# Service difficulty reports: N186FE A list on [N186FE](https://openairdocs.org/aircraft/N186FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 54 reports - [SDR FDEA202606160766](https://openairdocs.org/sdr/FDEA202606160766.md): Floor Panel · punctured · Jun 16, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL ON 242HFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 242HFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-G (2) FIG 201 SHEET 5 REV. 94. - [SDR FDEA202606140736](https://openairdocs.org/sdr/FDEA202606140736.md): Floor Panel · cracked · Jun 14, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > CRACK ON LOWER SURFACE OF FLOOR PANEL 241WFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241WFF ON MAIN CARGO COMPARTMENT WAS REPAIRED I.A.W. B767 SRM 53-00-50- 2R PAR. 4-B FIG.201 SHEET 2 REV.94. - [SDR FDEA202606140734](https://openairdocs.org/sdr/FDEA202606140734.md): Floor Panel · damaged · Jun 14, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > TWELVE CRACKS ON UPPER SURFACE OF FLOOR PANEL 241WFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241WFF ON MAIN CARGO COMPARTMENT WAS REPAIRED I.A.W. B767 SRM 53-00- 50-2R PAR. 4-B FIG.201 SHEET 2 REV.94. - [SDR FDEA202606140733](https://openairdocs.org/sdr/FDEA202606140733.md): Floor Panel · damaged · Jun 14, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > TWO PUNCTURES ON FLOOR PANEL 241EFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241EFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV. 94. - [SDR FDEA202606110724](https://openairdocs.org/sdr/FDEA202606110724.md): Skin · punctured · Jun 11, 2026 · N186FE · Boeing 7673S2F · Trailing Edge Flaps > SECONDARY FINDING, PUNCTURE ON HONEYCOMB OF THE RIGHT OUTBOARD FLAP AT UPPER PANEL, OTEF 89.25 AND 9" FROM LEADING EDGE HONEYCOMB OF THE RIGHT OUTBOSRD FLAP AT UPPER PANEL, OTEF 89.25 AND 9" FROM LEADING EDGE WAS REPAIRED IAW B767 SRM 57-53-01-1A AND SRM 5 - [SDR FDEA202606110723](https://openairdocs.org/sdr/FDEA202606110723.md): Floor Panel · cracked · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > CRACK ON FLOOR PANEL ON 242TFA ON MAIN CARGO COMPARTMENT FLOOR PANEL 242TFA ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R REV 94 DEC 15/2025 - [SDR FDEA202606110722](https://openairdocs.org/sdr/FDEA202606110722.md): Floor Panel · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATION ON FLOOR PANEL 241EFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241EFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G (2) FIG. 201 DETAIL V REV. 94 DEC 15/2025. - [SDR FDEA202606110721](https://openairdocs.org/sdr/FDEA202606110721.md): Floor Panel · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED LOWER SURFACE EDGES ON FLOOR PANEL 241DFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241DFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G (2) FIG 201 DETAIL V REV 94 DEC 15/2025 - [SDR FDEA202606110720](https://openairdocs.org/sdr/FDEA202606110720.md): Floor Panel · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED CORNER ON FLOOR PANEL 241HFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241HFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G (2) FIG. 201 DETAIL V REV 94 DEC 15/2025 - [SDR FDEA202606110719](https://openairdocs.org/sdr/FDEA202606110719.md): Floor Panel · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED EDGES OF FLOOR PANEL ON 242HFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 242HFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G (2) FIG 201 DETAIL V REV. 94 DEC 15/2025 - [SDR FDEA202606110718](https://openairdocs.org/sdr/FDEA202606110718.md): Floor Panel · punctured · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL ON 242HFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 242HFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-G (2) FIG. 201 SHEET 5 REV. 94. - [SDR FDEA202606110717](https://openairdocs.org/sdr/FDEA202606110717.md): Floor Panel · cracked · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > CRACK ON LOWER SURFACE OF FLOOR PANEL ON 242EFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 242EFF 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 