# Service difficulty reports: N276FE A list on [N276FE](https://openairdocs.org/aircraft/N276FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202508201516](https://openairdocs.org/sdr/FDEA202508201516.md): Battery Pack · no test · Aug 20, 2025 · N276FE · Boeing 7673S2F · Emergency Lighting > DURING POST FLIGHT FOUND EMERGENCY LIGHTS WILL NOT TURN ON REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER AMM. A/C OK FOR SERVICE. - [SDR FDEA202505260805](https://openairdocs.org/sdr/FDEA202505260805.md): Floor Panel · dented · May 26, 2025 · N276FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231RFF DENTED, APPROXIMATELY STATION 770 LBL 6. GM34 FABRICATED NEW FLOOR PANEL 241 AFF MPN:145T5876-38 LBL 11, RBL 11, STATION: 731.11 - STATION: 850 IN REF. TO DRW 145T5876-38 AND B767 SRM 53-00-50-2R. THIS IS A - [SDR FDEA202502200255](https://openairdocs.org/sdr/FDEA202502200255.md): Skin · chafed · Feb 20, 2025 · N276FE · Boeing 7673S2F · Rudder, Plate/Skin > RUDDER CAP AFT UPPER LH INTERIOR COMPOSITE DAMAGED. BONDED A (1X1 INCH) SANDING PLY ON THE RUDDER CAP AFT UPPER LH INTERRIOR AREA. IN REF. TO 767 SRM: 55-40-30-2R FIG.201 SHEET:2 AND 767 SRM 51-70-17. RE-APLIED PRIMER IN THE INNER SURFACE IN REF. TO 767 A - [SDR FDEA202502180244](https://openairdocs.org/sdr/FDEA202502180244.md): Fairing · damaged · Feb 18, 2025 · N276FE · Boeing 7673S2F · Rudder, Plate/Skin > RUDDER CAP HAS A LIGHTNING STRIKE LOCATED 12" FROM L/E. REPAIRED AND BLENDED RUDDER CAP, AREA IS WITHIN ALLOWABLE DAMAGE LIMITS PER EVALUATION IN REF. TO B767 SRM 51-70-14-0G, PREPPED, PRIMED AND PAINTED IN REF. TO AMM 51-21-00-7. REFER TO JPF FOR OTHER W - [SDR FDEA202502100205](https://openairdocs.org/sdr/FDEA202502100205.md): Floor Panel · damaged · Feb 10, 2025 · N276FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 242VFF HAS PUNCHER. REPAIRED MAIN DECK CARGO COMPARTMENT FLOORBOARD PANEL #242VFF P/N 145T5876-114AT STA 984.95 TO STA1087 RBL74.25 TO RBL 86.25 IN REF TO SRM 53-00-50-2R FIG 201 REPAIR 1 SHEET 1. SEE JPF FOR OTHER WORK ACCOMPLISHED. - [SDR FDEA202502100204](https://openairdocs.org/sdr/FDEA202502100204.md): Floor Panel · damaged · Feb 10, 2025 · N276FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 241QFF IS DELAMINATED ON BOTTOM SIDE CORNER OF PANEL. REPAIRED MAIN DECK CARGO COMPARTMENT FLOORBOARD PANEL #241QFF P/N 145T5876-15 AT STA 933 TO STA 984.95 LBL 77.50 TO LBL 89.50 IN REF TO SRM 53-00.50.2R FIG 201 REPAIR 1 SHEET 1. T - [SDR FDEA202502100203](https://openairdocs.org/sdr/FDEA202502100203.md): Floor Panel · damaged · Feb 10, 2025 · N276FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 242WFF SCREW INSERTS PULLED THROUGH. REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 971.82 - 1114.82, RBL 33"- RBL 54.75" (MPN: 145T5876-112 / PNL# 242WFF) IN REF. B767 SRM 53-00-50-2R FIG.201 REPAIR 1 SHEET 1. THIS IS A MAJOR REPAIR. - [SDR FDEA202502100202](https://openairdocs.org/sdr/FDEA202502100202.md): Floor Panel · damaged · Feb 10, 2025 · N276FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 241AGF HAS PUNCTURE. REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 984.95- 1087, LBL 77.50"- LBL 89.50" (MPN: 145T5876-113 / PNL# 241AGF) IN REF. B767 SRM 53-00-50-2R FIG.201 REPAIR 1 SHEET 1. SEE JPF FOR OTHER WORK ACCOMPLISHED. THIS - [SDR