N851FD

Service difficulty reports · 37

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 = 'N851FD' 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 FDEA202606040671Lamp · inoperativePOST-FLT INSP, L1 OVERHEAD EMERGENCY LT INOP. AMM: 33-51-04-2 RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.Jun 4, 2026 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA202512042219Lamp · inoperativeEMERGENCY LIGHT OVERHEAD DOOR 1L INOPERATIVE. REPLACED THE LAMP OF EMERGENCY AREA LIGHT OVERHEAD DOOR 1L REF AMM 33-51-03-2 , TEST NORMAL. A/C OK TO CONTINUE.Dec 4, 2025 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA202507121185Floor Panel · crackedREWORK: MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 FOUND CRACKED AT STA1010 LBL85. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA1010 LBL85 DAMAGE SIZE: L=3.5" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLWABLE DAMAGE 1 FIGJul 12, 2025 · N851FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202507111177Floor Support · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA1434 RBL40. MAIN DECK CARGO FLOOR FITTING CORROSION AT STA1434 RBL40 REMOVED AND EVALUATED: THE REWORKED AREA AT ZONE "B", THE MAX ALLOWABLE BLEND OUT IS 0.030", THE MAX CLEAN UP DEPTH IS X=0.092", FOUND Jul 11, 2025 · N851FD · Boeing 777FS2 · Fuselage Miscellaneous StructureSDR FDEA202507101167Fitting · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA 1393 LBL6.5 MAIN DECK CARGO FLOOR FITTING CORROSION AT STA 1393 LBL6.5 REMOVED AND EVALUATED : THE REWORKED AREA AT ZONE "C", THE MAX ALLOWABLE BLEND OUT IS 0.002". THE MAX CLEAN UP DEPTH IS X = 0.033", Jul 10, 2025 · N851FD · Boeing 777FS2 · Fuselage Miscellaneous StructureSDR FDEA202507101166Fitting · corrodedMAIN DECK CARGO FLOOR FITING FOUND CORROSION AT STA1393 RBL6.5. MAIN DECK CARGO FLOOR FITTING CORROSION AT STA 1393 RBL6.5 REMOVED AND EVALUATED : THE REWORKED AREA AT ZONE "C", THE MAX ALLOWABLE BLEND OUT IS 0.002". THE MAX CLEAN UP DEPTH IS X = 0.022", FJul 10, 2025 · N851FD · Boeing 777FS2 · Fuselage Main, Attach FittingsSDR FDEA202507061125Skin · delaminatedLH WING OB FLAP LWR SURFACE FROM IB TO OB 20 INCH CROSS TE TO LE 5 INCH FOUND DELAMINATION.Jul 6, 2025 · N851FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202507041114Skin · crackedMFEC INSPECTION OF THE OUTBOARD SLAT NO.10 OUTER SKIN DETECTED 1EA FASTENER WITH TWO CRACKS, APPROXIMATELY 4MM AND 6MM IN LENGTH RESPECTIVELY. RH WING NO.10 SLAT OUTER SKIN CRACK AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIG 202 REV47.6 AND EA GJul 4, 2025 · N851FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA202507041113Skin · bulgedRH WING NO.11 SLAT OUTER SKIN FOUND BULGE AT 28-33 INCH TO OB EDGE. RH WING NO.11 SLAT OUTER SKIN BULGE AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIG 202 REV 47.6 AND EA G-5750-T0384008 P1. TITLE : WING - FLIGHT SURFACES - RH WING #11 SLAT OUTER SJul 4, 2025 · N851FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA202507031101Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE LEFT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 02EA CRCAK AT HOLE #5. LEFT WING UPPER SKIN #5 HOLE 02EA CRACKS REPAIRED AS PER B777 SRM 51-40-05-0G, SRM 51-40-04-0G, SRM 51-40-02-0G REV47.6 AND EJul 3, 2025 · N851FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202507031100Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE RIGHT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 02EA CRCAK AT HOLE #5. RIGHT WING UPPER SKIN #5 HOLE 02EA CRACKS REPAIRED AS PER B777 SRM 51-40-02-0G, SRM 51-40-04-0G, SRM 51-40-05-0G REV47.6 ANDJul 3, 2025 · N851FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202507021098Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA1010 