# Service difficulty reports: N162FE

A list on [N162FE](https://openairdocs.org/aircraft/N162FE.md).

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

- [SDR FDEA202603210363](https://openairdocs.org/sdr/FDEA202603210363.md): Skin · dented · Mar 21, 2026 · N162FE · Boeing 7673S2F · Leading Edge Devices
  > INDUCED DAMAGE SLAT #8 L/E SKIN AT INB EDGE OSS389 ON SLAT #8 WAS REPAIRED IAW E.A. H-5750-T0386687.
- [SDR FDEA202603180357](https://openairdocs.org/sdr/FDEA202603180357.md): Floor Panel · damaged · Mar 18, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > SCREWS THROUGH 241PFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241PFF BOTTOM SIDE WAS REPAIRED AND SCREWS WERE CORRECTLY INSTALLED IN THE FLOOR PANEL IAW SRM 53-00-50-2R REPAIR GENERAL PAR B FIG 201 AND SRM 51-40-02-0G PAR 9 REV 94 DEC 15,2025
- [SDR FDEA202603130349](https://openairdocs.org/sdr/FDEA202603130349.md): Floor Panel · punctured · Mar 13, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURES ON 231LFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT, FLOOR PANEL 231LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B. FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202603130348](https://openairdocs.org/sdr/FDEA202603130348.md): Floor Panel · debonded · Mar 13, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > DISBONDING FLOOR PANEL 242KFF FLOOR PANEL 242KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202603130343](https://openairdocs.org/sdr/FDEA202603130343.md): Floor Panel · damaged · Mar 13, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > GROOVE ON 241DFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT, FLOOR PANEL 241DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PARA 4.B FIG 201 SHEET 2 REV. 94 DEC 15 / 2025
- [SDR FDEA202603130342](https://openairdocs.org/sdr/FDEA202603130342.md): Floor Panel · punctured · Mar 13, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUCTURES ON 241DFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. MAIN CARGO COMPARTMENT, FLOOR PANEL 241DFF WAS REPAIRED IAW. B767 SRM 53-00-50-2R PARA. 4.B FIG. 201 SHEET 2 REV. 94 DEC 15 / 2025
- [SDR FDEA202603120341](https://openairdocs.org/sdr/FDEA202603120341.md): Floor Panel · punctured · Mar 12, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON 231JFF FLOOR PANEL ON MAIN CARGO COMPARTMENT 231JFF FLOOR PANEL ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV. 94 DEC 15,2025
- [SDR FDEA202603120340](https://openairdocs.org/sdr/FDEA202603120340.md): Floor Panel · cracked · Mar 12, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL 241YFA FLOOR PANEL 241YFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 (B) REV 94 DEC 15/2025
- [SDR FDEA202603120339](https://openairdocs.org/sdr/FDEA202603120339.md): Floor Panel · damaged · Mar 12, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON 251KFF FLOOR PANEL ON MAIN CARGO COMPARTMENT FLOOR PANEL 251KFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 (B) REV 94 DEC 15/2025
- [SDR FDEA202603120338](https://openairdocs.org/sdr/FDEA202603120338.md): Floor Panel · damaged · Mar 12, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON 251EFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. 251EFF FLOOR PANEL ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15,2025
- [SDR FDEA202603120337](https://openairdocs.org/sdr/FDEA202603120337.md): Floor Panel · damaged · Mar 12, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON 242GFF FLOOR PANEL ON MAIN CARGO COMPARTMENT 242GFF FLOOR PANEL ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV.94 DEC 15, 2025
- [SDR FDEA202603120336](https://openairdocs.org/sdr/FDEA202603120336.md): Floor Panel · damaged · Mar 12, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON 231EFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. 231EFF FLOOR PANEL ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 94 DEC 15,2025
- [SDR FDEA202603100332](https://openairdocs.org/sdr/FDEA202603100332.md): Floor Panel · cracked · Mar 10, 2026 · N162FE · Boeing 7673S2F · Fuselage Structure (General)
  > CRACK ON 242TFA FLOOR PANEL ON MAIN DECK CARGO COMPARTMENT 242TFA FLOOR PANEL ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR.4-B FIG. 201 SHEET REV.94.
- [SDR FDEA202603080330](https://openairdocs.org/sdr/FDEA202603080330.md): Floor Panel · punctured · Mar 8, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURES ON 232MFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT, FLOOR PANEL 232MFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4B FIG. 201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202603080329](https://openairdocs.org/sdr/FDEA202603080329.md): Floor Panel · punctured · Mar 8, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURES ON 231RFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT, FLOOR PANEL 231 RFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4.B FIG. 201 SHEET 2 RE.94 DEC15/2025
