N851GT

Service difficulty reports · 80

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 = 'N851GT' 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 P5CA2022032700105None · noneLHW I/B T/E LWR PNL AT WS 129.86 TO 228.05 FWD SUPPORT BEAM O/B BRACKET CRACKED(<P>SUPPORT BEAM FITTING P/N : 115U2252-19 FASBRICATED AS PER RI NO.RI-57-00-15477 REV A AND BOEING DRAWING 115U2252-19PL</P>)Apr 1, 2022 · N851GT · Boeing 74787UF · Wing StructureSDR P5CA2022032800107None · noneBULK CGO STA 2160 ENDWALL FOUND TORN AS MARKED(<P>BULK CGO STA 2160 ENDWALL REPAIRED AS PER RI-25-54-15456 REV.A</P>)Apr 1, 2022 · N851GT · Boeing 74787UF · Cabin Equipment/FurnishingsSDR P5CA2022032800108Wire · brokenAPU FIRE DETECTOR LOOP A (W0906) WIRE FOUND BROKEN AT L/H AFT APU COMPT(<P>WIRE REPLACED BUT BEN-HAR SLEEVE TEMPOARY REPAIRED AS PER <SPAN>BOEING RDR NO.HKA-PAO-22-0028-07B</SPAN></P>)Apr 1, 2022 · N851GT · Boeing 74787UF · Fire Protection System WiringSDR P5CA2022011800004Fmc · noneRIGHT FMC FAILURE AFTER DEPARTURE, DUAL FMC FAILURE ENROUTE.(<P>REMOVED AND REPLACED RT FMC PERFORMED SOFTWARE CROSSLOAD & CONFIG CHECK , PERFORMED GROUND TESTS THROUGH CMC ALL TESTS PASSED PER AMM 34-61-01 34-61-00-472-105 34-61-000-752-101</P>)Jan 17, 2022 · N851GT · Boeing 74787UF · Flight Management Computing Software SystemSDR P5CA2020060800176Rib · crackedCRACK ON RIB OF LT WING FIXED TRAILING EDGE AT WBL 448.7. ACCOMPLISHED EI NO T2020A57M-1374 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Wing, Rib/BulkheadSDR P5CA2020060800177Stringer · crackedCRACK DAMAGES ON THE STRINGER S-8L BETWEEN STA 870 AND STA 890. REPAIRED DAMAGED AREA IAW EI NO T2020A53M-1373 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR P5CA2020060800178Stringer · crackedCRACK DAMAGES ON THE STRINGERS S-11L BETWEEN STA 860 AND STA 900. REPAIRED DAMAGED AREA IAW EI NO T2020A53M-1458 REV 3. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR P5CA2020060800179Stringer · crackedCRACK DAMAGES ON THE STRINGER S-9L BETWEEN STA 860 AND STA 900. REPAIRED DAMAGED AREA IAW EI NO T2020A53M-1449 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR P5CA2020060800180Stringer · crackedCRACK DAMAGE ON THE STRINGER S-10L BETWEEN STA 860 AND STA 900. ACCOMPLISHED EI NO T2020A53M-1390 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR P5CA2020060800181Stringer · crackedCRACK DAMAGES ON THE STRINGER S-10R BETWEEN STA 860 AND STA 880. REPAIRED THE CRACKED AREA IAW EI NO T2020A53M-1459 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR P5CA2020060800182Stringer · crackedCRACK DAMAGES ON THE STRINGER S-9R BETWEEN STA 880 AND STA 900. ACCOMPLISHED STRINGER REPAIR IAW EI NO T2020A53M-1378 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR P5CA2020060800183Stringer · crackedCRACK DAMAGES ON THE STRINGER S-11R BETWEEN STA 850 AND STA 900. ACCOMPLISHED STRINGER REPAIR IAW EI NO T2020A53M-1443 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR P5CA2020060800184Web · crackedCRACK ON UPPER AND LOWER CHORD AND WEB OF LH SIDE HORIZONTAL STABILIZER T/E AT HSB 421.5. