# Service difficulty reports: N140FE

A list on [N140FE](https://openairdocs.org/aircraft/N140FE.md).

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

- [SDR FDEA202607100891](https://openairdocs.org/sdr/FDEA202607100891.md): Skin · dented · Jul 10, 2026 · N140FE · Boeing 767300 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (P/N 141T3221-7 (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE D
- [SDR FDEA202607100889](https://openairdocs.org/sdr/FDEA202607100889.md): Skin · unknown · Jul 10, 2026 · N140FE · Boeing 767300 · Leading Edge Devices
  > NEED TO REPAIR DAMAGE ON #4 SLAT, OTBD CLOSURE PANEL (MPN: 114T4151-7) AT OSS 641. REPAIRED #4 SLAT OTBD CLOSE OUT PANEL AT OSS 641 MPN# 114T4104-407G SN# 000359 IN REF TO B767 SRM 57-43-01-2R FIG 201 SHT. 3, REPAIR 2 AND B767 SRM 51-70-07-0G PAR. 5.G. SEE J
- [SDR FDEA202607100888](https://openairdocs.org/sdr/FDEA202607100888.md): Skin · delaminated · Jul 10, 2026 · N140FE · Boeing 767300 · Leading Edge Devices
  > NEED TO REPAIR DAMAGE ON #4 SLAT, INBD CLOSURE PANEL (MPN: 114T4151-5) AT OSS 572. REPAIRED #4 SLAT INBD CLOSE OUT PANEL AT OSS 572 MPN# 114T4104-407G SN# 000359 IN REF TO B767 SRM 57-43-01-2R FIG 201 SH 3 REPAIR 2 AND B767 SRM 51-70-07-0G PAR. 5.G. SEE JPF
- [SDR FDEA202607090869](https://openairdocs.org/sdr/FDEA202607090869.md): Skin · dented · Jul 9, 2026 · N140FE · Boeing 7673S2F · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE DENT WAS MEASURED A
- [SDR FDEA202607090868](https://openairdocs.org/sdr/FDEA202607090868.md): Skin · cracked · Jul 9, 2026 · N140FE · Boeing 7673S2F · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (P/N 141T3221-7 (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE D
- [SDR FDEA202606300821](https://openairdocs.org/sdr/FDEA202606300821.md): Floor Panel · punctured · Jun 30, 2026 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT,L/H FLOOR PANEL 231QFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 231QFF, MPN: 143T5876-19, LBL 9.13 LBL 77.5, STA 654.22-784.22 IN REF.TO BOEING DWG 143T5876-19, AND SR67-53-009. THIS IS A MAJOR REPAIR.
- [SDR FDEA202606270812](https://openairdocs.org/sdr/FDEA202606270812.md): Floor Panel · punctured · Jun 27, 2026 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, L/H FLOOR PANEL 241KFFHAS PUNCTURE DAMAGE. JM10 FABRICATED NEW FLOOR PANEL 241KFF, MPN: 145T5876-8, LBL 77.5 - LBL 89.5, STA 821 - 933 IN REF. TO BOEING DWG 145T5876-8, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS
- [SDR FDEA202606270811](https://openairdocs.org/sdr/FDEA202606270811.md): Floor Panel · damaged · Jun 27, 2026 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, R/H OUTBD FLOOR PANEL 232NFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 232NFF, RBL 86.5 - RBL 77.5, BS 654 22 - 675 IAW DWG 143T5876-20, AND SRM 67-53-009. PERFORMED. THIS IS A MAJOR REPAIR. FOR INSTALLATION OF THIS PANE
