# Service difficulty reports: N125FE

A list on [N125FE](https://openairdocs.org/aircraft/N125FE.md).

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

- [SDR FDEA202608211212](https://openairdocs.org/sdr/FDEA202608211212.md): Skin · dented · Aug 21, 2026 · N125FE · Boeing 7673S2F · Fuselage Main, Plate/Skin
  > DURING INSPECTION FOUND EVIDENCE OF STRIKE AT BS 368, STRINGER 5R, DOOR STA 108 3/4" INBD OF STR 5R, REPAIRED SKIN USING COMPLING WITH EA.H-5330-T0388341P1 (PART 1 OF THIS EA PROVIDES INSTRUCTIONS TO ACCOMPLISH SRM 53-00-01-2R, REPAIR 29, WITH CLARIFICATION
- [SDR FDEA202608201196](https://openairdocs.org/sdr/FDEA202608201196.md): Panel · delaminated · Aug 20, 2026 · N125FE · Boeing 7673S2F · Wing, Plate/Skin
  > RIGHT WING UPPER L/E PANEL ABOVE PYLON AT ISS 337.60 HAS EROSION ACROSS L/E, WITH NUMEROUS FASTENER HEADS PULLING THROUGH SKIN. ALSO FOUND SEVERAL DOUBLE DRILLED HOLES ON THE RT WING LEADING EDGE RIBS AND CHORDS BETWEEN WS 337 & 356. THERE ARE NO PUBLISHED
- [SDR FDEA202608061090](https://openairdocs.org/sdr/FDEA202608061090.md): Skin · dented · Aug 6, 2026 · N125FE · Boeing 7673S2F · Leading Edge Devices
  > #4 SLAT T/E WEDGE UPPER SURFACE, 22" FROM THE OUTBD END AND 7" FROM THE AFT EDGE HAS SMALL DENT.MWT, REPAIRED DENT ON # 4 SLAT ON UPPER SURFACE 22" FROM OB EDGE AND 7" FROM AFT EDGE. REF B767 SRM 51-70-10-2R REPAIR 2 FIG 201 SHEET (1 OF 5). SEE JPF, THIS I
- [SDR FDEA202608041083](https://openairdocs.org/sdr/FDEA202608041083.md): Skin · dented · Aug 4, 2026 · N125FE · Boeing 7673S2F · Leading Edge Devices
  > RIGHT WING NR 8 SLAT TOP SIDE APPROX IN THE MIDDLE HAS A DENT. REPAIRED RT WING NR 8 SLAT TRAILING EDGE WEDGE TOP SKIN SURFACE AT WS.465.65 IAW SRM: 57-43-02-2R AND SRM 51-70-10-2R. THIS IS A MAJOR REPAIR, SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.
- [SDR FDEA202608011075](https://openairdocs.org/sdr/FDEA202608011075.md): Skin · dented · Aug 1, 2026 · N125FE · Boeing 7673S2F · Leading Edge Devices
  > RIGHT WING, NR 7 SLAT, UPPER SURFACE T/E WEDGE HAS 2EA DENTS APPROX 28" FROM OUTBD EDGE. REPAIRED DENTS ON RT WING, NR 7 SLAT, UPPER SURFACE T/E WEDGE AT ISS 317 IAW SRM 57-43-02-2R AND SRM 51-70-10-2R. SEE JPF FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.
- [SDR FDEA202509141704](https://openairdocs.org/sdr/FDEA202509141704.md): Warning Message · illuminated · Sep 14, 2025 · N125FE · Boeing 7673S2F · Door Warning System
  > ENROUTE MAIN CARGO DOOR LIGHT ILLUMINATED. ON DESCENT PASSING 22K, LIGHT WENT OUT. RELEASED FOR SERVICE PER MEL: 52-71-01-02 CATEGORY: C. MAIN DECK CARGO DOOR INDICATION SYSTEM - INOP. VERIFY AND RECORD IN AML/EAML THAT MAIN DECK CARGO DOOR IS CLOSED
- [SDR FDEA202508171491](https://openairdocs.org/sdr/FDEA202508171491.md): Escape Rope · dislodged · Aug 17, 2025 · N125FE · Boeing 7673S2F · Emergency Equipment
  > ESCAPE ROPE FROM MAIN ENTRY DOOR DISLODGED FROM FRAME AMM 25 61-02-2 ESCAPE ROPE REPOSITIONED IN YOUR PLACE A/C OK FOR SVC.
- [SDR FDEA202507031111](https://openairdocs.org/sdr/FDEA202507031111.md): Slat System · malfunctioned · Jul 3, 2025 · N125FE · Boeing 7673S2F · Leading Edge Slat Control System
