# Service difficulty reports: N123FE

A list on [N123FE](https://openairdocs.org/aircraft/N123FE.md).

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

- [SDR FDEA202510292103](https://openairdocs.org/sdr/FDEA202510292103.md): Windshield · failed · Oct 29, 2025 · N123FE · Boeing 7673S2F · Flight Compartment Windows
  > IN FLIGHT AT FL 340 OFFICERS FRONT WINDSHIELD SHATTERED. EMERGENCY DECLARED. REMOVED AND INSTALLED FO #1 WINDOW UP TO AND INCLUDING 3.G.(31). AND STEPS 3.G(34)-3.G.(40).
- [SDR FDEA202507081142](https://openairdocs.org/sdr/FDEA202507081142.md): Skin · dented · Jul 8, 2025 · N123FE · Boeing 7673S2F · Trailing Edge Flaps
  > DENT ON RH WING, INBD TE FLAP, AFT FLAP LOWER SURFACE, AT 60" FROM INBD EDGE AND 2" FROM TE DENT ON RH WING, INBD TE FLAP, AFT FLAP LOWER SURFACE WAS REPAIRED IAW B767 SRM 51- 70-10-2R AND SRM 51-70-03-0G REV 92 APR 15 2025 AND SRM 57-53-01-2R FIG 201 SHEET
- [SDR FDEA202507071131](https://openairdocs.org/sdr/FDEA202507071131.md): Skin · dented · Jul 7, 2025 · N123FE · Boeing 7673S2F · Trailing Edge Flaps
  > DENT ON OUTBOARD FLAP LOWER SKIN, BETWEEN WS 746 AND 772 LH WING OUTBOARD FLAP LOWER SKIN BETWEEN WS 746 AND 772 LH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE II FIG 201 SHEET 6 AND SRM 51-70-17-0G PARAGRAPH 4A FIGURE 10 REVISION 92.0 APR 15/2025 PA
- [SDR FDEA202507071130](https://openairdocs.org/sdr/FDEA202507071130.md): Skin · corroded · Jul 7, 2025 · N123FE · Boeing 7673S2F · Trailing Edge Flaps
  > EVIDENCE OF CORROSION ON RH WING, INBD TE FLAP, AFT FLAP UPPER SURFACE, 5'' FROM OUTBD EDGE AND 7'' FROM TE RH WING, INBD TE FLAP, AFT FLAP UPPER SURFACE, 5'' FROM OUTBD EDGE AND 7'' FROM TE WAS REPAIRED IAW B767 SRM 51-70-10-2R PAR F TABLE 208 AND B767 S
- [SDR FDEA202507041120](https://openairdocs.org/sdr/FDEA202507041120.md): Skin · damaged · Jul 4, 2025 · N123FE · Boeing 7673S2F · Trailing Edge Flaps
  > DENT ON OUTBOARD FLAP LOWER SKIN, BETWEEN WS 746 AND 772 LH WING. OUTBOARD FLAP LOWER SKIN, BETWEEN WS 746 ON 772 LH WING WAS REPAIRED IAW B767 SRM 57-53-012R TABLE II FIGURA 201 SHEET 6 AND SRM 51-70-17-09 PARAGRAPH 4.A, FIGURE 10 REV 92.0 APR 15/2025. P
- [SDR FDEA202507031110](https://openairdocs.org/sdr/FDEA202507031110.md): Skin · dented · Jul 3, 2025 · N123FE · Boeing 7673S2F · Trailing Edge Flaps
  > TWO DENTS ON RH WING, INBD TE FLAP, AFT FLAP UPPER SURFACE, AT 20" FROM OUTBD EDGE AND 12" AND 2" FROM TE RH WING, INBD FLAP, AFT FLAP UPPER SURFACE, TWO DENTS WERE EVALUATED AND FOUND ONE DENT WITHIN LIMITS IAW B767 SRM 57-53-01-1A FIG 101 SHEET 4 REV 92
- [SDR FDEA202507031109](https://openairdocs.org/sdr/FDEA202507031109.md): Floor Panel · punctured · Jul 3, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 251DFF WITH PUNCTURES MDC FLOOR PANEL 251DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 REV 92 APR 15,2025
- [SDR FDEA202507031108](https://openairdocs.org/sdr/FDEA202507031108.md): Floor Panel · punctured · Jul 3, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 251QFF WITH PUNCTURES MDC FLOOR PANEL 251QFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 PAR 15/2025
