# Service difficulty reports: N884FD

A list on [N884FD](https://openairdocs.org/aircraft/N884FD.md).

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

- [SDR FDEA202606010665](https://openairdocs.org/sdr/FDEA202606010665.md): Fire Bottle · failed · Jun 1, 2026 · N884FD · Boeing 777FS2 · Fire Bottle, Fixed
  > AT 2335Z (APPROX 1:15 INTO THE FLIGHT), FL340, TAT -11,.838MACH, GOT BOTTLE DISCHARGE APU CAUTION WITH LIGHT APU BTL DSCG ON OVERHEAD AND BOTTLE APU ON STATUS PAGE. PERFORMED APU FIRE EXTINGUISHING BOTTLE PRESSURE SWITCH TEST PER ABOVE REF, TEST PASS, AND
- [SDR FDEA202605030534](https://openairdocs.org/sdr/FDEA202605030534.md): Skin · dented · May 3, 2026 · N884FD · Boeing 777FS2 · Trailing Edge Flaps
  > FOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 127 INCHES AND T/E 10 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 127 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIG
- [SDR FDEA202605030533](https://openairdocs.org/sdr/FDEA202605030533.md): Skin · dented · May 3, 2026 · N884FD · Boeing 777FS2 · Trailing Edge Flaps
  > FOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 231 INCHES AND T/E 8 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 231 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIGU
- [SDR FDEA202604300524](https://openairdocs.org/sdr/FDEA202604300524.md): Skin · cracked · Apr 30, 2026 · N884FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT RH WING UPPER WING SKIN COMMON TO FASTENER 5. RT WING UPPER SKIN 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51-50-02-0G, FIG 1, SRM 51-40-02-0G, FIG 12,
- [SDR FDEA202604300523](https://openairdocs.org/sdr/FDEA202604300523.md): Skin · cracked · Apr 30, 2026 · N884FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT LT WING UPPER WING SKIN COMMON TO FASTENER 5. LT WING UPPER SKIN NR 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51-50- 02-0G, FIGURE 1, SRM 51-40-02-0G F
- [SDR FDEA202509231776](https://openairdocs.org/sdr/FDEA202509231776.md): Spring · damaged · Sep 23, 2025 · N884FD · Boeing 777FS2 · Passenger/Crew Doors
  > WHILE CLOSING DOOR 1L, AN INTERIOR SPRING BROKEN. REMOVED AND REPLACED 2 EACH SPRINGS ON VENT DOOR ASSY IAW AMM 52-11-04-4-0.
- [SDR FDEA202411231725](https://openairdocs.org/sdr/FDEA202411231725.md): Module · inoperative · Nov 23, 2024 · N884FD · Boeing 777FS2 · Emergency Lighting
  > REF MTSI 33-50/4453, EMERGENCY LIGHT SW ON OVHD PANEL FOUND TO BE INTERMITTENT INOP. R/RED WINDOW HEAT/EMER LIGHTS MODULE, INSTALLATION TEST PASSED. EMERGENCY LIGHT TESTED NORMAL. WORK PERFORMED PER REF AMM 30-41-02-4, AMM 33-51-00-5
- [SDR FDEA202411191687](https://openairdocs.org/sdr/FDEA202411191687.md): Light · malfunctioned · Nov 19, 2024 · N884FD · Boeing 777FS2 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT SHUTOFF ON ENGINE SHUTDOWN CHECKLIST PERFORMED ENG SHUTDOWN CHKL RESET. EMER LT OPTION TURN GREEN, CHKL BACK TO NORMAL. A/C OK FOR SVC.
- [SDR FDEA202403200317](https://openairdocs.org/sdr/FDEA202403200317.md): Power Cable · chafed · Mar 20, 2024 · N884FD · Boeing 777FS2 · Electrical Power System Wiring
  > FO EFB POWER CORD AT MAGNETIC PLUG HAD ELECTRICAL SPARKS AND ARCING IN FLIGHT. DISCONNECTED POWER CORD FROM EFB. DO NOT RECONNECT THE OLD CORD. F/O EFB POWER CORD REMOVED AND REPLACED AS PER AMM 46-11-96-4, TEST OK. A/C OK FOR SERVICE.
