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 UIEA2022021500136Panel · dentedM/D - STA 1700-1760 LBL 33-55 CASTER MAT FOUND DENT MARK.(<P>CASTER PANEL REPLACEMENT AS PER AMM 25-57-16 REV 37, 15 NOV 2021.</P>)Feb 23, 2022 · N850GT · Boeing 74787UF · Cargo CompartmentsSDR UIEA2022021600140Floorbeam · damagedFWD CGO COMPT L/H O/B AT BS 740 FLOOR BEAM FOUND DAMAGED.(<P>FWD CARGO COMPT LH BS 740 LBL 47.25 FLOOR STRUCTURE CHORD REPAIR AS PER RI-53-65-15384 REV A.</P>)Feb 23, 2022 · N850GT · Boeing 74787UF · Fuselage Structure (General)SDR UIEA2022021600141Vapor Barrier · cracked#4 PYLON TO WING L/E CAVITY, VAPOR BARRIER PANEL FOUND CRACKED AT I/B CORNER.(<P>PERFORM A DVI OF THE REPAIR AREA TO MAKE SURE THERE IS NO OTHER DAMAGE. SEAL THE PANEL AFFECTED FLANGE UPPER SURFACE WITH BMS5-95 SEALANT APPLIED IN A STRIP 0.25" EITHER SIDE OF TFeb 23, 2022 · N850GT · Boeing 74787UF · Wing, Fuselage Attach FittingsSDR UIEA2022021700142Flap · erodedRHW NO.20 V/C FLAP EXT. LSA FOUND EROSION.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1.</P>)Feb 23, 2022 · N850GT · Boeing 74787UF · Leading Edge Slat Control SystemSDR UIEA2022021700143Flap · corrodedRHW NO.20 V/C FLAP EXT. LSA FOUND EROSION(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1.</P>)Feb 23, 2022 · N850GT · Boeing 74787UF · Leading Edge Slat Control SystemSDR UIEA2022022000148Channel · crackedL/H HORI STAB TIP FAIRING ATTACHED U CHANNEL CRACKED.(<P>L/H HORI STAB T/E BOND ASSY. ATTACHED U CHANNEL WAS REPLACED AND INSTALLED AS PER RI-55-10-15385 REV A.</P>)Feb 23, 2022 · N850GT · Boeing 74787UF · Empennage StructureSDR UIEA2022022500169Battery · failedU/D EMER LT POWER SUPPLY (M516B) CAPACITY TEST FAIL(<P>U/D EMER LT POWER SUPPLY BATTERY REPLACED AND OPERATIONAL TEST NORMAL IAW AMM 33-51-00, REV 37 15 NOV 2021.</P>)Feb 23, 2022 · N850GT · Boeing 74787UF · Emergency LightingSDR UIEA2021111002389Fairing · noneON ARRIVAL #2 FLAP TRACK MOVEABLE FAIRING NOT FLUSH WITH FLAPS UP(<P ><SPAN>ON INSPECTION FOUND AFT SUPPORT LINK DAMAGED AND DETACHED, LOOSE EQUIPTMENT / FAIRING LUG PUNCTURED 2 HOLES IN CANOE. MOVEABLE FAIRING AND LINKAGE REMOVED IAW AMM 27-51-31-000-802 AND Nov 6, 2021 · N850GT · Boeing 74787UF · Trailing Flap Position Indicating SystemSDR UIEA2020052701046Fitting · brokenRT WING NR 6 FLAP TRACK CANOE FAIRING FWD SUPPORT FRAME I/B ATT BONDING FOUND BROKEN. RT WING NR 6 FLAP TRACK CANOE FAIRING FWD SUPPORT FRAME DETAILED VISUAL INSPECTION CARRIED OUT OF THE INSTALLED REPAIR AND ALL ADJACENT VISIBLE SURFACE OF THE INITIAL FRAME TMay 23, 2020 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2020052711053Seat Track · corrodedM/D - STA 1600 RBL 11 SEAT TRACK FOUND CORRODED.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.009" WIDTH 0.7" LENGTH 2" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711054Seat Track · corrodedM/D - STA 1445-1450 RBL 11 SEAT TRACK CROWN FOUND CORRODED.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.007" WIDTH 0.7" LENGTH 3 WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711055Seat Track · corrodedM/D - STA 1850-1865 RBL 11 SEAT TRACK FOUND CORRODED.