N857GT

Service difficulty reports · 97

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 = 'N857GT' 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 P5CA2023072200049Support Rib · unknownRH HORI STAB ACCESS PANEL 344QB O/B SUPPORT RIB UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPLACEMENT AS PER SRM 51-10-02, NEW UPPER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW UPPER CHORD INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023 )</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous StructureSDR P5CA2023072200050Unknown · unknownRH HORI STAB ACCESS PANEL 344QB O/B SUPPORT RIB LWR CHORD FOUND CRACK(<P>LOWER CHORD CRACK AREA REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 FIG 201 REV 40 DATE 20 JUN 2023</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous StructureSDR P5CA2023072200051Web · unknownRH HORI STAB ACCESS PANEL 344QB O/B SUPPORT WEB FOUND CRACK(<P>WEB REPLACEMENT AS PER SRM 51-10-02, NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW WEB INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023 )</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous StructureSDR P5CA2023072500052Support Rib · unknownLH HORI STAB TIP FAIRING SUPPORT RIB NO.8 FOUND CRACK ( COUNT FROM FWD )(<P>CRACK SUPPORT RIB REPLACED AS PER SRM 51-10-02, NEW RIB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW RIB INSTALLED AS PER SRM 51-40-02 ( SRM REV 40, DATE 20 JUN 2023 )</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous StructureSDR P5CA2023072500053Stringer · unknownSTA 2598 - 2618 STR 42R FOUND CRACK(<P>CRACK STRINGER REPLACED AS PER RI NO : RI-53-80-16393 REV A ( CATERGORY C ) </P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR P5CA2023080100055Unknown · unknownRHW NO.20 V/C FLAP LSA FOUND DAMAGE(<P>PERFORMED REPAIR AT LSA DAMAGE AREA PER CMM 57-55-42 REPAIR 17-1</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Wing StructureSDR P5CA2023080100056Unknown · unknownRHW NO.19 V/C FLAP LSA FOUND DAMAGE(<P>PERFORMED REPAIR AT LSA DAMAGE AREA PER CMM 57-55-42 REPAIR 17-1</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Wing StructureSDR P5CA2023080100057Unknown · unknownRHW NO.20 V/C FLAP LSA FOUND DAMAGE(<P>PERFORMED REPAIR AT LSA DAMAGE AREA PER CMM 57-55-42 REPAIR 17-1</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Wing StructureSDR P5CA2023080200058Unknown · unknownLH HORI. STAB. TIP SUPPORT U CHNNEL FOUND CRACK(<P>BONDED NEW U CHANNEL PER RI NO: RI-55-10-16388 REV.A</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Empennage StructureSDR P5CA2023080200059Unknown · unknownRHW I/B FLAP FOUND FASTENER HOLES ELONGATED(<P>PERFORMED REPAIR AT ELONGATED FASTENER HOLES AREA PER