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV 30. INSTALLED NEW PARTS IAW SRM 51-40-02 REV 30 AND DWG NR 182U5800, SHEET 1, REV B. REPAIRED DAMAGED AREA IAW EI NO T2020A5Jun 4, 2020 · N851GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous StructureSDR P5CA2020060800185Rotary Actuator · failedLT WING ALTERNATE EXTEND SYSTEM OPERATIONAL TEST FAIL. IAW AMM 32-36-01-004-001 REV 32 AND AMM 32-36-01-404-009 REV 32 REPLACED LT WING ROTARY ACTUATOR. IAW AMM 32-36-00-705-009 REV 32 PERFORM WLG LT ALTERNATE EXTENSION SYSTEM OPERATIONAL TEST. RESULT WAS NORMJun 4, 2020 · N851GT · Boeing 74787UF · Landing Gear ActuatorSDR P5CA2020060800186Rotary Actuator · failedRT BLG ALTERNATE EXTEND SYSTEM OPERATIONAL TEST FAIL. IAW AMM 32-35-01-004-001 REV 32 AND AMM 32-35-01-404-007 REV 32 REPLACE RT BLG ROTARY ACTUATOR. IAW AMM 32-35-00-715-059 REV 32 PERFORM RT BLG ALTERNATE EXTEND SYSTEM OPER TEST. RESULT WAS NORMAL.Jun 4, 2020 · N851GT · Boeing 74787UF · Landing Gear ActuatorSDR P5CA2019070200139Fairing · dentedLT HORIZONTAL STAB L/E FAIRING #331CL FOUND DENT. (<P>LT HORIZONTAL STAB L/E FAIRING #331CL DENT AREAS REPAIRED IAW SRM 55-10-01-2R-2 REPAIR 2.</P>)Jun 29, 2019 · N851GT · Boeing 74787UF · Horizontal Stabilizer, Plate/SkinSDR P5CA2019040500048Line · leakingGEAR TILT CAUTION MESSAGE DURING CLIMB. FOUND HYDRAULIC LINE TO LEFT BODY GEAR TILT ACTUATOR LEAKING. REMOVED AND REPLACED LINE. LEAK CHECK NORMAL I.A.W. AMM 32-13-14.<BR /></P>)Apr 5, 2019 · N851GT · Boeing 74787UF · Hydraulic System, MainSDR P5CA2018091400256Relay · faultyREJECTED T/O AT LOW SPEED DUE TO "CONFIG PARK BRAKE" T/O WARNING. SHOWED CMC NO REPORTED FOUND AND CHECKED PARKING BRAKE STS THEN FOUND PARKING BRAKE VLV NOT MOVE AND R&R PARKING BRAKE VLV CLOSE RELAY ( R7514) PER FIM 32-04-00-810-802 AND SYS TEST NORMAL PER ASep 8, 2018 · N851GT · Boeing 74787UF · Landing Gear Brake SystemSDR P5CA2017072500226Circuit Card · failedDURING CRUISE, HAD A EICAS MESSAGES FOR HYD PRESSURE, SYS 3. PERFORMED QRH PROCED WITH NR 3 DMD ENG PUMPS OFF PRIOR TO PROCEDURE EICAS MESSAGES HYD PRESSURE NR 3 ENG, GPS, ADC CENTER MESSAGES. QRH/ ELC LIST COMPLETE BUT AURAL WARNING CONTINUED. NR 3 HYD SYS Jul 24, 2017 · N851GT · Boeing 74787UF · Hydraulic Pressure SensorSDR P5CA2016062900158Hinge · looseNR 1 RAM AIR OUTLET HINGE FOUND LOOSE. NR 1 RAM AIR OUTLET LOOSED HINGE, REPLACED IAW SRM 51-10-02 AND FASTENERS INSTALLED SRM 51-40-02 AND SHEET 6, REV A.Jun 30, 2016 · N851GT · Boeing 74787UF · Fuselage, Door HingeSDR P5CA2016062900157Panel · crackedLEFT WING UPPER, WING T/E FIXED PANEL FOUND CRACKED AT JUST FWD OF NR 6 SPOILER. LT WING UPPER T/E FIXED PANEL AT JUST FWD OF NR 6 SPOILER CRACKED AREA COMPOSITE REPAIRED IAW RI-57-51-11434, REV A.Jun 30, 2016 · N851GT · Boeing 74787UF · Wing, Plate/SkinSDR P5CA2016062900156Bracket · crackedNR 3 PYLON OTBD WING ACCESS NR 621AB INTERIOR INBD BEAM AFT