N641GT

Service difficulty reports · 1,011

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 = 'N641GT' 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 UIEA2012031500093Apu · faultedAPU FAULT ON START. PERFORMED APU BITE PROCEDURE IAW FIM 49-11-00/103, NO FAULTS NOTED. RESET ECU, APU START NORMAL ON SECOND ATTEMPT.Mar 13, 2012 · N641GT · Boeing 76738E · APU Start/Ignition SystemSDR UIEA2012030900087Slide · unwanted deployL1 DOOR SLIDE INADVERTENTLY DEPLOYED. R & R L-1 DOOR SLIDE IAW AMM 25-66-00, PG 201 & AMM 25-66-01, 401 & NBSP; INSTALL CHECKED GOOD.Mar 9, 2012 · N641GT · Boeing 76738E · Escape SlideSDR UIEA2012030700081Slide · unwanted deployL1 DOOR SLIDE WAS ACCIDENTALLY DEPLOYED AT GATE. REMOVED DEPLOYED SLIDE AND TRANSFERRED TO MDDR 29960, MEL 52-11-04-01 CAT. "A" ONE DAY.Mar 7, 2012 · N641GT · Boeing 76738E · Escape SlideSDR UIEA2012022600062Filter · failedAPU GENERATOR DIFFERENTIAL PRESSURE INDICATOR CHECK. ACCOMPLISHED W/C A-49-024-C1 APU/GEN DIFFERENTIAL PRESSURE INDICATOR CHECK. R & R SCAVENGE FILTER IAW AMM 49-27-03/401, LEAK CHECKED GOOD.Feb 26, 2012 · N641GT · Boeing 76738E · APU Oil SystemSDR UIEA2012021700053Igniter · unknownAPU IGNITOR PLUG TO BE REPLACED AS PRECAUTION DUE TO SLOW START. R & R APU IGNITOR PLUG IAW AMM 49-41-02 & NBSP; OPS CHECKED GOOD.Feb 17, 2012 · N641GT · Boeing 76738E · APU Start/Ignition SystemSDR UIEA2012021200044Warning Message · false activationRT OIL FILTER STATUS MESSAGE. STATUS MESSAGE ON ENGINE START SUSPECT EXTREME COLD CONDITIONS CAUSED MESSAGE. ALL TEMPS AND PRESSURES NORMAL, NON BY-PASS CONDITION. MESSAGE CLEARED AFTER NORMAL TEMPERTURE RANGE ACHIEVED REF AMM 79-35-00. CHIP DETECTOR CLEANFeb 12, 2012 · N641GT · Boeing 76738E · Central WarningSDR UIEA2012021100043Warning Message · false activationSTATUS " CAB ALT AUTO 1", PERFORMED FIM 21-31-00 FIG 103, NO FAULTS FOUND. OK FOR CONTINUED SERVICE, GROUND CHECKS GOOD IAW AMM 21-31-00)Feb 11, 2012 · N641GT · Boeing 7673S1 · Cabin Pressure Control SystemSDR UIEA2012012400025Relay · faultedSQUIB TEST PANEL ON TEST 1 "EMERGENCY ESCAPE" RT DOES NOT ILLUMINATE DURING TEST. TROUBLESHOT IAW WDM 25-65-12, FOUND TIME DELAY RELAY FAULTY. R & R, REF AMM 20-00-00.Jan 24, 2012 · N641GT · Boeing 76738E · Emergency EquipmentSDR UIEA2012011000008Lens · crackedCENTER OBSERVERS SEAT SMOKE GOGGLES LENS CRACKED (TRANSFERRED TO MDDR 28903. MEL 25-11-02-01B; OBSERVERS SEAT BLOCKED OUT FOR USE.)Jan 10, 2012 · N641GT · Boeing 76738E · Emergency EquipmentSDR UIEA2012010900007Controller · inoperativeRIGHT SIDE WINDOW HEAT INOPERATIVE, NR 2 WINDOW. MX R & R HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECKED GOOD.Jan 9, 2012 · N641GT · Boeing 76738E · Windshield/Door Rain/Ice RemovalSDR UIEA2012010800004Warning Message · false activationRT ENGINE CONTROL MESSAGE. PEFORMED "PIMU" RESET PROCEDURES IAW FIM 73-21-00. NO FAULTS NOTED. MESSAGE CLEARED.Jan 8, 2012 · N641GT · Boeing 76738E · Engine Indicating SystemSDR UIEA2012010300001Warning Message · false activationEICAS MESSAGE "RT SIDE WINDOW". PERFORMED FIM 30-41-00, FIG 103, ALL COMPONENTS CHECKED GOOD, OK FOR SERVICE.Jan 3, 2012 · N641GT · Boeing 76738E · Central WarningSDR UIEA2011121800719Flashlight · inoperativeAFT RT F/A SEAT EMERGENCY FLASHLIGHT INOPERATIVE. ITEM TRANSFERRED