# Service difficulty reports: N858FD A list on [N858FD](https://openairdocs.org/aircraft/N858FD.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202602160217](https://openairdocs.org/sdr/FDEA202602160217.md): Safety Wire · wrong part · Feb 16, 2026 · N858FD · Boeing 777FS2 · Escape Slide > LEFT SLIDE ASSY. SN 3359, FOUND BREAK AWAY WIRE SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. RELEASED FOR SERVICE PER MEL: 52-11-01-02 CATEGORY: C EXPIRATION: 22FEB26 "MEL 52-11-01-02: DOOR _L1__ DOOR - INOP. IF SLID E/RAFT TO BE - [SDR FDEA202602120183](https://openairdocs.org/sdr/FDEA202602120183.md): Wire · wrong part · Feb 12, 2026 · N858FD · Boeing 777FS2 · Emergency Equipment > FOUND BREAKAWAY WIRE THAT SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. REMOVED LT DOOR SLIDE IAW MM 25-66-01-4. REMOVED STAINLESS SAFETY WIRE AND INSTALLED CORRECT WIRE IAW FEA G-2560-F0386282C. REINSTALLED DOOR SLIDE IAW 25-66-01-4. DO - [SDR FDEA202403210329](https://openairdocs.org/sdr/FDEA202403210329.md): Skin · cracked · Mar 21, 2024 · N858FD · Boeing 777FS2 · Leading Edge Devices > LH WING NO.7 SLAT OUTER SKIN FOUND CRACK AT ISS193. CRACK LENGTH 1.44 INCHES, NUMBER OF CRACK: 01 EA. LH WING NO.7 SLAT OUTER SKIN CRACKED AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 14, SRM 51-20-06-0G, SRM 51-30-01-0G, SRM 51-20-01-0G, SRM 57-43-01 - [SDR FDEA202403140284](https://openairdocs.org/sdr/FDEA202403140284.md): Skin · dented · Mar 14, 2024 · N858FD · Boeing 777FS2 · Trailing Edge Flaps > RH WING OB FLAP LWR SURFACE FOUND DENT AT 261 IN AWAY FROM OB EDGE AND 6 IN AWAY FROM AFT EDGE. EVALUATED RH WING OB FLAP LWR SURFACE DENT AT 261 IN AWAY FROM OB EDGE AND 6 IN AWAY FROM AFT EDGE DAMAGE SIZE L X W= 4.2"X 2.4" OUT OF ALLOWABLE LIMIT AS PER - [SDR FDEA202403140283](https://openairdocs.org/sdr/FDEA202403140283.md): Skin · dented · Mar 14, 2024 · N858FD · Boeing 777FS2 · Trailing Edge Flaps > RH WING OB FLAP LWR SURFACE FOUND DENT AT 257 IN AWAY FROM OB EDGE AND 14.5 IN AWAY FROM AFT EDGE. EVALUATED RH WING OB FLAP LWR SURFACE DENT AT 257 IN AWAY FROM OB EDGE AND 14.5 IN AWAY FROM AFT EDGE DAMAGE SIZE L X W= 4.0"X 1.2" OUT OF ALLOWABLE LIMIT A - [SDR FDEA202107281886](https://openairdocs.org/sdr/FDEA202107281886.md): Unknown · odor · Jul 28, 2021 · N858FD · Boeing 777FS2 · Air Distribution System > AFTER BLOCK-IN AND SHUTDOWN ENTIRE CREW SMELLED AN ELECTRICAL TYPE BURNING SMELL IN THE GALLEY. THIS WAS SLIGHTLY NOTICEABLE DURING THE FLIGHT AND THE RFO WHO WAS SEATED IN THE GALLEY AREA DURING THE APPROACH AND LANDING SAID THE GALLEY AREA LOST COMPLETE PO - [SDR FDEA202106231585](https://openairdocs.org/sdr/FDEA202106231585.md): Floor Panel · cracked · Jun 23, 2021 · N858FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK FLOOR PNL P/N:152W8652-16 FOUND CRACKED AT STA 1622 RBL75. THE CARACKED MAIN DECK FLOOR PNL P/N:152W8652-16 AT STA 1622 RBL 75 REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 38.0. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100. - [SDR FDEA202106231584](https://openairdocs.org/sdr/FDEA202106231584.md): Floor Panel · cracked · Jun 23, 2021 · N858FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK FLOOR PNL P/N: 152W8652-4 FOUND CRACKED AT STA 1455 RBL 60. THE CARACKED MAIN DECK FLOOR PNL P/N:152W8652-4 AT STA 1455 RBL 60 REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 38.0. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100. - [SDR FDEA202106231583](https://openairdocs.org/sdr/FDEA202106231583.md): Floor Panel · cracked · Jun 23, 2021 · N858FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK FLOOR PNL P/N: 152W8652-6 FOUND CRACKED AT STA 1470 RBL 33. THE CARACKED MAIN DECK FLOOR PNL P/N:152W8652-6 AT STA 1470 RBL 33 REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 38.0. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100. - [SDR FDEA202106231582](https://openairdocs.org/sdr/FDEA202106231582.md): Floor Panel · cracked · Jun 23, 2021 · N858FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK FLOOR PNL P/N: 152W8652-3 FOUND CRACKED AT STA 1488 LBL53. THE CARACKED MAIN DECK FLOOR PNL P/N:152W8652-3 AT STA 1488 LBL 53 REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 38.0. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100. - [SDR FDEA202106231581](https://openairdocs.org/sdr/FDEA202106231581.md): Floor Panel · cracked · Jun 23, 2021 · N858FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK FLOOR PNL P/N:152W8452-21 FOUND CRACKED AT STA 1325 LBL 43. THE CRACKED MAIN DECK FLOOR PNL P/N:152W8452-21 AT STA 1325 LBL 43 REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1,REV 38.0.REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100. - [SDR FDEA202106231580](https://openairdocs.org/sdr/FDEA202106231580.md): Floor Panel · cracked · Jun 23, 2021 · N858FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK FLOOR PNL P/N: 152W8452-19 FOUND CRACKED AT STA 1355 LBL 25. THE CRACKED MAIN DECK FLOOR PNL P/N:152W8452-19 AT STA 1355 LBL 25 REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1 REV 38.0. REPAIR CLASSIFIED AS MAJOR PER GMM 06-2-100. - [SDR FDEA201909202294](https://openairdocs.org/sdr/FDEA201909202294.md): Tire · low pressure · Sep 20, 2019 · N858FD · Boeing 777FS2 · Tire > 20 MINUTES INTO FLIGHT, REC'D TIRE PRESS EICAS. #12 TIRE SHOWED 199 PSI AT 1 HOUR 30 MINUTES SHOWS 173PSI ALL OTHER TIRES PRESSURE APPROX 235 PSI. PRESSURE ON LANDING 123 PSI. REMOVED AND REPLACE #11 TIRE AND #12 TIRE AS REQUIRED IAW AMM 32-45-01-4. - [SDR FDEA201712283459](https://openairdocs.org/sdr/FDEA201712283459.md): Lamp · burned out · Dec 28, 2017 · N858FD · Boeing 777FS2 · Emergency Lighting > EMERGENCY LIGHTS REMAINED ON DURING PREFLIGHT. RED LIGHT ILLUMINATED IN THE GUARDED SWITCH. PERFORMED AN EMERGENCY LIGHT TEST IAW MM 33-51-00-05, AND FOUND ONE CEILING EMERGENCY LIGHT BURNED OUT. REPLACED THE LAMPS IAW MM 33-51-03-02 AND PERFORMED A TEST. - [SDR FDEA201711183271](https://openairdocs.org/sdr/FDEA201711183271.md): Door · binding · Nov 18, 2017 · N858FD · Boeing 777FS2 · Passenger/Crew Doors > THERE WAS A LOT OF RESISTANANCE WHEN ATTEMPTED TO OPEN L1 DOOR. LEFT DOOR CLOSED. USED R1 DOOR. VERIFIED ARM & DIARM FUNCTION WAS OK AND L1 DOOR POSSIBLE TO OPEN. - [SDR FDEA201607242610](https://openairdocs.org/sdr/FDEA201607242610.md): Floor Support · cracked · Jul 24, 2016 · N858FD · Boeing 777FS2 · Fuselage Miscellaneous Structure > BULK CARGO FLOOR SUPPORT AT BS 1980.5 APPROXIMATELY AT RBL 34 FOUND CRACKED. - [SDR FDEA201412124117](https://openairdocs.org/sdr/FDEA201412124117.md): Light · inoperative · Dec 12, 2014 · N858FD · Boeing 777FS2 · Emergency Lighting > EMERGENCY CEILING LIGHT IN CABIN AREA NEAR L1 DOOR WOULD NOT ILLUMINATE DURING TEST. R & R THE LIGHT IAW AMM 33-51-03-2. ACFT OK FOR SERVICE. ## 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 = 'N858FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N858FD/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.