# Service difficulty reports: N855FD

A list on [N855FD](https://openairdocs.org/aircraft/N855FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA202605140595](https://openairdocs.org/sdr/FDEA202605140595.md): Skin · debonded · May 14, 2026 · N855FD · Boeing 777FS2 · Trailing Edge Flaps
  > LEFT OTBD FLAP LWR SURFACE FROM OTBD TO INBD 268 INCHES CROSS TE TO LE 10 INCHES FOUND DEBONDED. REPAIRED LH OB FLAP LWR SURFACE DISBOND AT OTEF STA 260 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 AND SRM 51-70-04-2R-0 PARA 4N FIGURE
- [SDR FDEA202605110581](https://openairdocs.org/sdr/FDEA202605110581.md): Skin · bulged · May 11, 2026 · N855FD · Boeing 777FS2 · Leading Edge Devices
  > FOUND RT WING LE NR 11 SLAT EXTERNAL SURFACE A BULGE AT STA 873. BULGE REPAIRED AS PER B777 SRM57- 43-01-2R REPAIR 9 FIGURE 202 REV:51.0 AND EA G-5750-T0387321 P1. TITLE: WING-FLIGHT SURFACES-RH WING #11 SLAT OUTER SKIN BULGES AT NOSE BEAM AREA BETWEEN OSB
- [SDR FDEA202605110580](https://openairdocs.org/sdr/FDEA202605110580.md): Skin · bulged · May 11, 2026 · N855FD · Boeing 777FS2 · Leading Edge Devices
  > FOUND RT WING LE NR 9 SLAT EXTERNAL SURFACE A BULGE AT STA 564. BULGE REPAIRED AS PER B777 SRM57-43- 01-2R REPAIR 16 FIGURE 202 REV:53.0. AND EA G-5750-T0387322 P1. TITLE: WING - FLIGHT SURFACES-RH WING #9 SLAT OUTER SKIN BULGE AT NOSE RIB AT OSCS 564 - SR
- [SDR FDEA202605100579](https://openairdocs.org/sdr/FDEA202605100579.md): Skin · cracked · May 10, 2026 · N855FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP3.B & STEP5.A.(2) THEN FOUND 01EA CRACK ON THE RH UPPER WING SKIN FASTENER #5. RH UPPER WING SKIN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C,51-40-02-0G,51-40-
- [SDR FDEA202605100578](https://openairdocs.org/sdr/FDEA202605100578.md): Skin · cracked · May 10, 2026 · N855FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP3.B & STEP5.A.(2) FOUND TWO CRACKS ON THE LT UPPER WING SKIN FASTENER #5. H WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-50- 02-0G FINGURE 1,51-40-02-0G,51-10-01-0G,51-20
- [SDR FDEA202508181496](https://openairdocs.org/sdr/FDEA202508181496.md): Power Supply · no test · Aug 18, 2025 · N855FD · Boeing 777FS2 · Emergency Lighting
  > 2 EMERGENCY LIGHTS IN COURIER AREA ABOVE R1 ARE INOP. ONE INOPERATIVE LIGHT LOCATED ABOVE GALLEY AREA, SECOND INOPERATIVE LIGHT LOCATED NEAR R1 DOOR. AMM: 33-51-06-2, AMM: 33-51-00-5. REPLACED RIGHT POWER SUPPLY PER AMM 33-51-06-2, ACCOMPLISHED EMERGENCY
- [SDR FDEA202410091453](https://openairdocs.org/sdr/FDEA202410091453.md): Throttle Control · malfunctioned · Oct 9, 2024 · N855FD · Boeing 777FS2 · Power Lever
  > DURING LEFT ENGINE START, WITH THE RIGHT ENGINE SHUTDOWN, BOTH THROTTLES ADVANCED UNCOMMANDED TOWARDS MAX POWER. CREW PULLED BOTH THROTTLES TO FLIGHT IDLE AND APPLIED MAX WHEEL BRAKING. NO STATUS OR MAINTENANCE MSGS RELATED TO THIS OBSERVED FAULT. RAN ALL
- [SDR FDEA202308151433](https://openairdocs.org/sdr/FDEA202308151433.md): Flap · dented · Aug 15, 2023 · N855FD · Boeing 777FS2 · Trailing Edge Flaps