SRM 51-70-04 REPAIR 5</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Flight Control SystemSDR P5CA2023080300065Unknown · unknownLHW L/E LOWER PANEL UNDER #1E V/C FLAP FOUND CRACK(<P>PERFORMED REPAIR AT CRACK AREA PER RI-57-41-16401 REV.A</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Wing StructureSDR P5CA2023080400066Unknown · unknownRETAINER BROKEN AT LH I/B AIL I/B UPPER AFTPOSITION(<P>BROKEN RETAINER REPAIRED AS PER RI NO : RI-57-51-46408 REV B</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Flight Control SystemSDR P5CA2023080700068Unknown · unknownRHW T/E O/B FLAP TORQUE TUBE FOUND CHAFING AT 673BB UPPER AREA(<P>SMOOTHER SURFACE ROUGHNESS AND RUN OUT BLEND IAW RI NO : RI-27-51-16400 REV B</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Flight Control SystemSDR P5CA2023081300073Unknown · unknownRH HORIZ STAB AFT SUPPORT CHANNEL FOUND CRACK(<P>RH HORIZ STAB ACCESS PANEL 344GB AFT SUPPORT CHANNEL REPLACED AND INSTALLED AS PER RI-55-10-16398 REV A DATE 15 AUG 2023.</P>)Aug 18, 2023 · N857GT · Boeing 74787UF · Empennage StructureSDR P5CA2023062000032Control Unit · unknownAIR RETURN DUE TO RH OTBD AILERON INOP(<P>R/R RH OTBD AILERON PER AMM 27-11-13, LEAK CHECK GOOD, MSG CLEARED. OPS CHECK GOOD PER AMM 27-11-13. DMI 187643 CLOSED.</P>)Jun 19, 2023 · N857GT · Boeing 74787UF · Flight Control SystemSDR P5CA2021063000251Fitting · crackedRH CANTED PRESSURE DECK, A FASTENER HOLE OF OUTERMOST FITTING WAS FOUND 2EA CRACKS AT APPROX. STA 1241 RBL 125.(<P>RH CANTED PRESSURE DECK. STA 1241 RBL 125 FASTENER HOLE REPAIRED AS PER RI-53-45-14705 REV A.</P>)Jul 6, 2021 · N857GT · Boeing 74787UF · Fuselage Main, StructureSDR P5CA2021062900250Partition · damagedBULK CARGO - STA 2160 PARTITION LOWER EDGE TORN AND L/R ATT FABRIC LINER.(<P>BULK CARGO - STA 2160 PARTITION LOWER FABRIC LINER REPAIRED AS PER RI NO. RI-25-54-14673 REV A 24 JUN 2021.</P>)Jul 6, 2021 · N857GT · Boeing 74787UF · Cargo CompartmentsSDR P5CA2021062800248Spar · damagedRH ELEVATOR FRONT SPAR STA 186.80 STIFFENER HAS HOLES ELONGATE AT I/B AND O/B SIDE.(<P>RH ELEVATOR FRONT SPAR STA 186.80 STIFFENER ELONGATED HOLES REPAIRED AS PER RI-55-33-14694 REV A. </P>)Jul 6, 2021 · N857GT · Boeing 74787UF · Elevator, Spar/RibSDR P5CA2021062000245Switch · faultedEO. 4852A037 PART 1, SB 747-52-2307 FWD CARGO DOOR CONTROL SWITCH PAN CLIPS FOUND DISCREPANCIES.