TO MDDR 28497. MEL 25-63-04.Dec 18, 2011 · N641GT · Boeing 76738E · Emergency EquipmentSDR UIEA2011121800720Warning Light · false activationSTATUS MESSAGE RT ENGINE CONTROL. PEFORMED FIM TABLES IAW FIM 73-21-00/71-PIMU. FAULT CLEARED, MESSAGE CLEARED PERFORMED GROUND TEST IAW FIM 71-PIMU. NO DEFECTS NOTED.Dec 18, 2011 · N641GT · Boeing 76738E · Engine Indicating SystemSDR UIEA2011121800721Processing Unit · malfunctionedFUEL QUANTITY CHANNEL MESSAGE, RT DISPLAYED STATUS MESSAGE. RESET FUEL QTY PROCESSOR IAW FIM 28-41-00/101, FIG 106. FAULT CLEARED NO FURTHER ISSUES.Dec 18, 2011 · N641GT · Boeing 76738E · Fuel Indicating SystemSDR UIEA2011121500717Controller · arcedLT WINDOW ARCING. R & R WINDOW HEAT CONTROL WITH REPAIRED UNIT IAW AMM 30-41-01, OPS CHECKED GOOD.Dec 15, 2011 · N641GT · Boeing 76738E · Windshield/Door Rain/Ice RemovalSDR UIEA2011121500718Window · crackedLT WINDOW CRACKED. REMOVED & INSTALLED NEW WINDOW AMM 56-11-01, INSTALLATION CHECKED GOOD, AND OPS CHECKED AMM 30-41-01.Dec 15, 2011 · N641GT · Boeing 76738E · Flight Compartment WindowsSDR UIEA2011121200716Outflow Valve · obstructedCABIN AUTO INOPERATIVE MESSAGE, FOUND INSULATION BLOCKING PRESSURE RELIEF VALVE. REMOVED INSULATION. CLEARED FAULT ON PRESSURE CONTROLLER. GROUND CHECKS GOOD IAW AMM 21-31-00, 21-32-00.Dec 12, 2011 · N641GT · Boeing 76738E · Pressure Regulator/Outflow ValveSDR UIEA2011120800706Pcb · failedAPU FIRE WARNING TEST HAS NO SPEAKER AURAL WARNING. REPLACED WARNING MODULE "M1000" IAW AMM 31-51-04. OPS CHECKED GOOD. REPLACED PRINTED CIRCUIT CARD "M618" IAW AMM 31-51-04. OPS CHECKED GOOD.Dec 10, 2011 · N641GT · Boeing 76738E · Fire DetectionSDR UIEA2011120700705Valve · failedFUEL MIGRATION FROM RT TO LT TANK. LT 18.2, CTR 0.2, RIGHT 3.8. FOUND DURING MX CHECK. (REPLACED RT TANK INBD FUELING SHUT-OFF VALVE IAW AMM 28-21-02, REF:W/O 7507, REPLACED RT MAIN TANK DEFUEL VALVE IAW AMM 28-26-01, REF W/O 7507, R & R FUEL PANEL DOORS 631Dec 7, 2011 · N641GT · Boeing 76738E · Aircraft Fuel Distribution SystemSDR UIEA2011120700704Warning System · malfunctionedAPU FIRE WARNING TEST HAS NO SPEAKER AURAL WARNING FOR T/S, WITH DOM'S APPROVAL IAW ETOPS MX MANUAL 5.1.5., SWAPPED M616 AND M621 POWER SUPPLY UNITS FOR TROUBLESHOOTING. NO HELP. RETURNED TO ORIGINAL POSITIONS. NG.)Dec 7, 2011 · N641GT · Boeing 76738E · Fire DetectionSDR UIEA2011113000701Fuel Sys · malfunctionedFUEL MIGRATION FROM RT TO LT TANK.; LT 18.2,; CENTER 0.2, RT 3.8. FOUND DURING MX CHECK. OPENNov 30, 2011 · N641GT · Boeing 76738E · Aircraft Fuel Distribution SystemSDR UIEA2011113000700Bulb · inoperativeEXTERNAL EMERGENCY LIGHT BURNED OUT AT R2 DOOR, RT ABOVE FLAP, LT AFT OF FLAP. R & R BULB.Nov 30, 2011 · N641GT · Boeing 76738E · Emergency LightingSDR UIEA2011110700641Starter · failedAPU WILL NOT START. R & R APU STARTER IAW MM 49-41-01. OPS CHECK OK. NO LEAK NOTEDNov 6, 2011 · N641GT · Boeing 76738E · APU Start/Ignition SystemSDR UIEA2011110700640Oil System · lowAPU FAILED TO START TWICE AFTER LANDING, OIL QTY SHOWS .25 (SERVICED APU ENGINE OIL WITH 1.5 QTS IAW AMM 49-90-00. NO LEAKS NOTED IN APU COMPARTMENT APU OPERATES NORMAL. BITE CHECK SHOWS NO FAULTS.)Nov 5, 2011 · N641GT · Boeing 76738E · APU Oil SystemSDR UIEA2011101900580Skin · puncturedDURING C-CHECK, FUSELAGE SKIN WAS FOUND