH NEW IAW SRM 51-42-01-0G-0 REV.110, DWG 453T1227, SH 2, REV A, AND 453T1223 SH 3.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, Attach FittingsSDR UIEA2019081435045Warning Light · false activationIDG QAD COUPLING-CHECK TORQUE AND CONDITION. PFM QAD COUPLING TORQUE CHECK. RESULT NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · AC Generator-AlternatorSDR UIEA2019081435043Warning Light · false activationIDG QAD COUPLING-CHECK TORQUE AND CONDITION. PERFORM QAD COUPLING TORQUE CHECK. RESULT NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · AC Generator-AlternatorSDR UIEA2019081435041Warning Light · false activationIDG FILTER- CHECK OIL FILTER PRESSURE INDICATOR POSITION. EXAMINED OIL FILTER PRESSURE INDICATOR POSITION. RESULT NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · AC Generator-AlternatorSDR UIEA2019081435039Warning Light · false activationSTARTER CHIP DETECTOR - PERFORM A VISUAL INSPECTION. PERFORM ENGINE STARTER CHIP INSPECTION. RESULT: COND CHK SATIS.</P>)Aug 12, 2019 · N663GT · Boeing 767324 · Engine StarterSDR UIEA2019081405161Bracket · wornBRACKET WORN, NR 1 PYLON PRV R/H PNEUMATIC DUCT SUPPORT LINK. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 REV.110 AND DWG 311T2150 SH 5, REV 0.Aug 12, 2019 · N663GT · Boeing 767324 · Nacelle/Pylon, Main FrameSDR UIEA2019081435069Support Plate · corrodedCORROSION DAMAGE ON RT WING INBD AILERON HINGE SUPPORT PLATE AT WS 508.(<P>REMOVED CORROSION SUPPORT PLATE IAW SRM 51-40-02-0G-0 REV 110. PERFORMED CORROSION AREA REPAIR IAW EI NO T2019A57M-3398 REV.1. INSTALLED SUPPORT PLATE IAW SRM 51-40-02-0G-0 REV.110 AND Aug 12, 2019 · N663GT · Boeing 767324 · AileronsSDR UIEA2019081305047Inlet · scratchedSCRATCHES ON THE INLET, NR 1 ENG NOSE COWL, FROM 5 TO 7 O'CLOCK. REMOVED SCRATCH AND MEASURED THE REWORKED AREA; DEPTH = 0.003", LENGTH = 2.8", WIDTH = 1.2". IT IS WITHIN ALLOWABLE LIMIT IAW SRM 54-12-01-1A-1 DETAIL III REV. 110 AND JOB CARD ATTACHING SHEET COAug 12, 2019 · N663GT · Boeing 767324 · Turbine Engine Air Inlet SectionSDR UIEA2019081435044Skin · corrodedFOUND AFT CARGO UNDER FLOOR AREA CORROSION AT BS 1197+22 - 1197+44, S-36R TO S-37R. REMOVED THE CORROSION IAW SRM 51-10-02-0G-0 REV. 110. REPAIRED IAW EI T2019A53M-3220 REV. 1. CONDITION CHECK NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, Plate/SkinSDR UIEA2019081435040Stringer · corrodedFOUND BS 1197+132, STRINGER 17R CORRODED. REPAIRED THE STRINGER IAW EI T2019A53M-2637 REV 1. CONDITION CHECKED NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, Longeron/StringerSDR UIEA2019081435030Stringer · corrodedFOUND STRINGER S-32L, STA 544 - 566 CORRODED. REPAIRED AREA IAW EI T2019A53M-2632, REV 2. CONDITION CHECKED NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, Longeron/StringerSDR UIEA2019081305068Support Channel · corrodedCORROSION - SUPPORT CHANNEL, BULK CGO COMPARTMENT SUPPORT CHANNEL STA 1415 TO STA 1540, RBL 42.(<P>REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS WITH FASTENERS IAW SRM 51-40-02-0G-0 REV 110, DWG 146T5002 SH 1 REV E, DWG 146T5002 SH 3 Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081305066Tray · corrodedFWD CGO ROLLER TRAY CORROSION AT STA 654+88, RBL 20.