N850GT

Service difficulty reports · 116

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 = 'N850GT' 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 UIEA2016061000413Bracket · crackedNR 2 PYLON OTBD WING ACCESS PANEL PANEL 521AB INTERIOR 1-13 BEAM AFT UPPER BRACKET FOUND CRACK. NR 2, PYLON OTBD WING ACCESS PANEL NR 521 INTERIOR CAVITY AREA VAPOR BARRIER FOUND ATTACHED TAG AT ILES697-48 IS REPAIRED IAW NR R1-57-41-11414, REV A. FOLLOW UP IJun 8, 2016 · N850GT · Boeing 74787UF · Wing Miscellaneous StructureSDR UIEA2016061000414Bracket · crackedNR 3 PYLON, OTBD WING ACESS PANEL NR 62IAB INTERIOR OTBD BEAM AFT UPPER BRACKET FOUND CRACK. NR 3 PYLON OTBD WING ACCESS PANEL NR 621AB INTERIOR CAVITY AREA VAPOR BARRIER FOUND ATTACHED, TAG AT ILES697-48 IS REPAIRED IAW NR R1-57-41-11414, REV A. FOLLOW UP INJun 8, 2016 · N850GT · Boeing 74787UF · Wing Miscellaneous StructureSDR UIEA2016061000415Beam · crackedLEFT BLG INBD W/W DOOR AFT LOWER EDGE BEAM AND SKIN FOUND CRACK. LT BLG INBD W/W DOOR AFT LOWER EDGE BEAM IS REPLACED AND INSTALLED SRM-51-10-02 AND 51-40-02. SKIN IS REPAIRED AT BS 1424 IAW R1-52-00-11418, REV B.Jun 8, 2016 · N850GT · Boeing 74787UF · Landing Gear DoorsSDR UIEA2016061000416Skin · dentedAIRCRAFT DAMAGE, LOG D 15-010, AFT LOWER CARGO DOOR SKIN SMALL DENT HFEC ACCOMPLISHED. WORKED IAW SRM STICK 6477 APPLIED, TO BE REPAIRED IAW SRM 52-30-30-01-2R-1 REPAIR 1, AFT LOWER CARGO DOOR AT BS 1906, STR 42R, AREA SKIN IS REPAIRED IAW SRM 52-30-01-2R-1, Jun 8, 2016 · N850GT · Boeing 74787UF · Cargo/Baggage DoorsSDR UIEA2016061000417Panel · crackedRT WING NR 7 SPOILER FWD INBD UPPER FIXED PANEL FOUND CRACKED. RT WING NR 7 SPOILER FWD I/R UPPER FIXED PANEL CRACKED AREA REPAIRED IAW NR R1-57-51-11406, REV A.Jun 8, 2016 · N850GT · Boeing 74787UF · SpoilersSDR UIEA2016061000418Panel · crackedLT WING NR 6 SPOILER FWD INBD UPPER FIXED PANEL FOUND CRACK. LT WING NR 6 SPOILER FWD INBD UPPER FIXED PANEL CRACKED AREA REPAIRED IAW NR R1-57-51-11406, REV A.Jun 8, 2016 · N850GT · Boeing 74787UF · SpoilersSDR UIEA2016061000419Skin · delaminatedFX BODY FAIRING NR 1R3CL EXT SURFACE MID AREA FOUND APPROXIMATELY 22" X 16" DELAMINATED, SEVERAL DENT MARKS. BODY FAIRING NR 1R3CL EXT SURFACE REPAIRED IAW NR R1-53-67-11428, REV A.Jun 8, 2016 · N850GT · Boeing 74787UF · Aerodynamic FairingsSDR UIEA2016061000411Frame · damagedIN REFERENCE TO EO 4853A026: MAIN DECK FUSELAGE FRAMES RT & LT BS 200, WL 202 DENT & DAMAGE C/W PART 1. PART 2, DVI EVERY 25 FT, PART 3 PERMANENT REPAIR PRIOR TO 200 FT. MDDR:58286: IN REFERENCE TO EO 4853A026: MAIN DECK FUSELAGE FRAMES RT & LT BS200, WL 20Jun 8, 2016 · N850GT · Boeing 74787UF · Fuselage Main, FrameSDR UIEA2014061200233Control Cable · out of adjustLEFT AILERON