# Service difficulty reports: N860RW A list on [N860RW](https://openairdocs.org/aircraft/N860RW.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 3 · 129 reports - [SDR R61A2025032600160](https://openairdocs.org/sdr/R61A2025032600160.md): Skin · damaged · Mar 25, 2025 · N860RW · Emb ERJ170100SE · Fuselage Main, Plate/Skin > LIGHTING STRIKE DAMAGE WITH CUTOUT FWD OF FR 24 AT STR 22L & FWD FR 25-26 AT STR 22L-21L. REPAIRED IAW SRM 51-23-01. - [SDR R61A2024031000106](https://openairdocs.org/sdr/R61A2024031000106.md): Fitting · cracked · Feb 26, 2024 · N860RW · Emb ERJ170100SE · Trailing Edge Flaps > SUSPECTED CRACK IB AFT FLAP, IB SIDE EMITING FROM BOLT. REQUIRED NDT TO CONFIRM. FITTING (R/H IB AFT FLAP- IB SIDE) REPLACED IAW EMBRAER 170/175 AMM 20-10-01-910-801-A TABLE 201 AND 203 AND SRM 51-21-05. - [SDR R61A2024031000102](https://openairdocs.org/sdr/R61A2024031000102.md): Hinge · corroded · Feb 25, 2024 · N860RW · Emb ERJ170100SE · Fuselage, Door Hinge > CF III WASTE ACCESS DOOR PANEL HINGE ASSY FOUND CORRODED. CF III WASTE ACCESS DOOR HINGE ASSY REPLACED AND INSTALLED IAW SRM 51-40-08. - [SDR R61A2024031000103](https://openairdocs.org/sdr/R61A2024031000103.md): Floor Support · corroded · Feb 22, 2024 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > PAX CABIN FWD LAV FLOOR BRACKET CORRODED. PAX CABIN, FWD LAV FLOOR BRACKET REPLACED IAW AMM TASK 25-41-02, SUBTASK 420-013-A. - [SDR R61A2024040300153](https://openairdocs.org/sdr/R61A2024040300153.md): Seal · damaged · Feb 20, 2024 · N860RW · Emb ERJ170100SE · Fuselage Main, Structure > SMOKE SEAL REMOVED FROM THE AFT AVIONICS BAY WAS DAMAGED. R&R RH SMOKE SEAL. - [SDR R61A2024031000107](https://openairdocs.org/sdr/R61A2024031000107.md): Intercostal · cracked · Feb 20, 2024 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > FOWARD FUSELAGE, CORROSION FOUND ON INTERCOSTAL AT FR 17, AT STR 21R. REPLACED SUPPORT AT FR 17, STR 21R WITH NEW PN: 170-06150-004 IAW EMBRAER SRM 51-41-02 AND 51-43-04. - [SDR R61A2024031000105](https://openairdocs.org/sdr/R61A2024031000105.md): Skin · cracked · Feb 20, 2024 · N860RW · Emb ERJ170100SE · Wing, Plate/Skin > R/H WING FLE SKIN TOP SIDE SLAT TRACK #5 CUTOUT BETWEEN L/E RIB19-L/E RIB220 FOUND CRACK. R/H WING FLE SKIN TOP SIDE, SLAT TRACK #5 CUTOUT BETWEEN L/E RIB19-L/E RIB20 HAS BEEN REPAIRED IAW ERJ-170-SRM 57-49-01. - [SDR R61A2024031000104](https://openairdocs.org/sdr/R61A2024031000104.md): Skin · cracked · Feb 20, 2024 · N860RW · Emb ERJ170100SE · Wing, Plate/Skin > L/H WING FLE SKIN TOP SIDE, SLAT TRACK#5 CUTOUT BETWEEN L/E RIB19-L/E RIB20 FOUND CRACKED. LH WING FLE SKIN TOP SIDE, SLAT TRACK#5 CUTOUT BETWEEN L/E RIB19-L/E RIB20 HAS BEEN REPAIRED IAW ERJ-170-SRM 57-49-01. - [SDR R61A2024031000101](https://openairdocs.org/sdr/R61A2024031000101.md): Seal Depressor · corroded · Feb 16, 2024 · N860RW · Emb ERJ170100SE · Fuselage Main, Structure > AFT CARGO DOOR SURROUND LOWER AFT CORNER