# Service difficulty reports: N165FE

A list on [N165FE](https://openairdocs.org/aircraft/N165FE.md).

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

- [SDR FDEA202604300528](https://openairdocs.org/sdr/FDEA202604300528.md): Skin · delaminated · Apr 30, 2026 · N165FE · Boeing 7673S2F · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP LEADING EDGE PANEL HAS SMALL AREA OF DELAM REPAIRED AREA OF (33.5" X 7") ON R/H WING O/B T/E FLAP I/B L/E PNL# 113T3110-402G IN REF TO B767 SRM 57-53-01-2R FIG 201 SHEET 5 REPAIR 1 & B767 SRM 51-70-05-0G. SEE JPF FOR ALL WORK ACCOM
- [SDR FDEA202604300527](https://openairdocs.org/sdr/FDEA202604300527.md): Skin · delaminated · Apr 30, 2026 · N165FE · Boeing 7673S2F · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP LEADING EDGE PANEL JUST INBOARD OF INBOARD FLAP FAIRINGS HAS POSSIBLE DELAMINATION REPAIRED AREA OF (33" X 7") ON R/H WING O/B T/E FLAP I/B L/E PNL# 113T3110-402G IN REF TO B767 SRM 57-53-01-2R FIG 201 SHEET 5 REPAIR 1 & B767 SRM 5
- [SDR FDEA202604250501](https://openairdocs.org/sdr/FDEA202604250501.md): Floor Panel · damaged · Apr 25, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOORBOARD 242TFA HAS HOLES. FABRICATED FLOOR PANEL 242TFA, RBL 33- RBL 54.75, STA. 961-1087 IAW SRM 53-00-50-2R, FIG 201, SHEET 2, AND DWG 145T5876-96. THIS IS A MAJOR REPAIR. THE INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED ON WO 91959 SEQ 114.
- [SDR FDEA202604210491](https://openairdocs.org/sdr/FDEA202604210491.md): Floor Panel · dented · Apr 21, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT FLOOR PANEL 232PFF DENTED WITH DELAMINIATION JM21. FABRICATE NEW FLOOR PANEL 231PFF REF WG 143T5876-129, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED
- [SDR FDEA202604210490](https://openairdocs.org/sdr/FDEA202604210490.md): Floor Panel · dented · Apr 21, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222AFF DENTED WITH DELAMINATION. JM13 FABRICATED FLOORPANEL# 222AFF MPN# 141T5856-107 RBL 11- RBL 33 STA: 285-412 IN REF TO BOEING DRAWING 141T5856-107 AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A
- [SDR FDEA202604210489](https://openairdocs.org/sdr/FDEA202604210489.md): Floor Panel · delaminated · Apr 21, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT PANEL 251QFF DENTED WITH DELAMINATION.JM20 REPAIRED FLOOR PANEL 251QFF, MPN: 146T5869-19, LBL 68.50- LBL 77.50, STA. 1208-1353 IN REF. TO B767 SRM 53-00-50-2R, FIG 201, REPAIR 1 SHT 1, AND BOEING DWG# 146T5869-19. THIS IS A MAJO
- [SDR FDEA202604210488](https://openairdocs.org/sdr/FDEA202604210488.md): Floor Panel · punctured · Apr 21, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT, FLOOR PANEL 251UFF HAS PUNCTURE DAMAGE.JM19 REPAIRED FLOOR PANEL 251UFF, MPN: 146T5869-163, LBL 54.75- LBL 77.50, STA. 1353-1430 IN REF. TO B767 SRM 53-00-50-2R, FIG 201, REPAIR 1 SHT 1, AND BOEING DWG# 146T5869-163. THIS IS A MAJOR
- [SDR FDEA202604190479](https://openairdocs.org/sdr/FDEA202604190479.md): Floor Panel · cracked · Apr 19, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOOR BOARD 241WFF HAS CRACKS FABRICATED NEW FLOOR PANEL 241WFF, MPN: 145T5876-51, LBL11- RBL11, STA 980 -1114.82 IN REF.TO BOEING DWG 145T5876-51, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL
- [SDR FDEA202604190483](https://openairdocs.org/sdr/FDEA202604190483.md): Floor Panel · damaged · Apr 19, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOORBOARD 242TFA HAS A HOLES. FABRICATED FLOOR PANEL 242TFA, MPN: 145T5876-96, RBL 33- RBL 54.75, STA. 961-1087 IN REF. TO B767 SRM 53-00-50-2R, FIG 201, SHEET 2, AND BOEING DWG# 145T5876-96. THIS IS A MAJOR REPAIR. THE INSTALLATION OF THIS PANEL WILL BE
- [SDR FDEA202604190480](https://openairdocs.org/sdr/FDEA202604190480.md): Floor Panel · damaged · Apr 19, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOOR BOARD 242SFF HAS HOLES FABRICATED NEW FLOOR PANEL 242SFF, MPN: 145T5876-104, RBL 11- RBL 33, STA 980 -1114.82 IN REF. TO BOEING DWG 145T5876-104, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL
