# Service difficulty reports: N110FE

A list on [N110FE](https://openairdocs.org/aircraft/N110FE.md).

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

- [SDR FDEA202604300525](https://openairdocs.org/sdr/FDEA202604300525.md): Lens · missing · Apr 30, 2026 · N110FE · Boeing 7673S2F · Emergency Lighting
  > L1 DOOR INTERIOR EXIT LIGHT LENS MISSING EMERGENCY EXIT SIGN LENS LOCATED IN FLT DECK, REFITTED PER AMM 33-51-01-2. CHECKS OK.
- [SDR FDEA202410151511](https://openairdocs.org/sdr/FDEA202410151511.md): Skin · punctured · Oct 15, 2024 · N110FE · Boeing 7673S2F · Leading Edge Devices
  > RH WING NO.7 SLAT MID SECTION LOW SURFACE FOUND PUNCTURE, AS MARKED REPAIRED THE RH WING NO.7 SLAT MID SECTION LOW SURFACE PER B767 SRM57-43-02-2R REPAIR 1 & SRM51-70-10-2R REPAIR 4. THIS IS CAT A REPAIR. RSC TRACKING EA: H-5750-T0380979 P1 ISSUED AND COMP
- [SDR FDEA202410151510](https://openairdocs.org/sdr/FDEA202410151510.md): Stringer · damaged · Oct 15, 2024 · N110FE · Boeing 7673S2F · Fuselage Main, Longeron/Stringer
  > FUSELAGE FRAME STA1502 - STRINGER CLIP AND S-20L STRINGER 1EA FASTENER HOLE ENLARGED REPAIRED THE DISCREPANT(ENLARGED) HOLE AT FUSELAGE FRAME STA1502 - STRINGER CLIP AND S-20L STRINGER PER EA H-5310-T0380977 P1. TITLE: FUSELAGE - MAINFRAME - MISS-DRILLED
- [SDR FDEA202405150673](https://openairdocs.org/sdr/FDEA202405150673.md): Skin · damaged · May 15, 2024 · N110FE · Boeing 7673S2F · Electrical/Electronic Compartment Doors
  > E&E BAY DOOR AND SURROUNDING STRUCTURE DAMAGED. E&E BAY DOOR REPLACE AND SURROUNDING STUCTURES REPAIRED UNDER FED-RE-2403203 REM 97-2.
- [SDR FDEA202405150672](https://openairdocs.org/sdr/FDEA202405150672.md): Skin · damaged · May 15, 2024 · N110FE · Boeing 7673S2F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN DAMAGED AT APPROX. STATION 157. FUSELAGE SKIN REPAIRED IAW FED-RE-2403203
- [SDR FDEA202405130657](https://openairdocs.org/sdr/FDEA202405130657.md): Actuator · failed · May 13, 2024 · N110FE · Boeing 7673S2F · Landing Gear Actuator
  > NLG FAILED TO EXTEND, UPON LANDING ACFT REMAINED ON CENTERLINE OF RUNWAY SURFACE. REF E.A H-5310-T0380090 P1 WORKED IN CONJUSCTION WITH 53-10/0463 COMPLETED INSTALLATION OF NOSE LANDING GEAR RETRACT ACUATOR REF B767 AMM 32-34-01-4 OPS AND LEAK CHECK GOOD.
- [SDR FDEA202401130076](https://openairdocs.org/sdr/FDEA202401130076.md): Unknown · unknown · Jan 13, 2024 · N110FE · Boeing 767300 · Standard Practices/Structures
  > WEIGHT CHECK DUE FOR THE FLIGHT DECK PORTABLE FIRE EXTINGUISHER MOUNTED IN FRONT OF RAFT STOWAGE. GMM: 9-4-404 AMM: 26-26-02-4-1 COMPLETED WEIGHT CHECK PROCEDURE PER ABOVE REFS. OK FOR SERVICE.
