# Service difficulty reports: N105FE A list on [N105FE](https://openairdocs.org/aircraft/N105FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202411231726](https://openairdocs.org/sdr/FDEA202411231726.md): Skin · damaged · Nov 23, 2024 · N105FE · Boeing 7673S2F · Fuselage Main, Plate/Skin > UPPER FUSELAGE SKIN BETWEEN STA 412/434 AND STG 8/9 RH WITH LIGHTNING STRIKE. UPPER FUSELAGE SKIN BETWEEN STA 412/434 AND STG 8/9 DAMAGE WAS REPAIRED I.A.W. E.A. #: H-5330-T0381396 RELEASE DATE: NOV 23, 2024 THE FIRST INSPECTION TO BE REALISED ON 30,000 CYC - [SDR FDEA202411221721](https://openairdocs.org/sdr/FDEA202411221721.md): Skin · damaged · Nov 22, 2024 · N105FE · Boeing 7673S2F · Fuselage Main, Plate/Skin > UPPER FUSELAGE SKIN BETWEEN STA 347/368 AND STG 9/10 RH WITH LIGTINING STRIKE DAMAGE ON UPPER FUSELAGE SKIN BETWEEN STA 347/368 AND STGR 9/10 RH WAS REPAIRED I.A.W. SRM 53-00-01-2R REPAIR 29 REV 90 AUG 15, 2024. THE FIRST INSPECTION TO BE REALISED ON 30,00 - [SDR FDEA202411201707](https://openairdocs.org/sdr/FDEA202411201707.md): Floor Panel · cracked · Nov 20, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 251NFF WITH CRACK MAIN CARGO COMPARTMENT, FLOOR PANEL 251NFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024 - [SDR FDEA202411191686](https://openairdocs.org/sdr/FDEA202411191686.md): Floor Panel · cracked · Nov 19, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 242TFA WITH PUNCTURE. MAIN DECK CARGO FLOOR PANEL 242 TFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV 90. - [SDR FDEA202411121671](https://openairdocs.org/sdr/FDEA202411121671.md): Skin · dented · Nov 12, 2024 · N105FE · Boeing 7673S2F · Trailing Edge Flaps > RH WING, DENT ON LOWER SKIN FLAP OUTBOARD, 23 TO LOWER EDGE AND 12 TO FAIRING. RH WING, LOWER SKIN FLAP OUTBOARD, 23 TO LOWER EDGE AND 12 TO FAIRING WAS REPAIRED IAW B767 SRM 51-70-10-2R REP 4 FIG 202 (SHEET 3) AND SRM 57-53-01-2R FIG 201 REP 1 (SHEE - [SDR FDEA202411121670](https://openairdocs.org/sdr/FDEA202411121670.md): Skin · dented · Nov 12, 2024 · N105FE · Boeing 7673S2F · Trailing Edge Flaps > RIGHT WING, INBOARD TRAILING EDGE FLAP (ZONE 655) WITH DENT. RIGHT WING, INBOARD TRAILING EDGE FLAP (ZONE 655) WAS REPAIRED IAW B767 SRM 57-53-01- 2R REP 1 FIG 201 (SHEET 4) AND SRM 51-70-10-2R REP 4 FIG 201 (SHEET 1) REV 90 AUG 15/2024 - [SDR FDEA202411091655](https://openairdocs.org/sdr/FDEA202411091655.md): Floor Panel · damaged · Nov 9, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > UPPER HALF FUSELAGE, MAIN DECK FLOOR PANEL 241 LFF, OUTTER SKIN, DISBONDED CORNER. MAIN DECK CARGO FLOOR PANEL 241LFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.G(2)(A) FIGURE 201 DETAIL V REV 90 AUG 15/2024 - [SDR FDEA202411091654](https://openairdocs.org/sdr/FDEA202411091654.md): Floor Panel · damaged · Nov 9, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > UPPER HALF FUSELAGE, MAIN DECK FLOOR PANEL 241 DFF, DISBONDED IN THE CORNER. MAIN DECK CARGO FLOOR PANEL 241DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.G(2)(A) FIGURE 201 DETAIL V REV 90 AUG 15/2024 - [SDR FDEA202411091653](https://openairdocs.org/sdr/FDEA202411091653.md): Floor Panel · cracked · Nov 9, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 251JFF BROKEN. MAIN DECK CARGO FLOOR PANEL 251JFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90. - [SDR