FLIGHT CONTROL CHECK. PRONOUNCED BUMP COMING BACK TO NEUTRAL. FOUND LOST MOTION DRUM OUT OF RIG. AILERON BUS CABLES ACBA & ACBB ADJUSTED IAW MM 27-11-00. AILERON SYS FUNCTIONAL CHECK OK IAW MM 27-11-00.Jun 12, 2014 · N850GT · Boeing 74787UF · Aileron Control SystemSDR UIEA2013111900562Wire · chafedREF: SPOILER PCU NR 7 PROBLEM HISTORY. DURING TROUBLESHOOTING CABLE W27R4-30-20R, CHAFED UNDER P-CLIP REF WDM 27-61-31 PAGE 1;SAME WIRE TEMPORARILY REPAIRED IAW EO 4827A014, REV 0, PART 1, PART 2, PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 10 FLIGHT CYCLES.Nov 19, 2013 · N850GT · Boeing 74787UF · Flight Control System WiringSDR UIEA2013062600343Controller · inoperative"CARGO DET AFT 28" STATUS MESSAGE APPEARED 40 MINUTES INTO FLIGHT FOLLOWED BY "FIRE CARGO AFT" & 20 MINUTES LATER. QRH EMERGENCY CHECKLIST FOLLOWED AND FLIGHT DIVERTED TO IAD. ON ARRIVAL, THE LOWER AFT CARGO BAY WAS INSPECTED AND FOUND THAT THERE WAS NO EVIDJun 26, 2013 · N850GT · Boeing 74787UF · Fire DetectionSDR UIEA2012121200545Structure · puncturedDURING WALKAROUND INSPECTION, MX FOUND THE NR 9 VARIABLE CAMBER FLAP - BULL NOSE PUNCTURE AND EDGE DAMAGE REF FIG 1. THE DAMAGE EXCEEDS THE LIMITS OF SRM 57-43-02, FIG 101, ALLOWABLE DAMAGE 3 - L/E FLAP SKIN. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REDec 12, 2012 · N850GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2012110500514Actuator · inoperativeMESSAGE REPORTED THAT THE GEAR DISAGREE MESSAGE FOR RT WING GEAR EXPERIENCED, REPLACED RT WING LANDING GEAR DOOR ACTUATOR IAW MM 32-32-07 HYD LEAK CHECKED OPS AND ADJUSTMENT CARRIED OUT SATISFACTORY IAW MM 32-12-00, NIL MESSAGE NOTED DURING DOOR OPERATION.Nov 5, 2012 · N850GT · Boeing 74787UF · Landing Gear ActuatorSDR UIEA2012110500512Proximity Switch · failedRT WING GEAR HAD AN UP INDICATION AFTER LOWERING GEAR FOR LANDING. QRH COMPLETED WITH ALL GEAR DOWN. CMC REPORTED FAILURE OF PRI AND ALT PROXIMITY SWITCHES FOR RT WING GEAR UP, DOWN AND DOORS. CYCLED GEAR SWITCHES BACK TO NORMAL, RUN CMC TEST IAW AMM 32-09-Nov 5, 2012 · N850GT · Boeing 74787UF · Landing Gear Position and WarningSDR UIEA2012082000366Control Unit · failedIN FLIGHT, RECEIVED "HYD PRESS 3", "GPS LEFT", "IRS MOTION", "IRS DC RIGHT";"IRS AC RIGHT", "YAW DAMPER UPPER", "ADC CENTER", AND "NO AUTOLAND"; EICAS MESSAGES. RETURNED TO DEPARTURE. R & R NR 2 BCU, OPS CHECKED GOOD IAW AMM 24-23-01 AND ALL MESSAGES CLEAREDAug 20, 2012 · N850GT · Boeing 74787UF · Electrical Power SystemSDR UIEA2012081300358Lamp · inoperativeMAIN DECK ZONE A CEILING EMERGENCY LIGHT AFT BULB FOUND INOPERATIVE. LAMP REPLACED AND CHECK NORMAL REF AMM 33-51-07.Aug 8, 2012 · N850GT · Boeing 74787UF · Emergency Lighting
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