# Service difficulty reports: N890FD

A list on [N890FD](https://openairdocs.org/aircraft/N890FD.md).

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

- [SDR FDEA202604240496](https://openairdocs.org/sdr/FDEA202604240496.md): Bulb · inoperative · Apr 24, 2026 · N890FD · Boeing 777FS2 · Emergency Lighting
  > R1 DOOR AFT EMERGENCY EXIT SIGN LIGHT INOP (1EA BULB). REPLACED THE BULB EMERGENCY EXIT LIGHT AT R1 DOOR IAW AMM 33-51-01-2.
- [SDR FDEA202602150211](https://openairdocs.org/sdr/FDEA202602150211.md): Safety Wire · wrong part · Feb 15, 2026 · N890FD · Boeing 777FS2 · Escape Slide
  > WRI TO REPLACE THE R1 DOOR SLIDE WIRE WITH MS20995CY16 WIRE. AMM: 25-66-01-4 REPLACED R1 DOOR SLIDE SHEAR WIRE WITH MS20995CY16 WIRE PER REF ABOVE
- [SDR FDEA202505010702](https://openairdocs.org/sdr/FDEA202505010702.md): Skin · chafed · May 1, 2025 · N890FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR SURROUND FWD EDGE AT 10.5" FROM BOTTOM FOUND CHAFFED. FWD CARGO DOOR SURROUND FWD EDGE AT 10.5" FROM BOTTOM CHAFFED AREA REPAIRED AS PER B777 SRM 51-40-02-0G, SRM 51-10-02-0G, SRM53-10-01-2R REPAIR 1, SRM 51-40-05-0G, SRM 51- 40-08-0G, SRM 51
- [SDR FDEA202505010701](https://openairdocs.org/sdr/FDEA202505010701.md): Skin · dented · May 1, 2025 · N890FD · Boeing 777FS2 · Trailing Edge Flaps
  > FOUND RHW T/E O/B FLAP LOWER SURFACE DENT 01 EA AT THE CROSS OTEF 263 AND T/E 4 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 01 EA AT THE CROSS OTEF 263 AND T/E 4 INCHES AS PER B777 SRM 57-53-01-2R-2 AND SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-T0
- [SDR FDEA202505010700](https://openairdocs.org/sdr/FDEA202505010700.md): Skin · dented · May 1, 2025 · N890FD · Boeing 777FS2 · Trailing Edge Flaps
  > FOUND RHW T/E I/B FLAP LOWER SURFACE DENT (LENGTH 15.5 INCHES AND WIDE 13.5 INCHES) AT THE CROSS ITEF 260 AND T/E 21 INCHES. REPAIRED RHW T/E I/B FLAP LOWER SURFACE DENT(LENGTH 15.5 INCHES AND WIDE 13.5 INCHES) AT THE CROSS ITEF 260 AND T/E 21 INCHES AS P
- [SDR FDEA202505010698](https://openairdocs.org/sdr/FDEA202505010698.md): Skin · cracked · May 1, 2025 · N890FD · Boeing 777FS2 · Wing, Plate/Skin
  > OPEN HOLE HFEC INSPECTION OF #5 HOLE AT RH WING UPPER SKIN WBL 262 AND FOUND 01EA CRACK AS MARKED. RH WING UPPER SKIN WBL 262 #5 HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51-40-05-0G, SRM51-40-02-0G, SRM51-40-04-0G AND EA G-5730-T0383252 P1 TITLE:WING-PLA
- [SDR FDEA202505010697](https://openairdocs.org/sdr/FDEA202505010697.md): Skin · cracked · May 1, 2025 · N890FD · Boeing 777FS2 · Wing, Plate/Skin
  > OPEN HOLE HFEC INSPECTION OF #5 HOLE AT LH WING UPPER SKIN WBL262 AND FOUND 01EA CRACK AS MARKED. LH WING UPPER SKIN WBL 262 #5 HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51-40-05-0G, SRM51-40-02-0G, SRM51-40-04-0G AND EA G-5730-T0383251 P1, TITLE:WING - P
- [SDR FDEA202412041774](https://openairdocs.org/sdr/FDEA202412041774.md): None · none · Dec 4, 2024 · N890FD · Boeing 777 · Standard Practices/Structures
  > CREW WAS NOTIFIED ENROUTE THAT PER MEL RESTRICTION THE AFT BELLY POSITION A3L WAS LOADED 736 POUNDS OVER THE MEL RESTRICTION. LOWER DECK CARGO RESTRAINING SYSTEM INSPECTION. ACCOMPLISHED IAW AMM 25-58-00-6 REV 101.5. THE CARGO GUIDES AND RESTRAINTS ARE INS
- [SDR FDEA202210072506](https://openairdocs.org/sdr/FDEA202210072506.md): Doubler · misrepaired · Oct 7, 2022 · N890FD · Boeing 777FS2 · Fuselage Structure (General)
  > DURING PERFORMING EO G-5710-E0365655 B P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N: 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE
- [SDR FDEA2022101172505](https://openairdocs.org/sdr/FDEA2022101172505.md): Doubler · misrepaired · Oct 7, 2022 · N890FD · Boeing 777FS2 · Fuselage Structure (General)
  > DURING PERFORMING EO G-5710-E0365655 B P7 STEP8.C.(5), FOUND 01EA ZLJ-8 COUNTERSUNK FASTENER AT STA 998 S35L TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUNK HOLE.