FDEA202502100201](https://openairdocs.org/sdr/FDEA202502100201.md): Floor Panel · damaged · Feb 10, 2025 · N276FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 241ZFF HAS DAMAGE. REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 971.82 - 1114.82, LBL 54.75"- LBL 77.50" (MPN: 141T5876-111 / PNL# 241ZFF) IN REF. B767 SRM 53-00-50-2R FIG.201 REPAIR 1 SHEET 1. SEE JPF FOR OTHER WORK ACCOMPLISHED. THI - [SDR FDEA202502100200](https://openairdocs.org/sdr/FDEA202502100200.md): Floorboard · damaged · Feb 10, 2025 · N276FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 241WFF HAS DAMAGE. REPAIRED MAIN DECK CARGO COMPARTMENT FLOORBOARD PANEL #241WFF P/N 145T5876-51 AT STA 971.82 TO 1114.82 LBL11" TO RBL 11" IN REF TO SRM 53-00-50-2R FIG. 201 REPAIR 1 SHEET 1. SEE JPF FOR OTHER WORK ACCOMPLISHED. THI - [SDR FDEA202404260297](https://openairdocs.org/sdr/FDEA202404260297.md): Switch · failed · Apr 26, 2024 · N276FE · Boeing 7673S2F · Light System Wiring > AIRPLANE HAD A STRONG ACRID SMOKE SMELL WHEN RUNWAY TURNOFF LIGHT WERE TURNED ON. FOUND RIGHT RUNWAY TURNOFF SWITCH BAD. WHEN SWITCH ACTIVATED SMOKE EMITS FROM RT RUNWAY TURNOFF SWITCH. REMOVED AND REPLACED OVERHEAD PANEL P5 PER SMP, OPS CHECK LIGHT FUN - [SDR FDEA202210072515](https://openairdocs.org/sdr/FDEA202210072515.md): Wedge · gouged · Oct 7, 2022 · N276FE · Boeing 7673S2F · Leading Edge Devices > RS WING #8 SLAT AT FLE OSS 499 ON TRAILING EDGE UNDERNEATH AT GOUGED (1" FWD OF TRAILING EDGGE) #8 SLAT GOUGED AREA ON LWR TRAILING EDGE WEDGE, REPAIR DONE AT RS SLAT LOCATION OSS 499 (SIZE 2.4Ï¿½ X.3Ï¿½) USING EA H-5750-T0371016P1 (REPAIR & RSC EA) & 767 - [SDR FDEA202210072513](https://openairdocs.org/sdr/FDEA202210072513.md): Former · cracked · Oct 7, 2022 · N276FE · Boeing 7673S2F · Wing Main, Frame Structure > R/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-14) REPLACED PARTS WITH NEW FORMER B67-57-002-04 ALONG WITH ANGLE B67-57-003-04 ON RS FOR FLE OSS 499, ATTACH FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND N - [SDR FDEA202210072512](https://openairdocs.org/sdr/FDEA202210072512.md): Former · cracked · Oct 7, 2022 · N276FE · Boeing 7673S2F · Wing Main, Frame Structure > R/H WING AT STATION OSS.441 L/E FORMER IS CRACKED (P/N: 114T2170-6) REPLACED PARTS WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FOR FLE OSS 441, ATTACHED FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND - [SDR FDEA202210072511](https://openairdocs.org/sdr/FDEA202210072511.md): Former · cracked · Oct 7, 2022 · N276FE · Boeing 7673S2F · Wing Main, Frame Structure > L/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-13) REPLACED PARTS WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON LS FOR FLE OSS 499, ATTACH FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND N - [SDR FDEA202210072510](https://openairdocs.org/sdr/FDEA202210072510.md): Former · cracked · Oct 7, 2022 · N276FE · Boeing 7673S2F · Wing Main, Frame Structure > L/H WING AT STATION OSS.441 L/E FORMER IS CRACKED (P/N: 114T2170-5) REPLACED PARTS WITH NEW FORMER B67-57-002-01 ALONG WITH ANGLE B67-57-003-01 ON LS FOR FLE OSS 441, ATTACHED FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND ## 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 = 'N276FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N276FE/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.