- [SDR FDEA202311061831](https://openairdocs.org/sdr/FDEA202311061831.md): Flap · damaged · Nov 6, 2023 · N110FE · Boeing 767300 · Trailing Edge Flaps
  > LH WING, INBOARD AFT FLAP LOWER SURFACE RH SIDE WITH PUNCTURE LH WING INBOARD AFT FLAP LOWER SURFACE, RH SIDE WAS REPAIRED IAW B767 SRM 57-53-01- 2R FIG 201 TABLE 1 PAG 1,4,5 AND SRM 51-70-03-0G PAR 5B FIG 15 SHEET 4 PAG 19,20,51. REV 87 AUG 15/2023
- [SDR FDEA202305260966](https://openairdocs.org/sdr/FDEA202305260966.md): Elt · unknown · May 26, 2023 · N110FE · Boeing 767300 · Emergency Locator Beacon
  > ELT HAS BEEN DETECTED EMITTING DURING FLIGHT. FOR INFO: IST STATION LOCAL TOWER WARNED US FOR ELT SIGNAL. RELEASED FOR SERVICE PER MEL: 25-63-10-02-A ON ARRIVAL ELT SWITCH (GUARDED) THAT IN THE OVERHEAD PANEL FOUND ARM POSITION. YESTERDAY HAPPENED ONE
- [SDR FDEA202210082517](https://openairdocs.org/sdr/FDEA202210082517.md): Skin · dented · Oct 8, 2022 · N110FE · Boeing 7673S2F · Trailing Edge Flaps
  > LEFT WING OUT BOARD TRAILING EDGE FLAP WITH DENT (LOWER SURFACE) LEFT WING OUTBOARD FLAP T/E, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG. 1-7 AND B767 SRM 51-70-03-0G PARAG. 5.A.(1) FIG. 5 PAG. 19, 36 REV. 82 DEC 15/2021
- [SDR FDEA202210052471](https://openairdocs.org/sdr/FDEA202210052471.md): Wedge · dented · Oct 5, 2022 · N110FE · Boeing 7673S2F · Leading Edge Devices
  > LEFT WING SLAT NO. 6 TRAILING EDGE WEDGE WITH DENT. RH WING SLAT #6 TRAILING EDGE WEDGE UPPER SURFACE AT POSITION ISS 231-236 SKIN WAS REPAIRED IAW SRM 51-70-10-2R REP. 4 PAG. 143-154 FIG. 201, SRM 57-43-02-2R FIG. 201 PAG. 1-2 REV. 82 DEC15/2021
- [SDR FDEA202208161984](https://openairdocs.org/sdr/FDEA202208161984.md): Fire Bottle · failed · Aug 16, 2022 · N110FE · Boeing 767300 · Fire Bottle, Fixed
  > MDIS 110 26-11 8313 16AUG22 MXP OPEN U APU FIRE EXT. BOTTLE DISCHARGE LIGHT ILLUMINATED. MEL 16AUG22 15:22 MXP U RELEASED FOR SERVICE PER MEL: 26-22-01-B CATEGORY: B EXPIRATION: 19AUG22 "MEL 26-22-01-B: APU FIRE EXTINGUISHER - INOP. APU
- [SDR FDEA202205141205](https://openairdocs.org/sdr/FDEA202205141205.md): Insert · failed · May 14, 2022 · N110FE · Boeing 767300 · Landing Gear Doors
  > FOUND RH MLG FWD DOOR STOP FASTENERS TO BE LOOSE AND SHIM FASTENER HOLES TO BE ELONGATED. REMOVED INSERTS FROM RH MLG FWD DOOR STOP AND REPLACED FASTENERS REF E.A. TH- 3212-T0368483P1 AND REPLACED SHIMS REF 767 SRM 51-20-11 AND 51-20-12.
- [SDR FDEA202205141204](https://openairdocs.org/sdr/FDEA202205141204.md): Insert · failed · May 14, 2022 · N110FE · Boeing 767300 · Landing Gear Doors
  > FOUND LH MLG FWD DOOR STOP FASTENERS TO BE LOOSE AND SHIMS TO HAVE MIGRATED. REMOVED INSERTS FROM LH MLG FWD DOOR STOP AND REPLACED FASTENERS REF E.A. TH- 3212-T0368483P1 AND REPLACED SHIMS REF 767 SRM 51-20-11 AND 51-20-12.
- [SDR FDEA202111242929](https://openairdocs.org/sdr/FDEA202111242929.md): None · none · Nov 24, 2021 · N110FE · Boeing 767300 · Emergency Lighting
  > MDIS 110 33-50 7324 24NOV21 CDG FACT U EMERGENCY LIGHT GUARD IS BROKEN. FACT 24NOV21 03:19 CDG U R&R'D EMERGENCY LIGHT GUARD PER MM:33-51-08-4, OPS CHK OK.