BRACKET FOUND CRACKED. NR 3 PYLON OTBD WING ACCESS NR 621AB INTERIOR CAVITY AREA VAPOR BARRIER FWD ATTACHED TAG AT ILE 697.48 IS REPAIRED IAW NR:RI-57-41-11433, REV A FOLLOW UP INSPECTION IS REQUIREDJun 30, 2016 · N851GT · Boeing 74787UF · Wing Miscellaneous StructureSDR P5CA2016062900155Bracket · crackedNR 2 PYLON OTBD WING ACCESS NR 521AB INTERIOR INBD BEAM AFT BRACKET FOUND CRACKED. NR 2 PYLON OTBD WING ACCESS NR 521AB INTERIOR CAVITY AREA VAPOR BARRIER FWD ATTACHED TAG AT ILE 697.48 IS REPAIRED IAW NR :RI-57-41-11433, REV A FOLLOW UP INSPECTION REQUIRED IJun 30, 2016 · N851GT · Boeing 74787UF · Wing Miscellaneous StructureSDR P5CA2016062900154Skin · damagedACFT DAMAGED, LT NOSE GEAR DOOR DENT DAMAGE, BIRD STRIKE, D=0.120", W=4", L=6", W/Y=33.3, SRM 52-80-01-1A, DETAIL V. LT NLG DOOR SMALL EXTERNAL SKIN REPAIRED IAW NR: RI-52-84-11435, REV A.Jun 30, 2016 · N851GT · Boeing 74787UF · Landing Gear DoorsSDR P5CA2015090700133Plug · missingNR 4 ENGINE SHUTDOWN DUE TO LOW OIL QUANTITY AND PRESSURE. FOUND EDP DEACTIVATION KIT GEARBOX PLUG NOT INSTALLED. INSTALLED PLUG AS REQUIRED IAW AMM 29-11-02. LEAK CHECK NORMAL IAW AMM 71-00-00. ALSO, ACCOMPLISHED WINDMILL INSPECTION IAW AMM 71-00-00-200-8Sep 7, 2015 · N851GT · Boeing 74787UF · Engine Oil Indicating SystemSDR P5CA2015090700132Pump · leakingNR 4 HYDRAULIC SYSTEM FAILED APPROACHING LEVEL AT 11,000 FT. ACCOMPLISHED CHECKLIST. SHUTDOWN NR 4 ENGINE DRIVEN PUMP. FOUND NR 4 EDP LEAKING FROM PRESSURE SENSOR AND CASE DRAIN. TRANSFER TO MDDR 59865, MEL 29-11-01-02B. PUMP REMOVED AND PLATE INSTALLED ISep 6, 2015 · N851GT · Boeing 74787UF · Hydraulic Pump (Electric/Engine), MainSDR P5CA2015080300059Filter · contaminatedDURING CLIMBOUT, EICAS MESSAGE, ENGINE 3 THRUST. PRELIMINARY INSPECTIONS SHOWED FUEL FILTER CONTAMINATION. NR 3 ENGINE REPLACEMENT IN WORK.Aug 3, 2015 · N851GT · Boeing 74787UF · Engine Fuel DistributionSDR P5CA2015080100058Pump · failedNR 3 ENGINE ROLLED BACK AND FLAMEOUT, OIL PRESSURE STABILIZED AT 14 PSI DURING CRUISE. N1 & N2 ROTATION 17.8/ 17.7. FIRE SWITCH NOT PULLED. NR 3 ENGINE FUEL PUMP REPLACED IAW AMM 73-11-01. OPS AND LEAK CHECKED OK.Jul 30, 2015 · N851GT · Boeing 74787UF · Engine Fuel PumpSDR P5CA2015073100057Fmu · power lossENGINE NR 3 ROLLED BACK AND FLAMEOUT AT APPROXIMATE 16:42Z OIL PRESSURE STABILIZED AT 14 PSI IN CRUISE. N1 & N2 ROTATION 17.8/ 17.7. FIRE SWITCH NOT PULLED. PULLED AND INSPECTED NR 3 ENGINE FUEL FILTER FOR INSPECTION. FOUND CONTAMINATION. R & R FUEL & METJul 30, 2015 · N851GT · Boeing 74787UF · Engine (Turbine/Turboprop)SDR UIEA2014021200053Engine · power lossDURING TAKEOFF ROLL AT VERY LOW SPEED, NR 4 ENG ROLLED BACK TO IDLE. DURING TAKEOFF REJECTION THERE WAS A BURNING ODOR FOR APPROXIMATELY 20 SECONDS IN THE AIR CONDITIONING SYS & THEN THE ODOR DISSIPATED COMPLETELY. ACCOMPLISHED INLET & EXHAUST INSPECTION, NOFeb 12, 2014 · N851GT · Boeing 74787UF · Engine (Turbine/Turboprop)
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