# Service difficulty reports: N124FE

A list on [N124FE](https://openairdocs.org/aircraft/N124FE.md).

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

- [SDR FDEA202609241437](https://openairdocs.org/sdr/FDEA202609241437.md): Engine · bird ingestion · Sep 24, 2026 · N124FE · Boeing 7673S2F · Engine (Turbine/Turboprop)
  > CLIMBING THRU APPROXIMATELY 500-600FT AGL DEPARTING VCP WE STRUCK A LARGE BLACK BIRD ON THE NOSE CONE OF THE LEFT ENGINE. A LOUD BANG WAS HEARD ALONG WITH A PUTRID SMELL BEING OBSERVED. THE LEFT VIB INDICATOR DOUBLED FROM.6 TO 1.7 AND MOMENTARILY REACH
- [SDR FDEA202505290824](https://openairdocs.org/sdr/FDEA202505290824.md): Skin · dented · May 29, 2025 · N124FE · Boeing 7673S2F · Trailing Edge Flaps
  > LH WING, INBOARD FLAP WITH SEVERAL DENTS LH WING, INBOARD FLAP WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R FIG. 201 (SHEET 2) DETAIL I,SRM 51-70-10-2R REPAIR 2 FIG. 201 (SHEET 2) "C" AND SRM 51-70-03-0G PAR. 5.L FIG 16 REV. 90 AUG 15/2024. ONE DENT ON IFS 229
- [SDR FDEA202505290823](https://openairdocs.org/sdr/FDEA202505290823.md): Skin · dented · May 29, 2025 · N124FE · Boeing 7673S2F · Trailing Edge Flaps
  > LH WING, INBOARD TRAILING FLAP WITH SEVERAL DENTS LH WING, INBOARD TRAILING FLAP WAS REPAIRED I.A.W. B767 57-53-01-2R FIG. 201 (SHEET 4) NOTE "A" AND SRM 51-70-03-0G PAR. 5.A FIG. 16 REV. 90 AUG 15/2024
- [SDR FDEA202505290822](https://openairdocs.org/sdr/FDEA202505290822.md): Skin · dented · May 29, 2025 · N124FE · Boeing 7673S2F · Trailing Edge Flaps
  > LH WING, INBOARD FLAP WITH SEVERAL DENTS LH WING, INBOARD FLAP WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R FIG. 201 (SHEET 2) DETAIL I,SRM 51-70-10-2R REPAIR 2 FIG. 201 (SHEET 2) "C" AND SRM 51-70-03-0G PAR. 5.L FIG 16 REV. 90 AUG 15/2024
- [SDR FDEA202505260802](https://openairdocs.org/sdr/FDEA202505260802.md): Floor Panel · punctured · May 26, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231DFA SECTION 43 OF MDC FLOOR PANEL 231DFA SECTION 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAE 4 B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505260801](https://openairdocs.org/sdr/FDEA202505260801.md): Floor Panel · punctured · May 26, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231CFF SECTION 43 OF MDC FLOOR PANEL 231CFF SECTION 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15/24
- [SDR FDEA202505260800](https://openairdocs.org/sdr/FDEA202505260800.md): Floor Panel · punctured · May 26, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231EFF SECTION 43 OF MDC FLOOR PANEL 231EFF SECTION 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15-2024
- [SDR FDEA202505220791](https://openairdocs.org/sdr/FDEA202505220791.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231AFF SECTION 43 OF MDC FLOOR PANEL 231AFF SECTION 43 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505220790](https://openairdocs.org/sdr/FDEA202505220790.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > SECONDARY FINDING PUNCTURE ON FLOOR PANEL 231UFF SECTION 43 OF MDC FLOOR PANEL 231UFF SECTION 43 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505220789](https://openairdocs.org/sdr/FDEA202505220789.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > SECONDARY FINDING PUNCTURE ON FLOOR PANEL 241LFF ON SECTION 45 OF MDC. FLOOR PANEL 241LFF SECTION 45 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505220788](https://openairdocs.org/sdr/FDEA202505220788.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 251QFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 251QFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 SHEET 2 PAR 4 B REV 90 AUG 15/2024
