# Service difficulty reports: N277FE

A list on [N277FE](https://openairdocs.org/aircraft/N277FE.md).

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

- [SDR FDEA202503070339](https://openairdocs.org/sdr/FDEA202503070339.md): Tube · loose · Mar 7, 2025 · N277FE · Boeing 7673S2F · Smoke Detection
  > ZONE F RIGHT HAND SIDE LAST 2 SMOKE DETECTORS INOP. ABOVE CEILING SECTION OF TUBE MISSING. FOUND SMOKE DETECTOR TUBING HAD PULLED OUT OF RUBBER BOOT. LOOSENED CLAMPS AND PROPERLY REINSTALLED TUBING AND ZIP TIED INTO PLACE. RE-TIGHTENED CLAMPS. REF AMM 20-1
- [SDR FDEA202503010310](https://openairdocs.org/sdr/FDEA202503010310.md): Skin · damaged · Mar 1, 2025 · N277FE · Boeing 7673S2F · Leading Edge Devices
  > #5 SLAT LWR PANEL BELOW OB AUX TRACK AT AFT FASTENER HAS ERODED COMPOSITE. MARKED. REPAIRED #5 SLAT (MPN: 114T4105-409G) LWR EDGE CLOSE OUT PNL @ WS 490 Ï¿½A (1X1 INCH) REPAIR MOST AFT FASTENER HOLE. IN REF. TO 767 SRM 57-43-01-2R FIG.201 SHEET:4, 767 SRM 51
- [SDR FDEA202502270305](https://openairdocs.org/sdr/FDEA202502270305.md): Floorboard · dented · Feb 27, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT - FLOOR PANEL 241WFF HAS SEVERAL PUNCTURES AND DENTS ON TOP SIDE AND DELAMINATED AT LH AFT CORNER. REPAIRED MAIN CARGO COMPT. (MARKED) DENTED AREAS AT STA.984-1114.82 LBL 11 TO RBL 11 PNL# 241WFF TOP SKIN OF FLOORBOARD. IN REF. TO 76
- [SDR FDEA202502270304](https://openairdocs.org/sdr/FDEA202502270304.md): Floorboard · dented · Feb 27, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT - FLOOR PANEL 242SFF HAS DAMAGE AT THE RH AFT CORNER AND UNDERSIDE OF PANEL. REPAIRED MAIN CARGO COMPT. (MARKED) DENTED AREAS AT STA.984-1114.82 RBL 33 TO RBL 11 PNL# 242SFF TOP SKIN OF FLOORBOARD. IN REF. TO 767 SRM 53-00-50-2R FIG.
- [SDR FDEA202502260299](https://openairdocs.org/sdr/FDEA202502260299.md): Floor Panel · damaged · Feb 26, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT - FLOOR BOARD PANEL 241NFF HAS EDGE FILLER MISSING AT RH AFT CORNER. REPAIRED MAIN CARGO COMPT FLOORBOARD PANEL 241NFF MPN:145T5876-93 EDGE AT RH AFT CORNER IN REF TO B767 SRM 53-00-50-2R REPAIR #4 PARAGRAPH G, ITEM 2. THIS IS A MAJO
- [SDR FDEA202502260298](https://openairdocs.org/sdr/FDEA202502260298.md): Floorboard · damaged · Feb 26, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT - FLOOR BOARD PANEL 242JFF HAS A SMALL PUNCTURE ON TOP SIDE OF PANEL. (MARKED IN RED). REPAIRED MAIN CARGO COMPT FLOORBOARD TOP SKIN (MARKED) PUNCTURED AREA PNL# 242JFF MPN:145T5876-102 IN REF. TO B767 SRM 53-00-50-2R REPAIR#:4(B). T
- [SDR FDEA202502260293](https://openairdocs.org/sdr/FDEA202502260293.md): Floor Panel · damaged · Feb 26, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT- FLOOR BOARD PANEL 241AGF HAS EDGE FILLER MISSING AT RH AFT CORNER OF PANEL. REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 984.50- STA 1087, LBL 77.50 TO LBL 89.50 (MPN:145T5876-113/PNL# 241AGF) IN REF. B767 SRM 53-00-50-2R REPAIR 1 F