LBL85 DAMAGE SIZE:L=3.5" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGURE 101-106 REV 47.6 AND REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1 FIGURE 201-20Jul 2, 2025 · N851FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202410011412Engine · damagedSTARTING CLIMB FROM FL380 TO FL400. WHEN THRUST STARTED TO INCREASE, FELT A MAJOR JOLT FOLLOWED BY MAJOR VIBRATIONS, SMOKE & FUMES IN COCKPIT. LT GEN DRIVE & L ENG OIL PRESSURE LIGHTS ILLUMINATED. DONNED MASKS, DECLARED EMERGENCY & RAN CHECKLISTS. SHUTDOWOct 1, 2024 · N851FD · Boeing 777FS2 · Engine (Turbine/Turboprop)SDR FDEA202302080230Flap · dentedLH OB FLAP LWR SURFACE FROM OB TO IB 98 INCH CROSS TE TO LE 8 INCH FOUND ONE DENT LH O/B FLAP LWR SURACE FROM O/B TO I/B 98 INCH CROSS T/E TO L/E 8 INCH DENT DAMAGE SIZE: L XW=1.7" X 1.5", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMAGE 2,Feb 8, 2023 · N851FD · Boeing 777FS2 · Wing, Control SurfacesSDR FDEA202302080229Flap · damagedRH WING OB FLAP LEADING EDGE FOUND BROKEN AT OTEF STA 437. RH WING OB FLAP LEADING EDGE PUNCTURE DAMAGE SIZE L X W: 1.0" X 0.5", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMAGE 2, REV 43.1, REPAIRED AS PER WORK CARD TG-5750-T0372808 P1, TIFeb 8, 2023 · N851FD · Boeing 777FS2 · Wing, Control SurfacesSDR FDEA202201210752Power Supply · no testEMERGENCY LIGHT TEST IN SUPERNUMERARY COMPARTMENT DID NOT TEST PROPERLY. L1 DOOR LIGHTS DID NOT ILLUMINATE. REPLACED L1 DOOR POWER SUPPLY IAW AMM 31-51-06-2, EMERGENCY LIGHT OPS TEST SATISFACTORY.Jan 21, 2022 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA2020052230881Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAN HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.1" AND 0.9' AT STAMay 3, 2020 · N851FD · Boeing 777FS2 · Fuselage Main, Plate/SkinSDR FDEA2020050430881Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHR HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.1" AND 0.9' AT STATION 1033 STRINGMay 3, 2020 · N851FD · Boeing 777FS2 · Fuselage Main, Plate/SkinSDR FDEA2020050430880Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.0" AT STATION 1028 SRINGMay 3, 2020 · N851FD · Boeing 777FS2 · Fuselage Main, Plate/SkinSDR FDEA202004300852Structure · crackedDURING ACCOMPLISHMENT OF HIGH FFEQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON LEFT FRONT LOWER CHORD 04 EACH FASTENER HOLES AT STATION 1035 LEFT BUTT LINE 82 AND FOUND WITH CRACK INDICATION AT LOWER ROW OUTBOARD HOLE AS MARKED.Apr 30, 2020 · N851FD · Boeing 777FS2 · Fuselage Miscellaneous StructureSDR FDEA202004300851Spar · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON RIGHT HAND FRONT LOWER SPAR CHORD 04 EACH FASTENER HOLES AT STATION 1035 RIGHT BUTT LINE 82 FOUND WITH CRACK INDICATION AT LOWER ROW OUTBORAD HOLE AS MARKED.Apr 30, 2020 · N851FD · Boeing 777FS2 · Wing SparSDR FDEA202004270801Longeron · crackedULTRASONIC INSPECTION CARRIED OUT AND FOUND THE LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 WITH CRACK INDICATION.Apr 27, 2020 · N851FD · Boeing 777FS2 · Fuselage Main, Longeron/StringerSDR FDEA202004270800Longeron · crackedULTRASONIC INSPECTION CARRIED OUT AND FOUND THE RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 WITH CRACK INDICATION.Apr 27, 2020 · N851FD · Boeing 777FS2 · Fuselage Main, Longeron/StringerSDR FDEA2019122313285Tire · wornRECEIVED EICAS MESSAGE OF TIRE PRESS. PRESSURE ON NR 7 INDICATED 180 PSI AND DURING FLIGHT CONTINUED DOWN TO 113 PSI. EMERGENCY WAS DECLARED AND TIRE REMAINED IN TACT DURING LANDING & SUBSEQUENT TAXI IN INITIAL INDICATION AT APPROXIMATELY 2 HOURS 30 MINUTES IDec 21, 2019 · N851FD · Boeing 777FS2 · TireSDR FDEA201907151576Slide · unwanted deployMDIS 851 52-10 0202 