  > LH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH ONE DENT WITH DAMAGE SIZE L*W=3"*2.75" WITHIN REPAIR LIMIT AS PER B777 SRM 57-53-01-1A ALLOW
- [SDR FDEA202308101393](https://openairdocs.org/sdr/FDEA202308101393.md): Floor Panel · cracked · Aug 10, 2023 · N855FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) AT STA1290/LBL105.5-107.5 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) CRACK, THE DAMAGE SIZE: L=2.2", OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE D
- [SDR FDEA202308101392](https://openairdocs.org/sdr/FDEA202308101392.md): Floor Panel · cracked · Aug 10, 2023 · N855FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) AT STA1269.5/RBL81-83.25 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) CRACK,THE DAMAGE SIZE:L=2.3", OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE D
- [SDR FDEA202308081373](https://openairdocs.org/sdr/FDEA202308081373.md): Skin · corroded · Aug 8, 2023 · N855FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > FOUND THE LOWER FUSELAGE SKIN CORROSION INSIDE BODY FAIRING 192JR AT BS 930 TO BS 940 AND S-49L TO S-49R. THE LOWER FUSELGE SKIN CORRODED AREA AT BS 930 TO BS 940 AND S-49L TO S-49R REMOVED & THE REWORKED AREA MEASURED THE ORIGINAL THICKNESS IS T=0.100",
- [SDR FDEA202101280212](https://openairdocs.org/sdr/FDEA202101280212.md): Skin · cracked · Jan 28, 2021 · N855FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HFEC INSPECTION ON RH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATIONS AROUND 01 EA FASTENER HOLE AT STA 1033 STR 37R, APPROX 1.5" IN LENGTH. COMPLIED WITH E.O.#:G-5310-E0332629 I P6 TITLE:FUSELAGE-MAINFRAME-INSP
- [SDR FDEA202101150117](https://openairdocs.org/sdr/FDEA202101150117.md): Doubler · misinstalled · Jan 15, 2021 · N855FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING LH E.O.#G-5310-E0332629 I P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR. S-35L NEAR MILLED EDGE COMPLIED WITH E.A.#:G-5310-T0359410 P1 TITLE: FUSELAGE-MAINFRAME-DEVIATIONS TO SB- 777-53-0087 R1 - LHS AND RHS UNDERWING
- [SDR FDEA202101150116](https://openairdocs.org/sdr/FDEA202101150116.md): Doubler · misinstalled · Jan 15, 2021 · N855FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING RH E.O.#G-5310-E0332629 I P6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR. S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.#:G-5310-T0359410 P2 TITLE: FUSELAGE-MAINFRAME-DEVIATIONS TO SB- 777-53-0087 R1 - LHS AND RHS UNDERWING
- [SDR FDEA202101150115](https://openairdocs.org/sdr/FDEA202101150115.md): Skin · cracked · Jan 15, 2021 · N855FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HFEC INSPECTION ON RH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATIONS AROUND 01 EA FASTENER HOLE STA 1028 STR 37R, APPROX 1.5" IN LENGTH. COMPLIED WITH E.O.#:G-5310-E0332629 I P6. TITLE: FUSELAGE-MAINFRAME-INSPE
- [SDR FDEA202101150109](https://openairdocs.org/sdr/FDEA202101150109.md): Spar · cracked · Jan 15, 2021 · N855FD · Boeing 777FS2 · Fuselage Main, Frame
  > DURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO:E G-5310-E0332629 I P6 ON OVERSIZED FASTENER HOLES AND FOUND (01 EA) CRACK INDICATION ON RHS VERTICAL FLANGE OF THE FRONT LOWER SPAR CHORD AT BS 1035 APPROX. RBL 81.30 LOWER O/B HOLE. WING CENTER
- [SDR FDEA202101150114](https://openairdocs.org/sdr/FDEA202101150114.md): Skin · cracked · Jan 15, 2021 · N855FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HFEC INSPECTION ON LH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STA 1033 STR 37L, APPROX 1.5" IN LENGTH, AS MARKED. COMPLIED WITH E.O.#G-5310-E0332629 I P5. TITLE:FUSELAGE- MAINFRAM
- [SDR FDEA202101110038](https://openairdocs.org/sdr/FDEA202101110038.md): Floor Support · cracked · Jan 11, 2021 · N855FD · Boeing 777FS2 · Fuselage Miscellaneous Structure
  > LOWER BULK CARGO COMPARTMENT STATION 1937, RIGHT BUTT LINE 41 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTT LINE 41 FLOOR STRINGER CRACKED REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STATION
- [SDR FDEA202101100032](https://openairdocs.org/sdr/FDEA202101100032.md): Floor Support · cracked · Jan 10, 2021 · N855FD · Boeing 777FS2 · Fuselage Miscellaneous Structure
  > LOWER BULK CARGO COMPARTMENT STATION 1980, RIGHT BUTT LINE 33 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1980 RIGHT BUTT LINE 33. FLOOR STRINGER CRACKED REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM EXISTI
- [SDR FDEA202101100031](https://openairdocs.org/sdr/FDEA202101100031.md): Floor Support · cracked · Jan 10, 2021 · N855FD · Boeing 777FS2 · Fuselage Miscellaneous Structure
  > LOWER BULK CARGO COMPARTMENT STATION 1980, RIGHT BUTT LINE 41 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1980 RIGHT BUTT LINE 41 FLOOR STRINGER CRACKED REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STATION
- [SDR FDEA201710152964](https://openairdocs.org/sdr/FDEA201710152964.md): Frame · cracked · Oct 15, 2017 · N855FD · Boeing 777FS2 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE PYLON HAS AN INTERNAL FRAME CRACKED. CRACK LOCATED INBOARD SIDE NAC STA 325.3, JUST ABOVE AFT ACCESS DOOR FOR AFT ENGINE MOUNT BOLTS. CRACK CONFIRMED WITH HFEC AND MEASURES APPROXIMATELY 2.5 INCH. FABRICATED A DOUBLER. CLEANED PART, PRIMED,
- [SDR FDEA201703270995](https://openairdocs.org/sdr/FDEA201703270995.md): Duct · ruptured · Mar 27, 2017 · N855FD · Boeing 777FS2 · Pneumatic Distribution System
  > CARGO FIRE WARNING DURING TAXI, BOTTLES DISCHARGED, STATUS MESSAGE FOR BOTTLE 1B AND BOTTLE 1A. REPLACED A RUPTURED DUCT.
- [SDR FDEA201610063476](https://openairdocs.org/sdr/FDEA201610063476.md): Switch · out of position · Oct 6, 2016 · N855FD · Boeing 777FS2 · Emergency Lighting
  > EICAS MESSAGE FOR EMERGENCY LIGHTS. ACFT RETURNED TO BLOCKS. FOUND EMERGENCY SWITCH GUIDE RING OUT OF RANK. REPOSITION AND PERFORMED RTS PASSED IAW MM 33-50-00. ACFT OK FOR SERVICE
- [SDR FDEA201507112197](https://openairdocs.org/sdr/FDEA201507112197.md): Link · broken · Jul 11, 2015 · N855FD · Boeing 777FS2 · Landing Gear Door Retract Section
  > ON ARRIVAL, FOUND LT MAIN GEAR DOOR & MLG DRAG STRUT DOOR DAMAGED DUE TO LINK BROKEN ON MLG DRAG STRUT DOOR. REINSTALLED LT MAIN LANDING GEAR SHOCK STRUT DOOR IAW AMM 32-12-06-4, REINSTALLED LT MAIN LANDING GEAR DRAG STRUT DOOR AND LINKAGE IAW AMM 32-12-08-4
