# Service difficulty reports: N859FD A list on [N859FD](https://openairdocs.org/aircraft/N859FD.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202606110701](https://openairdocs.org/sdr/FDEA202606110701.md): Skin · delaminated · Jun 11, 2026 · N859FD · Boeing 777222 · Trailing Edge Flaps > LHW OB FLAP LWR SURFACE 265IN FROM IB EDGE, 10IN FROM LWR EDGE FOUND DELAMINATION. REPAIRED LHW OB FLAP LWR SURFACE DELAMINATION AT OTEF STA 281 AS PER B777 SRM 57-53- 01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4 FIGURE 210 REV 53.0 AND EA: G-5750- T - [SDR FDEA202606090690](https://openairdocs.org/sdr/FDEA202606090690.md): Retainer · damaged · Jun 9, 2026 · N859FD · Boeing 777FS2 · Leading Edge Devices > FOUND RH WING SLAT NR 8 IB EDGE SEAL RETAINER UPPER SURFACE AFT SECOND FASTENER HOLE WORN. RH WING NO.8 SLAT IB EDGE OUTER SKIN FASTENER HOLE WORN AREA REPAIRED IAW SRM 57-43-01-2R REPAIR 6 FIGURE 203, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-20-01-0G, REV - [SDR FDEA202606090689](https://openairdocs.org/sdr/FDEA202606090689.md): Skin · damaged · Jun 9, 2026 · N859FD · Boeing 777FS2 · Leading Edge Devices > NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE FOUND WORN. NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE WORN AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 6 FIGURE 203, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-20- - [SDR FDEA202606060678](https://openairdocs.org/sdr/FDEA202606060678.md): Skin · cracked · Jun 6, 2026 · N859FD · Boeing 777FS2 · Wing, Plate/Skin > DURING PERFORM WORK CARD: E G-5710-E0376285 G P11 STEP 5.A.(2) THEN FOUND 01 EA CRACKED ON LT UPPER WING SKIN FASTENER NR 5. REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C, SRM 51-40-02-0G FIGURE 12, SRM 51-40-04-0G FIGURE 2 TABLE A, REV 53.0 AND - [SDR FDEA202606060677](https://openairdocs.org/sdr/FDEA202606060677.md): Skin · cracked · Jun 6, 2026 · N859FD · Boeing 777FS2 · Wing, Plate/Skin > DURING PERFORM WORK CARD:E G-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 01 EA CRACK ON RH UPPER WING SKIN FASTENER #5. REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C, SRM 51-40-02-0G FIGURE 12, SRM 51-40-04-0G FIGURE 2 TABLE A, REV 53.0 AND EA G - [SDR FDEA202606050673](https://openairdocs.org/sdr/FDEA202606050673.md): Skin · damaged · Jun 5, 2026 · N859FD · Boeing 777FS2 · Fuselage Main, Plate/Skin > REQUEST A PERMANENT REPAIR ON AFT FUSELAGE SKIN STA 2319 TO STA 2344.5, S-48R TO S-49R. - [SDR FDEA202602180233](https://openairdocs.org/sdr/FDEA202602180233.md): Slide · damaged · Feb 18, 2026 · N859FD · Boeing 777FS2 · Escape Slide > R1 DOOR SLIDE REQUIRES CORRECT BREAKAWAY WIRE TO BE INSTALLED ON PACKBOARD RELEASE CABLE. REF F.E.A. G2560-F0386294 C P1. INSTALLED CAD-PLATED COPPER BREAKAWAY WIRE MS20995CY16 ON R1 DOOR SLIDE SERIAL # M10771 PACKBOARD RELEASE CABLE PER F.E.A. WORK CARD IN - [SDR FDEA202309051545](https://openairdocs.org/sdr/FDEA202309051545.md): Floor Panel · cracked · Sep 5, 2023 · N859FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 FOUND CRACKED AT STA1706 RBL1 EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 AT STA 1706 RBL 1 CRACK SIZE L=3.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM53-00-50-1A ALLOWABLE DAMAGE 1 REV 44.0.REPAIRED THE DA - [SDR FDEA202309051544](https://openairdocs.org/sdr/FDEA202309051544.md): Floor Panel · cracked · Sep 5, 2023 · N859FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA1660 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 AT STA 1660 RBL 1 CRACK SIZE L=3.0" OUT OF ALLOWABLE LIMIT AS PER B777 SRM53-00-50-1A ALLOWABLE DAMAGE 1 REV 44.0.REPAIRED THE D - [SDR FDEA202106101495](https://openairdocs.org/sdr/FDEA202106101495.md): Brake Assy · burned · Jun 10, 2021 · N859FD · Boeing 