# Service difficulty reports: N143FE

A list on [N143FE](https://openairdocs.org/aircraft/N143FE.md).

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

- [SDR FDEA202607100901](https://openairdocs.org/sdr/FDEA202607100901.md): Skin · worn · Jul 10, 2026 · N143FE · Boeing 767300 · Ailerons
  > RIGHT WING, INBD AILERON, LOWER SURFACE L/E BULLNOSE, INBD SIDE HAS AREA OF WEAR DOWN TO COMPOSITE. MK22 REPAIRED RT WING, INBD AILERON, LOWER SURFACE (PANEL#: 656AB) AT WS 443 IAW SRM 57-60-01-2R FIG 201 REPAIR 1 SH 9. PREPPED AND PAINTED REPAIR IAW AMM 51-
- [SDR FDEA202607100900](https://openairdocs.org/sdr/FDEA202607100900.md): Skin · worn · Jul 10, 2026 · N143FE · Boeing 767300 · Ailerons
  > RIGHT WING, INBD AILERON, LOWER SURFACE L/E BULLNOSE, OUTBD SIDE HAS AREA OF WEAR DOWN TO COMPOSITE. MK21 REPAIRED RT WING, INBD AILERON, LOWER SURFACE (PANEL#: 656AB) AT WS 533 IN REF TO B767 SRM 57-60-01-2R FIG 201 REPAIR 1 SH 9. PREPPED AND PAINTED REPAI
- [SDR FDEA202607100897](https://openairdocs.org/sdr/FDEA202607100897.md): Floor Panel · punctured · Jul 10, 2026 · N143FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231JFF HAS PUNCTURE DAMAGE JM32. REPAIRED FLOOR PANEL 231JFF MPN 143T5876-123 LBL54-LBL77 STA 654 IN REF TO B767 SRM 53- 00-50-2R FIG 201 REPAIR 1 SHEET 1 THIS IS A MAJOR REPAIR THIS FLOOR PANEL WAS REPAIRED ON AIRCR
- [SDR FDEA202607100895](https://openairdocs.org/sdr/FDEA202607100895.md): Floor Panel · punctured · Jul 10, 2026 · N143FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT FLOOR PNL 251HFF HAS PUNCTURE DAMAGE. JM30. REPAIRED FLOOR PANEL 251HFF MPN 146T5869-143 LBL 33-LBL 54 STA 1197 110 IN REF TO B767 SRM 53-00-50-2R FIG 201 REPAIR 1 SHEET 1 THIS IS A MAJOR REPAIR THIS WAS REPAIRED ON AIRCRAFT.
- [SDR FDEA202607100894](https://openairdocs.org/sdr/FDEA202607100894.md): Floor Panel · punctured · Jul 10, 2026 · N143FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DEXJ CARGO COMPARTMENT FLOOR PANEL 241BFF HAS PUNCTURE DAMAGE. JM29. REPAIRED FLOOR PANEL 241BFF MPN145T5876-97 LBL11-LBL33 STA 755 IN REF TO B767 53-00-50- 2R FIG 201, REPAIR 1 SHEET, 2 THIS IS A MAJOR REPAIR THIS FLOOR PANEL WAS REPAIRED ON AIRCRAFT
- [SDR FDEA202607090878](https://openairdocs.org/sdr/FDEA202607090878.md): Floor Panel · punctured · Jul 9, 2026 · N143FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232MFF HAS PUNCTURE DAMAGE. JM25 REPAIRED FLOOR PANEL 232MFF (P/N:143T5876-128) AT APPROXIMATELY AT STA 654 22 THRU 654 88 BETWEEN RBL-55 AND RBL 77. USING B767 SRM 53-00-50-2R FIG. 201. REPAIR 1. SH 1. THIS IS A MAJ
- [SDR FDEA202607090875](https://openairdocs.org/sdr/FDEA202607090875.md): Floor Panel · punctured · Jul 9, 2026 · N143FE · Boeing 76732LF · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, 232NFF HAS PUNCTURE DAMAGE.JM24. REPAIRD FLOOR PANEL 232NFF, RBL77-TO RBL 88 BS 654.22 TO 676 IAW SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 2. MAJOR REPAIR. THIS FLOOR PANEL WAS REPAIRED ON AIRCRAFT.