(<P>EO. 4852A037 PART 1, SB 747-52-2307 FWD CARGO DOOR CONTROL SWITCH PAN CLIPS INSTALLED IAW RI-52-00-14681 REV A. </P>)Jul 6, 2021 · N857GT · Boeing 74787UF · Cargo/Baggage DoorsSDR P5CA2021022200048Tube · crackedNUMBER 4 ENGINE OIL SYS STATUS MESSAGE, PRECAUTIONARY SHUTDOWN OF NR 4 ENG PER QRH. M12 - DURING A/C BACK TO GATE W/ REGARDS TO ENG NR 4 OIL SYS STATUS MSG FOUND OIL CAP NOT INSTALLED PROPERLY. (PERFORMED PRECAUTIONARY INSPECTION OF NR 4 ENG FUEL OIL HEAT EXCFeb 21, 2021 · N857GT · Boeing 74787UF · Turbine Engine Oil SystemSDR P5CA2020121900407Connector · damagedGEAR CENTER CONFIG EICAS, REJECTED TAKE OFF DUE TO GEAR HORN BODY GEAR STEERING, REF MDDR NR 139776. BODY GEAR STEERING INOPERABLE, MEL CHANGED FROM 32-53-01 TO 32-53-02, CAT C. COMPLETED MAINT PROCEDURES. REMOVED CONNECTOR ON LT BG-RH ACT.Dec 19, 2020 · N857GT · Boeing 74787UF · Landing Gear System WiringSDR P5CA2020091510306Actuator · malfunctionedUPON GEAR RETRACTION ON T/OFF 'GEAR TILT' EICAS MSG, UNABLE TO RETRACT GEAR PER ECL CHECKLIST, AIR TURN BACK. REMOVED AND REPLACED GEAR TILT/ACTUATOR, IAW AMM 32-11-20. FOUND NR 13 BRAKE TORQUE SENSOR DAMAGE, REPLACED NR 13 BRAKE TORQUE SENSOR, IAW AMM 32-42Sep 11, 2020 · N857GT · Boeing 74787UF · Landing Gear ActuatorSDR P5CA2019081200168Wire · damagedFOUND THE NR 1 APU GENERATOR PIN N HAD SPARK MARK. DISCONNECTED APU GENERATOR 1 WIRE IAW JC ATTACHING SHEET 0192683. REPLACED THE GENERATOR WITH NEW PARTS IAW AMM 24-21-03-004-001, REV 30, AND AMM 24-21-03-404-023, REV 30. PERFORMED APU GENERATION INSTALLATAug 11, 2019 · N857GT · Boeing 74787UF · Electrical Power System WiringSDR P5CA2019081200167Ram Air Turb · inoperativeFOUND RAT RPM SHOWING ZERO WHEN PERFORMING FUNCTIONAL CHECK OF THE RAT SYSTEM. REMOVED AND REPLACED RAT PUMP IAW AMM 29-21-02-000-801, REV 30, AND AMM 29-21-02-400-801, REV 30, STEP 2A - 2F. REMOVED AND REPLACED RAT GCM IAW AMM 29-21-20-000-801 AND 29-21-400-Aug 11, 2019 · N857GT · Boeing 74787UF · Hydraulic Accumulator, AuxiliarySDR P5CA2019081200166Rib · crackedRIGHT WING, INBD L/E CAVITY UPPER RIB CRACKED AT LOWER SUPPORT ATTACH AREA, IFSS 439.34. REPAIRED THE DAMAGED AREA IAW EI T2019A57M-3413, REV 1, AND DWG 11642014, SH 3, REV A. CHECKED NORMAL.Aug 11, 2019 · N857GT · Boeing 74787UF · Wing, Rib/BulkheadSDR P5CA2019021900024Engine · making metalAFTER LEVELING OFF AT FL 320, # 2 ENGINE OIL PRESSURE WENT TO ZERO. SHUT DOWN ENGINE. NO N1 AFTER FIVE MINUTES.(<P>REMOVED # 2 ENGINE DMS AND FOUND MULTIPLE METAL CHIPS (LP: 719032, ITEM: 1). CARRIED OUT INSPECTIONS OF #2 ENGINE DMS OIL FILTER, A, B, C SUMP, Feb 16, 2019 · N857GT · Boeing 74787UF · Engine (Turbine/Turboprop)SDR P5CA2017072600234Fitting · damagedNR 1 PYLON AFT STRUT UPPER LATERAL RESTRAINT FITTING INBD LOWER CORNER FOUND CONDUCTIVITY IS 37.6% IACS. THE RESTRAINT FITTING REPLACED IAW R1-54-00-11949, REV B.Jul 24, 2017 · N857GT · Boeing 74787UF · Nacelle/Pylon, Main FrameSDR P5CA2017072600235Panel · crackedNR 3 PYLON TOP PANEL 611GT INTERIOR VAPOR PANEL OTBD AND AFT CORNER FOUND CRACKED. REPAIRED