# Service difficulty reports: N887FD A list on [N887FD](https://openairdocs.org/aircraft/N887FD.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202602160215](https://openairdocs.org/sdr/FDEA202602160215.md): Safety Wire · wrong part · Feb 16, 2026 · N887FD · Boeing 777FS2 · Escape Slide > RH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/5696 (F.E.A.# G-2560-F0386294 C PART 1) RH SLIDE - REPLACE THE BREAKAWAY WIRE SE - [SDR FDEA202602160214](https://openairdocs.org/sdr/FDEA202602160214.md): Safety Wire · wrong part · Feb 16, 2026 · N887FD · Boeing 777FS2 · Escape Slide > LH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOAR RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/3937 (FEA G-2560-F0386282 C P1). REMOVED AND REPLACED BREAKAWAY WIRE SECURING RELE - [SDR FDEA202510101945](https://openairdocs.org/sdr/FDEA202510101945.md): Skin · worn · Oct 10, 2025 · N887FD · Boeing 777FS2 · Leading Edge Devices > NUMBER 7 SLAT OUTER SKIN FASTENER HOLE FOUND WORN OUT AT ISS 184. NR 7 SLAT OUTER SKIN FASTENER HOLE AT ISS 184 REPAIRED IAW SRM 57-43-01-2R, REPAIR 6, FIGURE 203, REV 51, & EA G-5750-T0385264 P1, MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA202510081920](https://openairdocs.org/sdr/FDEA202510081920.md): Skin · cracked · Oct 8, 2025 · N887FD · Boeing 777FS2 · Wing, Plate/Skin > DURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF LT WING UPPER SKIN COMMON TO FASTENERS 0-5, FOUND ONE CRACK AT 6 O'CLOCK ON HOLE NR 5. NR 5 HOLE AT LT WING UPPER SKIN RIB BAY 10 TRAILING EDGE WAS REPAIRED IAW SRM 51-40-05-0G, 51-40-02-0G, 51-40-04-0G, REV 5 - [SDR FDEA202510081918](https://openairdocs.org/sdr/FDEA202510081918.md): Skin · cracked · Oct 8, 2025 · N887FD · Boeing 777FS2 · Wing, Plate/Skin > DURING PERFORMANCE OF UT &OPEN HOLE HFEC INSPECTION OF RT WING UPPER SKIN COMMON TO FASTENERS 0-5 & FOUND TWO CRACKS AT 6 O'CLOCK & 12 O'CLOCK ON HOLE NR 5. NR 5 HOLE AT RT WING UPPER SKIN RIB BAY 10 TRAILING EDGE REPAIRED IAW SRM 51-40-05-0G, 51-40-02-0G, 5 - [SDR FDEA202412121812](https://openairdocs.org/sdr/FDEA202412121812.md): Life Raft · damaged · Dec 12, 2024 · N887FD · Boeing 777FS2 · Life Raft > AFTER ARRIVAL IN MEMPHIS L1 DOOR VERY DIFFICULT TO OPEN. DURING T/S AS PER FIM 52-11-00-810-814 FOUND FLUF AND OTHER DEBRIE HINDERING THE PROPER OPERATION AND INTERCONNECTION BETWEEN THE GIRT BAR AND THE FWD GIRT BAR FLOOR FITTING. ALL FLUF AND DEBRIE REMO - [SDR FDEA202304190676](https://openairdocs.org/sdr/FDEA202304190676.md): Floor Panel · cracked · Apr 19, 2023 · N887FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK CARGO FLLOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL73.5-76 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL73.5-76 CRACK(OFF WING), CRACK SIZE L =2.5" IN LOWER SURFACE WITHIN LIMIT. EVALUATED AS PER B777 SRM 53-00- - [SDR FDEA202304180666](https://openairdocs.org/sdr/FDEA202304180666.md): Floor Panel · cracked · Apr 18, 2023 · N887FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8652-19) AT STA1393/LBL20-21.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1393/LBL20-21.5 CRACK(OFF WING), CRACK SIZE L =1.4" IN LOWER SURFACE WITHIN LIMIT, EVALUATED AS PER B777 SRM 53-00 - [SDR FDEA202304180665](https://openairdocs.org/sdr/FDEA202304180665.md): Floor Panel · cracked · Apr 18, 2023 · N887FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8652-21) AT STA1363/LBL43.75-44.75 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1363/LBL43.75-44.75 CRACK(OFF WING), CRACK SIZE L =0.9" IN LOWER SURFACE WITHIN LIMIT, EVALUATED AS PER B777 - [SDR FDEA202304180664](https://openairdocs.org/sdr/FDEA202304180664.md): Floor Panel · cracked · Apr 18, 2023 · N887FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1435.75/RBL76.25-77.25 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1435.75/RBL76.25-77.25 