# Service difficulty reports: N281FE

A list on [N281FE](https://openairdocs.org/aircraft/N281FE.md).

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

- [SDR FDEA202609301455](https://openairdocs.org/sdr/FDEA202609301455.md): Fseu · failed · Sep 30, 2026 · N281FE · Boeing 767300 · Trailing Edge Flap Control System
  > DURING APPROACH, WHEN CONFIGURING FROM FLAPS 1 TO 5, RECEIVED TRAILING EDGE FLAP DISAGREE. FLAP INDICATOR STAYED AT FLAPS 1 WITH THE FLAP HANDLE IN FLAPS 5 DETECT. COMPLIED WITH QRH. USING ALTERNATE SYS CONFIGURED TO FLAPS 20 FOR LANDING IAW QRH GUIDANCE. RE
- [SDR FDEA202609291450](https://openairdocs.org/sdr/FDEA202609291450.md): Flap System · faulted · Sep 29, 2026 · N281FE · Boeing 767300 · Trailing Edge Flap Control System
  > DURING APPROACH, CONFIGURING FLAPS 1 TO FLAPS 5, RECEIVED T/E FLAP DISAGREE. FLAP IND STAYED AT FLAPS 1 WITH FLAP HANDLE IN FLAPS 5 DETECT. COMPLIED WITH QRH. USING ALT SYS CONFIGURED TO FLAPS 20 FOR LANDING IAW QRH. CLEARED STORED FAULTS ON FSEU,PERFORMED OP
- [SDR FDEA202609151351](https://openairdocs.org/sdr/FDEA202609151351.md): Flap System · faulted · Sep 15, 2026 · N281FE · Boeing 767300 · Trailing Edge Flap Control System
  > GOT TRAILING EDGE FLAP DISAGREE LIGHT,WE DID A GO AROUND, DURING THE PROCESS OF GETTING THE CHECKLIST OUT THE FLAPS STARTED TO FUNCTION NORMALLY, RETURNED TO THE FIELD. AMM: 27-51-00 IAW M/M 27-51-00-5 CYCLED FLAPS OPERATION AND INDICATIONS WERE NORMAL.
- [SDR FDEA202604160448](https://openairdocs.org/sdr/FDEA202604160448.md): Skin · delaminated · Apr 16, 2026 · N281FE · Boeing 767300 · Trailing Edge Flaps
  > DELAMINATION IN LEADING EDGE AT 9" OF INBOARD END ON OUTBOARD FLAP LH WING LH WING, OUTBOARD FLAP AT LEADING EDGE ON 9" OF INB. EDGE WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R TABLE I, 51-70-17-0G PARAGRAPH 4A FIGURE 10 AND AMM 51-21-10-7 REV. 94 DEC 15,2025
- [SDR FDEA202604140445](https://openairdocs.org/sdr/FDEA202604140445.md): Skin · delaminated · Apr 14, 2026 · N281FE · Boeing 767300 · Trailing Edge Flaps
  > DELAMINATION ON L EDGE INB MAIN FLAP AT 20" FROM OUTB EDGE. RH WING L/E INBD MAIN FLAP AT 20" FROM OUTBD EDGE RH WING WAS REPAIRED IAW B767 SRM 57-53-01- 2R FIG 201 SHEET 5 TABLE 1 AND SRM 51-70-03-0G PAR 5A FIG 5 REV 94 DEC 15/2025
- [SDR FDEA202604140444](https://openairdocs.org/sdr/FDEA202604140444.md): Skin · dented · Apr 14, 2026 · N281FE · Boeing 767300 · Trailing Edge Flaps
  > DENT IN LOWER SURFACE ON AFT FLAP AT 35.5" OF OUTBOARD FAIRING FLAP AND 8.25" OF LEADING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON AFT FLAP AT 35.5" OF OUTBOARD FLAP AND 8.25" OF LEADING EDGE ON INBOARD FLAP. LH WING WAS REPAIRED IAW B767 SRM 57-53-01
- [SDR FDEA202604140443](https://openairdocs.org/sdr/FDEA202604140443.md): Skin · dented · Apr 14, 2026 · N281FE · Boeing 767300 · Trailing Edge Flaps
  > DENT IN LOWER SURFACE ON AFT FLAP AT 33" OF OUTBOARD FAIRING FLAP AND 11" OF LEADING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON AFT FLAP AT 33" OF OUTBOARD FAIRING FLAP AND 11" OF LEADING EDGE ON INBOARD FLAP, LH WING WAS REPAIRED IAW B767 SRM 57-53-01
- [SDR FDEA202604140442](https://openairdocs.org/sdr/FDEA202604140442.md): Skin · dented · Apr 14, 2026 · N281FE · Boeing 767300 · Trailing Edge Flaps
  > DENT IN LOWER SURFACE ON MAIN FLAP AT 35'' OF OUTBOARD FAIRING FLAP AND 14.25" OF TRAILING EDGE ON INBOARD FLAP, LH WING LOWER SURFACE ON MAIN FLAP AT 35" ON OUTBOARD FAIRING FLAP AND 14.2" OF TRAILING EDGE ON INBOARD FLAP LH WING WAS REPAIRED IAW SRM 57-5