- [SDR FDEA202309271662](https://openairdocs.org/sdr/FDEA202309271662.md): Power Supply · failed · Sep 27, 2023 · N884FD · Boeing 777FS2 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN TESTED. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLIES ABOVE L1 DOOR AND R1 DOOR REF. AMM 33-51-06-2. ALL LIGHTS OPERATE NORMALLY PER ABOVE AMM REF. A/C OK FOR SERVICE.
- [SDR FDEA202308171453](https://openairdocs.org/sdr/FDEA202308171453.md): Skin · bent · Aug 17, 2023 · N884FD · Boeing 777FS2 · Leading Edge Devices
  > RH WING NO.10 SLAT OUTER SKIN FOUND BULGE AT WS 657-661 AND 19.5 IN AWAY FROM AFT EDEG. RH WING NO.10 SLAT OUTER SKIN BULGE AREA AT WS 657-661 AND 19.5 IN AWAY FROM AFT EDGE REPAIRED AS PER B777 SRM 57-43-01-2R-9, SRM 51-40-05, SRM51-20-01 REV 44.0 AND EA
- [SDR FDEA202308161448](https://openairdocs.org/sdr/FDEA202308161448.md): Skin · dented · Aug 16, 2023 · N884FD · Boeing 777FS2 · Trailing Edge Flaps
  > LH OB FLAP LOWER SURFACE FROM IB TO OB 15.5 INCH CROSS TE TO LE 4 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LOWER SURFACE FROM IB TO OB 15.5 INCH CROSS TE TO LE 4 INCH ONE DENT DAMAGE SIZE L X W=4"X2" WITH DISBOND WITHIN REPAIR LIMIT AS PER B777 SRM 57-53
- [SDR FDEA202104090855](https://openairdocs.org/sdr/FDEA202104090855.md): Skin · cracked · Apr 9, 2021 · N884FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > FUSELAGE LEFT HAND BILGE AREA AT STATION 1685 AREA FOUND WITH EXISTING BLENDOUT. FUSELAGE LEFT HAND BILGE AREA AT STATION 1685 AREA STRINGER-47 LEFT EXISTING BLENDOUT HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTED FOUND CRACK APPROXIMATELY 1/8 INCH PER B77
- [SDR FDEA202104010805](https://openairdocs.org/sdr/FDEA202104010805.md): Floor Support · cracked · Apr 1, 2021 · N884FD · Boeing 777FS2 · Fuselage Miscellaneous Structure
  > BULK CARGO - FLOOR PANEL STRINGER AT RBL 41.5 FOUND 02 EA CRACKS AT STA 1937 AND STA 1958 AS MARKED. BULK CARGO FLOOR PANEL STRINGER AT RBL 41.5 AT STA 1937 AND STA 1958 02EA CRACKED REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STA 1926 -
- [SDR FDEA202103300798](https://openairdocs.org/sdr/FDEA202103300798.md): Doubler · misaligned · Mar 30, 2021 · N884FD · Boeing 777FS2 · Fuselage Main, Structure
  > WHILE ACCOMPLISHING LH E.O.#G-5310-E0332629 K P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR S-35L NEAR MILLED EDGE. COMPLIED WITH E.A.# G-5310-T0360894 P1 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202103300797](https://openairdocs.org/sdr/FDEA202103300797.md): Doubler · misaligned · Mar 30, 2021 · N884FD · Boeing 777FS2 · Fuselage Main, Structure
  > WHILE ACCOMPLISHING RH E.O.#G-5310-E0332629 K P6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.# G-5310-T0360894 P2, DEVIATION TO SB 777-53- 0087 REV 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA202103290793](https://openairdocs.org/sdr/FDEA202103290793.md): Fitting · cracked · Mar 29, 2021 · N884FD · Boeing 777FS2 · Fuselage Main, Structure
  > DURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO: E-G-5310-E0332629 K P5 ON REMOVED FASTENER HOLES AND FOUND 01 EA CRACK INDICTION ON LHS VERTICAL FLANGE OF THE FRONT LOWER SPAR CHORD AT BS 1035 APPROX LBL 81.30 LOWER O/B HOLE AS MARKED. WING C
- [SDR FDEA202103290792](https://openairdocs.org/sdr/FDEA202103290792.md): Fitting · cracked · Mar 29, 2021 · N884FD · Boeing 777FS2 · Fuselage Main, Structure
  > DURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO: E-G-5310-E0332629 K P6 ON REMOVED 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 AS MARKED. WING
- [SDR FDEA201908211991](https://openairdocs.org/sdr/FDEA201908211991.md): Lamp · inoperative · Aug 21, 2019 · N884FD · Boeing 777FS2 · Emergency Lighting
  > POST-FLT INSP, ONE OVERHEAD SUPRNMRY EMERGENCY LIGHT INOPERATIVE DURING A LIGHTS TEST. REPLACED THE LAMP, IAW AMM: 33-51-04-2. LIGHT TESTED SATIS, OK FOR SERVICE.