- [SDR FDEA202104271048](https://openairdocs.org/sdr/FDEA202104271048.md): Engine · overtemp · Apr 27, 2021 · N110FE · Boeing 767300 · Engine Oil Temperature
  > STARTED DESCENT FROM FL 310, THE OIL TEMP SPIKED UP TO 165 ON THE LT ENGINE. THROTTLE WAS PULLED TO IDLE, & CHECKLIST RUN FOR HIGH OIL TEMP, LT ENGINE. OIL QUANTITY INDICATED 0 (ZERO). AFTER 7 MINUTES OIL TEMP REDUCED BELOW AMBER BAND. ENGINE REMAINED AT
- [SDR FDEA202012153166](https://openairdocs.org/sdr/FDEA202012153166.md): Floor Panel · delaminated · Dec 15, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241YFA MISSING EDGE FILLER AT LBL 54. FABRICATED NEW FLOOR PANEL 241YFA, IAW FEDEX DWG SRZ-25-005 REV C.
- [SDR FDEA202012153167](https://openairdocs.org/sdr/FDEA202012153167.md): Floor Panel · delaminated · Dec 15, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242SFF HAS SEVERAL AREAS OF DELAMINATION AND CRUSH DAMAGE AROUND FLOOR FITTING CUTOUTS. FABRICATED NEW FLOOR PANEL 241SFF, IAW FEDEX DWG SRZ-25-005, REV R.
- [SDR FDEA202012153165](https://openairdocs.org/sdr/FDEA202012153165.md): Floor Panel · delaminated · Dec 15, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242TFA IS PUNCTURED TWO PLACES. FABRICATED NEW FLOOR PANEL 242TFA, IAW FEDEX DWG SRZ-25-005, REV R.
- [SDR FDEA202012153164](https://openairdocs.org/sdr/FDEA202012153164.md): Floor Panel · delaminated · Dec 15, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241ZFF HAS CRUSH AND DELAM DAMAGE, SEVERAL AREAS ALONG THE ENTIRE LENGTH. FABRICATED NEW FLOOR PANEL 241ZFF, IAW FEDEX DWG SRZ-25-005, REV R.
- [SDR FDEA202012153163](https://openairdocs.org/sdr/FDEA202012153163.md): Floor Support · cracked · Dec 15, 2020 · N110FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > RT AFT FUSELAGE, AFT CARGO BS 1576 RBL 78, MAIN CARGO DECK FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE RIGHT AFT FUSELAGE MAIN CARGO DECK FLOOR SUPPORT SPLICE ANGLE AT STA 1576 AND RBL 78, IAW BAC DWG 146T5650, REV C AND B767 SRM 51-40-02-0G.
- [SDR FDEA202012153162](https://openairdocs.org/sdr/FDEA202012153162.md): Floor Support · cracked · Dec 15, 2020 · N110FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > LT AFT FUSELAGE, AFT CARGO BS 1576 LBL 78, MAIN CARGO DECK FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE LEFT AFT FUSELAGE MAIN CARGO DECK FLOOR SUPPORT SPLICE ANGLE AT STA 1576 AND LBL 78, IAW BAC DWG 146T5650, REV C AND B767 SRM 51-40-02-0G.
- [SDR FDEA202012093082](https://openairdocs.org/sdr/FDEA202012093082.md): Skin · chafed · Dec 9, 2020 · N110FE · Boeing 7673S2F · Leading Edge Devices
  > RIGHT WING NR 9 SLAT LOWER TRAILING EDGE WEDGE SKIN CHAFED. REPAIRED NR 9 SLAT RIGHT WING LOWER TRAILING EDGE WEDGE 33.75" FROM INBOARD END BY BONDING FILLER SKIN, INTERNAL DOUBLER, CORE, FIBERGLASS WEDGE AND EXTERNAL DOUBLER, IAW B767 SRM: 57-43-02-2R REPAI
- [SDR FDEA202012083072](https://openairdocs.org/sdr/FDEA202012083072.md): Floor Panel · delaminated · Dec 8, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241NFF HAS BROKEN INSERTS AND DELAMINATION DAMAGE ALONG THE FORWARD EDGE. FABRICATED NEW MAIN CABIN FLOOR PANEL 241NFF, IAW FEDEX DWG SRZ-25-005 REV R.
