N852FD

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 = 'N852FD' 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 FDEA202605310656Skin · damagedREQUEST A PERMANENT REPAIR ON LT AFT FUSELAGE AT APPROXIMATELY STA 1895 TO 1958 AND S-40L TO S-43L. LT AFT FUSELAGE AT APPROXIMATELY BS 1895 TO 1958 AND S-40L TO S-43L. DAMAGED SKIN & STRINGER PERFORMED PERMANENT REPAIR IAW SRM51-10-02-0G. SRM51-20-01-0G. May 31, 2026 · N852FD · Boeing 777FS2 · Fuselage Main, Plate/SkinSDR FDEA202602230259Safety Wire · wrong partFOUND INCORRECT SAFETY WIRE ON L1 DOOR SLIDE. AMM: 25-66-01-4 REPLACED SAFETY WIRE WITH CAD COPPER.Feb 23, 2026 · N852FD · Boeing 777FS2 · Passenger/Crew DoorsSDR FDEA202506251045Fitting · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA1434 RBL6.5. MAIN DECK CARGO FLOOR FITTING CORROSION REMOVED AND EVALUATED : MEASURED THE REWORKED AREA BELONG TO ZONE C,THE MAX ALLOWABLE BLEND OUT IS 0.002, THE MAX CLEAN UP DEPTH IS X=0.058Ï¿½>0.002Ï¿½Jun 25, 2025 · N852FD · Boeing 777F · Fuselage Main, Attach FittingsSDR FDEA202506251044Fitting · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA1434 LBL6.5. MAIN DECK CARGO FLOOR FITTING CORROSION REMOVED AND EVALUATED : MEASURED THE REWORKED AREA BELONG TO ZONE C, THE MAX ALLOWABLE BLEND OUT IS 0.002, THE MAX CLEAN UP DEPTH IS X=0.022Ï¿½>0.002ÏJun 25, 2025 · N852FD · Boeing 777F · Fuselage Main, Attach FittingsSDR FDEA202506251043Fitting · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA1413 LBL6.5. MAIN DECK CARGO FLOOR FITTING CORROSION REMOVED AND EVALUATED : MEASURED THE REWORKED AREA BELONG TO ZONE C,THE MAX ALLOWABLE BLEND OUT IS 0.002. THE MAX CLEAN UP DEPTH IS X=0.022 - 0.002 AND FJun 25, 2025 · N852FD · Boeing 777F · Fuselage Main, Attach FittingsSDR FDEA202506251042Fitting · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA 1193 RBL79. MAIN DECK CARGO FLOOR FITTING CORROSION REMOVED AND EVALUATED : MEASURED THE REWORKED AREA BELONG TO ZONE B,THE MAX ALLOWABLE BLEND OUT IS 0.030Ï¿½, THE MAX CLEAN UP DEPTH IS X=0.045Ï¿½>0.0Jun 25, 2025 · N852FD · Boeing 777F · Fuselage Main, Attach FittingsSDR FDEA202506251041Fitting · corrodedMAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA 1232 RBL79. MAIN DECK CARGO FLOOR FITTING CORROSION REMOVED AND EVALUATED : MEASURED THE REWORKED AREA BELONG TO ZONE Ï¿½BÏ¿½,THE MAX ALLOWABLE BLEND OUT IS 0.030Ï¿½, THE MAX CLEAN UP DEPTH IS X=0.041ÏJun 25, 2025 · N852FD · Boeing 777F · Fuselage Main, Attach FittingsSDR FDEA202506100881Skin · nickedFOUND A NICK AT RH LOWER FWD FUSELAGE SKIN AT STA 518.5 S-47R. A NICK AT RH LOWER FWD FUSELAGE SKIN AT STA 518.5 S-47R REPAIRED AS PER B777 SRM 53-00- 01-2R REPAIR 3 FIGURE 202 REV 47.5. THIS IS A CATEGORY B REPAIR PER B777 SRM 53-00-01-2R REPAIR 3 REV 47.5Jun 10, 2025 · N852FD · Boeing 777FS2 · Fuselage Main, Plate/SkinSDR FDEA202506060845Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8302-31 FOUND CARCKED AT STA1010 LBL85. DAMAGE SIZE:L=4.5" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 REV 47.5 AND REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1 REV 47.5.THIS IS A MAJOR RJun 6, 2025 · N852FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202506060844Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8302-34 FOUND CRACKED AT STA 1010 RBL85. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-34 CRACKED AT STA 1010 RBL 85.DAMAGE SIZE:L=4.9" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 REV 47.5 ANDJun 6, 2025 · N852FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202506060843Skin · dentedLEFT WING OTBD FLAP LOWER SKIN FOUND DENT AT 300 MM FROM T/E AND 1700 MM FROM INBOARD SIDE OF FLAP. REPAIRED LH WING OTBD FLAP LOWER SKIN DENT AT 300MM FROM T/E AND 1700MM FROM INBOARD SIDE OF FLAP AS PER B777 SRM 57-53-01-2R-2 & SRM 51-70-04-2R-1 REV 47.5 AJun 6, 2025 · N852FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202506060842Skin · dentedRIGHT WING OB FLAP LWR SURFACE FOUND MATERIAL MISSING AT 305 IN TO IB AND 3 IN TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFAE MATERIAL MISSING AT 305 IN TO IB AND 3 IN TO AFT EDGE AS PER B777 SRM 57-53-01-2R-2 & SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-TJun 6, 2025 · N852FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202506060841Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 159 IN TO IB AND 10 IN TO AFT EDGE AND CRACK AND MATERIAL MISSING, TOTAL DAMAGE SIZE 10 INCHES BY 10 INCHES. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT 159 IN TO IB AND 10 IN TO AFT EDGE AND CRACK AND MATERIAL MIJun 6, 2025 · N852FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA202506050839Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE LEFT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 01EA CRACK AT HOLE #5 AS MARKED. LH WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40- 02-0G, SRM 51-40-04-0G, SRM Jun 5, 2025 · N852FD · Boeing 777F · Wing, Plate/SkinSDR FDEA202506050838Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE RIGHT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 01EA CRACK AT HOLE #5 AS MARKED. RH WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40- 02-0G, SRM 51-40-04-0G, SRJun 5, 2025 · N852FD · Boeing 777F · Wing, Plate/SkinSDR FDEA202107021650Lamp · inoperativePOST-FLT INSP, L-1 DOOR EXTERIOR EMERGENCY LT INOP. RELAMPED, REF AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVCJul 2, 2021 · N852FD · Boeing 777FS2 · Emergency LightingSDR FDEA202104170946Line · looseHYD QTY LOW C AT 4:21 INTO FLIGHT FOLLOWED BY RESERVE BRAKES/STRG. HYDRAULIC QUANTITY CENTER DECREASED FROM .41 AT TIME OF EICAS TO .30 BY END OF FLIGHT. ALL SYSTEMS FUNCTIONED NORMALLY ON APPROACH, LANDING AND TAXI. ON BLOCK IN FOUND #5 BRAKE LINE LOOSEApr 17, 2021 · N852FD · Boeing 777FS2 · Hydraulic System, MainSDR FDEA202006261367Spar · crackedDURING ULTRASONIC INSPECTION ON THE VERTICAL FLANGE OF THE SPAR CHORD AND HIGH FREQENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES AT RIGHT HAND SIDE UNDERWING LONGERON LOWER WING, BUTT STATION 1035, VERTICAL FLANGE OF THE SPAR CHJun 26, 2020 · N852FD · Boeing 777FS2 · Wing SparSDR FDEA202006261366Skin · 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 01 EACH CRACKS ON THE SKIN APPROXIMATE 0.7" AT STATION 1030 BETWEENJun 26, 2020 · N852FD · Boeing 777FS2 · Fuselage Main, Plate/SkinSDR FDEA202006261365Skin · 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 HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 01 EACH CRACKS ON THE SKIN APPROXIMATE 0.6" AT STATION 1030 BETWEEJun 26, 2020 · N852FD · Boeing 777FS2 · Fuselage Main, Plate/SkinSDR FDEA202006191279Longeron · crackedCRACK INDICATION FOUND DURING ULTRASONIC INSPECTION ON LEFT HAND SIDE UNDERWING LONGERON FITTING AT BODY STATION 1035. COMPLIANCE WITH EO G-5310-E0332629 G (P5). TITLE: FUSELAGE - MAINFRAME - INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATJun 19, 2020 · N852FD · Boeing 777FS2 · Fuselage Main, Longeron/StringerSDR FDEA202006191278Longeron · crackedCRACK INDICATION FOUND DURING ULTRASONIC INSPECTION ON RIGHT HAND SIDE UNDERWING LONGERON FITTING AT BODY STATION 1035. COMPLIANCE WITH EO G-5310-E0332629 G (P6). TITLE: FUSELAGE - MAINFRAME - INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STAJun 19, 2020 · N852FD · Boeing 777FS2 · Fuselage Main, Longeron/StringerSDR FDEA2019061101266Wheel · damagedEICAS STATUS " TIRE PRESSURE" #10 TIRE PRESSURE BEFORE LANDING 157 EICAS STATUS " TIRE PRESSURE" #9 TIRE PRESSURE BEFORE LANDING 204 PER CREW DEBRIEF, #9 WHEEL IS AT 157 PSI AND #10 WHEEL IS AT 204 PSI . CHECK #9 AND #10 TIRE PRESS WITH EXTERNAL Jun 10, 2019 · N852FD · Boeing 777FS2 · Wheel/Ski/FloatSDR FDEA2018092522654Tube · damagedREF WRI 29-02/8711 NEED TO INSTALL FLEX LINE IN PLACE OF SEVERED RIDGID HYD PRESSURE LINE ON THE #12 SPOILER PCU PRESSURE LINE . NUMBER 12 SPOILER HAS TEMP FLEX LINE INSTALLED PER MM-NEEDS RE-INSPECT EVERY 7 DAYS AND FINAL REPAIR AT NEXT B CHECK INSSep 22, 2018 · N852FD · Boeing 777FS2 · Drag Control SystemSDR FDEA201809202643Flap · gougedFOUND DAMAGE ON LEADING EDGE OF OUTBOARD FLAP ADJACENT TO NR 12 SPOILER ACTUATOR. REF WRI 29-02/8711 LEADING EDGE FLAP GOUGE IS OUT OF LIMITS REF SRM 57-53-01-1A. COMPLIED WITH EA G-2750-T0342462 PART1. REPAIRED RT WING OUTBOARD FLAP LEADING EDGE PER SRM 51-70Sep 20, 2018 · N852FD · Boeing 777FS2 · Trailing Edge FlapsSDR FDEA2018092502653Tube · severedHYD PRESS SYS, R HYD QUANITY 0. FOUND #12 SPOILER ACTUATOR TUBE SEVERED. ALSO FOUND ACTUATOR MOUNT BRACKETS BROKEN. WILL NEED NEW SPOILER ACTUATOR ASSY. ACTUATOR MOUNT BOLTS SHEARED IN ATTACH FITTING. REMOVED AND REPLACED #12 SPOILER PCU REF MM 27-61-Sep 20, 2018 · N852FD · Boeing 777FS2 · Hydraulic System, MainSDR FDEA2018092502652Tube · severedHYD PRESS SYS, R HYD QUANITY 0. FOUND #12 SPOILER ACTUATOR TUBE SEVERED. ALSO FOUND ACTUATOR MOUNT BRACKETS BROKEN. WILL