# Service difficulty reports: N880FD

A list on [N880FD](https://openairdocs.org/aircraft/N880FD.md).

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

- [SDR FDEA202602170225](https://openairdocs.org/sdr/FDEA202602170225.md): Safety Wire · wrong part · Feb 17, 2026 · N880FD · Boeing 777F28 · Escape Slide
  > RIGHT SIDE DOOR SLIDE INSPECTION REVEALED THAT THE WRONG SAFETY WIRE WAS USED. THE WO REQUIRES REPLACING THE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. RH DOOR SLIDE RAFT RETURN TO NORMAL OPS, AIRCRAFT READY FOR SERVICE
- [SDR FDEA202508021365](https://openairdocs.org/sdr/FDEA202508021365.md): Light · malfunctioned · Aug 2, 2025 · N880FD · Boeing 777F28 · Emergency Lighting
  > EMERGENCY LIGHTS ILLUMINATED DURING BEFORE START CHECKLIST. AMM 33-51-00-5 FOUND EMERGENCY LIGHT SWITCH AT THE OVERHEAD PANEL IN THE OFF POSITION. SWITCH PUT BACK TO ARM POSITION AND OPERATIONAL TEST PERFORMED IAW AMM 33-51-00-5
- [SDR FDEA202503140410](https://openairdocs.org/sdr/FDEA202503140410.md): Skin · cracked · Mar 14, 2025 · N880FD · Boeing 777F28 · Leading Edge Devices
  > RH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 51 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 51 INCH TO I/B EDGE CRACK AREA REPAIRED AS PER B777 SRM51-10-02-0G,51-20-01-0G,51-20-05-0G,51-40-02-0G,51-40-05-0G,51-40-08-0G,57-43-01-2R REPAIR 13 REV:47.5 AN
- [SDR FDEA202503050333](https://openairdocs.org/sdr/FDEA202503050333.md): Skin · cracked · Mar 5, 2025 · N880FD · Boeing 777F28 · Leading Edge Devices
  > RH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 39 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 39 IN TO IB EDGE CRACK REPAIRED AS PER B777 SRM51-10- 02-0G,51-20-01-0G,51-20-05-0G,51-40-02-0G,51-40-05-0G,51-40-08-0G,57-43-01-2R REPAIR 13 REV:47.5 AND EA G-5
- [SDR FDEA202503050332](https://openairdocs.org/sdr/FDEA202503050332.md): Skin · cracked · Mar 5, 2025 · N880FD · Boeing 777F28 · Wing, Plate/Skin
  > OPEN HOLE HFEC INSPECTION ON THE RH WING WBL 262 THEN FOUND HOLE #6 CRACK IN UPPER WING SKIN AS MARKED. RH WING WBL 262 UPPER SKIN #6 HOLE CRACK REPAIRED AS PER B777 SRM51-10-01-0G, 51-20-01- 0G, 51-20-05-0G,51-20-06-0G, 51-20-07-0G, 51-40-08-0G, 51-40-02
- [SDR FDEA202503040326](https://openairdocs.org/sdr/FDEA202503040326.md): Floor Panel · cracked · Mar 4, 2025 · N880FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 231RF P/N:152W8301-67 FOUND CRACKED AT STA 1014 LBL 84. MAIN DECK CARGO FLOOR PANEL 231RF P/N:152W8301-67 CRACKED AT STA 1014 LBL 84. DAMAGE SIZE: L=2.9" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 REV
- [SDR FDEA202410031414](https://openairdocs.org/sdr/FDEA202410031414.md): Outflow Valve · faulted · Oct 3, 2024 · N880FD · Boeing 777F28 · Pressure Regulator/Outflow Valve
  > ON DEPARTURE, ACFT WOULD NOT PRESSURIZE. THE FWD OUTFLOW VALVE ON MEL. THE REMAINING AFT OUTFLOW VALVE INDICATED CLOSED ON DEPART BUT WOULD NOT ALLOW ACFT TO PRESSURIZE. AIR RETURN OMDWB. ON ARRIVAL VERIFIED FWD OUTFLOW VALVE WAS STILL AT 7% OPEN. STATUS
- [SDR FDEA202304240753](https://openairdocs.org/sdr/FDEA202304240753.md): Unknown · unknown · Apr 24, 2023 · N880FD · Boeing 777F28 · Central Warning