- [SDR FDEA202604130436](https://openairdocs.org/sdr/FDEA202604130436.md): Floor Panel · cracked · Apr 13, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > TWO (2) CRACKS ON FLOOR PANEL 222BFF ON PREVIOUS REPAIR AT MAIN DECK CARGO FLOOR PANEL 222BFF AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202604130435](https://openairdocs.org/sdr/FDEA202604130435.md): Floor Panel · punctured · Apr 13, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > 2 PUNCTURES ON FLOOR PANEL 241AFF AT MAIN DECK CARGO FLOOR PANEL 241AFF AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202604130434](https://openairdocs.org/sdr/FDEA202604130434.md): Floor Panel · broken · Apr 13, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > BROKEN FLOOR PANEL 222AFF ON PREVIOUS REPAIR AT MAIN DECK CARGO FLOOR PANEL 222AFF AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15/2025.
- [SDR FDEA202604130433](https://openairdocs.org/sdr/FDEA202604130433.md): Floor Panel · cracked · Apr 13, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 241CFA MAIN DECK CARGO FLOOR PANEL 241CFA AT MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202604120428](https://openairdocs.org/sdr/FDEA202604120428.md): Floor Panel · punctured · Apr 12, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > 2 PUNCTURES ON FLOOR PANEL 232 NFF AT MAIN DECK CARGO FLOOR PANEL 232 NFF AT MAIN DECK CARGO WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REP. GEN. REV. 94 DEC 15, 2025
- [SDR FDEA202604120427](https://openairdocs.org/sdr/FDEA202604120427.md): Floor Panel · punctured · Apr 12, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 232 SFF AT MAIN DECK CARGO FLOOR PANEL 232 SFF AT MAIN DECK CARGO WAS REPAIRED IAW SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 94 DEC 15, 2025
- [SDR FDEA202604100425](https://openairdocs.org/sdr/FDEA202604100425.md): Floor Panel · punctured · Apr 10, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 242UFF AT MAIN DECK CARGO FLOOR PANEL 242UFF AT MAIN DECK CARGO WAR REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202604090423](https://openairdocs.org/sdr/FDEA202604090423.md): Floor Panel · punctured · Apr 9, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > 2 PUNCTURES ON FLOOR PANEL 251EFF AT MAIN DECK FLOOR PANEL 251EFF AT MAIN DECK WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15, 2025
- [SDR FDEA202604090422](https://openairdocs.org/sdr/FDEA202604090422.md): Floor Panel · punctured · Apr 9, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 251DFF AT MAIN DECK FLOOR PANEL 251DFF AT MAIN DECK WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15, 2025
- [SDR FDEA202604090421](https://openairdocs.org/sdr/FDEA202604090421.md): Floor Panel · punctured · Apr 9, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 242VFF AT MAIN DECK CARGO FLOOR PANEL 242VFF AT MAIN DECK CARGO WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15, 2025
- [SDR FDEA202604090420](https://openairdocs.org/sdr/FDEA202604090420.md): Floor Panel · cracked · Apr 9, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > 2 PUNCTURES ON FLOOR PANEL 251KFF AT MAIN DECK FLOOR PANEL 251KFF AT MAIN DECK WAS REPAIRED IAW SRM B767 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15, 2025