- [SDR FDEA202507031107](https://openairdocs.org/sdr/FDEA202507031107.md): Floor Panel · punctured · Jul 3, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 252DFF WITH PUNCTURES MDC FLOOR PANEL 252DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507031106](https://openairdocs.org/sdr/FDEA202507031106.md): Floor Panel · punctured · Jul 3, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 251EFF WITH PUNCTURES MDC FLOOR PANEL 251EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507031105](https://openairdocs.org/sdr/FDEA202507031105.md): Floor Panel · cracked · Jul 3, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 241KFF WIYH PUNCTURES MDC FLOOR PANEL 241KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 PAR 4B SHEET 2, REV 92. APR 15/2025.
- [SDR FDEA202507031104](https://openairdocs.org/sdr/FDEA202507031104.md): Floor Panel · cracked · Jul 3, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 242HFF WITH CRACK MDC FLOOR PANEL 242HFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201 SHEET 2 REV 92 APR 15/2025
- [SDR FDEA202507031103](https://openairdocs.org/sdr/FDEA202507031103.md): Skin · dented · Jul 3, 2025 · N123FE · Boeing 7673S2F · Trailing Edge Flaps
  > DENT ON OUTBOARD LOWER SKIN, BETWEEN WS 720 AND 746 LH WING LH WING, OUTBOARD FLAP LOWER SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 SHEET 3 DETAIL II AND SRM 51-70-10-2R REPAIR 4 REV 92 15/2025
- [SDR FDEA202507011092](https://openairdocs.org/sdr/FDEA202507011092.md): Floor Panel · cracked · Jul 1, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 252JFF WITH PUNTURES MDC FLOOR PANEL 252JFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025
- [SDR FDEA202507011091](https://openairdocs.org/sdr/FDEA202507011091.md): Floor Panel · cracked · Jul 1, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 251AFF WITH PUNCTURES MDC FLOOR PANEL 251AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202507011090](https://openairdocs.org/sdr/FDEA202507011090.md): Floor Panel · cracked · Jul 1, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 252SFF WITH PUNCTURES MDC FLOOR PANEL 252SFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202507011089](https://openairdocs.org/sdr/FDEA202507011089.md): Floor Panel · cracked · Jul 1, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 252HFF WITH PUNCTURES MDC FLOOR PANEL 252HFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15, 2025
- [SDR FDEA202507011088](https://openairdocs.org/sdr/FDEA202507011088.md): Floor Panel · cracked · Jul 1, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 251KFF WITH PUNCTURES MDC FLOOR PANEL 251KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202506301085](https://openairdocs.org/sdr/FDEA202506301085.md): Floor Panel · cracked · Jun 30, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 251LFF WITH PUNCTURES MDC FLOOR PANEL 251LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202506301084](https://openairdocs.org/sdr/FDEA202506301084.md): Floor Panel · cracked · Jun 30, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 251PFF WITH CRACK MDC FLOOR PANEL 251PFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202506301083](https://openairdocs.org/sdr/FDEA202506301083.md): Floor Panel · cracked · Jun 30, 2025 · N123FE · Boeing 7673S2F · Fuselage Floor Panel