777FS2 · Landing Gear Brake System > MDIS 859 32-40 8127 10JUN21 CDG FACT U AT ARRIVAL, #1 BRAKE FIRE. MAX VALUES: #1 WHEEL/BRAKE: 265PSI TEMP:4.4 #2 WHEEL/BRAKE: 270PSI 4.3 #3 WHEEL/BRAKE: 250PSI 1.8 #4 WHEEL/BRAKE: 245PSI 1.7 #5 WHEEL/BRAKE: 275PSI 4.1 #6 WHEEL/BRAKE: 289PS - [SDR FDEA202106101494](https://openairdocs.org/sdr/FDEA202106101494.md): Brake Assy · fire · Jun 10, 2021 · N859FD · Boeing 777FS2 · Landing Gear Brake System > MDIS 859 32-40 8127 10JUN21 CDG AT ARRIVAL, #1 BRAKE FIRE. MAX VALUES: #1 WHEEL/BRAKE: 265PSI TEMP:4.4 #2 WHEEL/BRAKE: 270PSI 4.3 #3 WHEEL/BRAKE: 250PSI 1.8 #4 WHEEL/BRAKE: 245PSI 1.7 #5 WHEEL/BRAKE: 275PSI 4.1 #6 WHEEL/BRAKE: 289PSI 4.6 - [SDR FDEA2020052211028](https://openairdocs.org/sdr/FDEA2020052211028.md): Pseu · loose · May 21, 2020 · N859FD · Boeing 777FS2 · Landing Gear Position and Warning > NUMEROUS STATUS MESSAGES RELATED TO EICAS CAUTION AUTOSPEED BRAKES. PSEU 2, PSEU 1, GEAR CONTROL...AND MANY MORE. ALL CAME ON WHEN CAUTION CAME UP. FOUND PSEU #1 LOOSE IN THE RACK, RESET PSEU #1 IN IT'S RACK REF B777 M.M. 32-08-01-4, VERIFIED #2 PSEU IS - [SDR FDEA201902210470](https://openairdocs.org/sdr/FDEA201902210470.md): Light · inoperative · Feb 21, 2019 · N859FD · Boeing 777FS2 · Emergency Lighting > POST-FLT INSP, ONE OVRHD LT INOP ON EMERGENCY LT'S TEST. RE-LAMPED, REF AMM 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC. - [SDR FDEA201902190452](https://openairdocs.org/sdr/FDEA201902190452.md): Window · dirty · Feb 19, 2019 · N859FD · Boeing 777FS2 · Passenger/Crew Doors > DOOR 1L FORWARD WINDOW FOR GIRT BAR FLAG ON RIGHT SIDE (NOSE) SIDE DOES NOT FULLY SHOW YELLOW FLAG IN THE WINDOW WHEN 1L DOOR ARMED. DIFFICULT TO TELL IN THAT WINDOW IF YELLOW FLAG SHOWN IN WINDOW WHEN DOOR IS ARMED. CLEANED THE GIRT BAR FLAG VIEWPORTS FOR TH - [SDR FDEA2018092532658](https://openairdocs.org/sdr/FDEA2018092532658.md): Floor Support · cracked · Sep 23, 2018 · N859FD · Boeing 777FS2 · Fuselage Miscellaneous Structure > LOWER BULK CARGO COMPARTMENT STA 1932, RBL 36 FLOOR SUPPORT FOUND CRACK. REPAIRED AS PER SRM 53-70-53-2R FIG 202 REPAIR 2 FROM STATION 1925 TO STATION 1968 RBL 36. REPAIR CLASSIFIED AS MAJOR AS PER GMM6-2-100. - [SDR FDEA201711083189](https://openairdocs.org/sdr/FDEA201711083189.md): Cover · broken · Nov 8, 2017 · N859FD · Boeing 777FS2 · Emergency Lighting > 1R ENTRY DOOR, SIDE EXIT LIGHT COVER BROKEN OFF. REMOVED AND REPLACED BROKEN EMERGENCY EXIT LIGHT IAW AMM 33-51-01-2. OPS CHECKED GOOD AT THIS TIME. A/C OK FOR SERVICE. (EXIT INDICATOR ASSY, GOODRICH P/N 702409-1001) - [SDR FDEA201706281780](https://openairdocs.org/sdr/FDEA201706281780.md): Door · out of adjust · Jun 28, 2017 · N859FD · Boeing 777FS2 · Passenger/Crew Doors > L1 DOOR HARD TO ARM AND ONCE ARMED, RAMP AGENT INFORMED CREW THAT THE DOOR DID NOT APPEAR CLOSED. PREFORMED PASSANGER DOOR ENTRY ADJUSTMENT AND TEST IAW AMM 52-11-00-5. TESTED GOOD. - [SDR FDEA201608283063](https://openairdocs.org/sdr/FDEA201608283063.md): Apu · smoke · Aug 28, 2016 · N859FD · Boeing 777FS2 · APU Core Engine > APU OIL QTY STATUS MESSAGE FOLLOWED BY SMOKE IN THE COCKPIT. PERFORMED AIR CONDITIONING SYSTEM OIL CONTAMINATION REMOVAL IAW AMM 21-00-01-2, AND AMM 05-51-50-2. DID NOT NOTICE ANY SMOKE OR FUMES DURING ENGINE OPERATION AND TAXI. R & R THE APU, OPS AND L - [SDR FDEA201401070065](https://openairdocs.org/sdr/FDEA201401070065.md): Guard · broken · Jan 7, 2014 · N859FD · Boeing 777FS2 · Emergency Lighting > PER CREW DEBRIEF EMERGENCY LIGHTS SWITCH GUARD BROKEN. GUARD SPRING IS BROKEN, SWITCH WORKS OK. REPLACED SWITCH GUARD IAW SMP. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N859FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N859FD/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.