NEED NEW SPOILER ACTUATOR ASSY. ACTUATOR MOUNT BOLTS SHEARED IN ATTACH FITTING. REMOVED AND REPLACED #12 SPOILER PCU REF MM 27-61-Sep 20, 2018 · N852FD · Boeing 777FS2 · Hydraulic System, MainSDR FDEA2018092102642Spoiler · damagedWHILE INSPECTION OF DAMAGE ON WRI 29-02/8711. ALSO FOUND NR 12 SPOILER TRAILING EDGE DAMAGE AT 5 DIFFERENT LOCATIONS. REMOVED AND REPLACED NR 12 SPOILER REF AMM 27-61-11-4.Sep 20, 2018 · N852FD · Boeing 777FS2 · SpoilersSDR FDEA201809202634Hydraulic Line · severedHYD PRESS SYS, R HYD QUANTITY 0. FOUND NR 12 SPOILER ACTUATOR TUBE SEVERED. REF IPC 27-11-05-66 ITEM 455. ALSO FOUND ACTUATOR MOUNT BRACKETS BROKEN. WILL NEED NEW SPOILER ACTUATOR ASSY ACTUATOR MOUNT BOLTS SHEARED IN ATTACH FITTING REF IPC 57-52-51-38 FIG 38 SSep 20, 2018 · N852FD · Boeing 777FS2 · Hydraulic System, MainSDR FDEA201703280996Light · inoperativeDURING PREFLIGHT INSPECTION, L1 DOOR FWD EMERGENCY EXIT LIGHT NOT ILLUMINATED.Mar 28, 2017 · N852FD · Boeing 777FS2 · Emergency LightingSDR FDEA201504101210Unknown · malfunctionedEMERGENCY LIGHT LINE ON SHUTDOWN CHECKLIST REMAINS WHITE WITH SWITCH IN OFF POSITION. CYCLED EMER LIGHT SWITCH, CHANGED TO GREEN SEVERAL TIMES IAW MM 31-61-00-2. ACFT OK FOR SERVICE.Apr 10, 2015 · N852FD · Boeing 777FS2 · Central DisplaySDR FDEA201406011256Hook And Loop · unsecureCAPTAIN'S LIFE VEST POUCH HOOK AND LOOP HAS COME OFF OF SEAT. SECURED CAPTAIN`S LIFE VEST POUCH HOOK AND LOOP IAW SMP. OK FOR SERVICE.Jun 1, 2014 · N852FD · Boeing 777FS2 · Emergency EquipmentSDR FDEA201302030263Socket · failedEXTERIOR EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. R & R SOCKET ASSY IAW WDM 33-51-41. OPS CHECK GOOD. ACFT OK FOR SERVICE,Feb 3, 2013 · N852FD · Boeing 777FS2 · Emergency LightingSDR FDEA201301290216Lamp · inoperativeRT EMERGENCY LIGHT NEAR R1 DOOR INOPERATIVE. REPLACED LAMP IAW AMM 33-50-00-2, OK FOR SERVICE.Jan 29, 2013 · N852FD · Boeing 777FS2 · Emergency LightingSDR FDEA201209113284Skin · crackedLEFT WING NR 7 SLAT OUTER SKIN INBD AREA FOUND CRACKED. REPAIRED IAW SRM 57-43-01 FIGURE 201 REPAIR 8 AND EA G-5750-159900. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 11, 2012 · N852FD · Boeing 777FS2 · Leading Edge DevicesSDR FDEA201101200318Engine · fodDURING CLIMB & LEVEL OFF, VIBRATION SHOWED 4.0 LT & 5.0 RT ABLE TO REDUCE LT TO 1.3 BUT UNABLE TO REDUCE RT. AFTER CONSULT WITH MOCC & FLT OPS WERE INSTRUCTED TO RTB PANC, NO FUEL DUMP REQUIRED. MODERATE AIRFRAME VIBRATION ASSOCIATED WITH THE RT ENGINE VIBJan 20, 2011 · N852FD · Boeing 777FS2 · Engine (Turbine/Turboprop)SDR FDEA201004181243Hose · failedLT MLG TIRES DEFLATED DURING TAXI CHECK. SHOWS EVIDENCE OF FIRE/OVERHEAT AND FIRE SUPPRESSION AGENTS. R & R THE NR 1 FWD BRAKE LINE, THE NR 1 AFT BRAKE LINE AND SWIVEL ASSY AND THE NR 5 BRAKE LINE. R & R LT MLG BRAKE ASSEMBLIES IAW MM 32-45-07-4-0. BLEED Apr 18, 2010 · N852FD · Boeing 777* · Hydraulic System, Main
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