  > MDC FLOOR PANEL 252NFF WITH PUNCTURES MDC FLOOR PANEL 252NFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 92 APR 15,2025
- [SDR FDEA202410061440](https://openairdocs.org/sdr/FDEA202410061440.md): Escape Reel · failed · Oct 6, 2024 · N123FE · Boeing 7673S2F · Emergency Equipment
  > MDIS 123 25-60 8503 06OCT24 08:56 MEM FACT #2 EMERGENCY DESCENT DEVICE FOUND EXPIRED. R/I 06OCT24 16:01 MEM REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 379103D25 CPN: 2524075 POS: P2 ON MPN: 379103D-25
- [SDR FDEA202406060775](https://openairdocs.org/sdr/FDEA202406060775.md): Floorbeam · cracked · Jun 6, 2024 · N123FE · Boeing 7673S2F · Fuselage Main, Floor Beam
  > [MEC, LT TUNNEL, STA 246 (LBL 26.06) FLOOR BEAM, FWD SIDE, "L" BRACKET CRACKED. (PN 141T5814-136) INSTALLED NEW FABRICARTED SUPPORT (PN 141T5814-136) USING DRW 141T5814, NA: 141T5104 ALONG WITH 767 SRM 51-40-02-0G. MINOR REPAIR
- [SDR FDEA202406050772](https://openairdocs.org/sdr/FDEA202406050772.md): Tee Angle · cracked · Jun 5, 2024 · N123FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > MEC, LT TUNNEL, STA 246, APROX BL 20 LT, "T" BRACKET CRACKED. INSTALLED NEW FABERCATED T-CLIP 141T5603-6 IAW DRAWING #141T5601 & 141T5600, SRM 51-40-02-0G.
- [SDR FDEA202406050771](https://openairdocs.org/sdr/FDEA202406050771.md): Tee Angle · damaged · Jun 5, 2024 · N123FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > T CLIP CRACKED AT APPROX. STA 266 BL 0. INSTALLED NEW FABERCATED T-CLIP 141T5603-7 IAW DRAWING #141T5601, SRM 51-40-02-0G.
- [SDR FDEA202307181239](https://openairdocs.org/sdr/FDEA202307181239.md): Rudder · damaged · Jul 18, 2023 · N123FE · Boeing 767300 · Rudder Structure
  > VERT STAB, RUDDER, L/H SIDE, TRAILING EDGE HAS EDGE DAMAGE AT APPROX RUDDER STA 305 REPAIRED RUDDER TRAILING EDGE IAW FEDEX EA# H-5540-T0375223-P1, RELEASED JUL 15, 2023, TITLED "STABILIZERS - RUDDER - LH SIDE, UPPER PANEL ASSY, RUDDER STA 320, TRAILING EDGE
- [SDR FDEA202307181238](https://openairdocs.org/sdr/FDEA202307181238.md): Skin · damaged · Jul 18, 2023 · N123FE · Boeing 767300 · Horizontal Stabilizer, Plate/Skin
  > L/H HOR. STAB, UPPER SKIN IS DENTED AND GOUGED AT APPROX 75" O/B OF STAB ROOT JUST AFT OF L/E PANEL 332BL REPAIRED L/H HOR STAB, UPPER SKIN DENT AND GOUGE APPROX 75" O/B OF THE STAB ROOT, JUST AFT OF L/E PANEL 332BL AS REQUIRED IAW FDX B767 SRM 51-70-10-2R
- [SDR FDEA202307181237](https://openairdocs.org/sdr/FDEA202307181237.md): Angle · cracked · Jul 18, 2023 · N123FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT IS CRACKED AT APPROX STA 1575, LBL 68 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C
- [SDR FDEA202307181236](https://openairdocs.org/sdr/FDEA202307181236.md): Angle · cracked · Jul 18, 2023 · N123FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX STA 1575, LBL 65 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C
- [SDR FDEA202307181235](https://openairdocs.org/sdr/FDEA202307181235.md): Angle · cracked · Jul 18, 2023 · N123FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT APPROX STA 1575, RBL 68 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C.