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01. BLENDED OUT AREA DEPTH 0.007", WIDTH 0.7", LENGTH 2" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS REV 30-20FEB2020.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711056Seat Track · corrodedM/D - STA 1880-1890 RBL 11 SEAT TRACK FOUND CORRODED.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.006" WIDTH 0.7" LENGTH 1" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711057Seat Track · corrodedM/D - STA 1900-1905 RBL 11 SEAT TRACK CROWN FOUND CORRODED.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.005" WIDTH 0.4" LENGTH 1" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711058Seat Track · corrodedM/D - STA 1990 RBL 11 SEAT TRACK FOUND CORRODED.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.005" WIDTH 0.7" LENGTH 1" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711059Seat Track · corrodedM/D - STA 1550-1560 LBL 11 SEAT TRACK FOUND CORRODED.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.008" WIDTH 0.7" LENGTH 6" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711060Seat Track · corrodedM/D - LBL 99 STA 1720 TO 1760 SEAT TRACK FOUND CORROSION.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.008" WIDTH 0.7" LENGTH 1" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711061Seat Track · corrodedM/D - LBL 99 STA 1700 TO 1720 SEAT TRACK FOUND CORROSION.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.025" WIDTH 0.7" LENGTH 1" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711062Seat Track · corrodedM/D - LBL 99 STA 1840 TO 1860 SEAT TRACK FOUND CORROSION.CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 BLENDED OUT AREA DEPTH 0.010" WIDTH 0.7" LENGTH 1" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052711063Rod · damagedLH OUTBD T/E FLAP #2 CANOE ROD DAMAGE. PERFORM HFEC ON LEFT OUTBOARD TRAILING EDGE FLAP ATTACH FITTING (P/N 113U3572-1)BLENDED OUT AREAS OF GOUGES ON LEFT OUTBOARD FLAP #2 FLAP TRACK FAIRING AFT FITTING. CARRIED OUT, CONDITION SATISFACTORY IAW RI-57-53-14030 RMay 23, 2020 · N850GT · Boeing 74787UF · Trailing Edge Flap Control SystemSDR UIEA2020052791081Strap · crackedAFT OF BULK CARGO BS 2180 BETWEEN S35R-S36R FRAME ATTACH STRAP FOUND CRACKED.TENSION STRAP REPAIRED IAW RI-53-60-14058 REV A.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage Miscellaneous StructureSDR UIEA2020052711094Rib · crackedLHW I/B FLAP T/E #3 MOVEABLE FAIRING FWD FRAME FOUND CRACKED. RIB REPAIRED IAW RI-57-50-14045 REV AMay 23, 2020 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2020052711096Bushing · corrodedDURING LUBRICATION, LH WLG DRAG BRACE LWR FITTING BOTH BUSHING FOUND CORROSION.LH WLG DRAG BRACE LWR FITTING CORROSION REMOVED PER CMM 32-11-86 REPAIR 6-2.May 23, 2020 · N850GT · Boeing 74787UF · Wing, Landing Gear Attach FittingsSDR UIEA2020052711097Bushing · corrodedDURING LUBRICATION, R/H WLG DRAG BRACE LOWER FITTING BOTH BUSHING FOUND CORROSION.RH WLG DRAG BRACE LWR FITTING CORROSION REMOVED PER CMM 32-11-86 REPAIR 6-2.May 23, 2020 · N850GT · Boeing 74787UF · Wing, Landing