- [SDR FDEA202012083071](https://openairdocs.org/sdr/FDEA202012083071.md): Floor Panel · damaged · Dec 8, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241JFF HAS CRUSH AND DELAMINATION DAMAGE ALONG THE LBL 55 SIDE, ENTIRE LENGTH. FABRICATED NEW MAIN CABIN FLOOR PANEL 241JFF, IAW FEDEX DWG SRZ-25-005, REV R.
- [SDR FDEA202012083070](https://openairdocs.org/sdr/FDEA202012083070.md): Floor Panel · damaged · Dec 8, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241WFF HAS THREE SEPARATE AREAS OF DAMAGE. REPAIRED 3 EA DAMAGE AREAS ON FLOOR PANEL 241WFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202012073171](https://openairdocs.org/sdr/FDEA202012073171.md): Beam · damaged · Dec 7, 2020 · N110FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame
  > NR 2 PYLON INBOARD SKIRT BEAM FWD FLANGE HAS ELONGATED HOLES. REPAIRED ELONGATED HOLES ON NR 2 PYLON INBOARD SKIRT BEAM FWD FLANGE, IAW FEDEX EA H-5450-T0358609-P1.
- [SDR FDEA202012073056](https://openairdocs.org/sdr/FDEA202012073056.md): Floor Panel · damaged · Dec 7, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241HFF HAS MISSING EDGE FILLER SEVERAL AREAS. REPAIRED EDGE FILLER ON FLOOR PANEL 241HFF, IAW B767 SRM 53-00-50-2R PARA 4G (2).
- [SDR FDEA202012063051](https://openairdocs.org/sdr/FDEA202012063051.md): Angle · cracked · Dec 6, 2020 · N110FE · Boeing 7673S2F · Fuselage Main, Floor Beam
  > FWD LT FRAME STA 246 LBL 50 BELOW FLOOR INTERCOSTAL ANGLE CRACKED. REMOVED AND REPLACED ANGLE P/N 141T5146-16, IAW B767 SRM 51-40-02 AND BAC DWG 141T5600 REV-.
- [SDR FDEA202012053039](https://openairdocs.org/sdr/FDEA202012053039.md): Floor Panel · delaminated · Dec 5, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242BFA IS PUNCTURED TWO PLACES. REPAIRED DAMAGES TO FLOOR PANEL 242BFA, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202012053038](https://openairdocs.org/sdr/FDEA202012053038.md): Floor Panel · delaminated · Dec 5, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241LFF PUNCTURED TWO PLACES AND HAS MISSING EDGE FILLER. REPAIRED DAMAGES TO FLOOR PANEL 241LFF, IAW B767 SRM 53-00-50-2R, PARA 4C AND 4G (2).
- [SDR FDEA202012053037](https://openairdocs.org/sdr/FDEA202012053037.md): Floor Panel · delaminated · Dec 5, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241FFF PUNCTURED THREE PLACES. REPAIRED DAMAGES TO FLOOR PANEL 241FFF, IAW B767 SRM 53-00-50-2R, PARA 4D AND 4E.
- [SDR FDEA202012053036](https://openairdocs.org/sdr/FDEA202012053036.md): Floor Panel · delaminated · Dec 5, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242VFF HAS A PUNCTURE. REPAIRED FLOOR PANEL 242VFF, IAW B767 SRM 53-00-50-2R, PARA 4D.
- [SDR FDEA202012053035](https://openairdocs.org/sdr/FDEA202012053035.md): Floor Panel · delaminated · Dec 5, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242HFF IS PUNCTURED, MARKED. REPAIRED FLOOR PANEL 242HFF, IAW B767 SRM 53-00-50-2R, PARA 4C.
- [SDR FDEA202012053033](https://openairdocs.org/sdr/FDEA202012053033.md): Floor Panel · delaminated · Dec 5, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241KFF IS DAMAGED AT 3 SEPARATE AREAS, MARKED. REPAIRED 3 EA DAMAGES ON FLOOR PANEL 241KFF, IAW B767 SRM 53-00-50-2R, PARA 4C AND 4D.
- [SDR FDEA202012053032](https://openairdocs.org/sdr/FDEA202012053032.md): Floor Panel · delaminated · Dec 5, 2020 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241QFF HAS PUNCTURE DAMAGE, MARKED. REPAIRED FLOOR PANEL 241QFF, IAW B767 SRM 53-00-50-2R, PARA 4D.