WITH A SMALL PUNCTURE AT BS 1881-1890, S6-8L. DAMAGED AREA TRIMMED OUT AND A REPAIR DOUBLER INSTALLED IAW SR 1- 2006471601.Oct 19, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011101900583Skin · damagedPREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS WERE REMOVED AND THE DISCREPANT AREAS REWORKED, HFEC WAS PERFORMED AT EACH AREA. FASTENOct 19, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011101900570Floorbeam · corrodedDURING ROUTINE C4/A4 CHECK MX, DISCOVERED CORROSION ON THE FLOORBEAM UPPER TEE FORWARD FLANGE AT BS 1518 BETWEEN LBL 25.5 AND LBL 35.5. DAMAGED SECTION OF THE FLOORBEAM TEE WAS REPAIRED IAW SRM 53-10-51, FIG 201, REPAIR 4. THE REPAIR IS CLASSIFIED AS A CATAGOct 19, 2011 · N641GT · Boeing 76738E · Fuselage Main, Floor BeamSDR UIEA2011101900586Skin · damagedPREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED. HFEC WAS PERFORMED. REPLACEMENT FASTENERS INSTALLEOct 13, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011101900585Skin · damagedPREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS 307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED, HFEC WAS PERFORMED, REPLACEMENT FASTENERS WERE IOct 13, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011101900584Skin · damagedPREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED, HFEC WAS PERFORMED. REPLACEMENT FASTENERS INSTOct 13, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011101900582Skin · damagedPREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS BECAUSE THEY WERE LOCATED AT FASTENER LOCATIONS. REPAIR ACCOMPLISHED.Oct 13, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011102100606Trunnion · gougedLT MLG AFT TRUNNION BEARING, AFT ACCESS CAVITY EDGE HAS SEVERAL GOUGES. REPAIRED LT MLG AFT TRUNNION BEARING AFT ACCESS CAVITY IAW SRM 51-70-13.Oct 12, 2011 · N641GT · Boeing 76738E · Wing, Landing Gear Attach FittingsSDR UIEA2011102100605Floor Support · corrodedCORROSION ON KEELBEAM SUPPORT PANEL BRACE, BELOW PANEL 139E2. REMOVED CORROSION ON SUPPORT PANEL BRACE. FOUND CORROSION OUT OF LIMITS. R & R SUPPORT IAW SRM 51-10-02, 51-40-02. 53-30-12.Oct 12, 2011 · N641GT · Boeing 76738E · Fuselage Miscellaneous StructureSDR UIEA2011101900579Step · missingTHE STEP PORTION OF THE RT AFT OVERWING ESCAPE HATCH ASSY WAS FOUND MISSING. A REPLACEMENT STEP WAS FABRICATED.Oct 12, 2011 · N641GT · Boeing 76738E · Emergency ExitsSDR UIEA2011101900589Skin · damagedDURING C-CHECK, PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S33-35R AND FROM BS 307-384. BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED. HFEC PERFORMED. REPLACEMENT FASTENERS INOct 10, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011101900588Skin · damagedDURING C-CHECK, PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED. HFEC PERFORMED. REPLACEMENT FASTENOct 10, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011101900587Skin · damagedDURING C-CHECK, PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED. HFEC WAS PERFORMED. REPLACEMENT FASOct 10, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/SkinSDR UIEA2011101000566Floorbeam · damagedDURING ROUTINE C4/A4 CHECK MX DISCOVERED CORROSION ON THE UPPER TEE OF FLOORBEAM BS 1480 BETWEEN LBL 34 AND 60.5. THE DAMAGED SECTION OF THE FLOORBEAM TEE WAS REMOVED AND