Gear Attach FittingsSDR UIEA2020052721114Support Web · crackedR/H ELEVATOR MOST O/B TIP FAIRING SUPPORT WEB FOUND CRACK.RH ELEVATOR MOST O/B TIP FAIRING SUPPORT WEB REPLACED PER SRM 51-40-02 SRM 51-10-02 .May 23, 2020 · N850GT · Boeing 74787UF · Elevator StructureSDR UIEA2020052201115Support · crackedR/H ELEVATOR MOST O/B FAIRING PNL SUPPORY FOUND CRACK.RH ELEVATOR MOST O/B FAIRING PNL LWR SUPPORT REPLACED PER SRM 51-40-02 SRM 51-10-02.May 23, 2020 · N850GT · Boeing 74787UF · Elevator StructureSDR UIEA2020052701135Stringer · crackedM/D STRINGER AT STA 882 S8L FOUND CRACKED.STRINGER REPAIRED IAW RI-53-21-14033 REV AMay 23, 2020 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2020052701137Stringer · crackedM/D STRINGER AT STA 870 S10R FOUND CRACKED.STRINGER REPAIRED IAW RI-53-21-14040 REV. A.May 23, 2020 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2020052701138Stringer · crackedM/D STRINGER AT STA 878-890 S9R FOUND CRACKED.(<P>STRINGER REPAIRED IAW RI-53-21-14034 REV A. </P>)May 23, 2020 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2020052701140Rib · crackedLHW WS743 T/E RIB UPPER AFT END FOUND CRACKED. RIB REPAIRED IAW RI-57-50-14035 REV A.</P>)May 23, 2020 · N850GT · Boeing 74787UF · Wing, Rib/BulkheadSDR UIEA2020052701141Rib · crackedRHW I/B FLAP T/E #2 RIB LOWER END FOUND CRACKED(<P>RIB REPAIRED IAW RI-57-50-14037 REV A. </P>)May 23, 2020 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2020052701142Rib · crackedRHW WS743 T/E RIB UPPER AFT END FOUND CRACKED.(<P>RIB REPAIRED IAW RI-57-50-14036 REV A.May 23, 2020 · N850GT · Boeing 74787UF · Wing, Rib/BulkheadSDR UIEA2020052701143Stringer · crackedM/D STRINGER AT ST 883 S10L FOUND CRACKED.(<P>STRINGER REPAIRED IAW RI-53-21-14062 REV A.</P>)May 23, 2020 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2020052701144Stringer · crackedM/D STRINGER AT STA 883 S11L FOUND CRACKED(<P>STRINGER REPAIRED IAW RI-53-21-14061 REV A. </P>)May 23, 2020 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2020052701145Seat Track · damagedM/D SEAT TRACK UPPER CENTER GUIDE HOLE FOUND ELONGATED AT STA 1512, STA 1532, AND STA 1552. (<P>SEAT TRACK REPAIRED IAW RI-53-21-14034 REV A</P>)May 23, 2020 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020052701146Tee Fitting · crackedLH HORI STAB O/B TIP LOWER TEE CHORD FOUND CRACKED.(<P>TEE CHORD REPAIRED IAW RI-55-10-14054 REV A.</P>)May 23, 2020 · N850GT · Boeing 74787UF · Horizontal Stabilizer StructureSDR UIEA2020052701147Channel · crackedR/H HORI STAB O/B T/E WEDGE "U" CHANNEL FOUND CRACKED.(<P>"U" CHANNEL REPLACED IAW RI-55-10-14048 REV A.</P>)May 23, 2020 · N850GT · Boeing 74787UF · Horizontal Stabilizer StructureSDR UIEA2019101325706Lamp · inoperativeUPPER DECK EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP, OPS CHECK OK IAW AMM 33-51-00.Oct 13, 2019 · N850GT · Boeing 74787UF · Emergency LightingSDR UIEA2018070601356Actuator · faultyDURING INITIAL CRUISE AT FL37.0 GOT DOOR NOSE CARGO CAUTION MSG. FOLLOWED ELECTRONIC CHECKLIST, DESCENDED TO 8000', DURING DESCENT EICAS MSG WENT AWAY. DIVERT TO MIA. INITIAL