- [SDR FDEA202505220787](https://openairdocs.org/sdr/FDEA202505220787.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 251PFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 251PFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505220786](https://openairdocs.org/sdr/FDEA202505220786.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL (252DFF) WITH PUNCTION MAIN DECK CARGO COMPARTMENT MAIN DECK FLOOR PANEL 252DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505220785](https://openairdocs.org/sdr/FDEA202505220785.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242LFA WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 242LFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505220784](https://openairdocs.org/sdr/FDEA202505220784.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 251YFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 251YFF WAS REPAIRED IAW SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505220783](https://openairdocs.org/sdr/FDEA202505220783.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 251VFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 251VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202505220782](https://openairdocs.org/sdr/FDEA202505220782.md): Floor Panel · cracked · May 22, 2025 · N124FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242GFF WITH A PUNCTURE MAIN DECK CARGO FLOOR PANEL 242GFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202405180687](https://openairdocs.org/sdr/FDEA202405180687.md): Support Angle · cracked · May 18, 2024 · N124FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > MEC, LT TUNNEL, AFT SIDE OF STA 246 BEAM HAS 1 EACH CRACKED "L" BRACKET. (PN: 141T5146- 16) REMOVED AND REPLACED SUPPORT ANGLE 147T5146-16 AT STA 246 PER DWG 141T5146 AND SRM 51-40-02-0G-0 "MINOR REPAIR"
- [SDR FDEA202405180684](https://openairdocs.org/sdr/FDEA202405180684.md): Stiffener · cracked · May 18, 2024 · N124FE · Boeing 7673S2F · Fuselage Structure (General)
  > MEC, LT TUNNEL, FWD SIDE OF STA 246 BEAM HAS 1 EACH CRACKED "L" BRACKET (PN: 141T5814- 136) REMOVED AND INSTALLED NEW STIFFENER PN: 141T5814-136. REF SRM 51-40-02-0G AND BOEING DWG 141T5104, ALODINE AND PRIMED AS REQUIRED. REF SRM 51-20-01-0G. (MINOR REPAI
- [SDR FDEA202306151044](https://openairdocs.org/sdr/FDEA202306151044.md): Skin · delaminated · Jun 15, 2023 · N124FE · Boeing 767300 · Wing, Nacelle/Pylon Attach Fittings
  > RUDDER, R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE ON THE AFT EDGE. REPAIRED RUDDER, R/H EXTERNAL SURFACE APPROX 8FT UP FROM THE FUSELAGE ON THE AFT EDGE BY REMOVING DAMAGE, CLEANING AREA, LAYING UP REPAIR PLIES AND CURED IAW B76
- [SDR FDEA202306151043](https://openairdocs.org/sdr/FDEA202306151043.md): Skin · delaminated · Jun 15, 2023 · N124FE · Boeing 767300 · Rudder, Plate/Skin
  > RUDDER, R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE APPROX 10" FWD OF THE AFT EDGE REPAIRED R/H EXTERNAL SURFACE OF RUDDER APPROX 8FT UP FROM THE FUSELAGE,APPROX 10" FWD OF AFT EDGE BY REMOVING DAMAGE, CLEANING AREA, LAYING UP RE
- [SDR FDEA202306151042](https://openairdocs.org/sdr/FDEA202306151042.md): Skin · delaminated · Jun 15, 2023 · N124FE · Boeing 767300 · Rudder, Plate/Skin
  > RUDDER, R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE APPROX 27" FWD OF THE AFT EDGE REPAIRED RUDDER, R/H EXTERNAL SURFACE, APPROX 8FT UP FROM THE FUSELAGE, APPROX. 27" FWD OF THE AFT EDGE BY REMOVING DAMAGE, CLEANING, LAYING UP
- [SDR FDEA202306141036](https://openairdocs.org/sdr/FDEA202306141036.md): Beam · cracked · Jun 14, 2023 · N124FE · Boeing 767300 · Wing Main, Frame Structure
  > L/H WING T/E SUPPORT STRUCTURE IS CRACKED AT APPROX WS 1030 REMOVED & REPLACED LEFT WING TRAILING EDGE PANEL SUPPORT BEAM IAW BAC DWG 113T1913, REVISION A
- [SDR FDEA202306131030](https://openairdocs.org/sdr/FDEA202306131030.md): Angle · cracked · Jun 13, 2023 · N124FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOORBEAM AT STA 1575 RBL 65-68, ATTACH ANGLE IS CRACKED FABRICATED AND REPLACED CRACKED ATTACH ANGLE AT STA 1575, RBL 65-68, PER BOEING DWG 146T5650, SHT 5, REV C. FABRICATION OF ATTACH ANGLE, 146T5651-6 AND 146T5651-8, COMPLETED ON WORK CARD,