CRACK(OFF WING), CRACK SIZE L =0.9" IN LOWER SURFACE WITHIN LIMIT, EVALUATED AS PER - [SDR FDEA202304180663](https://openairdocs.org/sdr/FDEA202304180663.md): Floor Panel · cracked · Apr 18, 2023 · N887FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1292/LBL110-111 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1292/LBL110-111 CRACK(OFF WING), CRACK SIZE L =1.0" IN LOWER SURFACE WITHIN LIMIT, EVALUATED AS PER SRM 53-00- 50 - [SDR FDEA202304180662](https://openairdocs.org/sdr/FDEA202304180662.md): Floor Panel · cracked · Apr 18, 2023 · N887FD · Boeing 777FS2 · Fuselage Floor Panel > MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT SVTA1272/RBL110-113 FOUND CRACK. CRACK SIZE L =3.0" IN LOWER SKIN WITHIN LIMIT. EVALUATED AS PER B777 SRM 53-00-50- 1A,REV 43.1. REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 43.1. REPAIR CLASSIFIE - [SDR FDEA202108031924](https://openairdocs.org/sdr/FDEA202108031924.md): Control Unit · malfunctioned · Aug 3, 2021 · N887FD · Boeing 777FS2 · AC Generator-Alternator > 03AUG21 MEM OVER NORTH ATLANTIC, ELEC GEN OFF R, STARTED THE APU WITH APU GEN OFF, RESET GEN PER ECL.. APPROX 2.5 LATER, GOT ELEC AC BUS R. RESE THE R BUS TIE PER ECL, RESULTING IN SINGLE GEN OPS. CONF CALL WITH GOC, MOCC AND TECH PILOT AGAIN, USED - [SDR FDEA2019120433163](https://openairdocs.org/sdr/FDEA2019120433163.md): Tire · leaking · Dec 3, 2019 · N887FD · Boeing 777FS2 · Tire > PDIS 887 32-42 6858 03DEC19 MEM OPEN U LOGPAGES:3182122 TIRE PRESS EICAS ON DEPARTURE FROM ZSPD, TIRE #12 PRESSURE IS LOW AND DECREASING. REMOVED AND REPLACED #12 MLG TIRE C/W 777AMM32-45-01-4. FIRE TRUCKS PRESENT ON TAXI IN - [SDR FDEA201911223047](https://openairdocs.org/sdr/FDEA201911223047.md): Pcu · leaking · Nov 22, 2019 · N887FD · Boeing 777FS2 · Drag Control Actuator > ON CLIMBOUT RECEIVED "HYD QTY LOW R" EICAS, FOLLOWED BY "HYD PRESS PRI R" EICAS AND THEN "HYD PRESS SYS R" EICAS, COMPLIED WITH ALL NON-NORMAL CHECKLISTS. CHECKED FOUND RT ENGINE EDP HYD LEAK, ALSO FOUND HYD LEAK FROM NR 6 SPOILER PCA. CHECK THE RT EDP AND ACM - [SDR FDEA201707091886](https://openairdocs.org/sdr/FDEA201707091886.md): Autothrottle Sys · malfunctioned · Jul 9, 2017 · N887FD · Boeing 777FS2 · Auto Throttle System > AFTER BOTH ENGINES WERE STARTED. WHILE AWAITING THE GROUND CREW TO CLEAR THE WING. THE AUTO THROTTLE SERVO ENGAGED AND ATTEMPTED TO ADVANCE THE POWER. CAPTAIN RESTRAINED THRUST LEVER MOVEMENT, NO INDICATIONS OR COCKPIT EFFECTS OTHER THAN THE AUDIBLE NOIS - [SDR FDEA201609293403](https://openairdocs.org/sdr/FDEA201609293403.md): Floor Panel · cracked · Sep 29, 2016 · N887FD · Boeing 777FS2 · Fuselage Floor Panel > FOUND FLOOR SURFACE PLATE HAS CRACK 12 INCH, TWO LOCATION ON SAME PANEL AT POSITION 7R ON MDC. TEMPORARY REPAIR TO FLOOR PANEL AT POSITION 6R,7R, AND 8R. ROLLER TRAYS ARE REMOVED FROM REPAIR AREA. OK PER EA G-5321-T0328672. C/W EA G-5321-T0328672 P1. - [SDR FDEA201301230164](https://openairdocs.org/sdr/FDEA201301230164.md): Cover · faulty · Jan 23, 2013 · N887FD · Boeing 777FS2 · Emergency Lighting > EMERGENCY LIGHTS SWITCH RETURN SPRING FAULTY. DOES NOT RETURN SWITCH TO ARM WITH COVER CLOSED. R & R LIGHT SWITCH GUARD COVER IAW SMP OPS CHECKED NORMAL, ACFT OK FOR SERVICE. - [SDR FDEA201212204340](https://openairdocs.org/sdr/FDEA201212204340.md): Smoke Detector · malfunctioned · Dec 20, 2012 · N887FD · Boeing 777FS2 · Smoke Detection > AFTER BLOCK IN AND SHUTTING DOWN BOTH ENGINES, THE CREW SLEEP ROOM HAD AN AURAL SMOKE ALARM. THE ASSOCIATED ALARM LIGHT, NO APPARENT SMOKE WAS SEEN OR DETECTED. LIGHT ALARM WENT OUT AFTER APPROX 2 MINUTES. PERFORMED FLIGHT CREW REST SMOKE DETECTION IAW MM 2 ## 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 = 'N887FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N887FD/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.