- [SDR FDEA202307181234](https://openairdocs.org/sdr/FDEA202307181234.md): Angle · cracked · Jul 18, 2023 · N123FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX STA 1575, RBL 65 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C
- [SDR FDEA202307141216](https://openairdocs.org/sdr/FDEA202307141216.md): Shear Tie · cracked · Jul 14, 2023 · N123FE · Boeing 767300 · Nacelle/Pylon Structure
  > 1EA ATTACH CLIP IS CRACKED AT #2 PYLON AFT BULKHEAD ON INBD SIDE AT APPROX NAC STA 295, JUST BELOW INBD MID-SPAR FITTING REMOVED AND REPLACED #2 PYLON, INBOARD SHEAR TIE AT NAC STA 297 IAW BAC DWG 313T2310, SHEET 95, REVISION -
- [SDR FDEA202307121203](https://openairdocs.org/sdr/FDEA202307121203.md): Bracket · cracked · Jul 12, 2023 · N123FE · Boeing 767300 · Nacelle/Pylon Structure
  > #1 PYLON/NACELLE, I/B SIDE, ACCESSED BY PANEL 437BR, HYD. RESERVOIR BAY FWD BULKHEAD UPPER CORNER ATTACH BRACKET CRACKED REMOVED AND REPLACED ATTACH BRACKET LOCATED ON #1 PYLON/NACELLE, I/B SIDE, ACCESSED BY PANEL 437BR, HYD. RESERVOIR BAY FWD BULKHEAD UPP
- [SDR FDEA202307101195](https://openairdocs.org/sdr/FDEA202307101195.md): Fitting · cracked · Jul 10, 2023 · N123FE · Boeing 767300 · Nacelle/Pylon Structure
  > #1 PYLON AFT FAIRING, INBD SIDE FRAME, NAC STA 380, MID ATTACH CLIP, IS CRACKED. REMOVED AND REPLACED ATTACH CLIP (BRACKET) LOCATED ON #1 PYLON AFT FAIRING, INBD SIDE FRAME, NAC STA 380, PER BOEING DWG 313T2303, REV -
- [SDR FDEA202307101194](https://openairdocs.org/sdr/FDEA202307101194.md): Fitting · cracked · Jul 10, 2023 · N123FE · Boeing 767300 · Nacelle/Pylon Structure
  > #2 PYLON AFT FAIRING, OTBD SIDE, FRAME ATTACH CLIP, AT APPROX. NAC STA 380, IS CRACKED REMOVED AND REPLACED ATTACH CLIP LOCATED ON #2 PYLON AFT FAIRING, OTBD SIDE, FRAME ATTACH CLIP, AT APPROX. NAC STA 380, PER BOEING DWG 313T2303, REV -
- [SDR FDEA202307071169](https://openairdocs.org/sdr/FDEA202307071169.md): Bracket · cracked · Jul 7, 2023 · N123FE · Boeing 767300 · Wing Main, Frame Structure
  > RIGHT WING FUELING STATION PANEL HOLD OPEN SUPPORT BRACKET CRACKED REMOVED AND REPLACED SUPPORT BRACKET ON RIGHT WING FUELING STATION PANEL PER BOEING DWG 114T2450, SHT 1, REV J
- [SDR FDEA202307071168](https://openairdocs.org/sdr/FDEA202307071168.md): Bracket · cracked · Jul 7, 2023 · N123FE · Boeing 767300 · Wing Main, Frame Structure
  > RIGHT WING FUELING STATION PANEL LIGHT SUPPORT BRACKET CRACKED REMOVED AND REPLACED LIGHT SUPPORT BRACKET ON RIGHT WING FUELING STATION PANEL PER BOEING DWG 284T0562, SHT 1, REV B,
- [SDR FDEA202307061217](https://openairdocs.org/sdr/FDEA202307061217.md): Skin · gouged · Jul 6, 2023 · N123FE · Boeing 767300 · Horizontal Stabilizer, Plate/Skin
  > LH HORIZONTAL STAB. UPPER SKIN IS DENTED AND GOUGED AT APPROX 75" OB OF STAB. ROOT, JUST AFT OF LE PANEL 332BL. REPAIRED LH HORIZONTAL STABILIZER UPPER SKIN DENT AND GOUGE APPROX 75" OB OF STAB. ROOT, JUST AFT OF LE PANEL 332BL AS REQUIRED IAW FDX B767 SRM
- [SDR FDEA202203290798](https://openairdocs.org/sdr/FDEA202203290798.md): Former · cracked · Mar 29, 2022 · N123FE · Boeing 767300 · Wing Structure
  > RH WING LE AT STA OSS-441 HAS LOOSE RIVETS AND A BROKEN FORMER P/N 114T2170-6. 0000301922: VERNON, JAMES L - 30-MAR-2022 01:18 REPLACED R/W L/E FORMER AT WS 441 REF E.A. TH-5720-T0367716 P1, W/O 82632, SEQ. 155.