(<P>REPAIRED THE CORROSION AREA IAW SRM 53-00-53-2R-1 REV.110 AND EI NO T2019A53M-3086 REV 1. JOB COMPLETED AND CONDITION CHECKS NORMAL. ORIGINAL EI ATTACH ON W/O NO 3434859.</P>)Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081435060Tee Fitting · crackedCRACK -TEE, NOSE WHEEL WELL BULKHEAD VERTICAL TEE LH SIDE AT STA 287, BL 25, WL 172.(<P>PERFORMED CRACK AREA REPAIR IAW EO NO 6753A027 PART 3 AND SRM 51-70-12-0G-0 REV 110. JOB COMPLETED AND CONDITION CHECKS NORMAL.</P>)Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081435059Angle · brokenBROKEN - ANGLE, AFT CGO DOOR ANGLE INNER LOWER SIDE.(<P>REPAIRED DAMAGE AREA IAW EI NO T2019A52M-2884 REV 1. JOB COMPLETED AND CONDITION CHECKS NORMAL.</P>)Aug 12, 2019 · N663GT · Boeing 767324 · Cargo/Baggage DoorsSDR UIEA2019081435058Tray · corrodedFWD CARGO ROLLER TRAY HAS CORROSION AT STA 610, RBL 6. REPAIRED THE CORROSION AREA IAW SRM 53-00-53-2R-1 REV 110 AND EI T2019A53M-3086 REV 1. CONDITION CHECKS NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, StructureSDR UIEA2019081435051Structure · corrodedFOUND THAT OVERWING FILL PORT ON BOTH WINGS HAS CORROSION AROUND THE STRUCTURE.(<P>REPAIRED CORROSION AREA IAW EI NO T2019A57M-2788 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Aug 12, 2019 · N663GT · Boeing 767324 · Wing Main, Frame StructureSDR UIEA2019081435042Skin · crackedCRACK-SKIN, OSS 646.35, RH WING NO. 9 SLAT, UPPER SURFACE(<P>REPAIRED THE CRACK AREA IAW SRM 57-43-01-2R-2, REPAIR 2, REV 110. JOB COMPLETED AND CONDITION CHECKS NORMAL.</P>)Aug 12, 2019 · N663GT · Boeing 767324 · Leading Edge DevicesSDR UIEA2019081305034Skin · crackedOSS 792.54, WING NR 10 SLAT UPPER SURFACE SKIN CRACKED. REPAIRED THE CRACKED AREA IAW SRM 57-43-01-2R-2, REPAIR 2, REV 110. CONDITION CHECKED NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Leading Edge DevicesSDR UIEA2019081305035Skin · crackedNR 3 SLAT DAMAGED, OUTBOARD NOSE SKIN RIVET SURROUND MINOR CRACK DAMAGE OSS 792. REPAIRED THE CRACKED AREA IAW SRM 57-43-01-2R-2, REPAIR 2, REVISION 110. CONDITION CHECKED NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Leading Edge DevicesSDR UIEA2019081305037Angle · corrodedANGLE CORRODED, BULK CARGO COMPARTMENT, LOWER SIDE ANGLE BS 1540, RBL 0 TO RBL 32. REMOVED DAMAGE PARTS IAW SRM 51-40-02-02-0G-0 REV.110. FABRICATED NEW ANGLE IAW EI T2019P53M-2874 REV.0. INSTALLED THE NEW ANGLE WITH FASTENERS IAW SRM 51-40-02-0G-0 REV.110,Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081325012Door Frame · corrodedCORROSION ON THE FRAME CHANNEL OF L1 DOOR SURROUND AT DOOR STA 123.7 NEAR S-11L.(<P>PERFORMED CORROSION REPAIR ON THE FRAME CHANNEL OF L1 DOOR SURROUND AT DOOR STA 123.7, NEAR S-11L IAW EI NO: T2019A53M-2633 REV 1. JOB COMPLETED AND CONDITION CHECKS NORMAL.</Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, StructureSDR UIEA2019081305029Floor Support · corrodedFLOOR SUPPORT CORRODED, FWD CARGO COMPARTMENT, BS 544 TO 632, LBL 44. REMOVED FLOOR SUPPORT IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 REV 110, DWG 451T1504, SH4, REV. C, AND DWG 143T5010, SH17, REV E. CONDITION CHECKED Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081305031Skin · crackedNR 3 SLAT, INBOARD NOSE SKIN RIVET SURROUND SKIN MINOR CRACK DAMAGE OSS 723.