- [SDR FDEA202606260809](https://openairdocs.org/sdr/FDEA202606260809.md): Floor Panel · delaminated · Jun 26, 2026 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251BFF DENTED WITH DELAMINATION. JM11 REPAIRED FLOOR PANEL 251BFF, MPN: 146T5869-155, LBL 11- LBL 33, BS 1160-11166 IAW SRM 53-00-50-2R, FIG 201, REPAIR 1 SHT 1, AND DWG 146T5869-155. THIS IS A MAJOR REPAIR. THIS FLOOR
- [SDR FDEA202606260808](https://openairdocs.org/sdr/FDEA202606260808.md): Floor Panel · damaged · Jun 26, 2026 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, CENTER FLOOR PANEL 251LFF HAS PUNCTURE DAMAGE. REPAIRED FLOOR PANEL 251LFF, RBL 11- LBL 11, BS 1263-1267 IAW SRM 53-00-50-2R, FIG 201, REPAIR 1 SHT 1, AND DWG 146T5869-127. THIS IS A MAJOR REPAIR. THIS FLOOR PANEL WAS REPAIR
- [SDR FDEA202407080971](https://openairdocs.org/sdr/FDEA202407080971.md): Skin · delaminated · Jul 8, 2024 · N140FE · Boeing 7673S2F · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION AT 60" FROM OUTBOARD FITTING NO 1. LEFT WING OUTBOARD FLAP LEADING EDGE AT 60" FROM OUTBOARD FITTING NO 1 WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE I AND SRM 51-70-03-0G PAR 5.A FIG 9 REV 88 DEC 15
- [SDR FDEA202407080970](https://openairdocs.org/sdr/FDEA202407080970.md): Floor Panel · cracked · Jul 8, 2024 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, SEC 46, FLOOR PANEL 251FFF WITH HOLE. MAIN DECK CARGO COMPARTMENT, SEC 46 FLOOR PANEL 251FFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023
- [SDR FDEA202407080969](https://openairdocs.org/sdr/FDEA202407080969.md): Floor Panel · cracked · Jul 8, 2024 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, SEC 46, FLOOR PANEL 251EFF WITH PUNCTURE. MDC, SEC 46, FLOOR PANEL 251EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023
- [SDR FDEA202407080968](https://openairdocs.org/sdr/FDEA202407080968.md): Floor Panel · cracked · Jul 8, 2024 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, SEC 43, FLOOR PANEL 241DFF WITH PUNCTURE. MDC, SEC 43, FLOOR PANEL 241DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023
- [SDR FDEA202407080966](https://openairdocs.org/sdr/FDEA202407080966.md): Floor Panel · cracked · Jul 8, 2024 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, SEC 43, FLOOR PANEL 241AFF BROKEN. MAIN DECK CARGO COMPARTMENT SEC 43 FLOOR PANEL 241AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023
- [SDR FDEA202206271579](https://openairdocs.org/sdr/FDEA202206271579.md): Flap · delaminated · Jun 27, 2022 · N140FE · Boeing 767300 · Trailing Edge Flaps
  > RH WING OUTBOARD FLAP WITH DELAMINATION ON LEADING EDGE WBL: 379. R.H. WING OUTBOARD FLAP ON LEADING EDGE, OUTER SKIN, WBL: 379 WAS REPAIRED I.A.W. B767 S.R.M. 57-53-01-2R PAGE 1-5 FIG 201 SHEET 1, 3, 5 AND S.R.M. 51-70-17-0G FIG 10 SHEET 1 PARA. 4.A. PAGE
- [SDR FDEA202206271578](https://openairdocs.org/sdr/FDEA202206271578.md): Flap · delaminated · Jun 27, 2022 · N140FE · Boeing 767300 · Trailing Edge Flaps
  > RH WING OUTBOARD FLAP L.E. NEAR TO IB EDGE - PREVIOUSLY REPAIR DELAMINATED. R.H. WING OUTBOARD FLAP L.E. NEAR TO INBD EDGE, OUTER SKIN WAS REPAIRED I.A.W. B767 S.R.M. 57-53-01-2R PAGE 1-5 FIG 201 SHEET 1, 3, 5 AND S.R.M. 51-70-17-0G FIG 10 SHEET 1 PARA. 4.