EVALUATION FOUND INTERMITTENT CMC MSG 52044 AND 52052. FOLLOWED IFIM 52-31-00, REMOVEJul 6, 2018 · N850GT · Boeing 74787UF · Cargo/Baggage DoorsSDR UIEA2018050100818Door · crackedLEFT BODY LANDING GEAR INBD STRUT DOOR, AFT EDGE FOUND CRACKED. REPAIRED IAW RI-52-80-12655, REV A.Apr 27, 2018 · N850GT · Boeing 74787UF · Landing Gear DoorsSDR UIEA2018050100819Frame · crackedRIGHT WING INBD T/E FLAP NR 6 AFT FAIRING, FWD FRAME ASSY WAS FOUND CRACKED THROUGH THE THICKNESS OF FWD FRAME ALONG THE OTBD BEARING FITTING AREAS. REPAIRED IAW RI-57-50-12656, REV A.Apr 27, 2018 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2018050100820Frame · crackedAPU BAY, THE RT FRAME WAS FOUND CRACKED AT BS 2680, WL 305. THE FRAME WAS REPAIRED IAW RI-53-82-12665, REV A.Apr 27, 2018 · N850GT · Boeing 74787UF · Fuselage Main, FrameSDR UIEA2018050100821Frame · damagedAPU BAY, RT FRAME HOLES ELONGATED AT BS 2664, WL 305. THE FRAME WAS REPAIRED IAW RI-53-82-12665, REV A.Apr 27, 2018 · N850GT · Boeing 74787UF · Fuselage Main, FrameSDR UIEA2018050100822Frame · damagedAPU BAY RT FRAME HOLES ELONGATED AT BS 2669, WL 305. THE FRAME WAS REPAIRED IAW RI-53-82-12665, REV A.Apr 27, 2018 · N850GT · Boeing 74787UF · Fuselage Main, FrameSDR UIEA2018050100823Frame · crackedAPU BAY RT FRAME HOLES CRACKED AT BS 2674, WL 305. THE FRAME WAS REPAIRED IAW RI-53-82-12665 REV A.Apr 27, 2018 · N850GT · Boeing 74787UF · Fuselage Main, FrameSDR UIEA2017061901035Unknown · unknownAT APPLICATION OF TOGA, ON THE TAKEOFF ROLL WITH ALL ENGINES SPOOLED UP NORMALLY, THE AIRCRAFT VEERED VIOLENTLY TO THE RIGHT. ABORTED AT 30KTS. ACCOMPLISHED NOSE STEERING CHECK IAW AMM 32-51-00, ALL CHECKED NORMAL. ACCOMPLISHED BODY GEAR STEERING CHECK IAWJun 19, 2017 · N850GT · Boeing 74787UF · Standard Practices/StructuresSDR UIEA2016122301051Fuel Filter · failedNR 3 ENGINE FAILED TO MAKE TAKE OFF POWER OF 84.4%/ N1 ONLY 78%. PERFORMED POWER ASSURANCE TEST IAW AMM 71-02-00-770-802, ALL PARAMETERS PASSED. CHANGED NR 3 ENGINE FUEL FILTER IAW AMM 73-11-02-400-801-G00. LEAK CHECK GOOD.Dec 23, 2016 · N850GT · Boeing 74787UF · Engine Fuel DistributionSDR UIEA2016110300829Warning Message · false activationRTO, EICAS MESSAGE ON TAKE OFF & CONFIGURED GEAR CTR. TESTED BG STEERING ON RAMP IAW AMM 32-53-00. TESTED OK.Oct 29, 2016 · N850GT · Boeing 74787UF · Landing Gear Steering SystemSDR UIEA2016080300665Hydraulic System · malfunctionedLOW SPEED (40KTS) TAKEOFF REJECTION DUE TO STAB GREEN BAND DISAGREE WITH NOSE GEAR PRESSURE SWITCH. NO BRAKE TEMP HIGHER THAN 1.2. ACCOMPLISHED HIGH ENERGY STOP INSPECTION IAW AMM 5-51-10 ALL CHECKS NORMAL.Aug 3, 2016 · N850GT · Boeing 74787UF · Hydraulic System, MainSDR UIEA2016061000412Support Beam · crackedRT WING NR 5 FLAP TRACKS WS 500 AUXILIARY SPAR CHANNEL AFT AREA FOUND CRACK. RT WING #5 FLAP TRACK REAR SPAR WS500 PANEL SUPPORT BEAM AFT AREA REPAIRED IAW R1-57-22-11413, REV A. FOLLOW UP INSPECTION IS REQUIRED IAW NR R1-57-22-11413, REV A. THRESHOLD = 2400Jun 8, 2016 · N850GT · Boeing 74787UF · Wing Miscellaneous Structure
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