- [SDR FDEA202203290797](https://openairdocs.org/sdr/FDEA202203290797.md): Former · cracked · Mar 29, 2022 · N123FE · Boeing 767300 · Wing Structure
  > LH WING LE AT STA OSS499 HAS LOOSE RIVETS AND BROKEN FORMER P/N 114T2511-13 0000452710: ROSNER, DANIEL D - 30-MAR-2022 01:37 COMPLIED WITH EA TH-5720-T0367715P1...LH WING LE AT STA OSS499 HAS LOOSE RIVETS AND BROKEN FORMER P/N 114T2511-13
- [SDR FDEA202203290796](https://openairdocs.org/sdr/FDEA202203290796.md): Former · none · Mar 29, 2022 · N123FE · Boeing 767300 · Wing Structure
  > LH WING LE AT STA OSS441 HAS LOOSE RIVETS AND A BROKEN FORMER P/N 114T2170-5 0000493008: CRAIL, ROGER L - 30-MAR-2022 01:41 REPLACED LOOSE RIVETS AND BROKEN BRACKET AS REQUIRED. REF E.A. H-5720-T0367717 P1
- [SDR FDEA202107141773](https://openairdocs.org/sdr/FDEA202107141773.md): Skin · worn · Jul 14, 2021 · N123FE · Boeing 7673S2F · Leading Edge Devices
  > RH WING #7 SLAT T/E WORN BTW ISS160.41 - ISS180.56 PERFORMED THE REPAIR ON RH WING #7 SLAT T/E WEDGE PER B767 SRM 57-43-02-2R REPAIR 1 AND SRM 51-70-10-2R REPAIR 4 FIGURE 202 SHEET 8. THE RSC TRACKING EA #: H-5750- T0362888 P1,TITLE: WINGS T0362888 P1,T
- [SDR FDEA201807081648](https://openairdocs.org/sdr/FDEA201807081648.md): Skin · dented · Jul 8, 2018 · N123FE · Boeing 7673S2F · Fuselage Main, Plate/Skin
  > COMPLY WITH EA H-5330-T0340792-P1, FUSELAGE SKIN REPAIR AT STA 1430. REPAIRED FUSELAGE SKIN AT STA 1430 ABOVE STR 35L AND BELOW STR 39L IAW EA NR H-5330-T0340792A.
- [SDR FDEA201803310827](https://openairdocs.org/sdr/FDEA201803310827.md): Battery · failed · Mar 31, 2018 · N123FE · Boeing 7673S2F · APU Start/Ignition System
  > TRIED TO START THE APU TWICE, NO START. APU FAULT EICAS. OPENED PANEL ON THE E-6 RACK AND NOTICED APU BATTERY COMPARTMENT WAS FULL OF SMOKE AND SMELLED STRONG. CHECKED APU AUX CONT UNIT, NO FAULTS INDICATED. R AND R THE APU BATTERY IAW 24-31-04-4. OPS CHE

## 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 = 'N123FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N123FE/reports

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