  > PDIS 880 31-50 3973 24APR23 MEM VMO GEAR DOWN STATUS MESSAGE. RETURNED TO MEM DUE TO UNABLE HIGHER ALTITUDE/AIRSPEED. AMM: 27-32-01-4 FIM: 31-51-00-810-957 TROUBLESHOT VMO GEAR DOWN MESSAGE PER B777 FIM 31-51-00-810-957 AND FOUND ALTERNA
- [SDR FDEA202304240752](https://openairdocs.org/sdr/FDEA202304240752.md): Unknown · unknown · Apr 24, 2023 · N880FD · Boeing 777F28 · Central Warning
  > PDIS 880 31-50 3973 24APR23 MEM FACT U VMO GEAR DOWN STATUS MESSAGE. RETURNED TO MEM DUE TO UNABLE HIGHER ALTITUDE/AIRSPEED. FACT 24APR23 08:02 MEM U AMM: 27-32-01-4 FIM: 31-51-00-810-957 TROUBLESHOT VMO GEAR DOWN MESSAGE PER B777 FIM
- [SDR FDEA202209222354](https://openairdocs.org/sdr/FDEA202209222354.md): Lamp · inoperative · Sep 22, 2022 · N880FD · Boeing 777F28 · Emergency Lighting
  > MDIS 880 33-50 3430 21SEP22 ANC OPEN U DURING PREFLIGHT FOUND CENTER OVERHEAD EMERGENCY LIGHT OUT DURING EMERGENCY LIGHT TEST. ALL OTHER LIGHTS OPERATE NORMALLY. RELAMPED CENTER SUPERNUMERARY AREA LIGHT I..W. B777 M.M. TASK 33-51-03-960-801.
- [SDR FDEA202207291819](https://openairdocs.org/sdr/FDEA202207291819.md): Floor Panel · cracked · Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8701-11 FOUND CRACKED AT STA1970 LBL40. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8701-11 CRACKED AT STA 1970 LBL40 AS PER B777 SRM 53-00-50-2R REPAIR 1 REV 41.0.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202207291818](https://openairdocs.org/sdr/FDEA202207291818.md): Floor Panel · cracked · Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED AT STA1748 BL0. MAIN DECK CARGO FLOOR PANEL P/N: 152W8601-31 CRACKED AT STA1748 BL0 AS PER B777 SRM 53-00-50-2R REPAIR 1 REV 41.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202207291817](https://openairdocs.org/sdr/FDEA202207291817.md): Floor Panel · cracked · Jul 29, 2022 · N880FD · Boeing 777F28 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL P/N:152W8601-17 FOUND CRACKED AT STA1660 BL0. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 CRACKED AT STA1660 BL0 AS PER B777 SRM 53-00-50-2R REPAIR 1 REV41.0.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202206261566](https://openairdocs.org/sdr/FDEA202206261566.md): Tire · delaminated · Jun 26, 2022 · N880FD · Boeing 777F28 · Brake Anti-Skid Section
  > PDIS 880 32-41 3226 26JUN22 MEM FACT U SUSPECTED TIRE FAILURE ON TAKEOFF IN OSAKA. LANDED WITHOUT INCIDENT. TIRE DID INCUR FURTHER DAMAGE. NEED CHANGE RH NOSE WHEEL ***EMERGENCY DECLARED*** RH NOSE TIRE FOUND TO HAVE A COUPLE STRANDS OF CO
- [SDR FDEA202106021435](https://openairdocs.org/sdr/FDEA202106021435.md): Brake Assy · fire · Jun 2, 2021 · N880FD · Boeing 777F28 · Landing Gear Brake System
  > AFTER BLOCK IN, #8 BRAKE CAUGHT FIRE. FIRE EXTINGUISHED BY RAMP CREW, THEN BY FIRE DEPARTMENT. REMOVED #8 BRAKE & WHEEL & PERFORMED HIGH ENERGY STOP/ HEAT DAMAGE INSPECTION ON ALL WHEELS & BRAKES IAW AMM: 05-51-14-2. NO DEFECT FOUND. REPLACED # 8 BRAKE A
- [SDR FDEA202009302365](https://openairdocs.org/sdr/FDEA202009302365.md): Battery · corroded · Sep 30, 2020 · N880FD · Boeing 777F28 · Emergency Equipment