- [SDR FDEA202604080417](https://openairdocs.org/sdr/FDEA202604080417.md): Floor Panel · punctured · Apr 8, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > 3 PUNCTURES ON FLOOR PANEL 251UFF AT MAIN DECK FLOOR PANEL 251UFF AT MAIN DECK WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202604080416](https://openairdocs.org/sdr/FDEA202604080416.md): Floor Panel · punctured · Apr 8, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 252SFF AT MAIN DECK CARGO FLOOR PANEL 252SFF AT MAIN DECK CARGO WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94.
- [SDR FDEA202604080415](https://openairdocs.org/sdr/FDEA202604080415.md): Floor Panel · cracked · Apr 8, 2026 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNTURE ON FLOOR PANEL 251VFF AT MAIN DECK FLOOR PANEL 251VFF AT MAIN DECK WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94.
- [SDR FDEA202411131675](https://openairdocs.org/sdr/FDEA202411131675.md): Flap System · faulted · Nov 13, 2024 · N281FE · Boeing 7673S2F · Trailing Edge Flap Control System
  > ON FLAP EXTENSION JUST PRIOR TO FLAP 5 FULL EXTENSION THE AIRCRAFT ROLLED 5 DEGREES LEFT. AT FLAPS 5 FULL EXTENSION THE AIRCRAFT ROLLED WINGS LEVEL. ALTITUDE 3000FT SPEED 190 KNOTS. FULL SPOILERS WERE SELECTED AT THE TIME. LOWER THE FLAP TO 5 DEG AND VI
- [SDR FDEA202408281183](https://openairdocs.org/sdr/FDEA202408281183.md): Escape Rope · out of position · Aug 28, 2024 · N281FE · Boeing 7673S2F · Emergency Equipment
  > UPON ARRIVAL FOUND THE L1 DOOR ESCAPE ROPE NOT VISIBLE ON THE AFT L1 DOOR FRAME, FOUND ROPE STUFFED INTO THE CEILING POUCH. AMM: 25-10-00-2 RESTOWED THE L1 DOOR ESCAPE ROPE PER THE ABOVE AMM REFERENCE. PER GMM 12-7-600, NO PARTS REPLACED. A/C OK FO
- [SDR FDEA202402290223](https://openairdocs.org/sdr/FDEA202402290223.md): Floor Panel · damaged · Feb 29, 2024 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO FLOOD STA 1030/ RBL 33.0 HAS A HOLE 1 1/2 BY 1 INCH IN ZONE 2 SRM 53-00-50-1A AT 2,535:44 HOUR(S), 1,285 CYCLE(S) AMM: 53-01-06-4 WO#87852, SEQ160, FOR FLOORBOARD REMOVAL AND INSTALLATION
- [SDR FDEA202402280222](https://openairdocs.org/sdr/FDEA202402280222.md): Floorboard · damaged · Feb 28, 2024 · N281FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO FLOORBOARD (PN:14T5876-104) AT STA 1030 RBL 33. HAS A (1.5 IN X 1.0 IN) PUNCHURED HOLE DAMAGE. REPAIRED FLOORBOARD PANEL (PN:14T5876-104) AT STA. 1030 RBL 33 IN REF. TO 767 SRM 53-00- 50-2R PARA 4 STEPS. E 1-4 FIG. 201 SHEET 2 AND 4 DETAIL I / II
- [SDR FDEA202308151440](https://openairdocs.org/sdr/FDEA202308151440.md): Transmitter · unknown · Aug 15, 2023 · N281FE · Boeing 767300 · Trailing Flap Position Indicating System
  > GO AROUND FOR FLAP INDICATION. RIGHT FLAPS INDICATED 20 WHILE LEFT FLAPS INDICATED 25. NO MESSAGES OR ALERTS. SECOND APPROACH BOTH FLAPS WERE SET TO AND INDICATED 30 AS SELECTED. REMOVED AND REPLACED FLAP POSITION TRANSMITTER #8 PER AMM 27-51-45-2.
- [SDR FDEA202208021852](https://openairdocs.org/sdr/FDEA202208021852.md): Module · failed · Aug 2, 2022 · N281FE · Boeing 767300 · Landing Gear Position and Warning
  > PDIS 281 32-60 0214 02AUG22 LAS FACT U RIGHT MAIN LANDING GEAR LIGHT INOP. ***EMERGENCY DECLARED*** T/S FOUND LIGHT CAP AND DIODE MODULE AT FAULT REMOVED AND REPLACED PER AMM 33-16-02-2. OPS CHECKS

## 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 = 'N281FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N281FE/reports

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