- [SDR FDEA202502250292](https://openairdocs.org/sdr/FDEA202502250292.md): Floorboard · damaged · Feb 25, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT - FLOORBOARD 242UFF HAS A PUNCTURE ON THE TOPSIDE OF PANEL. REPAIRED MAIN CARGO COMPT FLOORBOARD TOP SKIN AT STA. 972-114.82 RBL 54.75 TO RBL 74.25 PNL# 242UFF MPN: 145T5876-112. IN REF. TO 767 SRM 53-00-50-2R FIG. 201 SHEET.2 REPAIR
- [SDR FDEA202502250278](https://openairdocs.org/sdr/FDEA202502250278.md): Floor Panel · damaged · Feb 25, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > SMALL HOLE.5 INCH MAIN DECK CARGO FLOOR PANEL STA 1263-1270, PANEL #251LFF. REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 1263- 1270, LBL 3 TO LBL 7 (MPN:146T5869- 127 / PNL# 251LFF) IN REF. B767 SRM 53-00-50-2R REPAIR 1 FIG.201 SHEET 1. FLOORBOARD (PNL# 2
- [SDR FDEA202502250275](https://openairdocs.org/sdr/FDEA202502250275.md): Floor Panel · delaminated · Feb 25, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT - FLOOR BOARD PNEL 242LFF IS DELAMINATED FROM LH FWD CORNER AND RH AFT CORNER. REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 930- STA 972, RBL 54.75" TO RBL 74.25" (MPN:145T5876-110 / PNL# 242LFF) IN REF. TO B767 SRM 53-00-50-2R REPAIR
- [SDR FDEA202502250274](https://openairdocs.org/sdr/FDEA202502250274.md): Floor Panel · worn · Feb 25, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT - FLOOR BOARD PANEL 242KFF IS DELAMINATED FROM BOTTTOM OF PANEL (MARKED WITH RED ARROWS) AND HAS 3 MISSING SCREWS INSERTS. REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 930- STA 972, RBL 33" TO RBL 54.75" (MPN:145T5876-94 / PNL# 242KFF
- [SDR FDEA202502250273](https://openairdocs.org/sdr/FDEA202502250273.md): Floor Panel · damaged · Feb 25, 2025 · N277FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPT FLOOR PANEL 241XFF HAS EDGE FILLER MISSING EXPOSING HONEYCOMB AT RH AFT CORNER AND 3 EACH MISIING INSERTS. REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 970-1114.82, LBL 11 TO LBL 33 (MPN: 145T5876-103 / PNL# 241XFF) IN REF. B767 SRM 53-00
- [SDR FDEA202502190251](https://openairdocs.org/sdr/FDEA202502190251.md): Link Assy · disconnected · Feb 19, 2025 · N277FE · Boeing 7673S2F · Engine Thrust Reverser
  > #2 ENG LH T/R, FWD HINGE STRUT FITTING LINK NOT CONNECTED TO T/R HINGE FITTING AND IS DAMAGED. 0000862587: DERYCKE,CHRISTOPHE D - 24-FEB-2025 06:30 REMOVED AND REPLACED #2 ENG LH T/R, FWD HINGE LINK REF. W/C 7800000-01-02 (SEQ 901). REMOVED AND REPLACED #
- [SDR FDEA202502190250](https://openairdocs.org/sdr/FDEA202502190250.md): Link Assy · gouged · Feb 19, 2025 · N277FE · Boeing 7673S2F · Engine Thrust Reverser
  > #2 ENG RH T/R, FWD HINGE STRUT FITTING LINK NOT CONNECTED TO T/R HINGE FITTING AND IS DAMAGED. REMOVED AND REPLACED #2 ENG RH T/R, FWD HINGE LINK REF. W/C 7800000-02-02 (SEQ 901).