  > MDIS 880 52-20 1013 30SEP20 MEM. L1 EPAS BATTERY UNIT TERMINALS ARE CORRODED. FACT 30SEP20 21:38 MEM 0000086819 STEVENSON, BRIAN A-30-SEP-2020 14:10. REPLACED L1 DOOR EPAS BATTERY PACK, REF B777 AMM 52-11-20-4-2. OPS CHECK GOOD. REMOVAL AND INSTALATION DO
- [SDR FDEA202005291078](https://openairdocs.org/sdr/FDEA202005291078.md): Battery · discharged · May 29, 2020 · N880FD · Boeing 777F28 · Passenger/Crew Doors
  > POST FLIGHT INSPECTION. L-1 DOOR EPAS BATTERY PACK STATUS LIGHT NOT FLASHING. REMOVED AND REPLACED THE 2 9V BATTERIES FOR THE L-1 EPAS BATTERY PACK IAW AMM 52-11-20-4-2. RE-ARMED L-1 EPAS SYS AND GREEN STATUS LT RESTORED. NORMAL ITEM OK FOR SERVICE.
- [SDR FDEA202002200358](https://openairdocs.org/sdr/FDEA202002200358.md): Skin · damaged · Feb 20, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING E.O. #G-5310-EO332629 D P5 FOUND EXISTING UNDERWING LONGERON FASTENER HOLE AT LEFT HAND STATION 1014 AND STRINGER 36 LEFT OVERSIZED TO 0.403" INSTEAD OF 0.371" AS PER DRAWING 675W0002 SHEET 8. WORK ACCOMPLISHED AS PER EA G-5310-T0352363
- [SDR FDEA202002200357](https://openairdocs.org/sdr/FDEA202002200357.md): Skin · cracked · Feb 20, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND 02 CRACK INDICATION AROUND FASTENER HOLES AT STATION 1024 AND STATION 1032, STRINGER 37 LEFT, APPROXIMATE 0.8" AND 1" IN L
- [SDR FDEA202002140333](https://openairdocs.org/sdr/FDEA202002140333.md): Skin · cracked · Feb 13, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Plate/Skin
  > DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UNDERWING LONGERON AND FUSELAGE SKIN FOUND 02 EACH CRACKS WHICH APPROXIMATE 0.3" AT STATION 1032. STRINGER 37 RIGH
- [SDR FDEA202002140332](https://openairdocs.org/sdr/FDEA202002140332.md): Spar · cracked · Feb 13, 2020 · N880FD · Boeing 777F28 · Wing Spar
  > DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON RIGHT HAND SIDE UNDERWING LONGERON LOWER WING FRONT SPAR CHORD AND FOUND 01 EACH HOLE WITH CRACK INDICATION AS MARKED. (STATION 1035 RBL 82) CRACKED RIGHT HAND SIDE UNDERWING LONGERON L
- [SDR FDEA2020020650268](https://openairdocs.org/sdr/FDEA2020020650268.md): Longeron · cracked · Feb 5, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Longeron/Stringer
  > DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT SIDE UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATIONS ON 02 EACH FASTENER AT VERTICAL FLANGE AND 01 EACH FASTENER AT HORIZONTAL FLANGE AS MARKED. WORK ACCOMPLISHED ON LEFT HAND SIDE UNDERWING
- [SDR FDEA202002060267](https://openairdocs.org/sdr/FDEA202002060267.md): Longeron · cracked · Feb 5, 2020 · N880FD · Boeing 777F28 · Fuselage Main, Longeron/Stringer
  > DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT SIDE UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATIONS ON 02 EACH FASTENER AT VERTICAL FLANGE AS MARKED. WORK ACCOMPLISHED ON RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AS PER
- [SDR FDEA2019101082496](https://openairdocs.org/sdr/FDEA2019101082496.md): Battery Pack · inoperative · Oct 8, 2019 · N880FD · Boeing 777F28 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAIL. FOUND LH SIDE EMERGENCY LIGHT BATTERY PACK UNSERVICEABLE. REPLACED BATTERY PACK ACC. AMM. 33-51-06. OPS CHECK FOUND SATISFACTORY.