- [SDR FDEA202603080328](https://openairdocs.org/sdr/FDEA202603080328.md): Floor Panel · damaged · Mar 8, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON 241FFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. MAIN CARGO COMPARTMENT, FLOOR PANEL 241 FFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4B FIG 201 SHEET 2 REV.94 DEC15/2025
- [SDR FDEA202603080327](https://openairdocs.org/sdr/FDEA202603080327.md): Floor Panel · punctured · Mar 8, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON 241 JFF FLOOR PANEL ON MAIN CARGO COMPARTMENT MAIN CARGO COMPARTMENT FLOOR PANEL 241 JFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG.201 SHEET 2 REV 94 DEC 15/2025
- [SDR FDEA202603080326](https://openairdocs.org/sdr/FDEA202603080326.md): Floor Panel · damaged · Mar 8, 2026 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON 231NFF FLOOR PANEL ON MAIN CARGO COMPARTMENT. MAIN CARGO COMPARTMENT, FLOOR PANEL 231 NFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV. 94 DEC15/2025
- [SDR FDEA202408281182](https://openairdocs.org/sdr/FDEA202408281182.md): Lamp · failed · Aug 28, 2024 · N162FE · Boeing 7673S2F · Landing Gear Position and Warning
  > RIGHT MAIN GEAR INDICATOR HAS BOTH BULBS OUT (OR IS INOPERATIVE). DISCONTINUED FIRST APPROACH WITH ONLY TWO GEAR INDICATIONS GREEN. RAN QRH AND DETERMINED THAT IN THE ABSENCE OF A GEAR DISAGREE MESSAGE OR CONFIG WARNING, THE RIGHT MAIN GEAR WAS INDEED DOWN
- [SDR FDEA202404240286](https://openairdocs.org/sdr/FDEA202404240286.md): Nut · loose · Apr 24, 2024 · N162FE · Boeing 7673S2F · Horizontal Stabilizer Structure
  > SECTION 48, LH HORIZONTAL PIVOT FITTING, INBOARD FACE, LOCKWIRE BROKEN. SECTION 48, LH HORIZONTAL PIVOT FITTING, INBOARD FACE NUT OF BEARING WAS TIGHTENED AND APPLIED TORQUE, AND INSTALLED LOCKWIRE IAW AMM 55-17-51-4 REV. 141. THE STABILIZER WAS OPERATED S
- [SDR FDEA202404130462](https://openairdocs.org/sdr/FDEA202404130462.md): Skin · dented · Apr 13, 2024 · N162FE · Boeing 7673S2F · Trailing Edge Flaps
  > DENT ON LOWER SKIN OF INBOARD TRAILING EDGE MAIN FLAP AT LH WING. LH WING INB. T/E MAIN FLAP LOWER SKIN WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R REPAIR 1 FIG. 201 SHEET 2 NOTE A AND B767 SRM 51-70-03-0G PARAGRAPH 5.L. FIG. 16 REV. 88.
- [SDR FDEA202404130461](https://openairdocs.org/sdr/FDEA202404130461.md): Skin · dented · Apr 13, 2024 · N162FE · Boeing 7673S2F · Trailing Edge Flaps
  > DENT ON LOWER SKIN OF INBOARD TRAILING EDGE AFT FLAP AT LH WING. LH WING, LOWER SKIN OF INBOARD TRAILING EDGE AFT FLAP WAS REPAIRED I.A.W. B767 SRM 57- 53-01-2R REP. 1 AND SRM 51-70-03-0G PAR. 5.L. FIG. 16 PAG. 27-52 REV. 88.
- [SDR FDEA202404130460](https://openairdocs.org/sdr/FDEA202404130460.md): Skin · dented · Apr 13, 2024 · N162FE · Boeing 7673S2F · Trailing Edge Flaps
  > SEVERAL DENTS, LOWER SURFACE, INBOARD TRAILING EDGE FLAP, RH WING. RH WING INB. T/E AFT FLAP LOWER SURFACE WAS EVALUATED AND FOUND 3 DENTS WITHIN LIMITS I.A.W. B767 SRM 57-53-01-1A FIG. 101 SHEET 4 NOTE C DET. IV. ONE DENT WAS FOUND OUT OF LIMITS AND WAS R
- [SDR FDEA202204070888](https://openairdocs.org/sdr/FDEA202204070888.md): None · delaminated · Apr 7, 2022 · N162FE · Boeing 767300 · Wing, Control Surfaces
  > RH WING OUTBOARD FLAP LOWER SKIN WITH DENT AT WBL: 435. RH WING OUTBOARD FLAP LOWER SKIN WITH DENT AT WBL 435 THAT WAS REPAIRED IAW SRM 57- 53-01-2R FIG. 201 PAGE 1-6 TABLE II AND SRM 51-70-17-0G-0 FIG. 10 PAGE 1, 24, 25, 36, 48 PARA. 4.A. REV. 82 DEC15/20
- [SDR FDEA2020051320922](https://openairdocs.org/sdr/FDEA2020051320922.md): Floor Panel · delaminated · May 12, 2020 · N162FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR 241PFF IS CRACKED FABRICATED NEW FLOOR PANEL PER FEDEX SRZ-25-005 REV R.
- [SDR FDEA202005110919](https://openairdocs.org/sdr/FDEA202005110919.md): Wedge · chafed · May 11, 2020 · N162FE · Boeing 7673S2F · Leading Edge Devices
  > LEFT WING #5 L/E SLAT TRAILING EDGE HAS A CHAFE AT APPROX LES 425 REPAIRED LEFT WING #5 SLAT L/E SLAT T/E WEDGE IAW B767 SRM 57-43-02-2R & 51-70-10-2R REPAIR 4. MAJOR REPAIR

## 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 = 'N162FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N162FE/reports

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