- [SDR FDEA202204281084](https://openairdocs.org/sdr/FDEA202204281084.md): Panel · delaminated · Apr 28, 2022 · N140FE · Boeing 767300 · Wing, Plate/Skin
  > LH WING - LEADING EDGE STRUCTURE UPPER SURFACE SKIN PANELS AT LOCATION OF ENGINE PYLON HAS AN AREA OF THE INBOARD PANEL WITH THE SKIN DELAMINATED. REPLACED PANEL USING BOEING DRW 114T6104 AND 767 SRM 51-40-03-0G-0.
- [SDR FDEA202204281078](https://openairdocs.org/sdr/FDEA202204281078.md): Former · cracked · Apr 28, 2022 · N140FE · Boeing 767300 · Leading Edge Devices
  > R/H WING LEADING EDGE AT WS 499 (SLAT # 8) HAS A CRACKED FORMER. REPLACED CRACKED FORMER REF E.A. H-5720-T0368255 P1.
- [SDR FDEA202007091478](https://openairdocs.org/sdr/FDEA202007091478.md): Ceiling Panel · cracked · Jul 9, 2020 · N140FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > FWD CARGO BAY CEILING PANEL CRACKED AND BROKEN AT CENTER OF CARGO DOOR. REPAIRED THE CEILING PANEL IAW AMM 25-52-10-8 AND RESTORED FINISH IAW AMM 25-00-00-7.
- [SDR FDEA202007081464](https://openairdocs.org/sdr/FDEA202007081464.md): Floor Panel · damaged · Jul 8, 2020 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 241FFF DAMAGED REPAIRED FLOOR PANEL 241FFF BY FABRICATION IAW B767 SRZ-25-005 REV: R MAJOR REPAIR
- [SDR FDEA202007081463](https://openairdocs.org/sdr/FDEA202007081463.md): Floor Panel · damaged · Jul 8, 2020 · N140FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 241JFF DAMAGED REPAIRED FLOOR PANEL 241JFF BY FABRICATION IAW B767 SRZ-25-005 REV: R MAJOR REPAIR
- [SDR FDEA202007061450](https://openairdocs.org/sdr/FDEA202007061450.md): Skin · dented · Jul 6, 2020 · N140FE · Boeing 7673S2F · Spoilers
  > RIGHT WING SPLR NR 12 UPPER O/B SURFACE HAS A DENT. REPAIRED RIGHT WING SPLR NR 12 UPPER SURFACE O/B DENT IAW SRM 57-70-01-0I, 57-70-01-1A, 57-70-01-2R AND 51-73-03-0G. RESTORED FINISH IAW AMM 51-21-10.
- [SDR FDEA202007061448](https://openairdocs.org/sdr/FDEA202007061448.md): Skin · chafed · Jul 6, 2020 · N140FE · Boeing 7673S2F · Leading Edge Devices
  > LEFT WING NR 5 SLAT T/E LOWER SURFACE HAS CHAFING MARK. REPAIRED LT WING NR 5 SLAT T/E LOWER SURFACE CHAFING IAW SRM 57-53-02-2R AND 51-70-10-2R.