- [SDR FDEA201805241313](https://openairdocs.org/sdr/FDEA201805241313.md): Transducer · leaking · May 24, 2018 · N880FD · Boeing 777F28 · Hydraulic Pressure Indicator
  > 2.5 HOURS OUT OF ANC GOT "HYD QTY LOW C" FOLLOWED BY "RESERVE BRAKE/STEERING" EICAS. HYD QTY C STARTED AT.4 WHEN GOT EICAS AND OVER 1 HOUR WENT.01. FLAPS SLOW-GEAR NORMAL AND SPEED BRAKES NORMAL. TOWED OFF RUNWAY. RESEALED CENTER HYDRAULIC SYSTEM PRESSURE TR
- [SDR FDEA201710203012](https://openairdocs.org/sdr/FDEA201710203012.md): Lamp · failed · Oct 20, 2017 · N880FD · Boeing 777F28 · Emergency Lighting
  > FOWARD STARBOARD EMERGENCY LIGHT DOES NOT WORK. REPLACED THE LAMPS AND TESTED OK IAW AMM 33-51-03-2.
- [SDR FDEA201706091598](https://openairdocs.org/sdr/FDEA201706091598.md): Skin · cracked · Jun 9, 2017 · N880FD · Boeing 777F28 · Leading Edge Devices
  > DURING HFEC OPEN-HOLE INSPECION ON THE RT WING LEADING EDGE INBOARD SLAT NR 8 OUTER SKIN, FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS. REPAIRED IAW SRM 57-43-01-2R, FIGURE 202, SHEET 2, REPAIR 8, AND EA G-5750-T0333893, PART 1. REPAIR CLASSIFIED AS MAJ
- [SDR FDEA201706091597](https://openairdocs.org/sdr/FDEA201706091597.md): Skin · cracked · Jun 9, 2017 · N880FD · Boeing 777F28 · Leading Edge Devices
  > DURING HFEC OPEN-HOLE INSPECION ON THE LT WING LEADING EDGE INBOARD SLAT NR 7 OUTER SKIN, FASTENER HOLES FOUND CRACK INDICATIONS. REPAIRED IAW SRM 57-43-01-2R, FIGURE 202, SHEET 1, REPAIR 8, AND EA G-5750-T0333917 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-
- [SDR FDEA201510163262](https://openairdocs.org/sdr/FDEA201510163262.md): Light · inoperative · Oct 16, 2015 · N880FD · Boeing 777F28 · Emergency Lighting
  > EMERGENCY LIGHT OVER R1 EXIT INOPERATIVE. RELAMPED & OPERATIONS CHECKED NORMAL, OK FOR SERVICE IAW MM 33-50-00-2.