FDEA202606110716](https://openairdocs.org/sdr/FDEA202606110716.md): Floor Panel · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED EDGES ON LOWER SURFACE OF FLOOR PANEL ON 242AFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 242AFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G (2) FIG 201 SHEET 5 REV 94 DEC 15/2025 - [SDR FDEA202606110715](https://openairdocs.org/sdr/FDEA202606110715.md): Floor Panel · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED LOWER SURFACE ON EDGE OF FLOOR PANEL ON 242EFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 242EFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G (2) FIG 201 SHEET 5 REV 94 DEC 15/2025. - [SDR FDEA202606110714](https://openairdocs.org/sdr/FDEA202606110714.md): Floor Panel · punctured · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > THREE PUNCTURES ON LOWER SURFACE OF FLOOR PANEL 241LFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241LFF 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 FDEA202606110713](https://openairdocs.org/sdr/FDEA202606110713.md): Floor Panel · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED LOWER SURFACE EDGE ON FLOOR PANEL 241FFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241FFF IN MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15 2025 - [SDR FDEA202606110711](https://openairdocs.org/sdr/FDEA202606110711.md): Skin · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Trailing Edge Flaps > DELAMINATION ON L. EDGE SKIN AT 20" FROM OUTB EDGE. RH INB MAIN FLAP L. EDGE SKIN AT 20" FROM OUTB EDGE RH INB MAIN FLAP WAS REPAIRED IAW B767 SRM 57-53-01- 2R FIG 201 REP 1 SHEET 5 AND 51-70-17-0G REV 94 DEC 15/2025 - [SDR FDEA202606110710](https://openairdocs.org/sdr/FDEA202606110710.md): Skin · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Trailing Edge Flaps > DELAMINATION ON L. EDGE SKIN AT 32" FROM OUTB EDGE. RT INBD MAIN FLAP L. EDGE SKIN AT 32" FROM OUTB EDGE RH INBD MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R AND 51-70-17-0G, REV 94. DEC 15/2025 - [SDR FDEA202606110709](https://openairdocs.org/sdr/FDEA202606110709.md): Floor Panel · punctured · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 241KFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241KFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIGURE 201 SHEET 2 REV. 94 DEC 15/2025 - [SDR FDEA202606110708](https://openairdocs.org/sdr/FDEA202606110708.md): Floor Panel · punctured · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 241QFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241QFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025 - [SDR FDEA202606110707](https://openairdocs.org/sdr/FDEA202606110707.md): Floor Panel · delaminated · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED CORNER ON FLOOR PANEL 241KFF ON MAIN CARGO COMPARTMENT CORNER ON FLOOR PANEL 241KFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4F, FIGURE 201, SHEET 2, REV 94. - [SDR FDEA202606110706](https://openairdocs.org/sdr/FDEA202606110706.md): Floor Panel · cracked · Jun 11, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > CRACK ON LOWER SURFACE OF FLOOR PANEL ON 242UFF ON MAIN CARGO COMPARTMENT LOWER SURFACE OF FLOOR PANEL ON 242UFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R, PAR F FIG 201, SHEET 2, REV 94. DEC 15/2025. - [SDR FDEA202606080687](https://openairdocs.org/sdr/FDEA202606080687.md): Floor Panel · delaminated · Jun 8, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED CORNER ON FLOOR PANEL ON 241AFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241AFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G(2) FIG.201 DETAIL V REV. 94. - [SDR FDEA202606080686](https://openairdocs.org/sdr/FDEA202606080686.md): Floor Panel · damaged · Jun 8, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED CORNER OF FLOOR PANEL ON 242UFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 242UFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G(2) FIG.201 DETAIL V REV 94. - [SDR FDEA202606080685](https://openairdocs.org/sdr/FDEA202606080685.md): Floor Panel · damaged · Jun 8, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED CORNER ON FLOOR PANEL ON 242LFA ON MAIN CARGO COMPARTMENT