- [SDR FDEA201705041358](https://openairdocs.org/sdr/FDEA201705041358.md): Latch · damaged · May 4, 2017 · N884FD · Boeing 777FS2 · Escape Slide
  > PREFLIGHT MX CHECK, FOUND THE L1 DOOR EMERGENCY ESCAPE SLIDE COVER SHROUD FWD LATCH DEFORMED AND NOT RETAINING SHROUD ASSY. REMOVED AND REPLACED L1 DOOR BUSTLE FORWARD LATCH IAW CMM 25-66-06, REINSTALLED BUSTLE IAW MM 25-66-06-4.
- [SDR FDEA201702220625](https://openairdocs.org/sdr/FDEA201702220625.md): Lamp · inoperative · Feb 22, 2017 · N884FD · Boeing 777FS2 · Emergency Lighting
  > DURING A POST FLIGHT INSPECTION, ONE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-50-00-2. LIGHTS TESTED GOOD, OK FOR SERVICE.
- [SDR FDEA201601210273](https://openairdocs.org/sdr/FDEA201601210273.md): Skin · punctured · Jan 21, 2016 · N884FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > FORWARD LOWER FUSELAGE SKIN AT STATION 630, BETWEEN STRINGER 34R - 35R, FOUND A 2" PUNCTURE HOLE. REPAIR IDENTIFIED AS MAJOR REPAIR BY ENGINEERING. EA G-5330-T0322852A WAS COMPLIED WITH.
- [SDR FDEA201506101753](https://openairdocs.org/sdr/FDEA201506101753.md): Bulb · inoperative · Jun 10, 2015 · N884FD · Boeing 777FS2 · Emergency Lighting
  > ONE OVERHEAD EMERGENCY EXIT LIGHT DID NOT ILLUMINATE DURING CABIN INSPECTION. R & R THE OVERHEAD EMERGENCY EXIT LIGHT & OPS CHECKED NORMAL IAW AMM 33-51-03-2.
- [SDR FDEA201501130144](https://openairdocs.org/sdr/FDEA201501130144.md): Light · inoperative · Jan 13, 2015 · N884FD · Boeing 777FS2 · Emergency Lighting
  > POST FLIGHT CHECK FOUND 1 SUP AREA EMER LT INOPERATIVE. RELAMPED IAW AMM 33-51-03-2. EMER LIGHTS TESTED NORMAL. ITEM OK FOR SERVICE.
- [SDR FDEA201407041627](https://openairdocs.org/sdr/FDEA201407041627.md): Battery Pack · discharged · Jul 4, 2014 · N884FD · Boeing 777FS2 · Passenger/Crew Doors
  > ON POST FLIGHT CHECK FOUND L1 DOOR EMER ASSIST BATTERY PACK GREEN TEST LIGHT NOT FLASHING. R & R L1 DOOR ASSIST BATTERY PACK TEST LIGHT 9V BACK UP BATTERIES TWO EACH IAW AMM 52-11-20-4-2. OPERATIONS CHECKED NORMAL, ITEM OK FOR SERVICE.