FDEA202411091652](https://openairdocs.org/sdr/FDEA202411091652.md): Floor Panel · cracked · Nov 9, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 222BFF DAMAGED. MAIN CARGO COMPARTMENT, FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024 - [SDR FDEA202411091651](https://openairdocs.org/sdr/FDEA202411091651.md): Floor Panel · cracked · Nov 9, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 222AFF DAMAGED. MAIN DECK CARGO FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV 90 AUG 15/2024 - [SDR FDEA202411061646](https://openairdocs.org/sdr/FDEA202411061646.md): Floor Panel · dented · Nov 6, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK COMPARTMENT FLOOR PANEL 241WFF WITH CRACKS AND DENTS. MAIN DECK CARGO FLOOR PANEL 241 WFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV 90 AUG 15/2024. - [SDR FDEA202411061645](https://openairdocs.org/sdr/FDEA202411061645.md): Floor Panel · cracked · Nov 6, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > UPPER HALF FUSELAGE, MAIN DECK FLOOR PANEL 241 EFF, SEVERAL PUNCTURES. MAIN DECK CARGO FLOOR PANEL 241 EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV 90 AUG 15/2024. - [SDR FDEA202411061644](https://openairdocs.org/sdr/FDEA202411061644.md): Floor Panel · cracked · Nov 6, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK COMPARTMENT FLOOR PANEL 241AFF WITH PUNCTURES AND DISBOND. MAIN DECK CARGO FLOOR PANEL 241 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV 90 AUG 15/2024. - [SDR FDEA202411061643](https://openairdocs.org/sdr/FDEA202411061643.md): Floor Panel · cracked · Nov 6, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 251CFF BROKEN. MAIN DECK CARGO FLOOR PANEL 251 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV 90. - [SDR FDEA202411061642](https://openairdocs.org/sdr/FDEA202411061642.md): Floor Panel · dented · Nov 6, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > UPPER HALF FUSELAGE, MAIN DECK FLOOR PANEL 241 ZFF WITH DENT. MAIN DECK CARGO FLOOR PANEL 241 ZFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV 90 AUG 15/2024. - [SDR FDEA202411061641](https://openairdocs.org/sdr/FDEA202411061641.md): Floor Panel · cracked · Nov 6, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > UPPER HALF FUSELAGE, MAIN DECK FLOOR PANEL 241 YFA, INNER SKIN, WITH SEVERAL PUNCTURE. MAIN DECK CARGO FLOOR PANEL 241 YFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV 90 AUG 15/2024. - [SDR FDEA202411061640](https://openairdocs.org/sdr/FDEA202411061640.md): Floor Panel · cracked · Nov 6, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 232NFF WITH CRACK MAIN CARGO COMPARTMENT FLOOR PANEL 232NFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4.B REV.90 - [SDR FDEA202411061639](https://openairdocs.org/sdr/FDEA202411061639.md): Floor Panel · cracked · Nov 6, 2024 · N105FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN CARGO COMPARTMENT, FLOOR PANEL 231QFF DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL 231QFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B REV 90 AUG 15/2024 - [SDR FDEA202101180148](https://openairdocs.org/sdr/FDEA202101180148.md): Attach Angle · cracked · Jan 18, 2021 · N105FE · Boeing 7673S2F · Nacelle/Pylon, Attach Fittings > NR 1 PYLON AFT FIXED FAIRING FRAME AFT OF HYD BAY, AFT INBOARD SIDE CENTER ATTACH CLIP CRACKED. REMOVED DAMAGE CLIP, LOCATED, DRILLED