FLOOR PANEL 242LFA ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-G(2) FIG 201 DETAIL V REV 94. - [SDR FDEA202606080684](https://openairdocs.org/sdr/FDEA202606080684.md): Floor Panel · damaged · Jun 8, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED CORNER ON FLOOR PANEL 241MFF ON MAIN CARGO COMPARTMENT FLOOR PANEL 241MFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4.G(2) FIG. 201 DETAIL V REV 94 - [SDR FDEA202606080683](https://openairdocs.org/sdr/FDEA202606080683.md): Floor Panel · damaged · Jun 8, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DELAMINATED CORNER ON FLOOR PANEL ON 242BFA ON MAIN CARGO COMPARTMEN FLOOR PANEL 242BFA ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50-2R PAR 4.G(2) FIG. 201 DETAIL V REV 94. - [SDR FDEA202606010663](https://openairdocs.org/sdr/FDEA202606010663.md): Floor Panel · damaged · Jun 1, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 242 GFF MDCC. FLOOR PANEL 242GFF MDCC WAS REPAIRED I.A.W SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV 94. - [SDR FDEA202606010662](https://openairdocs.org/sdr/FDEA202606010662.md): Floor Panel · damaged · Jun 1, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PLANEL 241 WFF MDCC. FLOOR PANEL 241 WFF MDCC WAS REPAIRED I.A.W SRM 53-00-50-2R PAR 4.B FIG. 201 SHEET 2 REV 94. - [SDR FDEA202606010660](https://openairdocs.org/sdr/FDEA202606010660.md): Floor Panel · delaminated · Jun 1, 2026 · N186FE · Boeing 7673S2F · Fuselage Main, Structure > DENT WITH DELAMINATION ON FLOOR PANEL 242HFF MDCC FLOOR PANEL 242HFF MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. - [SDR FDEA202605280646](https://openairdocs.org/sdr/FDEA202605280646.md): Floor Panel · cracked · May 28, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > THREE PUNCTURES ON FLOOR PANEL 231QFF MDCC. FLOOR PANEL 231QFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC. 15/2025 - [SDR FDEA202605280645](https://openairdocs.org/sdr/FDEA202605280645.md): Floor Panel · delaminated · May 28, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > TWO DELAMINATIONS ON FLOOR PANEL 231QFF MDCC. FLOOR PANEL 231QFF MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC 15/2025 - [SDR FDEA202605280644](https://openairdocs.org/sdr/FDEA202605280644.md): Floor Panel · worn · May 28, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > EXPOSED HONEY COMB ON FLOOR PANEL 231EFF AT MDCC. FLOOR PANEL 231EFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC. 15/2025 - [SDR FDEA202605280643](https://openairdocs.org/sdr/FDEA202605280643.md): Floor Panel · delaminated · May 28, 2026 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > DENT WITH DELAMINATION ON FLOOR PANEL 231FFF MDCC. FLOOR PANEL 231FFF MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. - [SDR FDEA202407040934](https://openairdocs.org/sdr/FDEA202407040934.md): Escape Rope · stuck · Jul 4, 2024 · N186FE · Boeing 7673S2F · Emergency Equipment > ESCAPE ROPE CAUGHT IN DOOR TRACK. ESCAPE ROPE RETAINER DAMAGED. FREED EMERGENCY ESCAPE ROPE AND INSPECTED LOWER PORTION FOR DAMAGE REF AMM 25-61-02-2. NO DEFECTS NOTED. REPLACED ESCAPE ROPE RETAINER. - [SDR FDEA202405300753](https://openairdocs.org/sdr/FDEA202405300753.md): Floor Panel · dented · May 30, 2024 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 242TFA, SKIN WITH DENT. MDC, FLOOR PANEL 242TFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023 - [SDR FDEA202405300751](https://openairdocs.org/sdr/FDEA202405300751.md): Skin · dented · May 30, 2024 · N186FE · Boeing 7673S2F · Leading Edge Devices > SLAT #2, UPPER WEDGE, EXTERNAL SURFACE WITH 4 DENTS LOCATED AT 38.5" OF INBOARD FRAME OF SLAT AND 5" OF TE APPROX. SLAT #2, UPPER WEDGE, EXTERNAL SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R PAG 1-2 NOTE B AND SRM 51-70-10-2R REP 4 FIG 201 (SHEET 1) PAG 1 - [SDR FDEA202405300746](https://openairdocs.org/sdr/FDEA202405300746.md): Floor Panel · dented · May 30, 2024 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 222CFF, SKIN WITH DENTS. MDC, FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023 - [SDR FDEA202405300745](https://openairdocs.org/sdr/FDEA202405300745.md): Floor Panel · dented · May 30, 2024 