15JUL19 DEL OPEN U DURING PREFLIGHT CHECK, L1 DOOR SLIDE DEPLOYED. DURING PRE FLIGHT FOUND L1 DOOR HANDLE NOT FULLY STOWED DOWN IN OPEN POSITION. CLOSED L1 DOOR FROM INSIDE AND SAME WAS LOCKED NORMAL. WENT TO VERIFY L1 DOOR INJul 15, 2019 · N851FD · Boeing 777FS2 · Escape SlideSDR FDEA201811213348Power Supply · inoperativeTEST FAILS ON SUPRNMRY LIGHT TEST FOUR LIGHTS INOP. REMOVED AND REPLACED R1 OVRHD EMER LIGHTS POWER SUPPLY, REF AMM 33-51-06-2. EMER LIGHTS TEST SATIS, ITEM OK FOR SVC.Nov 21, 2018 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA201810232983Floorboard · crackedFOUND UPPER CARGO FLOORBOARD CRACKED AT STA 1000 RIGHT OUTBOARD. REMOVED AND REINSTALLED UPPER CARGE FLOORBOARD AT STA 1000 RIGHT & OUTBOARD REF B777 MM 53-01-01-4. ALL WORK STEPS COMPLETED REF E.A. G-5321-T0343082 FUSELAGE - CARGO COMPARTMENT FLOORS -INSOct 23, 2018 · N851FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA201707212014Floor Support · crackedBULK CARGO BAY FLOOR SUPPORT AT BS 1958, FOUND CRACKED. REPAIRED IAW SRM 53-70-53-2R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 21, 2017 · N851FD · Boeing 777FS2 · Fuselage Miscellaneous StructureSDR FDEA201707191993Slat · damagedLEFT WING NR 1 SLAT ASSY CENTER LEADING EDGE SURFACE FOUND DAMAGED. REPAIRED IAW SRM 57-43-01, REPAIR 2, AND EA G-5750-T0334492, PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 19, 2017 · N851FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA201703150918Transducer · out of adjustYOKE BECAME LOCKED IN POSITION DURING PRE TAKEOFF FLIGHT CONTROL CHECK. ADJUSTED PLATE ON CENTRAL WHEEL FORCE TRANSDUCER IAW MM 27-11-08-4-0. AILERON AND FLAPERON CONTROL SYSTEM TEST PERFORMED IAW MM 27-11-00-5-0. TEST PASSED.Mar 15, 2017 · N851FD · Boeing 777FS2 · Aileron Control SystemSDR FDEA201612154465Lamp · inoperativeR1 DOOR EXTERIOR EMERGENCY LIGHT INOP ON POST-FLT CHECK. REPLACED THE LAMP IAW AMM 33-51-04-2. EMERGENCY LIGHT TESTED GOOD, OK FOR SERVICE.Dec 15, 2016 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA201611224186Lamp · inoperativeR1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND ON POST FLIGHT OPS CHECK. REPLACED THE LAMP IAW AMM: 33-51-04-2. LIGHTS TESTED GOOD, OK FOR SERVICE.Nov 22, 2016 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA201501210245Skin · dentedBULK CARGO DOOR EXTERIOR SKIN FOUND DENTED. REPAIRED IAW SRM 52-30-01 FIGURE 202 REPAIR 13 AND EA G-5230-T0314944 PART 1.Jan 21, 2015 · N851FD · Boeing 777FS2 · Cargo/Baggage DoorsSDR FDEA201308011737Door Seal · lack of lubeL1 DOOR HARD TO OPEN. LUBRICATED DOOR SEAL. DOOR OPS CHECKED NORMAL AND WITHIN LIMITS IAW MM 52-11-00-5.Aug 1, 2013 · N851FD · Boeing 777FS2 · Passenger/Crew DoorsSDR FDEA201011194423Guard · out of rigEMERGENCY LIGHT SWITCH GUARD/WIRE ON OVERHEAD PANEL OUT OF RIG. CAP WILL NOT CLOSE PROPERLY WHEN EMERGENCY LIGHTS SWITCH IS IN " ARMED " POSITION. R & R SWITCH GUARD AND OPS NORMAL IAW SMP.Nov 19, 2010 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA201011184417Spring · looseWHEN GUARD COVER ON EMERGENCY LIGHTS IS CLOSED IT TURNS THE EMERGENCY LIGHTS TO OFF. FOUND SPRING IN GUARD COVER OF EMERGENCY LIGHT SWITCH LOOSE. ADJUSTED & REINSTALLED SPRING IAW SMP PERFORMED OPS TEST FOR EMERGENCY LIGHT WITH CONTROL SWITCH IAW AMM 33-51-Nov 18, 2010 · N851FD · Boeing 777FS2 · Emergency LightingSDR FDEA201004271377Slide · dislodgedRT EMERGENCY SLIDE DEPLOYED ON THE GROUND. ANC R RELEASED FOR SERVICE IAW MEL: 52-11-01-02 CATEGORY: C EXPIRATION: 07MAY10 "MEL 52-11-01-02: DOOR (R1 SLIDE/RAFT-INOP) IF SLIDE/RAFT TO BE RETAINED ONBOARD THEN PRIOR TO EACH DEPARTURE MX MUST VERIFY SLIDE Apr 27, 2010 · N851FD · Boeing 777* · Escape Slide
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