# Service difficulty reports: N751YX A list on [N751YX](https://openairdocs.org/aircraft/N751YX.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR R61A2025051500242](https://openairdocs.org/sdr/R61A2025051500242.md): Seat Track · corroded · Apr 27, 2025 · N751YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > CF3 AFT LH IB SEAT TRACK CORRODED FR 74LH TO FR84LH. MX REPAIRED SEAT TRACK IAE SRM 53-00-10 REPAIE 02. - [SDR R61A2025051500241](https://openairdocs.org/sdr/R61A2025051500241.md): Seat Track · corroded · Apr 27, 2025 · N751YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > CF3AFT RH IB SEAT TRACK CORRODED FR74-84. MX REPAIRED SEAT TRACK IAW SRM 53-00-10REPAIR 02. - [SDR R61A2025051500243](https://openairdocs.org/sdr/R61A2025051500243.md): Stiffener · cracked · Apr 24, 2025 · N751YX · Emb ERJ170200LR · Nacelle/Pylon Miscellaneous Structure > LH ENG OB TR REAR UPPER STIFFENER CRACKED. MX REPAIRED UPPER STIFFENER IAW ETD 2025-906814. - [SDR R61A2025051500240](https://openairdocs.org/sdr/R61A2025051500240.md): Doubler · dented · Apr 23, 2025 · N751YX · Emb ERJ170200LR · Fuselage Main, Plate/Skin > **MAJOR** CF1 EXT SKIN LH SIDE BTWN ST 13-14L AND FR 23-24 DENT FOUND. MX REPAIRED IAW ETD 2025-906817 AND SRM 51-10-05.**MAJOR** - [SDR R61A2022072000457](https://openairdocs.org/sdr/R61A2022072000457.md): Support · corroded · Jul 4, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE AC WAS IN FOR HVY CK FOUND INTERNAL FUSE CENTER SECTION 3 GALLEY SUPPORT U-CHANNEL FOUND CORRODED BTWN FR 87-88 RH SIDE. REPLACED SUPPORT PN 170-86131-001 IAW SRM 51-43-01, 51-41-01. AC WAS RETURNED TO SERVICE. - [SDR R61A2022071500442](https://openairdocs.org/sdr/R61A2022071500442.md): Support Channel · corroded · Jul 4, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CNTR FUSE III GALLEY SUPP U-CHANNEL AT FR 87-88 ON R/H UNDER SHEAR PNL CORRODED. R&R IAW SRM 51-43-01 AND 51-41-01. - [SDR R61A2022072000456](https://openairdocs.org/sdr/R61A2022072000456.md): Panel · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Floor Panel > WHILE AC WAS IN FOR HVY CK FOUND FWD SECTION INTERNAL FUSE CORROSION FOUND ON SILL PANEL RH SIDE OF FLOOR BTWN FR12-14. REPLACED SILL PN 170-05663-005 IAW SRM 51-41-02.51-43-02.AC WAS RETURNED TO SERVICE. - [SDR R61A2022072000455](https://openairdocs.org/sdr/R61A2022072000455.md): Support Angle · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Floor Panel > WHILE AC WAS IN FOR HVY CK FOUND CF3 RH FLOOR BOARD SUPPORT ANGLE AT FR 87 FOUND CORRODED. REPLACED SUPPORT PN 170-66797-001 IAW SRM 51-41-01.AC WAS RETURNED TO SERVICE. - [SDR R61A2022072000454](https://openairdocs.org/sdr/R61A2022072000454.md): Gusset · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE AC WAS IN FOR HVY CK FOUND CF3 RH GUSSET AT FR90 FOUND CORRODED. REPLACED GUSSET PN 170-60259-001 IAW SRM 51-41-02. AC RETURNED TO SERVICE - [SDR R61A2022072000452](https://openairdocs.org/sdr/R61A2022072000452.md): Shear Tie · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE AC WAS IN FOR HVY CK FOUND CF3 FUSE MID SHEAR PANEL AT FR 87-88 FOUND CORRODED. REPLACED SHEAR PANEL PN 170-65928-001 IAW SRM 51-42-01, 51-43-03. AC RETURNED TO SERVICE - [SDR R61A2022072000451](https://openairdocs.org/sdr/R61A2022072000451.md): Shear Tie · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE AC WAS IN FOR HVY CK FOUNDCF3 FUSE 3 RH SHEAR PANEL AT FR 87-88 FOUND CORRODED. REPLACED SHEAR PANEL PN 170-91919-001 IAW SRM 51-42-01, 51-42-02, 51-43-01. AC REMAINS IN YQG FOR COMPLETION - [SDR R61A2022072000450](https://openairdocs.org/sdr/R61A2022072000450.md): Seat Track · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE AC WAS IN FOR HVY