- [SDR FDEA201405110984](https://openairdocs.org/sdr/FDEA201405110984.md): Slide · deployed · May 11, 2014 · N884FD · Boeing 777FS2 · Escape Slide
  > DOOR L1 SLIDE DEPLOYED. REMOVED L1 DOOR MOUNTED SCAPE SYS IAW MM 25-66-00-2. RESTORED DOOR MOUNTED ESCAPE SLIDE SYS AFTER SLIDE DEPLOYMENT. 2 SLIDE SAFETY PINS, BOTTLE & GIRT REMOVED IAW AMM 25-66-00-2.
- [SDR FDEA201307231644](https://openairdocs.org/sdr/FDEA201307231644.md): Tire · leaking · Jul 23, 2013 · N884FD · Boeing 777FS2 · Tire
  > TIRE PRESSURE EICAS MESSAGE. NR 3 MLG TIRE PRESSURE 180 PSI DECREASED TO 160 PSI. REMAINED AT 160 PSI AFTER LANDING. VERIFIED NR 3 TIRE PRESSURE IS LOW. R & R NR 3 WHEEL ASSY IAW MM 32-45-01-4. ACFT OK TO CONTINUE.
- [SDR FDEA201306151305](https://openairdocs.org/sdr/FDEA201306151305.md): Autopilot Sys · malfunctioned · Jun 15, 2013 · N884FD · Boeing 777FS2 · Autopilot System
  > ACFT WENT INTO AN UNCOMMANDED RIGHT TURN. NOTICED IT HAD GONE INTO HDG MODE AND THE HDG WAS APPROX 112 DEGREES (VS. 030) F/O DISCONNECTED AUTOPILOT AND BANKS 30 LEFT TO REJOIN COURSE. INTERROGATED MAT AND FOUND MAINT MESSAGE 22-11635 NOT ACTIVE. FIM 34-3
- [SDR FDEA201211224125](https://openairdocs.org/sdr/FDEA201211224125.md): Interface Unit · inoperative · Nov 22, 2012 · N884FD · Boeing 777FS2 · Hydraulic Indicating System
  > APPROX 2.5 HRS INTO FLIGHT, RECIEVED HYD QTY LOW R CAUTION MESSAGE. OBSERVED CONTINUOUS DROP IN RIGHT HYD QTY THROUGHOUT REMAINDER OF FLIGHT, DIVERTED. R & R RT HYD INTERFACE MODULE. OPS CHECKED GOOD IAW MM 29-11-50-4. R & R RT HYD RESERVOIR QUANTITY TRANS
- [SDR FDEA201203281167](https://openairdocs.org/sdr/FDEA201203281167.md): Computer · malfunctioned · Mar 28, 2012 · N884FD · Boeing 777FS2 · Flight Management Computing Software System
  > FLIGHT PLAN WAS LOADED VIA UPLINK. FLIGHT PLAN WAS CHECKED IN CAPTAINS PREFIGHT ON PLAN PAGE FOR PROPER SEQUENCING AND VERIFIED WITH F/O THROUGH CFM PROCEDURES. WHEN ACFT WAS AT FL340 APPROACHING N45/W160, WHEN ACFT SEQUENCE POINT, NEXT POINT WAS N43/W150, A
- [SDR FDEA201110074382](https://openairdocs.org/sdr/FDEA201110074382.md): Battery · inoperative · Oct 7, 2011 · N884FD · Boeing 777FS2 · Passenger/Crew Doors
  > FOUND R1 DOOR EPAS POWER GREEN LIGHT DOES NOT COMES ON. REPLACED EPAS POWER PACK BACKUP BATT AND CHECK OK IAW MM52-11-20-4-2, 52-11-20-5-2. ACFT OK FOR SERVICE. FINAL CLOSED.
- [SDR FDEA201103150981](https://openairdocs.org/sdr/FDEA201103150981.md): Light · inoperative · Mar 15, 2011 · N884FD · Boeing 777FS2 · Emergency Lighting
  > R-1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE R1 DOOR EMERGENCY EXIT LIGHT.

## 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 = 'N884FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N884FD/reports

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