(<P>REPAIRED THE CRACKED AREA IAW SRM 57-43-01-2R-2, REV 110. CONDITION CHECK NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Leading Edge DevicesSDR UIEA2019081325008Angle · corrodedFOUND M/D BS 977, S-14.5L BRACKET CORRODED. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. FABRICATED NEW ANGLE IAW EI T2019P53M-2879, REV 0. INSTALLED A NEW ANGLE WITH FASTENERS IAW SRM 51-40-02-0G-0, REV 110, AND DWG 145T1308, SH 7, REV A. CONDITIOAug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081325010Stringer · corrodedFOUND M/D STRINGER CORRODED, BS 1406, S19R. REPAIRED CORROSION AREA IAW EI T2019A53M-2939 REV 1. CONDITION CHECKED NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, Longeron/StringerSDR UIEA2019081325011Support Angle · corrodedCORROSION - SUPPORT ANGLE, AFT CGO COMPARTMENT, STA 1329 TO STA 1335, RBL 14.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV. 110. FABRICATED NEW STRAP IAW EI NO T2019P53M-2875 REV. 0. INSTALLED NEW STRAP IAW SRM 51-40-02-0G-0 REV 110, DWG NO 146T5000 SH18Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081394983Skin · crackedCRACKED SKIN, OSS 871.63, RT WING NR 11 SLAT, UPPER SURFACE. REPAIRED THE AREA IAW SRM 57-43-01-2R-2, REPAIR 2 REV. 110. CONDITION CHECKED NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Leading Edge DevicesSDR UIEA2019081394985Support Channel · corrodedCORROSION - SUPPORT CHANNEL, BULK CARGO COMPARTMENT AT STA 1415 TO STA 1540, RBL 36.5.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 110 AND DWG NO: 146T5002 SH 1 REV E. JOB COMPLETED AND CONDITION CHECK Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081394986Support Channel · corrodedCORROSION - SUPPORT CHANNEL, BULK CARGO COMPARTMENT, STATION 1415 TO STA 1540, RBL 12.8.(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 110 AND DWG 146T5002 SH 1 REV E. JOB COMPLETED AND CONDITION CHECK NOAug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081394987Support Channel · corrodedCORROSION - SUPPORT CHANNEL, BULK CARGO COMPARTMENT STATION 1415 TO STA 1540, RBL 7.9. REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 110 AND DWG NO 146T5002 SH 1 REV E. CONDITION CHECKED NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Miscellaneous StructureSDR UIEA2019081394988Stringer Splice · corrodedSTRINGER SPLICE CORRODED, FWD CARGO COMPARTMENT, LOWER LOBE BS 429, STRINGER 39R. REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW PARTS WITH FASTENERS IAW SRM 51-40-02-0G-0 REV 110, DWG NO 140T0110 SH 30, AND 140T0110 SH 33.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, Longeron/StringerSDR UIEA2019081394989Frame · corrodedFOUND FRAME CORRODED AT BS 1109, STRINGER 17L. REPAIRED THE FRAME IAW EI T2019A53M-2786, REV 1.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, FrameSDR UIEA2019081325006Frame · corrodedFWD BS 1197 + 66, STRINGER 18L FRAME CORRODED. REPAIRED THE FRAME IAW EI T2019A53M-2779, REV 1. CONDITION CHECKED NORMAL.Aug 12, 2019 · N663GT · Boeing 767324 · Fuselage Main, Frame
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