- [SDR FDEA202309251658](https://openairdocs.org/sdr/FDEA202309251658.md): Slat · chafed · Sep 25, 2023 · N277FE · Boeing 767300 · Leading Edge Devices
  > FOUND LH SLAT #5 TO HAVE TRAILING EDGE DAMAGE AT STA 499. 0000583927: MAZELIN, MATTHEW J - 27-SEP-2023 09:26 COMPLETED REPAIR OF #5 SLAT BY TRIMMING, SEALING AND PAINTING REPAIR REF SRM 57-43-02-2R, SRM 51-70-10- 2R AND AMM 51-21-00-07. SEE JPF FOR ALL OTHE
- [SDR FDEA202304270770](https://openairdocs.org/sdr/FDEA202304270770.md): Unknown · unknown · Apr 27, 2023 · N277FE · Boeing 767300 · Leading Edge Slat Control System
  > ON APP RECEIVED LEADING EDGE LIGHT, AIRPLANE WAS FULLY CONFIGURED WITH FLAPS 25. RAN THE QRH FOR LE SLAT DISAGREE AND FOLLOWED THE CHECK LIST TO THE LEADING EDGE SLAT ASYMMETRY CHECK LIST. THE AIRPLANE FLEW NORMALLY WITH NO ASYMMETRIC INPUTS. NO ASSOCI
- [SDR FDEA202304080602](https://openairdocs.org/sdr/FDEA202304080602.md): Panel · dented · Apr 8, 2023 · N277FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222AFF, WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022.
- [SDR FDEA202304080601](https://openairdocs.org/sdr/FDEA202304080601.md): Panel · dented · Apr 8, 2023 · N277FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 CFF, WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC 15/2022
- [SDR FDEA202304080600](https://openairdocs.org/sdr/FDEA202304080600.md): Panel · dented · Apr 8, 2023 · N277FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF, WITH DENTS MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF WAS REPAIRED I.A.W. B767 SRM 53- 00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV 85 DEC. 15/2022
- [SDR FDEA202304080599](https://openairdocs.org/sdr/FDEA202304080599.md): Panel · dented · Apr 8, 2023 · N277FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221CFF, WITH DENTS. MAIN CARTGO COMPARTMENT ACCESS FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR.4.B. FIG.201 SHEET 2 REV.85 DEC 15/2022.
- [SDR FDEA202304080598](https://openairdocs.org/sdr/FDEA202304080598.md): Panel · dented · Apr 8, 2023 · N277FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222BFF, WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC 15/2022
- [SDR FDEA202206021368](https://openairdocs.org/sdr/FDEA202206021368.md): Former · cracked · Jun 2, 2022 · N277FE · Boeing 767300 · Wing Main, Frame Structure
  > CRACKED FORMER 114T2171-5 WITH LOOSE/DAMAGED FASTENERS LOCATED AT LS FLE OSS 441. REPLACED BRACKET AS REQUIRED PER EA H-5720-T0368775 REV A PT1.
- [SDR FDEA202206021367](https://openairdocs.org/sdr/FDEA202206021367.md): Former · cracked · Jun 2, 2022 · N277FE · Boeing 767300 · Wing Main, Frame Structure
  > CRACKED FORMER 114T2511-13 WITH LOOSE/DAMAGED FASTENERS LOCATED AT LS FLE OSS 499 REPAIRED FORMER REF EA H-5720-T0368775 A P1
- [SDR FDEA202206021366](https://openairdocs.org/sdr/FDEA202206021366.md): Former · cracked · Jun 2, 2022 · N277FE · Boeing 767300 · Wing Main, Frame Structure
  > CRACKED FORMER 114T 2511-14 LOOSE/DAMAGED FASTENERS LOCATED AT RS FLE OSS 499 REPLACED CRACKED FORMER AND REPLACED LOOSE RIVETS. REF. E.A. H-5720-T0368775 A P1
- [SDR FDEA202206021365](https://openairdocs.org/sdr/FDEA202206021365.md): Former · cracked · Jun 2, 2022 · N277FE · Boeing 767300 · Wing Main, Frame Structure
  > CRACKED FORMER 114T2170-6 LOOSE/DAMAGED FASTENERS LOCATED AT RS FLE OSS 441. REMOVED AND REPLACED CRACKED FORMER REF E.A H-5720-T0368775 A P1
- [SDR FDEA202111232944](https://openairdocs.org/sdr/FDEA202111232944.md): Autopilot Sys · faulted · Nov 23, 2021 · N277FE · Boeing 767300 · Autopilot System
  > PASSING 32,000 ON CLIMB OUT, WITH LT AUTOPILOT ENGAGED, RECEIVED A/P EICAS ALONG WITH A/P LIGHT ON UPPER FORWARD INST PANEL. A/P REMAINED ENGAGED. DISENGAGED A/P & REENGAGED LT A/P. AFTER PASSING 36,000 RECEIVED A/P EICAS AGAIN. MANUALLY DISCONNECTING A/P

## 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 = 'N277FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N277FE/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.