- [SDR FDEA202210032455](https://openairdocs.org/sdr/FDEA202210032455.md): Skin · dented · Oct 3, 2022 · N890FD · Boeing 777FS2 · Trailing Edge Flaps
  > RHW T/E O/B FLAP MIDDLE LOWER SURFACE FOUND 1EA DENT AT 310" TO O/B CROSS 10" TO T/E. RHW T/E O/B FLAP MIDDLE LOWER SURFACE AT 310" TO O/B CROSS 10" TO T/E REPAIRED AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1,REV 41.0. THE B777 SRM 5
- [SDR FDEA202210032454](https://openairdocs.org/sdr/FDEA202210032454.md): Skin · dented · Oct 3, 2022 · N890FD · Boeing 777FS2 · Trailing Edge Flaps
  > LH WING O/B FLAP LOWER SURFACE FROM O/B TO I/B 39" CROSS AFT TO FWD 6" AREA FOUND DENTED. LH WING O/B FLAP LOWER SURFACE FROM O/B TO I/B 39" CROSS AFT TO FWD 6"AREA REPAIRED AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR1,REV 41.0. THE B777
- [SDR FDEA202210022450](https://openairdocs.org/sdr/FDEA202210022450.md): Floor Panel · cracked · Oct 2, 2022 · N890FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1413/RBL38.5-40 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1413/RBL38.5-40 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GM
- [SDR FDEA202210022449](https://openairdocs.org/sdr/FDEA202210022449.md): Floor Panel · cracked · Oct 2, 2022 · N890FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242PF(P/N:152W8652-6) AT STA1439.5/RBL22-25.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242PF (P/N:152W8652-6)AT STA 1439.5/RBL22-25.5 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GM
- [SDR FDEA202210022448](https://openairdocs.org/sdr/FDEA202210022448.md): Floor Panel · cracked · Oct 2, 2022 · N890FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1445.5/RBL73-75 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1445.5/RBL73-75 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6
- [SDR FDEA202210022447](https://openairdocs.org/sdr/FDEA202210022447.md): Floor Panel · cracked · Oct 2, 2022 · N890FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1388.75/LBL38.5-40 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1388.75/LBL38.5-40 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER
- [SDR FDEA202210022446](https://openairdocs.org/sdr/FDEA202210022446.md): Floor Panel · cracked · Oct 2, 2022 · N890FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1383.5/LBL43.75-45.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1383.5/LBL43.75-45.5 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR
- [SDR FDEA202210022445](https://openairdocs.org/sdr/FDEA202210022445.md): Floor Panel · cracked · Oct 2, 2022 · N890FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1255-1256.25/RBL87.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1255 -1256.25/RBL87.5 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202210022444](https://openairdocs.org/sdr/FDEA202210022444.md): Floor Panel · cracked · Oct 2, 2022 · N890FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL57-57.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL57-57.5 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-
- [SDR FDEA202209032157](https://openairdocs.org/sdr/FDEA202209032157.md): Pump · failed · Sep 3, 2022 · N890FD · Boeing 777FS2 · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC QUANTITY CENTER LOW NNC FOLLOWED BY RESERVE BRAKES STRG NNC. BOTH ECL CHECKLISTS RUN, SLOW LOSS OF CENTER HYDRAULIC QUANTITY UNTIL TOUCHDOWN. NORMAL EXTENSION OF GEAR AND FLAPS. LANDED STRAIGHT AHEAD AND AIRCRAFT TOWED IN. CENTER HYDRAULIC QUANT
- [SDR FDEA202209022146](https://openairdocs.org/sdr/FDEA202209022146.md): Pump · leaking · Sep 2, 2022 · N890FD · Boeing 777FS2 · Hydraulic Pump (Electric/Engine), Main
  > PDIS 890 29-02 0368 02SEP22 KIX HYDRAULIC QUANTITY CENTER LOW NNC FOLLOWED BY RESERVE BRAKES STRG NNC. BOTH ECL CHECKLISTS RUN, SLOW LOSS OF CENTER HYDRAULIC QUANTITY UNTIL TOUCHDOWN. NORMAL EXTENSION OF GEAR AND FLAPS. LANDED STRAIGHT AHEAD AN
- [SDR FDEA2020061091156](https://openairdocs.org/sdr/FDEA2020061091156.md): Skin · punctured · Jun 9, 2020 · N890FD · Boeing 777FS2 · Spoilers