- [SDR FDEA202607080866](https://openairdocs.org/sdr/FDEA202607080866.md): Floorboard · damaged · Jul 8, 2026 · N143FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241KFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 241KFF, IN REF.TO BOEING DWG 145T5876-89 AND SR67-53-009. MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED ON WO 92384, NR 229.
- [SDR FDEA202607080865](https://openairdocs.org/sdr/FDEA202607080865.md): Floorboard · damaged · Jul 8, 2026 · N143FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242HFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 242HFF, IN REF.TO BOEING DWG 145T5876-14 AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLI
- [SDR FDEA202407271065](https://openairdocs.org/sdr/FDEA202407271065.md): Skin · delaminated · Jul 27, 2024 · N143FE · Boeing 7673S2F · Trailing Edge Flaps
  > LH, WING, OUTBOARD FLAP TRAILING EDGE WITH DELAMINATION AT 42" OF OUTER END LH, WING, OUTBOARD FLAP TRAILING EDGE AT 42" OF OUTER END WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG. 201 SHEET 5 TABLE I AND SRM 51-70-03-0G PAGRAP. 5.A FIG 5 SHEET 1 REV. 89 APR
- [SDR FDEA202407271064](https://openairdocs.org/sdr/FDEA202407271064.md): Floor Panel · dented · Jul 27, 2024 · N143FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPATMENT, STA 764,241AFF FLOOR PANEL WITH DENTS MAIN DECK CARGO COMPATMENT, STA 764,241AFF FLOOR PANEL WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B REV. 89 APR 15/2023
- [SDR FDEA202306171050](https://openairdocs.org/sdr/FDEA202306171050.md): Beam · cracked · Jun 17, 2023 · N143FE · Boeing 767300 · Wing Miscellaneous Structure
  > THIS SDR IS A CORRECTION TO SDR 23-1014 (AS IT CALLED OUT P5 INSTEAD OF P6 OF EO E.O. H- 5720-E0353920 REV A) A DETAILED INSPECTION OF THE 113T1913-24 SUPPORT BEAM AT THE WS 1054 UPPER CHORD ATTACHMENT SHOWED A CRACK INDICATION. REF IN STEP 5.E COMPLIED W
- [SDR FDEA202306171049](https://openairdocs.org/sdr/FDEA202306171049.md): Beam · cracked · Jun 17, 2023 · N143FE · Boeing 767300 · Wing Miscellaneous Structure
  > THIS SDR IS A CORRECTION TO SDR 23-1015 (AS IT CALLED OUT P5 INSTEAD OF P6 OF EO E.O. H- 5720-E0353920 REV A) A DETAILED INSPECTION OF THE 113T1913-26 SUPPORT BEAM AT THE WS 1098 UPPER CHORD ATTACHMENT SHOWED A CRACK INDICATION. REF IN STEP 5.E COMPLIED
- [SDR FDEA202306091015](https://openairdocs.org/sdr/FDEA202306091015.md): Support Beam · cracked · Jun 9, 2023 · N143FE · Boeing 767300 · Wing Miscellaneous Structure
  > A DETAILED INSPECTION OF THE 113T1913-26 SUPPORT BEAM AT THE WS 1098 UPPER CHORD ATTACHMENT SHOWED A CRACK INDICATION. REF IN STEP 5.E COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098
- [SDR FDEA202306091014](https://openairdocs.org/sdr/FDEA202306091014.md): Support Beam · cracked · Jun 9, 2023 · N143FE · Boeing 767300 · Wing Miscellaneous Structure
  > A DETAILED INSPECTION OF THE 113T1913-24 SUPPORT BEAM AT THE WS 1054 UPPER CHORD ATTACHMENT IN STEP 5.C SHOWED CRACK INDICATIONS. COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB
- [SDR FDEA202306091013](https://openairdocs.org/sdr/FDEA202306091013.md): Support Beam · cracked · Jun 9, 2023 · N143FE · Boeing 767300 · Wing Miscellaneous Structure
  > DURING DETAILED INSPECTION OF THE 113T1913-25 SUPPORT BEAM AT THE WS 1098 UPPER CHORD ATTACHMENT CRACKS WERE NOTED. COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136.