- [SDR FDEA202001050021](https://openairdocs.org/sdr/FDEA202001050021.md): Skin · dented · Jan 5, 2020 · N140FE · Boeing 7673S2F · Trailing Edge Flaps
  > MAINT FOUND A MINOR DENT OF THE LE OF THE RH OUTBOARD FLAP; ABOUT 4" LONG X 1" WIDE REPAIRED AREA USING EA H-5750-T0351730 PART 1,
- [SDR FDEA2020010650021](https://openairdocs.org/sdr/FDEA2020010650021.md): Skin · dented · Jan 5, 2020 · N140FE · Boeing 7673S2F · Trailing Edge Flaps
  > MAINT FOUND A MINOR DENT OF THE LE OF THE RH OUTBOARD FLAP; ABOUT 4" LONG X 1" WIDE REPAIRED AREA USING EA H-5750-T0351730 PART 1,
- [SDR FDEA201905261173](https://openairdocs.org/sdr/FDEA201905261173.md): Unknown · malfunctioned · May 26, 2019 · N140FE · Boeing 7673S2F · Altimeter, Barometric/Encoder
  > PDIS 140 34-10 2316 26MAY19 MEM OPEN U LOGPAGES:2923349 "ALT DISAGREE" EICAS WARNING IN DESCENT. F/O AND CAPT ALTIMETERS HAD 250 FT DIFFERENCE. AT ALTITUDE THE SPLIT WAS 180 FT, BUT "ALT DISAGREE" EICAS IN CRUISE, FL360. PERFORMED PITOT STATI
- [SDR FDEA201905231124](https://openairdocs.org/sdr/FDEA201905231124.md): Probe · defective · May 23, 2019 · N140FE · Boeing 7673S2F · Pitot/Static System
  > ON T/O ROLL CAPT AIRSPEED ERRATIC THEN BACK TO 30KTS AFTER LIFTOFF EICAS L & R EEC, AILERON LOCKOUT, RUDDER RATIO, AUTOTHROTTLES CLICKED OFF, F/O'S FLT DIR WENT OFF, CAPT RESET AND IT CAME BACK. CAPT'S AIRSPEED AND STBY AIRSPEED STAYED @ 30KTS. RTB. FOUND C
- [SDR FDEA201905171091](https://openairdocs.org/sdr/FDEA201905171091.md): Tire · punctured · May 17, 2019 · N140FE · Boeing 7673S2F · Tire
  > RIGHT NOSE TIRE FLAT, ZERO PSI DUE TO F.O.D. PUNCTURE, WAS FLAT ON ARRIVAL TO RDU. REMOVED AND REPLACED RT NOSE TIRE ASSY. REF. MM 32-45-02-4-0. SEE WRI 32-41-2281 FOR LEFT TIRE R&R. A/C OK FOR SERVICE.
- [SDR FDEA2018102973024](https://openairdocs.org/sdr/FDEA2018102973024.md): Cover · damaged · Oct 27, 2018 · N140FE · Boeing 7673S2F · Emergency Equipment
  > PDIS 140 25-60 1825 02OCT18 MEM FACT U LOGPAGES:2851938 ENTRY DOOR ESCAPE ROPE IS PARTIALLY DEPLOYED. OIL 02OCT18 04:30 MEM U NO RESTRICTION - ITEM DEFERRED PER THE NEF PROGRAM ITEM DEFERRED PER THE NEF: 25-10-26 ESCAPE ROPE/DESCENT DEVICE STOWAGE COVER (IF IN
- [SDR FDEA201810022764](https://openairdocs.org/sdr/FDEA201810022764.md): Escape Rope · partial deploy · Oct 2, 2018 · N140FE · Boeing 7673S2F · Emergency Equipment
  > PDIS 140 25-60 1825 02OCT18 MEM ENTRY DOOR ESCAPE ROPE IS PARTIALLY DEPLOYED. RE-INSTALLED ESCAPE ROPE IN REF TO AMM 25-61-04-2-1.
- [SDR FDEA2018082182106](https://openairdocs.org/sdr/FDEA2018082182106.md): Skin · punctured · Aug 18, 2018 · N140FE · Boeing 7673S2F · Trailing Edge Flaps
  > SMALL PUNCTURE ON THE UPPER SURFACE SKIN OF THE LT INBOARD MAIN FLAP, IFS 256. REMOVED DAMAGE AND REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, AND 51-70-17-0G.
- [SDR FDEA201706061582](https://openairdocs.org/sdr/FDEA201706061582.md): Control Lever · malfunctioned · Jun 6, 2017 · N140FE · Boeing 7673S2F · Landing Gear Retraction/Extension System
  > ON DEPARTURE, PILOT FLYING CALLED FOR GEAR UP, MOVED GEAR LEVER TO THE UP POSITION. ALL INDICATIONS NORMAL. AFTER TO CHECKLIST, MOVED GEAR LEVER TO OFF POSITION AND GEAR EXTENDED, AFTER FULL GEAR EXTENSION RECEIVED 2 GEAR DISAGREE EICAS WITH NOSE AND RT G

## 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 = 'N140FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N140FE/reports

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