- [SDR FDEA2020080751775](https://openairdocs.org/sdr/FDEA2020080751775.md): Drive Unit · malfunctioned · Aug 5, 2020 · N110FE · Boeing 7673S2F · Weather Radar System
  > WX FAIL ON EITHER SELECTED ON LT OR RT CTR CONTROL PANEL ON CENTER PEDESTAL. WINDSHEAR SYS EICAS LT WAS ALSO PRESENT DURING ENROUTE PHASE OF FLIGHT. R & R THE WEATHER RADAR ANTENNA DRIVE UNIT IAW AMM 34-43-05-47. A/C OK FOR SERVICE
- [SDR FDEA201804281143](https://openairdocs.org/sdr/FDEA201804281143.md): Lamp · inoperative · Apr 28, 2018 · N110FE · Boeing 7673S2F · Landing Gear Position and Warning
  > DURING APPROACH, THE LEFT LANDING GEAR LIGHT DID NOT ILLUMINATE. ACCOMPLISHED GO AROUND, QRH AND MOCC/GOC. GEAR CYCLED, DID NOT HELP. NO SECONDARY OR TERTIARY WARNING. NO EICAS WARNINGS. LANDING UNEVENTFUL. REPLACED THE LAMP IN THE INDICATOR IAW AMM 3
- [SDR FDEA201710052868](https://openairdocs.org/sdr/FDEA201710052868.md): Floor Panel · damaged · Oct 5, 2017 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > INCOMING DISCREPANCY WRI 53-21/2521, AFT PIT FLOOR PANEL STA 1197 DAMAGED. REMOVED AND REPLACED FLOOR BOARD ON WORK ORDER 00069928 SEQ 000807.
- [SDR FDEA201710042851](https://openairdocs.org/sdr/FDEA201710042851.md): Floorboard · gouged · Oct 4, 2017 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > IN LOWER AFT CARGO FOUND DAMAGE ON CARGO FLOOR BOARD AT STATION 1197 70 MEASURING 3 1/2" LONG X 3/4" WIDE. REMOVED DAMAGED AFT PIT FLOORBOARD PER SRM 51-40-02-06. FABRICATED NEW PANEL ON T17/1299248 PER SRZ-25-005. MAJOR REPAIR CAT A. INSTALLED FLOOR PANEL PER
- [SDR FDEA201710032847](https://openairdocs.org/sdr/FDEA201710032847.md): Floor Panel · gouged · Oct 3, 2017 · N110FE · Boeing 767300 · Fuselage Floor Panel
  > LOAD CREW REPORTS A GOUGE IN THE FIBERGLASS FLOOR PANEL OF THE AFT PIT AT STA 1197, ON THE OUTBOARD EDGE OF THE RIGHT SIDE PANEL. GOUGE IS APPROX 1 INCH LONG AND LESS THAN ONE INCH ACROSS. REMOVED DAMAGED FLOOR PANEL PER SRM 51-40-02-06. FABRICATED NEW PANEL O
- [SDR FDEA201710032845](https://openairdocs.org/sdr/FDEA201710032845.md): Floorboard · cracked · Oct 3, 2017 · N110FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOORBOARD 145T5876-94 CRACKED EDGES. FABRICATED FLOORBOARD 242FF 145T5876-94 ON T17/1299306 PER SRZ-25-005 REV M MAJOR REPAIR CAT A.
- [SDR FDEA201606232114](https://openairdocs.org/sdr/FDEA201606232114.md): Latch · damaged · Jun 23, 2016 · N110FE · Boeing 7673S2F · Emergency Equipment
  > ON PREFLIGHT, FOUND LATCH HANDLE ON EMERGENCY RAFT LOCKER JAMMED, PREVENTING ACCESS. COMPLIED WITH EA H-2560-T0326232 REV NO A POS P3, R&R THE LATCH ON THE LIFE RAFT STORAGE COVER PER SMP.
- [SDR FDEA201511183705](https://openairdocs.org/sdr/FDEA201511183705.md): Light · inoperative · Nov 18, 2015 · N110FE · Boeing 7673S2F · Emergency Lighting
  > FUSELAGE MOUNTED EMER EXIT LIGHT INOPERATIVE. RELAMPED FUSELAGE MOUNTED EMER EXIT LIGHT. OPERATIONS CHECKED OK.

## 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 = 'N110FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N110FE/reports

---
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