- [SDR FDEA202306091012](https://openairdocs.org/sdr/FDEA202306091012.md): Support Beam · cracked · Jun 9, 2023 · N143FE · Boeing 767300 · Wing Miscellaneous Structure
  > DURING DETAILED INSPECTION OF THE 113T1913-23 SUPPORT BEAM AT THE WS 1054 UPPER CHORD ATTACHMENT CRACKS WERE NOTED. COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5): LS WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-01
- [SDR FDEA202306071018](https://openairdocs.org/sdr/FDEA202306071018.md): Support · cracked · Jun 7, 2023 · N143FE · Boeing 767300 · Wing Miscellaneous Structure
  > L/W LWR T/E PANEL 113T1657-21 AFT UPPER SUPPORT CHORD CRACKED AT ATTACH POINTS WS 1072-1127. COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5) & PART 6 (P6): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136; WHICH CALL
- [SDR FDEA202306071017](https://openairdocs.org/sdr/FDEA202306071017.md): Support · cracked · Jun 7, 2023 · N143FE · Boeing 767300 · Wing Miscellaneous Structure
  > L/W LWR. T/E PANEL 113T165-29 UPPER SUPPORT CHORD CRACKED AT ATTACH POINTS WS 1032-1070 COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5) & PART 6 (P6): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136; WHICH CALL FOR
- [SDR FDEA202306071016](https://openairdocs.org/sdr/FDEA202306071016.md): Panel · damaged · Jun 7, 2023 · N143FE · Boeing 767300 · Wing Structure
  > LH WING-OUTBOARD TOP PANEL HAS SEVERAL MISSING RIVETS COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5) & PART 6 (P6): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136; WHICH CALL FOR BOTH SIDES TO HAVE PARTS REPLACE
- [SDR FDEA202304170661](https://openairdocs.org/sdr/FDEA202304170661.md): Unknown · unknown · Apr 17, 2023 · N143FE · Boeing 767 · Trailing Edge Flap Control System
  > ON APPROACH WHILE SELECTING FLAPS 5, GOT EICAS TE FLAP DISAG. COMPLETED QRH, LANDED WITH FLAPS 20. DECLARED EMERGENCY AIRBORNE, CANCELLED EMERGENCY UPON LANDING. APPROACH AND LANDING UNEVENTFUL. TE FLAP DISAG OCCURRED APPROX 2000 FEET ALTITUDE, 200
- [SDR FDEA202209242365](https://openairdocs.org/sdr/FDEA202209242365.md): Transmitter · out of limits · Sep 24, 2022 · N143FE · Boeing 7673S2F · Trailing Edge Flap Control System
  > TE FLAP DISAGREE EICAS AFTER SELECTING FLAPS 5 FROM FLAPS 1. WE VERIFIED FLAP HANDLE WAS SECURELY IN THE FLAPS 5 DETENT; EICAS MESSAGE REMAINED ILLUMINATED. DECLARED EMERGENCY AND COMPLETED QRH PROCEDURES. LANDED FLAPS 20 WITH NO ISSUES. PERFORMED TASK 27
- [SDR FDEA202106221579](https://openairdocs.org/sdr/FDEA202106221579.md): Unknown · malfunctioned · Jun 22, 2021 · N143FE · Boeing 7673S2F · Flight Control System
  > DURING APPROACH, LOWERING FLAPS FROM 20 TO 25, WITH WINGS LEVEL. LT AUTOPILOT USED 2 UNITS LT WING DOWN TO MAINTAIN HEADING. WITH AUTOPILOT DISENGAGED, ACFT HAD A STRONG RT ROLL. 2 UNITS OF LT TRIM REQUIRED FOR TRIMMED FLT. PREFORMED INBD AILERON DROOP CK I
- [SDR FDEA202009142174](https://openairdocs.org/sdr/FDEA202009142174.md): Floor Panel · delaminated · Sep 11, 2020 · N143FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL AT BL-0 AND STA 955 TO 1065 DAMAGED. FABRICATED NEW FLOOR PANEL, IAW FED EX EXPRESS SRZ-25-005.