- [SDR FDEA202306131029](https://openairdocs.org/sdr/FDEA202306131029.md): Angle · cracked · Jun 13, 2023 · N124FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOORBEAM AT STA 1575 LBL 65, ATTACH ANGLE IS CRACKED FABRICATED AND REPLACED CRACKED ATTACH ANGLE AT STA 1575, LBL 65, PER BOEING DWG 146T5650, SHT 5, REV C. FABRICATION OF ATTACH ANGLE, 146T5651-5, COMPLETED ON WORK CARD, WO#83419, NR#N00131.
- [SDR FDEA202306131028](https://openairdocs.org/sdr/FDEA202306131028.md): Slat · gouged · Jun 13, 2023 · N124FE · Boeing 767300 · Leading Edge Devices
  > LW #5 SLAT LWR TE HAS 2 GOUGES. CLEANED SANDED REMOVED DAMAGE AND REPAIRED LW #5 SLAT LWR TE 2 GOUGES WITH PERMANENT REPAIR IAW B767 SRM 57-43-02 AND 51-70-10-2R REPAIR 4
- [SDR FDEA202306111023](https://openairdocs.org/sdr/FDEA202306111023.md): Slat · dented · Jun 11, 2023 · N124FE · Boeing 767300 · Wing Structure
  > #8 SLAT LOCATED JUST OB OF OB TRACK, SLAT TE HAS A DENT. CLEANED SANDED AND REMOVED DAMAGE ON RIGHT WING #8 SLAT AND REPAIRED IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4, REPAIR WAS A PERMANENT REPAIR ON #8 SLAT JUST O/B OF O/B TRACK / SLAT T/E.
- [SDR FDEA202306050995](https://openairdocs.org/sdr/FDEA202306050995.md): Bracket · cracked · Jun 5, 2023 · N124FE · Boeing 767300 · Wing Structure
  > RW INBD L/E AT STA LES 285 TORQUE TUBE GUIDE BRACKET IS CRACKED REMOVED AND REPLACED RIGHT WING, INBOARD LEADING EDGE, TORQUE TUBE GUIDE BRACKET IAW B767 SRM 51-40-02-0G AND BAC DWG 114T1240, SHEET 6, REVISION -
- [SDR FDEA202211052733](https://openairdocs.org/sdr/FDEA202211052733.md): Former · cracked · Nov 5, 2022 · N124FE · Boeing 7673S2F · Wing Miscellaneous Structure
  > FORMER CRACKED AT R/W FLE OSS 441, (PN INSTALLED 114T2170-6, WITH 114T2171-3) REPLACED PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FLE OSS 441; WANT ALSO TO ATTACH FORMERS THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S.
- [SDR FDEA202205281324](https://openairdocs.org/sdr/FDEA202205281324.md): Former · cracked · May 28, 2022 · N124FE · Boeing 767300 · Wing Main, Frame Structure
  > ON LS FLE OSS 499 CRACKED FORMER 114T2511-13 W/ANGLE 114T2511-11 28-MAY-2022 22:54 REPLACED L/W L/E FORMER STA. OSS499 REF E.A. H-5720-TO368711 P1, SEQ. 165
- [SDR FDEA202104301077](https://openairdocs.org/sdr/FDEA202104301077.md): Evas Unit · no test · Apr 30, 2021 · N124FE · Boeing 7673S2F · Emergency Equipment
  > CAPT'S EVAS HAS AN UNSATISFACTORY OPS CKS PER WRI 25-60/5316 AND E.O. H-2560-E0324416 REV NO. G POS. P2. REMOVED AND REPLACE CAPT'S EVAS
- [SDR FDEA201911243085](https://openairdocs.org/sdr/FDEA201911243085.md): Skin · dented · Nov 24, 2019 · N124FE · Boeing 7673S2F · Fuselage Main, Plate/Skin
  > INCOMING ITEM: LOWER LH FUSELAGE AT STA 1225, BETWEENSTRINGERS 32L-33L HAS A DENT COMPLIED WITH EA H-5310-T0350997 A. TITLED "FUSELAGE-MAINFRAME-FUSELAGE SKIN, STA 1225 BETWEEN S32L-33L, DENT". REMOVED AND REINSTALLED PIT SIDEWALL PANEL IAW B767 AMM 25-
- [SDR FDEA201802130383](https://openairdocs.org/sdr/FDEA201802130383.md): Warning System · out of adjust · Feb 13, 2018 · N124FE · Boeing 7673S2F · Cabin Pressure Control System
  > WHILE PERFORMING THE CABIN ALTITUDE WARNING TEST DURING CRM INSTALLATION - FITMENT TESTING. DISCOVERED THE CABIN ALTITUDE WARNING SYSTEM WAS INOPERATIVE. ADJUSTED THE CABIN ALTITUDE WARNING SYSTEM IAW AMM 21-33-00-5 AND 21-33-00-5. TESTED GOOD.
- [SDR FDEA201709062461](https://openairdocs.org/sdr/FDEA201709062461.md): Fire Bottle · inoperative · Sep 6, 2017 · N124FE · Boeing 7673S2F · Fire Bottle, Fixed
  > APU FIRE EXTINGUISHER SYSTEM INOP. INSPECTED APU COMPT FOR ANY SIGNS OF FIRE OR LEAKS, NONE FOUND LOOKS PRISTINE. REMOVED AND REPLACED THE APU FIRE BOTTLE AND OPS CHECKED NORMAL PER MM 26-22-02-4 AND GMM 9-4-403. AS A PRECAUTION ALSO REPLACED K602 APU AUTO

## 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 = 'N124FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N124FE/reports

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