# Service difficulty reports: N896FD A list on [N896FD](https://openairdocs.org/aircraft/N896FD.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202607150925](https://openairdocs.org/sdr/FDEA202607150925.md): Skin · bulged · Jul 15, 2026 · N896FD · Boeing 777FS2 · Leading Edge Devices > RIGHT WING NR 9 SLAT UPPER SURFACE 32IN FROM OTBD EDGE FOUND BULGE. NR 9 SLAT UPPER SURFACE 32 INCH FROM OB EDGE BULGE AREA REPAIRED IAW SRM 51-40-02-0G, SRM 57-43-01-2R REPAIR 16 FIG 202, SRM 51-40-05-0G, SRM 51-20-01-0G REV 53.0 AND EA G-5750-T0388015 P1. - [SDR FDEA202607130917](https://openairdocs.org/sdr/FDEA202607130917.md): Skin · dented · Jul 13, 2026 · N896FD · Boeing 777F · Trailing Edge Flaps > FOUND LT WING T/E OTBD FLAP LOWER SURFACE 01EA DENT AT OTEF 44 INCHES AND T/E 4 INCHES. - [SDR FDEA202512062224](https://openairdocs.org/sdr/FDEA202512062224.md): Lamp · failed · Dec 6, 2025 · N896FD · Boeing 777F · Emergency Lighting > SUPERNUMERARY AREA CEILING EMERGENCY LIGHT WHICH LOCATED CLOSE TO LT ENTER DOOR INOPERATIVE. IAW AMM 33-51-03-2 RELAMPED LT ENTRY DOOR SUPERNUMERARY AREA CEILING EMERGENCY LIGHT, TEST PASSED. - [SDR FDEA202507201270](https://openairdocs.org/sdr/FDEA202507201270.md): Skin · cracked · Jul 20, 2025 · N896FD · Boeing 777F · Wing, Plate/Skin > UT & OPEN HOLE HFEC INSPECTION OF THE RIGHT HAND UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 01EA CRACK ON FASTENER #5 AS MARKED. THE RH WING UPPER SKIN CRACKED #5 FASTENER HOLE REPAIRED AS PER B777 SRM 51-40-05- 0G, SRM 51-40-02-0G, SRM51-40-04-0G, - [SDR FDEA202507201269](https://openairdocs.org/sdr/FDEA202507201269.md): Skin · cracked · Jul 20, 2025 · N896FD · Boeing 777F · Wing, Plate/Skin > UT & OPEN HOLE HFEC INSPECTION OF THE LEFT HAND UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 01EA CRACK ON FASTENER #5 AS MARKED. THE LH WING UPPER SKIN CRACKED #5 FASTENER HOLE REPAIRED AS PER B777 SRM 51-40-05- 0G, SRM 51-40-02-0G, SRM51-40-04-0G, - [SDR FDEA202312201949](https://openairdocs.org/sdr/FDEA202312201949.md): Blade · damaged · Dec 20, 2023 · N896FD · Boeing 777FS2 · Turbine Engine Air Inlet Section > AFTER AIRBORNE PASSING APPROXIMATELY 2500 FEET DURING THE CLIMB OUT, WE NOTICED VIBRATION BEGIN ON THE AIRCRAFT. IT CONTINUED TO WORSEN AND STABILIZED WITH THE RIGHT ENGINE EVM SHOWING 4.8 AT CLIMB THRUST WHICH WAS ABOUT 85%. REFERENCING THE APPROPRIATE - [SDR FDEA202310181772](https://openairdocs.org/sdr/FDEA202310181772.md): Floor Panel · cracked · Oct 18, 2023 · N896FD · Boeing 777FS2 · Fuselage Floor Panel > REWORK:MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA 1660 RBL 1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 CRACKED AT STA 1660 RBL 1, SIZE:L=1.2" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1,REV - [SDR FDEA202310091733](https://openairdocs.org/sdr/FDEA202310091733.md): Flap · damaged · Oct 9, 2023 · N896FD · Boeing 777FS2 · Trailing Edge Flaps > LH IB AFT FLAP I/B LWR SURFACE FROM IB TO OB 65INCH CROSS LE TO TE 34INCH FOUND ONE BIRD STRIKE. EVALUATED LH IB AFT FLAP I/B LWR SURFACE FROM IB TO OB 65INCH CROSS LE TO TE 34INCH ONE BIRD STRIKE, DAMAGE SIZE L*W=1" *0.75" WITHIN REPAIR LIMIT AS PER B777 - [SDR FDEA202310081728](https://openairdocs.org/sdr/FDEA202310081728.md): Flap · damaged · Oct 8, 2023 · N896FD · Boeing 777FS2 · Trailing Edge Flaps > LH OB FLAP LWR SURFACE FROM IB TO OB 52 INCH CROSS LE TO TE 67 INCH FOUND ONE BIRD STRIKE. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 52 INCH CROSS LE TO TE 67 INCH ONE BIRD STRIKE. DAMAGE SIZE L*W=1" *0.8" WITHIN REPAIR LIMIT AS PER B777 SRM 57-53-01- - [SDR FDEA202310061715](https://openairdocs.org/sdr/FDEA202310061715.md): Skin · dented · Oct 6, 2023 · N896FD · Boeing 777FS2 · Fuselage Main, Plate/Skin > FUSELAGE SKIN INTERIM REPAIR FOR DENT, AT STA 132.21 BELOW F/O WINDOW. FUSELAGE SKIN AT STA 132.21 BELOW F/O WINDOW DENT AREA REPAIRED AS PER B777 SRM 51- 40-02,SRM 51-10-02,SRM 51-70-01,SRM 51-40-08,SRM 51-40-05,SRM 53-00-01 REPAIR 4,SRM 51-20-01 AND SRM - [SDR FDEA202303030374](https://openairdocs.org/sdr/FDEA202303030374.md): Unknown · unknown · Mar 3, 2023 · N896FD · Boeing 777FS2 · Fuselage Main, Longeron/Stringer > UPON ARRIVAL FOUND DENT ON RT BS 132.21 BETWEEN F/O WINDOW & RADOME. SRM 53-00-01-1A. DENT IS 5 IN FROM RADOME CUTOUT, MEASUREMENT FOUND WIDTH 3.5 INCH, LENGTH 6 INCH AND DEPTH 0.11 INCH. REF. FIG 102 DETAIL E. NDTM PT6 PERFORMED HFEC OF SKIN CUTOUT AND INTER - [SDR FDEA202302071766](https://openairdocs.org/sdr/FDEA202302071766.md): Flap · damaged · Feb 7, 2023 · N896FD · Boeing 777FS2 · Trailing Edge Flaps > DUE BIRD STRIKE INSPECTION FOUND DAMAGE ON LH OUTBOARD FLAP BETWEEN INBOARD FAIRING AND FLAPERON. IT MEASURES 1"X 0,8" AND IT S LOCATED 2" FROM TRAILING EDGE. TERMINATING ACTION ACCOMPLISHED FOR SRM 57-53-01 - [SDR FDEA202111052784](https://openairdocs.org/sdr/FDEA202111052784.md): Door · cracked · Nov 5, 2021 · N896FD · Boeing 777FS2 · Nacelle/Pylon, Main Frame > #2 ENG PYLON DOOR 444CL LANDING AFT TOP CORNER HAS A CRACK ENDING AT FASTNER. COMPLIED WITH HFEC INSPECTION IAW NTM PART 6 VERIFIED CRACK MARKED UP CRACK AND WHERE IT ENDS. COMPLIED WITH EA. G 5400-T0365318.PART 1. - [SDR FDEA202111042782](https://openairdocs.org/sdr/FDEA202111042782.md): Fairing · cracked · Nov 4, 2021 · N896FD · Boeing 777FS2 · Nacelle/Pylon Miscellaneous Structure > MDIS 896 54-00 3217 03NOV21 MEM RIGHT ENGINE AFT PYLON FAIRING STRUCTURE HAS A SUSPECTED CRACK INDICATION IN ONE OF THE FRAMES REPAIRED CRACK IN R/H PYLON FRAME 3 PER EA G-5450-T0365281. EA TITLE "NACELLES / PYLON- WING PYLON/ STRUT- NO2 E - [SDR FDEA201909222315](https://openairdocs.org/sdr/FDEA201909222315.md): Steering Sys · contaminated · Sep 22, 2019 · N896FD · Boeing 777FS2 · Landing Gear Steering System > DURING TAXI NW TILLER WHEN MOVED PAST 180 DEGREES TO THE RIGHT IS EXTEMLY DIFFICULT TO TURN. WHEN MOVED PAST 270 DEGREES A DISTINCT RELEASE IS FELT. NOTE DURING FLIGHT WE NEVER MADE A LEFT HAND TURN. INSPECTED NOSE GEAR STEERING, FOUND NO DEFECTS, GREASED THE - [SDR FDEA201909122226](https://openairdocs.org/sdr/FDEA201909122226.md): Access Door · jammed · Sep 12, 2019 · N896FD · Boeing 777FS2 · Service Doors > AFTER TAKEOFF, VERY LOUD NOISE FROM NOSE WHEEL WELL AREA. ON CLIMBOUT. AIRCRAFT WOULD NOT PRESSURIZE. ALL DOOR INDICATIONS CLOSED. BOTH OUTFLOW VALVES SHOWED CLOSED. FOUND FWD ACCESS DOOR WAS JAMMED OPEN AT FRONT EDGE. NORMAL DOOR CLOSED INDICATION WAS DISPLAY ## 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 = 'N896FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N896FD/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.