SEAL DEPRESSOR CORRODED. REMOVED AND REPLACED SEAL REST ON AFT CARGO DOOR AFT CORNER IAW EMBRAER 170 SRM 51-40-02 AND 51-40-08. - [SDR R61A2021103100841](https://openairdocs.org/sdr/R61A2021103100841.md): Rib · cracked · Oct 31, 2021 · N860RW · Emb ERJ170100SE · Horizontal Stabilizer Structure > MAJOR LH HORZ STAB RIB 11A AND 12A BETWEEN FRONT SPAR AND MID SPAR IS CRACKED. BOTH RIBS REPLACED PER JC 170EO-55-10-0004-1 - [SDR R61A2021102700837](https://openairdocs.org/sdr/R61A2021102700837.md): Bracket · corroded · Oct 10, 2021 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > PASENGER FLOOR STRUCTURE, CORROSION FOUND ON PANEL SUPPORT BRACKET AT FR 87 RBL 29. PASSENGER FLOOR STRUCTURE CORRODED PANEL SUPPORT BRACKET AT FR 87 RBL 29 REPLACED IAW SRM 51-41-01.BRAC - [SDR R61A2021102700839](https://openairdocs.org/sdr/R61A2021102700839.md): None · corroded · Oct 8, 2021 · N860RW · Emb ERJ170100SE · Fuselage Structure (General) > FWD CARGO, SHEAR CLIP FOUND CORRODED AT FR 16 BETWEEN STR 28-27R. REMOVED AND REPLACED SHEAR CLIP IN FWD CARGO AT FR 16 BETWEEN STR 27-28R IAW EMBRAER 170-175 SRM 51-41-01 AND 51-41-02. - [SDR R61A2021102700838](https://openairdocs.org/sdr/R61A2021102700838.md): Support · corroded · Oct 8, 2021 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > INTERIOR FUSELAGE FWD CARGO BAY, OXYGEN CYLINDER SUPPORT ANGLE FOUND CORRODED BETWEEN FR 23 AND 24, ON STR 21R. INTERIOR FUSELAGE, FWD CARGO BAY, OXYGEN CYLINDER SUPPORT ANGLE REPLACED WITH NEW, BETWEEN FR 23-24, STR 21R IAW EMB 170/175 SRM 51-41-01 - [SDR R61A2021102700835](https://openairdocs.org/sdr/R61A2021102700835.md): None · corroded · Oct 8, 2021 · N860RW · Emb ERJ170100SE · Fuselage Structure (General) > FWD CARGO SHEAR CLIP AT FR 17 BETWEEN STR 28-27R. FWD CARGO SHEAR CLIP AT FR 17 BETWEEN STR 28-27R REPLACED IAW SRM 51-41-02. - [SDR R61A2021102700836](https://openairdocs.org/sdr/R61A2021102700836.md): Intercostal · corroded · Oct 6, 2021 · N860RW · Emb ERJ170100SE · Fuselage Structure (General) > EXTERIOR FUSELAGE, WASTE ACCESS DOOR INTERCOSTAL FOUND CORRODED. EXTERIOR FUSELAGE WASTE ACCESS DOOR INTERCOSTAL REPLACED IAW SRM 51-41-01 AND 51-41-02 - [SDR R61A2021102700834](https://openairdocs.org/sdr/R61A2021102700834.md): Rib · cracked · Oct 6, 2021 · N860RW · Emb ERJ170100SE · Horizontal Stabilizer Structure > LH H STAB, CRACK FOUND ON RIB 11A AND 12A BETWEEN FRONT SPAR AND MID SPAR L/H H STAB, RIB 11A AND 12A BETWEEN FRONT SPAR AND MID SPAR HAS BEEN REPLACED UNDER TASK CARD 170EO-55-10-0004_1 - [SDR R61A2021091000725](https://openairdocs.org/sdr/R61A2021091000725.md): Power Supply · inoperative · Sep 3, 2021 · N860RW · Emb ERJ170100SE · Emergency Lighting > ELPU 4 FAILED OPS CHECK AND WON'T CHARGE. R&R ELPU 4 - [SDR R61A2021091000726](https://openairdocs.org/sdr/R61A2021091000726.md): Power Supply · no test · Sep 3, 2021 · N860RW · Emb ERJ170100SE · Emergency Lighting > ELPU 3 FAILED OPS CHECK AND WON'T