A NEW SECTION SPLICED IAW SRM 53, FIG 201, REPAIR 1. THE REPAIR IS CLASSIFIED AS A CATAOct 10, 2011 · N641GT · Boeing 76738E · Fuselage Main, Floor BeamSDR UIEA2011101000567Floorbeam · corrodedDURING THE C4 PLUS A4 CHECKS, CORROSION WAS DETECTED AT EXISTING NUT PLATES (10 PLACES) ON THE UPPER SURFACE OF THE LOWER TEE OF FLOORBEAM 146T5119-1 AT BS 1502. NUT PLATES WERE LOCATED AROUND CUTOUTS IN THE LOWER TEE OF FLOORBEAM AT LBL 2, LBL 7, LBL 14, LBL Oct 9, 2011 · N641GT · Boeing 76738E · Fuselage Main, Floor BeamSDR UIEA2011102100619Spar Cap · corrodedCORROSION ON SPAR CAP STA 176.000. REMOVED LIGHT CORROSION BETWEEN FASTENERS PERFORMED LT THICKNESS INSPECTION FOUND TO BE WITHIN LIMITS. TREATED AND PRIMED AREA.Oct 8, 2011 · N641GT · Boeing 76738E · Wing SparSDR UIEA2011102100618Structure · crackedSTRUCTURE CRACKED AT BS 1081 WHERE HYDRAULIC LINE PASSES THROUGH OTBD OF LT OVERWING SLIDE CYLINDER FWD END. CUTOUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER.Oct 8, 2011 · N641GT · Boeing 76738E · Fuselage Main, StructureSDR UIEA2011100600563Tie Down · corrodedTHE AFT F/A STATION TIE DOWN FITTING INSTALLED AT BS 1519.2, LBL 18.50 FOUND CORRODED. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW EO IH-53-0460, REV 01, DWG 6-1041-00-000, REV 1 AND DWG 6-1041-00-001, REV 0.Oct 5, 2011 · N641GT · Boeing 76738E · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2011102100608Skin · dentedNR 1 SPOILER LOWER SKIN DENTED 1.115 DIA, 0.045" DEEP. REPARIED DAMAGE.Oct 4, 2011 · N641GT · Boeing 76738E · SpoilersSDR UIEA2011102100614Floorbeam · corrodedCORROSION ON FLOORBEAM, BS 1518, LBL 30. REMOVED CORROSION, FOUND OUT OF LIMITS. CUT OUT DAMAGE AND ACCOMPLISHED REPAIR.Sep 28, 2011 · N641GT · Boeing 76738E · Fuselage Main, Floor BeamSDR UIEA2011102100616Mount Fitting · corrodedAFT GALLEY MOUNT FITTINGS SHOWED SIGN OF SURFACE CORROSION. R & R GALLERY MOUNT FITTINGS.Sep 26, 2011 · N641GT · Boeing 76738E · Fuselage Main, Attach FittingsSDR UIEA2011101900593Structure · corrodedDURING C-CHECK, REAR GALLEY FOUND CORRODED. FACE TRIM WAS REPLACED, ANY REMAINING DAMAGE WAS REPAIRED IAW CMM 25-38-386, REV 2.Sep 22, 2011 · N641GT · Boeing 76738E · Buffet/GalleysSDR UIEA2011101900572Structure · corrodedTHE FWD GALLEY WAS FOUND WITH HONEYCOMB PANEL DAMAGE. CORROSION WAS FOUND ON THE FWD U-CHANNEL AND THE COUNTERTOP SURFACE WAS FOUND DAMAGED. REMOVAL OF THE BONDED COUNTERTOP SURFACE RESULTED IN MINOR DAMAGE TO THE UNDERLYING COMPOSITE PANEL. CORROSION WAS ASep 22, 2011 · N641GT · Boeing 76738E · Buffet/GalleysSDR UIEA2011102100615Structure · crackedNR 2 ENG OTBD STRUCTURE FWD LOWER CORNER OF THE ACCESS CUTOUT FOR FIRE BOTTLE WITH A CRACKED LOWER CORNER. REMOVED PANEL, STOPPED DRILL THE CRACK, PERFORMED NDT INSP. REPAIRED THE DAMAGE AREA AND INSTALLED THE PANEL.Sep 21, 2011 · N641GT · Boeing 76738E · Nacelle/Pylon, Main FrameSDR UIEA2011092900528Skin · crackedDURING THE C4/A4 CHECK, A 3.5 INCHES WIDE (A) WITH A DEPTH (Y) OF 0.030" DENT WAS FOUND ON THE FUSELAGE SKIN AT BS 1197+132, BETWEEN S39L AND S39R. DENT WAS DETERMINED TO BE WITHIN LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. HFEC INSPECTION DETECTED A CRSep 18, 2011 · N641GT · Boeing 76738E · Fuselage Main, Plate/Skin
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