  > LE SLAT DISAG ON RAISING FLAPS FROM 1 TO UP. RAN QRH. DECLARED EMERGENCY, UPON ARRIVAL. RECONFIGURED SLAT/FLAP SYS TO NORMAL OPS IAW MM 27-81-00-5. PERFORMED FSEU BITETEST IAW FIM 27-51 FT 809, FAULT HISTORY SHOWED: - LEG 0: TE FLAPS MAINT MSG 27-5110
- [SDR FDEA202408131120](https://openairdocs.org/sdr/FDEA202408131120.md): Fitting · cracked · Aug 13, 2024 · N125FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPARTMENT BETWEEN STA 977/999 AND RBL 11/33 FLOOR FITTING BROKEN. MAIN CARGO COMPARTMENT BTWN STA 977/999 AND RBL 11/33 FLOOR FITTING WAS REPLACED IAW E.A H-2550-T0380216
- [SDR FDEA202408101108](https://openairdocs.org/sdr/FDEA202408101108.md): Skin · burned · Aug 10, 2024 · N125FE · Boeing 7673S2F · Ailerons
  > RH WING, OUTBOARD AILERON BETWEEN WBL 910 AND WBL 890 WITH TWO LIGHTNING STRIKE. RH WING, OUTBOARD AILERON BTW WBL 910 AND WBL 890 WAS REPAIRED IAW B767 SRM 57-60- 02-2R PAG 1 AND SRM 51-70-14-0G REP 11 PAG 17-18 REV 89 APR 15/2024
- [SDR FDEA202408051086](https://openairdocs.org/sdr/FDEA202408051086.md): Floor Panel · dented · Aug 5, 2024 · N125FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF WITH SEVERAL DENTS. MAIN DECK CARGO, FLOOR PANEL 251KFF WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 89 APR 15/2023.
- [SDR FDEA202408051085](https://openairdocs.org/sdr/FDEA202408051085.md): Floor Panel · cracked · Aug 5, 2024 · N125FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241WFF WITH A PUNCTURE. MAIN DECK CARGO, FLOOR PANEL 241WFF WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR 4.B FIG. 201 SHEET 2 REV. 89 APR 15/2024.
- [SDR FDEA202408051084](https://openairdocs.org/sdr/FDEA202408051084.md): Skin · dented · Aug 5, 2024 · N125FE · Boeing 7673S2F · Leading Edge Devices
  > SLAT 11, EXTERNAL SURFACE, UPPER WEDGE WITH DENT NEXT TO INB FRAME. SLAT 11, EXTERNAL SURFACE, UPPER WEDGE WITH DENT NEXT TO INB FRAME WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRM 51-70-10-2R REPAIR 4 PAG 150-151 FIG 201 (SHEET 1) REV 89 APR
- [SDR FDEA202307081186](https://openairdocs.org/sdr/FDEA202307081186.md): Former · failed · Jul 8, 2023 · N125FE · Boeing 767300 · Wing Structure
  > NOSE FORMER ANGLE CRACKED AT RIGHT WING OSS 565. VISUALLY INSPECTED FORMER AT FLE OSS 565 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F & A WITH SRM TR 57-111 AS REFERENCE.
- [SDR FDEA202307081185](https://openairdocs.org/sdr/FDEA202307081185.md): Former · failed · Jul 8, 2023 · N125FE · Boeing 767300 · Wing Structure
  > NOSE FORMER ANGLE CRACKED AT THE RIGHT WING OSS 499.6. PER EA H-5720-T0367172 REV A VISUALLY INSPECTED FORMER AT FLE OSS 499.603 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F WITH SRM TR 57-111 AS REFERENCE.
- [SDR FDEA202211172811](https://openairdocs.org/sdr/FDEA202211172811.md): Skin · worn · Nov 17, 2022 · N125FE · Boeing 7673S2F · Leading Edge Devices
  > RH WING SLAT #8 INNER SKIN WEDGE AREA TWO PREVIUS REPAIR WITH WEAR. RH WING SLAT #8 T/E WEDGE INNER SKIN, ONE PREVIOUS REPAIR WAS REPLACED AND ONE FILLER WAS REPLACED IAW B767 SRM 57-43-02-2R REP. 1 FIG. 201 PAG. 1-2 AND SRM 51-70-10-2R REP. 4 PAG. 10, 11,
- [SDR FDEA202211172810](https://openairdocs.org/sdr/FDEA202211172810.md): Skin · worn · Nov 17, 2022 · N125FE · Boeing 7673S2F · Leading Edge Devices
  > LEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WITH WEAR (LOWER SURFACE). LEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WEDGE WAS REPAIRED IAW SRM 51-70-10-2R REPAIR 4 FIG. 202 SHEET 8 AND SRM 57-43-02-2R REP. 1 FIG. 201 PAG. 1-2 REV. 84 15-AUG-2022
- [SDR FDEA202007011419](https://openairdocs.org/sdr/FDEA202007011419.md): Slat · chafed · Jul 1, 2020 · N125FE · Boeing 767300 · Leading Edge Slat Control System
  > RW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED REPAIR IAW B767AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IAW
- [SDR FDEA2020070811419](https://openairdocs.org/sdr/FDEA2020070811419.md): Wedge · chafed · Jul 1, 2020 · N125FE · Boeing 7673S2F · Leading Edge Devices
  > RW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED REPAIR IAW B767AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IAW
- [SDR FDEA2020070211419](https://openairdocs.org/sdr/FDEA2020070211419.md): Wedge · gouged · Jul 1, 2020 · N125FE · Boeing 7673S2F · Leading Edge Devices
  > RT WING NR 8 SLAT TE GOUGED TWO PLACES. REPAIRED NR 8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED. REPAIR IAW AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IA
- [SDR FDEA2019111522939](https://openairdocs.org/sdr/FDEA2019111522939.md): Brake · damaged · Nov 12, 2019 · N125FE · Boeing 7673S2F · Landing Gear Brake System
  > PDIS 125 32-43 4006 12NOV19 CDG OPEN U LOGPAGES:2841209 ON LANDING ROLLOUT APPLIED BRAKES MANUALLY FELT VIBRATION. ON SHUTDOWN BRAKE TEMP LIGHT IS ON BRAKE TEMPS 4435 WITH LIGHT BRAKING SHGN 12NOV19 20:11 CDG U UPON CAPTAIN'S FEEDBACK DEC
- [SDR FDEA2018081752047](https://openairdocs.org/sdr/FDEA2018081752047.md): Sensor · fod · Aug 15, 2018 · N125FE · Boeing 7673S2F · Door Warning System
  > 1.25 HOURS INTO FLIGHT, RECEIVED A MAIN CARGO EICAS. COMPLIED WITH QRH. INDICATOR WENT OUT. DECENDING THRU FL220. PRESSURIZATION NORMAL THOUGHOUT. FOUND DEBRIS ON THE SENSOR TARGET S892. REMOVED THE DEBRIS. INSPECTION CHECKED GOOD. PERFORMED PSEU
- [SDR FDEA201806191544](https://openairdocs.org/sdr/FDEA201806191544.md): Smoke Barrier · damaged · Jun 19, 2018 · N125FE · Boeing 7673S2F · Emergency Equipment
  > CREW REST SMOKE CURTAIN HAS HOLE IN IN LEFT PLASTIC WINDOW. INSTALLED NEW CURTAIN PER IPC 26-29-01-01.
- [SDR FDEA201607312683](https://openairdocs.org/sdr/FDEA201607312683.md): Unknown · malfunctioned · Jul 31, 2016 · N125FE · Boeing 7673S2F · Trailing Edge Flap Control System
  > FLAPS STOPPED BETWEEN 20 AND 25 FLAPS ON INITIAL CONFIGURATION FOR LANDING WITH T/E FLAP DISAGREE. COMPLIED WITH QRH FOR REF FLAP 20 LANDING. VERIFIED OVERLOAD TRIP INDICATORS ON LT & RT WINGS AND VERIFIED FLAP TRANSMITTERS TO BE GOOD FOR SERVICE. PERFORMED
- [SDR FDEA201509132855](https://openairdocs.org/sdr/FDEA201509132855.md): Controller · malfunctioned · Sep 13, 2015 · N125FE · Boeing 7673S2F · Cabin Pressure Controller
  > AT FL 360 GOT A CABIN ALTITUDE MASTER WARNING. CABIN WAS SHOWING JUST OVER 10,000 FT WITH A 200 FT PER MIN CLIMB. WE WENT TO AUTO 2 BUT CABIN CONTINUED TO CLIMB, COMPLIED WITH QRH. ON DESCENT WE TRIED MANUAL & WERE ABLE TO CONTROL THE CABIN ALTITUDE. TROUB

## 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 = 'N125FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N125FE/reports

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