- [SDR FDEA201504171254](https://openairdocs.org/sdr/FDEA201504171254.md): Eec · inoperative · Apr 17, 2015 · N855FD · Boeing 777FS2 · Fuel Control/Reciprocating Engines
  > DURING CRUISE THE LT ENGINE FLAMED OUT, WOULD NOT RESTART. LEFT FUEL CONTROL VALVE ILUMINATED SHUTTING DOWN LEFT ENGINE. INFLIGHT START CHECKLIST ACCOMPLISHED LEFT ENGINE WOULD NOT RESTART. INTERROGATED MAT AND FOUND ENG EEC C1 L FAULT LATCHED (FAULT CODE)
- [SDR FDEA201406081361](https://openairdocs.org/sdr/FDEA201406081361.md): Tire · leaking · Jun 8, 2014 · N855FD · Boeing 777FS2 · Brake
  > ABOUT 90 MINUTES INTO THE FLIGHT, RECEIVED AN EICAS, TIRE PRESSURE NR 10. TIRE SHOWED AMBER AT 184 PSI. NR 10 TIRE PRESSURE CONTINUED TO SLOWLY DECREASE DURING FLIGHT. LOWEST PRESSURE OBSERVED 128 PSI. R & R NR 9 & 10 MLG WHEEL & TIRE ASSEMBLY IAW AMM 32-45
- [SDR FDEA201307101519](https://openairdocs.org/sdr/FDEA201307101519.md): Lamp · inoperative · Jul 10, 2013 · N855FD · Boeing 777FS2 · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECK GOOD IAW MM 33-51-00-5.
- [SDR FDEA201303300690](https://openairdocs.org/sdr/FDEA201303300690.md): Skin · damaged · Mar 30, 2013 · N855FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > RIGHT NOSE SKIN BEHIND F/O WINDOW FOUND 2 LIGHTNING STRIKES DAMAGED AT BS 246 AND 228. REPAIRED IAW EA G 5330-161299A PART 3.
- [SDR FDEA201205151811](https://openairdocs.org/sdr/FDEA201205151811.md): Handle · out of adjust · May 15, 2012 · N855FD · Boeing 777FS2 · Passenger/Crew Doors
  > L1 DOOR WAS HARD TO MOVE SLIDE HANDLE FROM DISARM TO ARMED POSITION ON BLOCKOUT. PERFORMED ADJUSTMENT AND TEST IAW MM 52-11-00-5. OPS CHECKED NORMAL. OK FOR SERVICE.
- [SDR FDEA201203070865](https://openairdocs.org/sdr/FDEA201203070865.md): Skin · delaminated · Mar 7, 2012 · N855FD · Boeing 777FS2 · Trailing Edge Flaps
  > LEFT WING FLAP DELAMINATED T/E BETWEEN NR 1 AND NR 2 CANOE APPROX 10" X 10" AREA. REMOVED LT OTBD T/E FLAP REF MM 27-51-21-4. T/E FLAP SYS MAINT PRACTICES COMPLIED WITH IAW MM 27-51-00-2. REMOVAL/INSTALLATION COMPLIED WITH IAW MM 27-51-21-4 AND OTBD T/E FLA
- [SDR FDEA201202150580](https://openairdocs.org/sdr/FDEA201202150580.md): Bracket · loose · Feb 15, 2012 · N855FD · Boeing 777FS2 · Escape Slide
  > L1 DOOR SLIDE CONTAINER LOWER BRACKET LOOSE. AFFIXED COMESTIC TRIM PIECE TO L1 DOOR BUSTLE IAW MM 25-66-06 AND SMP CH 20.
- [SDR FDEA201107082614](https://openairdocs.org/sdr/FDEA201107082614.md): Autothrottle Sys · malfunctioned · Jul 8, 2011 · N855FD · Boeing 777FS2 · Auto Throttle System
  > ON TAXI OUT, HAD AN UNCOMMANDED AUTO THROTTLE ENGAGEMENT TO TAKEOFF POWER. THROTTLES HAS JUST BEEN MOVED TO IDLE FROM ABOUT 30 PERCENT, AT WHICH TIME THE ATS ENGAGED. POWER CAME UP TO ABOUT 45 PERCENT BEFORE THROTTLES WERE OVER-RIDEN & THE A/T SWITCHES WERE

## 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 = 'N855FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N855FD/reports

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