IAW R1-57-41-11957, REV A.Jul 24, 2017 · N857GT · Boeing 74787UF · Nacelle/Pylon, Main FrameSDR P5CA2017072600236Panel · crackedLT PYLON TOP PANEL 511GT INTERIOR VAPOR PANEL OTBD AND AFT CORNER FOUND CRACKED. REPAIRED IAW R1-57-41-11956, REV A.Jul 24, 2017 · N857GT · Boeing 74787UF · Nacelle/Pylon, Main FrameSDR P5CA2017072600237Support Channel · crackedLEFT WING REAR SPAR TO MLG SUPPORT BEAM CAVITY, ABOVE THE NR 4 FLAP TRACK. SUPPORT CHANNEL AFT AREA FOUND CRACKED. REPAIRED IAW R1-57-22-11947, REV A.Jul 24, 2017 · N857GT · Boeing 74787UF · Wing Miscellaneous StructureSDR P5CA2017072600238Support · dentedAFT CARGO BAY BS, 1820 BL 0, CENTER GUILD SUPPORT FOUND DENTED. REPLACED IAW R1-53-65-11963, REV A.Jul 24, 2017 · N857GT · Boeing 74787UF · Fuselage Miscellaneous StructureSDR P5CA2017072600239Floor Support · crackedRIGHT BS 350, RBL 74, FLOOR SUPPORT CRACKED. THE FLOOR SUPPORT WAS REPAIRED IAW R1-25-55-11966, REV A.Jul 24, 2017 · N857GT · Boeing 74787UF · Fuselage Miscellaneous StructureSDR P5CA2017072600240Angle · crackedLEFT HORIZONTAL STAB TIP FAIRING LOWER SUPPORT ANGLE CRACKED AT HSS 421.5. REPAIRED IAW R1-55-10-11964, REV A.Jul 24, 2017 · N857GT · Boeing 74787UF · Horizontal Stabilizer StructureSDR P5CA2016062400150Pin · defectiveDOOR MAIN ELECTRICAL CENTER EICAS MESSAGE, DOOR INSPECTED AND FOUND AFT PIN WOULD NOT DISENGAGE AND DEFECTIVE. ITEM DEFERRED IAW DDG 52-48-01.Jun 24, 2016 · N857GT · Boeing 74787UF · Door Warning SystemSDR P5CA2016030100062Pneumatic System · malfunctionedSTARTER CUTOUT EICAS MESSAGE 1.5 HRS AFTER TAKEOFF. ON RETURN TO DEPARTURE MESSAGE WENT AWAY BUT GOT BLEED 4. CYCLING ON/OFF WITH 10-15 PSI DUCT PRESSURES ON ISOLATED SIDE. FOUND ENGINE 4 PRSOV PARTLY OPEN ON ENGINE SHUTDOWN CAUSING BACK PRESSURE AND STARTFeb 29, 2016 · N857GT · Boeing 74787UF · Pneumatic Distribution SystemSDR P5CA2015083100114Skin · dentedDENT FOUND ON EXTERNAL SKIN AT BS 2038, S39L. REPAIRED IAW E.I T2015 A 5, B1944, REV.4.Aug 29, 2015 · N857GT · Boeing 74787UF · Fuselage Main, Plate/SkinSDR P5CA2015051800041Smoke Detector · false activationAFT CARGO FIRE WARNING AND EICAS DURING CRUISE AT 35,000 FT. WARNINGS CLEARED AFTER 10 SECONDS. CMC REVIEWED AND AFT LOWER LOBE DETECTOR 11 FAILED. AFT CARGO SMOKE DETECTOR 11 REPLACED AND TEST OK IAW AMM 26-16-01.May 16, 2015 · N857GT · Boeing 74787UF · Smoke DetectionSDR P5CA2015031700018Fire Warning · false activationDURING CLIMB, APPROXIMATELY 11,000', FIRE BELL SOUNDED FOR 2 SECONDS. NO FIRE OR SMOKE INDICATIONS. NO EICAS WARNINGS, ALERTS OR FIRE LIGHTS. REPEAT WRITE UP. FIRE BELL SOUNDED REPEATEDLY EVERY 30 SECONDS FOR 3 SECONDS WITH WHEEL WELL EICAS MESSAGE AND MASMar 12, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015031100016Fire