- [SDR FDEA2020081431880](https://openairdocs.org/sdr/FDEA2020081431880.md): Channel · cracked · Aug 13, 2020 · N143FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > MCD CUTOUT FWD EDGE INTERNAL CLOSE OUT TRIM IS CRACKED AND GOUGED. COMPLIED WITH EA H-5320-T0355840 P1 DATED 8-10-20.
- [SDR FDEA2020072361533](https://openairdocs.org/sdr/FDEA2020072361533.md): Floorbeam · corroded · Jul 16, 2020 · N143FE · Boeing 7673S2F · Fuselage Main, Floor Beam
  > FLOOR BEAM LOWER NUT PLATE STRIP IS CORRODED BS 1681.8 LBL 4 REMOVED AND REPLACED FLOOR BEAM LWR NUTPLATE STRIP AT BS 1681.8 LBL 4 IAW FEDEX B757 SRM 51-40-02 AND DWG 146N5693 REV C
- [SDR FDEA2020071761533](https://openairdocs.org/sdr/FDEA2020071761533.md): Nut Plate · corroded · Jul 16, 2020 · N143FE · Boeing 7673S2F · Fuselage Main, Floor Beam
  > FLOORBEAM LOWER NUT PLATE STRIP WAS CORRODED AT BS 1681.8, LBL 4. REMOVED AND REPLACED THE FLOORBEAM LWR NUTPLATE STRIP IAW SRM 51-40-02, AND DWG 146N5693, REV C.
- [SDR FDEA2020062541330](https://openairdocs.org/sdr/FDEA2020062541330.md): Unknown · odor · Jun 24, 2020 · N143FE · Boeing 7673S2F · Flight Compartment Lighting
  > EXPERIENCED STRONG, BURNING SMELL WHEN LOGO LIGHT DEPRESSED. COMPLIED WITH REQUIREMENTS SPELLED OUT WITHIN ENGINEERING REQUEST SYSTEM (ERS 20-02266) AND OBSERVED NO SIGNS OF ANY BURNING OR ARCHING WITH ANY OF THE COMPONENTS REQUESTED TO INSPECT PER WDM 33-13.
- [SDR FDEA202006191285](https://openairdocs.org/sdr/FDEA202006191285.md): Transformer · contaminated · Jun 19, 2020 · N143FE · Boeing 7673S2F · Indicating/Recording System
  > FO'S EFB POWER PACK STARTED TO SMOKE AFTER GETTING WET BY AIRCRAFT DISINFECT (SPRAY BOTTLE LEAKED ON IT). PERFORMED INSPECTION OF SMOKE IN CABIN IAW MM 05-51-56-2. FOUND EFB POWER TRANSFORMER WET, REMOVED EFB TRANSFORMER FROM A/C. CAREFULLY PLUGGED TRANSFOR
- [SDR FDEA2020050870911](https://openairdocs.org/sdr/FDEA2020050870911.md): Light · inoperative · May 7, 2020 · N143FE · Boeing 7673S2F · Landing Gear Position and Warning
  > WHEN GEAR SELECTED DOWN GOT NO SAFE INDICATION ON THE LEFT MAIN GEAR. PERFORMED G/A AND PUT NEW BULB WHICH GAVE A SAFE DOWN AND LOCKED INDICATION. RELAMPED LEFT MAIN LANDING GEAR INDICATOR. LEFT MAIN LANDING GEAR INDICATION OP CK'D NORMAL AFTER BEING REL
- [SDR FDEA2020050420877](https://openairdocs.org/sdr/FDEA2020050420877.md): Seal · missing · May 2, 2020 · N143FE · Boeing 7673S2F · Leading Edge Devices
  > #12 SLAT LOWER SEAL STRIP IS MISSING ON INBD SIDE. *************************************************** DIMENSIONS ON MISSING PIECE IS 28.5" X 1.5" REMOVED AND REPLACED # 12 SLAT LOWER SEAL STRIP COMPLIED WITH E.A. # H-2780-T0353740-P.3 TITLE- FLIGHT CO

## 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 = 'N143FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N143FE/reports

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