AND INSTALLED NEW CLIP (P/N 313T3380-69), IAW B767 SRM 51-40-02 & BAC DWG 313T1380, REV C. - [SDR FDEA202101180147](https://openairdocs.org/sdr/FDEA202101180147.md): Spar · cracked · Jan 18, 2021 · N105FE · Boeing 7673S2F · Nacelle/Pylon, Frame/Spar/Rib > NR 2 PYLON AFT FAIRING MID SPAR FITTING UPPER OUTBOARD CORNER IS CRACKED AT APPROXIMATELY NAC STA 327 RT INSTALLED REPAIR, IAW B767SRM 54-52-71-2R, FIG 201/REPAIR 4. REMOVED AND RE-INSTALLED LATCH BEAM, IAW BAC DWG 313T2303, REV. - [SDR FDEA202101170143](https://openairdocs.org/sdr/FDEA202101170143.md): Attach Angle · cracked · Jan 17, 2021 · N105FE · Boeing 7673S2F · Nacelle/Pylon, Attach Fittings > NR 2 PYLON AFT BULKHEAD TO AFT FAIRING INBOARD ATTACH CLIP IS CRACKED AT APPROXIMATELY NAC STA LT. REMOVED OLD CLIP AND INSTALLED NEW CLIP, IAW BAC DWG 313T2310 REV. - [SDR FDEA202101170141](https://openairdocs.org/sdr/FDEA202101170141.md): Former · cracked · Jan 17, 2021 · N105FE · Boeing 7673S2F · Wing Main, Frame Structure > RT WING LEADING EDGE NOSE FORMER CRACKED AT APPROXIMATELY OSS490. REMOVED OLD AND INSTALLED NEW NOSE FORMER, IAW BAC DWG 114T2511 REV D AND FED EX EA H-5720-TO359038 P1. - [SDR FDEA202101170140](https://openairdocs.org/sdr/FDEA202101170140.md): Former · cracked · Jan 17, 2021 · N105FE · Boeing 7673S2F · Wing Main, Frame Structure > LT WING LEADING EDGE FORMER CRACKED APPROXIMATELY OSS490. REMOVED OLD AND INSTALLED NEW NOSE FORMER, IAW BAC DWG 114T2511 REV D AND FED EX EA H-5720-TO 359039. - [SDR FDEA202101170138](https://openairdocs.org/sdr/FDEA202101170138.md): Former · cracked · Jan 17, 2021 · N105FE · Boeing 7673S2F · Wing Main, Frame Structure > LT WING LEADING EDGE NOSE FORMER CRACKED APPROXIMATELY OSS435. FABRICATED NEW NOSE FORMER AND INSTALLED, IAW BAC DWG 114T2171, REV- & EA H-5720- TO 359037. - [SDR FDEA202101160130](https://openairdocs.org/sdr/FDEA202101160130.md): Former · cracked · Jan 16, 2021 · N105FE · Boeing 7673S2F · Wing Main, Frame Structure > RT WING FIXED LEADING EDGE FORMER IS CRACKED AT OFSS 436. REMOVED AND REPLACED P/N 114T2170-6 AND 114T2171-3, IAW B767 SRM 51-40-02 AND FEDEX EA H-5720-T039040 P1. - [SDR FDEA202101150129](https://openairdocs.org/sdr/FDEA202101150129.md): Former · cracked · Jan 15, 2021 · N105FE · Boeing 7673S2F · Wing Spar > RT WING FIXED LEADING EDGE FORMER CRACKED AT APPROXIMATELY OSS663. REMOVED OLD AND INSTALLED NEW NOSE FORMER, IAW BAC DWG 114T2512 AND FED EX EA H- 5720-T0359036. - [SDR FDEA202101140102](https://openairdocs.org/sdr/FDEA202101140102.md): Panel · worn · Jan 14, 2021 · N105FE · Boeing 7673S2F · Wing, Plate/Skin > LEFT WING INBOARD AILERON REMOVABLE LEADING EDGE PANEL HAS EXPOSED COMPOSITE. REPAIRED LEFT WING INBOARD AILERON REMOVABLE LEADING EDGE PANEL, IAW B767 SRM 57-60-01-2R AND 51- 70-17-0G PARA 4G. - [SDR FDEA202101130078](https://openairdocs.org/sdr/FDEA202101130078.md): Skin Splice · cracked · Jan 13, 2021 · N105FE · Boeing 7673S2F · Wing, Plate/Skin > RIGHT WING FIXED LEADING EDGE SKIN SPLICE STRAP IS CRACKED AT APPROXIMATELY OSS 514.167. REMOVED AND REPLACED RT WING LEADING EDGE SKIN SPLICE STRAP P/N 114T2800-165, IAW B767 SRM 51-40-02 AND BAC DWG 114T2800 REV C. ## 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 = 'N105FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N105FE/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.