Warning · false activationTWO TIMES DURING CRUISE FIRE BELL SOUNDED 1-2 SECONDS; NO FIRE OR SMOKE INDICATIONS, NO EICAS WARNING, ALERT OR FIRE LIGHTS. NO FAULTS NOTED IN CMC. RAN CMC GROUND TEST FIRE PROTECTION. TEST PASSED AND OPS CHECK NORMAL. REF AMM 26-11-00.Mar 10, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015030900014Unknown · unknownLOW SPEED RTO, ICN DEPT 33L AFTER T/O THRUST SET ACFT VEERED SHARPLY TO THE RT. EICAS MASTER WARNING CONFIGURATION GEAR CTR, MESSAGE. CHECKED PRESENT LEG, EXISTING FAULTS. NO MESSAGE FOUND. TESTED CONFIDENCE T/O WARNING, BODY GEAR STEERING. MAIN & NOSE TIREMar 7, 2015 · N857GT · Boeing 74787UF · Landing Gear SystemSDR P5CA2015022300012Fire Warning · false activationDURING CLIMB OUT, FIRE BELL AURAL SOUNDED TWICE WITHOUT OTHER VISUAL WARNINGS. ENTRY 689531-3, 22FEB15. CHECKED CMC. NO MESSAGE FOUND IN PRESENT LEG, EXISTING FAULT HISTORY. C/W FIRE TEST IAW AMM 26-10-00 AND TEST PASSED.Feb 23, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015022300011Fire Warning · false activationAFTER LANDING FIRE BELL OF UNKNOWN ORIGIN. NO CURRENT FAULTS AT THIS TIME COMPLIED WITH CMC TEST IAW AMM 26-10-00. OPS CHECK GOOD.Feb 22, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015021300010Fire Warning · false activationON TAKEOFF WHEN FLAPS 1 SELECTED MOMENTARY FIRE BELL WITH MASTER WARNING LIGHT. NO CMC MESSAGE PRESENT. PERFORMED FIRE SYSTEM TEST PER AMM 26-10-00. TEST PASSED.Feb 11, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2015021100009Fire Warning · false activationINTERMITTENT FIRE BELL WARNING WITH NO EICAS MESSAGE. NO CURRENT FAULTS AT THIS TIME. COMPLIED WITH CMC GROUND TEST IAW AMM 26-10-00. TEST GOOD.Feb 11, 2015 · N857GT · Boeing 74787UF · Fire DetectionSDR P5CA2014122000059Proximity Sensor · malfunctionedGEAR TILT EICAS MESSAGE. FOUND CMC CODE 32723 AND 32724; ACCOMPLISHED WIRING CHECK OF WIRES FROM PSEU TO THE SENSOR S2653 AND S2654 IAW WDM 32-61-15 AND WDM 32-61-16. NO FAULTS FOUND. SENSOR, S2653 AND S2654, REPLACED IAW AMM 32-61-12. OPS CHECK WAS GOOD.Dec 19, 2014 · N857GT · Boeing 74787UF · Landing Gear Position and WarningSDR P5CA2014093000041Tire · failedAFTER LANDING, FOUND TIRE MISSING CAP ON RT LANDING WING GEAR AFT INBD TIRE. REPLACED THE TIRE ASSY IAW AMM 32-45-04. ACCOMPLISHED CONDITIONAL INSPECTION IAW AMM 05-51-34. MULTIPLE DAMAGE FOUND.Sep 30, 2014 · N857GT · Boeing 74787UF · TireSDR P5CA2014070200019Window · delaminatedF/O FORWARD WINDOW DELAMINATING 11" X 3" AREA NEXT TO WINDOW HEAT ELEMENTS. R X R R1 WINDOW IAW AMM 56-11-01.Jul 2, 2014 · N857GT · Boeing 74787UF · Flight Compartment Windows
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