- [SDR FDEA202604190478](https://openairdocs.org/sdr/FDEA202604190478.md): Floor Panel · damaged · Apr 19, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOOR BOARD 241AGF HAS HOLES FABRICATED NEW FLOOR PANEL 241AGF, MPN: 145T5876-113, LBL 77.5- LBL 87.5, STA 984.95 -1087 IN REF.TO BOEING DWG 145T5876-113, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PA
- [SDR FDEA202604190477](https://openairdocs.org/sdr/FDEA202604190477.md): Floor Panel · punctured · Apr 19, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242VFF HAS PUNCTURE DAMAGE. JM18 FABRICATED NEW FLOOR PANEL 242VFF, MPN: 145T5876-114, RBL 74.25- RBL 84.25, STA 984.95 -1087 IN REF.TO BOEING DWG 145T5876-114, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED.
- [SDR FDEA202604180468](https://openairdocs.org/sdr/FDEA202604180468.md): Floor Panel · damaged · Apr 18, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO DECK, FLOOR PANEL 241PFF DAMAGED FABRICATED NEW FLOOR PANEL 241PFF, MPN: 145T5876-109, LBL 77.5 - LBL 54.75, STA 930-980 IN REF.TO BOEING DWG 145T5876-109, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATIO
- [SDR FDEA202604180467](https://openairdocs.org/sdr/FDEA202604180467.md): Floor Panel · damaged · Apr 18, 2026 · N165FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO DECK, FLOOR PANEL 241LFF DAMAGED FABRICATED NEW FLOOR PANEL 241LFF, MPN: 145T5876-19, LBL 11- RBL 11, STA 930-980 IN REF.TO BOEING DWG 145T5876-19, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS
- [SDR FDEA202404270517](https://openairdocs.org/sdr/FDEA202404270517.md): Warning Message · false activation · Apr 27, 2024 · N165FE · Boeing 7673S2F · Central Warning
  > REJECTED TAKEOFF AT ~35KTS. FOR CONFIG WARNING WITH SPOILERS EICAS. TO CONFIG TESTED NORMALLY PER BEFORE TAKEOFF CHECKLIST. TOGW 282.9. RETURNED TO RAMP. NO FURTHER DEFECTS NOTED. CAN AMM: 05-51-14-2 AMM: 32-41-08-216-001-003 PER AMM 32-41-08-216-001-00
- [SDR FDEA202309241656](https://openairdocs.org/sdr/FDEA202309241656.md): Idg · unknown · Sep 24, 2023 · N165FE · Boeing 767300 · AC Generator-Alternator
  > LEFT GEN. FAILURE AT 80KTS ON TAKEOFF ROLL. REJECTED T/O INSTALLED NEW LH ENG IDG REF MM 24-11-01-4-4. OPS CHECKS NORMAL REF 24-11-00-5. ACFT OK FOR SERVICE.
- [SDR FDEA202207011663](https://openairdocs.org/sdr/FDEA202207011663.md): Cdu · failed · Jul 1, 2022 · N165FE · Boeing 767300 · Flight Management Computing Software System
  > CA S FMC SHORTED (SMOKE) WITH POPPED CIRCUIT BREAKER. R/R CAPT'S CDU IAW BOEING 767 AMM 34-61-02-4, PERFORMED ADJ/TEST IAW AMM 34-61-02-5, ALL INDICATIONS NORMAL, OPS CHK GOOD.
- [SDR FDEA202205161223](https://openairdocs.org/sdr/FDEA202205161223.md): Skin · none · May 16, 2022 · N165FE · Boeing 767300 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 632/654 AND STG 2/3 RH FUSELAGE SKIN BETWEEN STA 632/654 AND STG 2/3 RH WAS REPAIRED. SRM 53-00-01-2R REV 82 DEC 15,2021
- [SDR FDEA202205161222](https://openairdocs.org/sdr/FDEA202205161222.md): Skin · none · May 16, 2022 · N165FE · Boeing 767300 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 220.5 / AND STG 30LH / BL0 FUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 220.5 / AND STGR 30LH WAS REPAIRED IAW E.A # M-5330-T0368423
- [SDR FDEA202101270197](https://openairdocs.org/sdr/FDEA202101270197.md): Rvdt · out of adjust · Jan 27, 2021 · N165FE · Boeing 7673S2F · Trailing Edge Flap Control System
  > ON APP MOVING FLAPS FROM 1 TO 5 TRAILING EDGE FLAP DISAGREE LIGHT. FOLLOWED QRH PROC AND FLAPS MOVED NORMALLY USING ALT FLAP SWITCH, REF WRI 27-50/1886 TSI. PERFORMED STEPS 1 THRU 6 OF TSI. FAULT HISTORY FOUND ON THE FSEU [ L FLAP STAB POS 27-51102. PERFOR

## 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 = 'N165FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N165FE/reports

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