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 221CFF, SKIN WITH DENTS. MDC, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023 - [SDR FDEA202405300744](https://openairdocs.org/sdr/FDEA202405300744.md): Floor Panel · dented · May 30, 2024 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 222BFF, SKIN WITH DENTS. MDC, FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023 - [SDR FDEA202405290743](https://openairdocs.org/sdr/FDEA202405290743.md): Floor Panel · dented · May 29, 2024 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 222AFF, SKIN WITH DENTS. MDC, FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023 - [SDR FDEA202405290742](https://openairdocs.org/sdr/FDEA202405290742.md): Floor Panel · dented · May 29, 2024 · N186FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 221DFF, SKIN WITH DENTS. MDC, FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023 - [SDR FDEA202205281320](https://openairdocs.org/sdr/FDEA202205281320.md): Angle · cracked · May 28, 2022 · N186FE · Boeing 767300 · Wing Miscellaneous Structure > RH WING OUTBD FIXED LEADING EDGE FORMER ATTACH ANGLE IS CRACKED AT RIB #5 REMOVED AND REPLACED THE RH WING O/B FIXED L/E FORMER ATTACH ANGLE AT STA OSS 437 IAW FEDEX EA H-5720-T0368613-P1, TITLE: WING - SECONDARY WING STRCT - FIELD SERVICE EVALUATION, RH W - [SDR FDEA202205281319](https://openairdocs.org/sdr/FDEA202205281319.md): Wedge · damaged · May 28, 2022 · N186FE · Boeing 767300 · Trailing Edge Flaps > RIGHT WING INBOARD AFT FLAP TRAILING EDGE DAMAGED REPAIRED RIGHT WING INBOARD AFT FLAP TRAILING EDGE IAW B767 SRM 57-53-01-2R FIG 201 SHEET 4 REPAIR 1 AND 51-70-10-2R. - [SDR FDEA202205281318](https://openairdocs.org/sdr/FDEA202205281318.md): Former · cracked · May 28, 2022 · N186FE · Boeing 767300 · Wing Main, Frame Structure > RH WING FIXED LEADING EDGE FORMER IS CRACKED AT RIB #13 REMOVED AND REPLACED THE R/H WING O/B FIXED LEADING EDGE NOSE FORMER AT OSS 499 IAW FEDEX EA H-5720-T0368613-P1, TITLE: WING - SECONDARY WING STRCT - FIELD SERVICE EVALUATION, RH WING OSS 437 AND LH & - [SDR FDEA202205271316](https://openairdocs.org/sdr/FDEA202205271316.md): Splice · cracked · May 27, 2022 · N186FE · Boeing 767300 · Wing, Plate/Skin > LW L/E SKIN SPLICE IS CRACKED AT LES 500.10 REMOVED AND REPLACED LH WING L/E SKIN SPLICE LES 500.10 (OSS 515) IAW B767 SRM 51-40-02- 0G AND BAC DWG 114T2800, REV. - - [SDR FDEA202205271315](https://openairdocs.org/sdr/FDEA202205271315.md): Former · cracked · May 27, 2022 · N186FE · Boeing 767300 · Wing Main, Frame Structure > LW AT THE #5 SLAT OTBD AUX TRACK, THE OTBD NOSE FORMER IS CRACKED REMOVED AND REPLACED THE OUTBOARD NOSE FORMER AT LW OSS 499 AT THE #5 SLAT O/B AUX TRACK IAW FEDEX EA H-5720-T0368613-P1, TITLE: WING - SECONDARY WING STRCT - FIELD SERVICE EVALUATION, RH WI - [SDR FDEA202205271314](https://openairdocs.org/sdr/FDEA202205271314.md): Former · cracked · May 27, 2022 · N186FE · Boeing 767300 · Wing Main, Frame Structure > LW L/E OSS 441 OTBD NOSE FORMER IS CRACKED REMOVED AND REPLACED THE LW LE NOSE FORMER AT OSS 441 IAW FEDEX EA H-5720-T0368613- P1, TITLE: WING - SECONDARY WING STRCT - FIELD SERVICE EVALUATION, RH WING OSS 437 AND LH & RH 441 & 499, LEADING EDGE NOSE FORMER - [SDR FDEA202205271313](https://openairdocs.org/sdr/FDEA202205271313.md): Former · cracked · May 27, 2022 · N186FE · Boeing 767300 · Wing Miscellaneous Structure > RH WING OUTBD FIXED LEADING EDGE FORMER IS CRACKED AT RIB #6 REMOVED AND REPLACED RH WING OB LE FORMER AT RIB #6, REF. FEDEX EA H-5720-T0368613- P1, TITLE: WING-SECONDARY WING STRCT-FIELD SERVICE EVALUATION, RH WING OSS 437 AND LH & RH 441 & 499, LEADING ED - [SDR FDEA202205251296](https://openairdocs.org/sdr/FDEA202205251296.md): Clamp · cracked · May 25, 2022 · N186FE · Boeing 767300 · Wing Main, Frame Structure > RIGHT WING LEADING EDGE FUEL PANEL IB HOLD OPEN BRACKET ATTACH ANGLE IS CRACKED REMOVED & REPLACED CLIP IAW BAC DWG 114T2450, SHEET 19, REV - Next page: https://openairdocs.org/aircraft/N186FE/reports.md?page=2 ## 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 = 'N186FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N186FE/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.