CK FOUND CENTER FUSE 3 RH IB SEAT TRACK FOUND CORRODED AT FR 84. REPAIRED IAW SRM 53-23-10 REPAIR 04.AC REMAINS IN YQG FOR COMPLETION - [SDR R61A2022071600443](https://openairdocs.org/sdr/R61A2022071600443.md): Panel · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > FWD SECTION R/H SIDE SILL PNL BETWEEN FR 12-14 CORRODED. R&R IAW EMB 170/175 SRM 51-41-02 AND 51-43-02. - [SDR R61A2022071500438](https://openairdocs.org/sdr/R61A2022071500438.md): Shear Panel · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CNTR FUSE III MID SHEAR PNL AT FR 87-88 CORRODED. R&R IAW SRM 51-42-01 AND 51-43-03. - [SDR R61A2022071500437](https://openairdocs.org/sdr/R61A2022071500437.md): Shear Panel · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CNTR FUSE III R/H SHEAR PNL AT FR 87-88 CORRODED. R&R IAW SRM 51-42-01, 51-42-02 AND 51-43-01. - [SDR R61A2022071500436](https://openairdocs.org/sdr/R61A2022071500436.md): Seat Track · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > CNTR FUSE III R/H I/B SEAT TRACK AT FR 84 CORRODED. R&R IAW SRM 53-23-10 REPAIR 04 - [SDR R61A2022071500435](https://openairdocs.org/sdr/R61A2022071500435.md): Floor Support · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Floor Panel > CNTR FUSE III R/H FLOOR BOARD SUPP ANGLE AT FR 87 CORRODED. R&R IAW SRM 51-41-01. - [SDR R61A2022071500434](https://openairdocs.org/sdr/R61A2022071500434.md): Gusset · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CNTR FUSE III R/H GUSSET AT FR 90 CORRODED. R&R IAW SRM 51-41-02 - [SDR R61A2022071500433](https://openairdocs.org/sdr/R61A2022071500433.md): Floor Support · corroded · Jul 1, 2022 · N751YX · Emb ERJ170200LR · Fuselage Floor Panel > CNTR FUSE III R/H FLOOR SUPPORT AT FR 88-90 CORRODED. R&R IAW SRM 51-43-01 & 51-42-01. - [SDR R61A2021011900070](https://openairdocs.org/sdr/R61A2021011900070.md): Strip · missing · Jan 15, 2021 · N751YX · Emb ERJ170200LR · Fuselage Miscellaneous Structure > TRIM STRIP IS MISSING FROM FLOOR IN FRONT OF WARDROBE CLOSET. R & R MISSING PHOTOLUMINESCENT STRIP. - [SDR R61A2020050500491](https://openairdocs.org/sdr/R61A2020050500491.md): Winglet · cracked · Apr 24, 2020 · N751YX · Emb ERJ170200LR · Wing, Plate/Skin > WHILE A/C WAS OUT OF SERVICE FOR A HEAVY MAINTENANCE CHECK, LT WINGTIP FRONT SPAR CRACKED. REPLACED WINGTIP IAW AMM 57-30-00-400-801-A AND T/C 170EO-57-30-0000_1. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION. - [SDR R61A2020022850273](https://openairdocs.org/sdr/R61A2020022850273.md): Module · failed · Feb 25, 2020 · N751YX · Emb ERJ170200LR · Landing Gear Position and Warning > LG WOW FAIL ON CLIMB, NUMEROUS OTHER MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R MAU 3 POWER SUPPLY 1 AND PSEM 2. - [SDR R61A2018102311059](https://openairdocs.org/sdr/R61A2018102311059.md): Slide · unwanted deploy · Oct 21, 2018 · N751YX · Emb ERJ170200LR · Escape Slide > R2 DOOR WILL NOT LATCH CORRECTLY. R2 DOOR SLIDE DEPLOYED. R&R R2 DOOR SLIDE IAW AMM 25-65-01. - [SDR R61A2018102311058](https://openairdocs.org/sdr/R61A2018102311058.md): Handle · lack of lube · Oct 21, 2018 · N751YX · Emb ERJ170200LR · Passenger/Crew Doors > R2 DOOR VENT FLAP HANDLE STUCK. WE ARE UNABLE TO DISARM THE DOOR. CLEANED AND LUBRICATED R2 DOOR VENT FLAP HANDLE IAW AMM 52-12-00. - [SDR R61A201801120051](https://openairdocs.org/sdr/R61A201801120051.md): Arming Lever · lack of lube · Jan 12, 2018 · N751YX · Emb ERJ170200LR · Service Doors > R2 ARMING HANDLE BINDING. CLEANED AND LUBED R2 ARM/DISARM HANDLE. ## 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 = 'N751YX' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N751YX/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.