- [SDR FDEA201409272823](https://openairdocs.org/sdr/FDEA201409272823.md): Balance Weight · out of position · Sep 27, 2014 · N880FD · Boeing 777F28 · Turbine Engine Compressor Section
  > AS THE THROTTLES DECREASED AT TOP OF CLIMB THE AIRCRAFT DEVELOPED A SIGNIFICANT VIBRATION THAT COULD BE FELT & HEARD. THE LT ENG N1 VIBRATION WAS 3.2, ALL OTHER PARAMETERS WERE NORMAL ON BOTH ENGS. RETARDING THE THROTTLE 10% N1 IN CRUISE AT FL310 DIMINISHED
- [SDR FDEA201409052470](https://openairdocs.org/sdr/FDEA201409052470.md): Warning System · false activation · Sep 5, 2014 · N880FD · Boeing 777F28 · Fire Bottle, Fixed
  > THE FSS DISCHARGE LIGHT ILLUMINATED WITH NO OTHER INDICATIONS IN THE COCKPIT. THE FSS CONTROL PANEL SHOWED SUPPRESSING FIRE WITH A FAULT ILLUMINATED IN POS 2R. THE FAULT ALSO SHOWED BURST DISK. TEMP WINDOW ALSO SHOWED MANY TEMP VARIATIONS BETWEEN -4 TO 500
- [SDR FDEA201309132205](https://openairdocs.org/sdr/FDEA201309132205.md): Lamp · inoperative · Sep 13, 2013 · N880FD · Boeing 777F28 · Emergency Lighting
  > RT EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMPS AND CHECKED OK IAW AMM 33-51-04-2.
- [SDR FDEA201301260191](https://openairdocs.org/sdr/FDEA201301260191.md): Switch · inoperative · Jan 26, 2013 · N880FD · Boeing 777F28 · Emergency Lighting
  > EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL IS OFF IN THE ARMED POSITION. REPAIRED EMERGENCY LIGHT SWITCH GUARD, OPS CHECKED OK.
- [SDR FDEA201210053568](https://openairdocs.org/sdr/FDEA201210053568.md): Lamp · inoperative · Oct 5, 2012 · N880FD · Boeing 777F28 · Emergency Lighting
  > LEFT FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. LAMPED IAW MM 33-50-00-003, ACFT OK FOR SERVICE.
- [SDR FDEA201109163929](https://openairdocs.org/sdr/FDEA201109163929.md): Fitting · damaged · Sep 16, 2011 · N880FD · Boeing 777F28 · Cargo/Baggage Doors
  > MAIN CARGO DOOR, LOCK BAR FITTINGS DAMAGED BY CONTACT WITH LOADING BRIDGE; 3 PLACES, LOCATED AT LATCH NR 2 FWD AND LATCH NR 3 FWD AND AFT. PERFORMED INTRIM REPAIR IAW EA G-5230-155420. COMPLIED WITH EA G-5230-155430, PT 1, PT 2 TO BE ACCOMPLISHED.
- [SDR FDEA201103281205](https://openairdocs.org/sdr/FDEA201103281205.md): Spring · out of position · Mar 28, 2011 · N880FD · Boeing 777F28 · Emergency Lighting
  > EMERGENCY LIGHTS SWITCH WILL NOT ARM WITH SWITCH GAURD CLOSED. REPOSITIONED RETURN SPRING ON SWITCH GAURD. COMPLETED COCKPIT EMERGENCY LIGHTS OPERATIONAL TEST REF TASK 33-51-00-710-004. OPS CHECKED GOOD.
- [SDR FDEA201008273172](https://openairdocs.org/sdr/FDEA201008273172.md): Engine · bird ingestion · Aug 27, 2010 · N880FD · Boeing 777* · Engine (Turbine/Turboprop)
  > THIS FLIGHT DEPARTED. STD TAKEOFF USED AND A BIRDSTRIKE OCCURRED AT HIGH SPEED, TWO THIRDS OF THE WAY DOWN THE RUNWAY. AN IMMEDIATE ODOR OCCURRED. TOWER REPORTED FOD, IDENTIFIED AS FROM OUR ACFT. DIVERTED AND DUMPED FUEL TO LAND JUST BELOW MLGW. ATC REPO

## 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 = 'N880FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N880FD/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.