  > LT WING NR 5 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS722. LEFT HAND WING NR 5 SPOILER UPPER SURFACE PUNCTURE DAMAGE AT WING STATION 717 TO WING STATION 722. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354457 PART1. TITLE: WINGS- FLIGH
- [SDR FDEA202006051132](https://openairdocs.org/sdr/FDEA202006051132.md): Skin · punctured · Jun 5, 2020 · N890FD · Boeing 777FS2 · Spoilers
  > LT WING NR 5 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS 717. LEFT HAND WING NR 5 SPOILER UPPER SURFACE AT WING STATION 717 TO WING STATION 722. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354457 PART1. TITLE: WING - FLIGHT SURFACES LT W
- [SDR FDEA202006051131](https://openairdocs.org/sdr/FDEA202006051131.md): Skin · punctured · Jun 5, 2020 · N890FD · Boeing 777FS2 · Spoilers
  > LT WING NR 3 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS907. LEFT HAND WING NR 3 SPOILER UPPER SURFACE PUNCTURE DAMAGE AT WING STATION 907. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354459 PART 1 TITLE: WINGS - FLIGHT SURFACES - LT WIN
- [SDR FDEA202005221030](https://openairdocs.org/sdr/FDEA202005221030.md): Skin · cracked · May 22, 2020 · N890FD · Boeing 777FS2 · Leading Edge Devices
  > DURING ACCOMPLISHMENT OF MEDIUM FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND WING SLAT NR 5 OUTER SKIN FOUND 01 EACH CRACK. INDICATION AT FASTENER HOLE AT STATION OSCS 713 APPROXIMATELY 0.2" IN LENGTH. LEFT HAND WING SLAT NR 5 OUTER SKIN REPAIRED AS PER SRM
- [SDR FDEA201907041482](https://openairdocs.org/sdr/FDEA201907041482.md): Cooling Fan · jammed · Jul 4, 2019 · N890FD · Boeing 777FS2 · Air Distribution Fan
  > FUMES IN COCKPIT NO CAUTION OR WARNING DISPLAYED FUMES DETECTED BY SMELL-DISIPATED AFTER RIGHT EQUIP COOLING FAN WAS DEACTIVATED. FLIGHT SAFETY REPORT FILED. DEBRIEFED WITH CREW WHEN RIGHT FAN C'B OPENED NO FUMES IN CABIN. CHECK MAT FOUND MX MESSAGE21-14024,
- [SDR FDEA201804281140](https://openairdocs.org/sdr/FDEA201804281140.md): Slide · low pressure · Apr 28, 2018 · N890FD · Boeing 777FS2 · Escape Slide
  > L1 SLIDE RAFT PRESSURE LOW. R/RD L1 SLIDE RAFT PER AMM 25-66-01-4. REMOVED SLIDE RAFT.
- [SDR FDEA201702090493](https://openairdocs.org/sdr/FDEA201702090493.md): Cover · missing · Feb 9, 2017 · N890FD · Boeing 777FS2 · Emergency Lighting
  > COVER FOR EXIT LIGHT ON LEFT SIDE OF L1 DOOR IS MISSING, INSTALLED A NEW EMERGENCY EXIT LIGHT COVER.
- [SDR FDEA201702090492](https://openairdocs.org/sdr/FDEA201702090492.md): Cover · missing · Feb 9, 2017 · N890FD · Boeing 777FS2 · Emergency Lighting
  > COVER FOR THE EXIT LIGHT ON THE LT SIDE OF THE L1 DOOR IS MISSING. INSTALLED THE EXIT SIGN ASSY AND COVER SMP. LIGHT CHECKED OK.
- [SDR FDEA201503050686](https://openairdocs.org/sdr/FDEA201503050686.md): Handle · out of position · Mar 5, 2015 · N890FD · Boeing 777FS2 · Flight Compartment Windows
  > HAD TO OPEN LT WINDOW TO MAKE TURN INTO GATE. WINDOW WILL NOT LOCK CLOSED. FOUND LT WINDOW LOCKING HANDLE IN THE INCORRECT POSITION. OPENED & CLOSED LT WINDOW SEVERAL TIMES ON GND, LT WINDOW CHECKS GOOD IAW MM CH 56-11-04-4-0. OK FOR SERVICE.
- [SDR FDEA201410042965](https://openairdocs.org/sdr/FDEA201410042965.md): Girt Bar · out of adjust · Oct 4, 2014 · N890FD · Boeing 777FS2 · Emergency Equipment
  > L1 DOOR WILL NOT ARM. ADJUSTED GIRT BAR, OPS CHECKED GOOD IAW MM 52-11-00-5.
- [SDR FDEA201409122603](https://openairdocs.org/sdr/FDEA201409122603.md): Spring · missing · Sep 12, 2014 · N890FD · Boeing 777FS2 · Emergency Lighting
  > EMERGENCY LIGHTS SWITCH IS MISSING INTERNAL SPRING CLIP, DOES NOT DISARM OR ARM EMER LIGHTS WHEN COVER IS POSITIONED DOWN OR WHEN SELECTED TO OFF. R & R EMER LIGHTS SWITCH GUARD COVER WITH SPRING CLIP PN 402-122 IAW SMP. PERFORMED EMER LIGHT OPERATIONAL TEST

## 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 = 'N890FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N890FD/reports

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