CHARGE. R&R ELPU 3 - [SDR R61A2021091000727](https://openairdocs.org/sdr/R61A2021091000727.md): Sign · faulted · Sep 3, 2021 · N860RW · Emb ERJ170100SE · Emergency Lighting > R1 DOOR SURROUND FWD SIDE, EMERGENCY EXIT SIGN IS ONLY HALF ILLUMINATED. R&R R1 DOOR EMERGENCY EXIT IDENTIFIER SIGN. - [SDR R61A2021091000724](https://openairdocs.org/sdr/R61A2021091000724.md): Power Supply · inoperative · Sep 3, 2021 · N860RW · Emb ERJ170100SE · Emergency Lighting > ELPU 2 FAILED OPS CHECK AND WON'T CHARGE. R&R ELPU 2. - [SDR R61A2020122200937](https://openairdocs.org/sdr/R61A2020122200937.md): Access Panel · out of alignment · Dec 20, 2020 · N860RW · Emb ERJ170100SE · Aerodynamic Fairings > DURING FLIGHT, CREW REPORTED STRONG VIBRATION AND VERY LOUD RUMBLING SOUND FROM BELOW. REPORTED TO BE LOUDEST AROUND ROWS 5-8. NOISE INCREASED WITH ALTITUDE AND SPEED. FLIGHT DIVERTED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PANEL 195BR TO BE - [SDR R61A2020111200749](https://openairdocs.org/sdr/R61A2020111200749.md): Power Supply · inoperative · Nov 8, 2020 · N860RW · Emb ERJ170100SE · Emergency Lighting > AFT LEFT, RIGHT, AND CENTER EMERGENCY LIGHTS NOT FUNCTIONING. R & R AFT INBOARD EMERGENCY LIGHT UNIT. - [SDR R61A2020111200748](https://openairdocs.org/sdr/R61A2020111200748.md): Power Supply · inoperative · Nov 8, 2020 · N860RW · Emb ERJ170100SE · Emergency Lighting > AFT LEFT, RIGHT, AND CENTER EMERGENCY LIGHTS NOT FUNCTIONING. R & R AFT INBOARD EMERGENCY LIGHT UNIT. - [SDR R61A2020022540259](https://openairdocs.org/sdr/R61A2020022540259.md): Mechanism · lack of lube · Feb 24, 2020 · N860RW · Emb ERJ170100SE · Service Doors > 2R DOOR VERY DIFFICULT TO OPEN PER THE FLIGHT ATTENDANT. LUBED R2 DOOR MECHANISM AND R2 DOOR OPEN AND CLOSES NORMALLY. - [SDR R61A201905150497](https://openairdocs.org/sdr/R61A201905150497.md): Spring · lack of lube · May 15, 2019 · N860RW · Emb ERJ170100SE · Service Doors > SERVICE DOOR R2 DIFFICULT TO OPEN AND CLOSE, VENT FLAP BINDING. LUBRICATED R2 DOOR GIRT BAR FLOOR FRAME RAMP SPRING AND PERFORMED R2 DOOR OPS CHECK IAW AMM 52-42-00. OPS CHECK GOOD. - [SDR R61A201904250471](https://openairdocs.org/sdr/R61A201904250471.md): Shear Tie · damaged · Apr 25, 2019 · N860RW · Emb ERJ170100SE · Fuselage Internal Mounting Structure > DURING HEAVY CHECK MAINTENANCE FOUND FAIRLEAD AT FR30 UNDER CARGO FLOOR PANEL FOUND FASTENER HOLES TO BE OVERSIZED ON SHEAR CLIPS AND FLOOR PANEL SUPPORT CAUSING A DEFLECTION OF AILERON CABLE WHEN TRYING TO LOCATE NEW FAIRLEAD. REMOVED, FABRICATED AND INSTALLE - [SDR R61A201904130470](https://openairdocs.org/sdr/R61A201904130470.md): Spar · damaged · Apr 13, 2019 · N860RW · Emb ERJ170100SE · Wing Spar > DURING HEAVY CHECK MAINTENANCE FOUND LT WING T/E AT SPAR 3 HAS HYD LINE FITTING HOLE THAT IS ELONGATED IN SPAR. REPAIRED LT WING T/E AT SPAR 3 HAS HYD LINE FITTING HOLE BY REAMING AND INSTALLING FABRICATED BUSHING REF. SRM 57-50-05/REPAIR 01P. A/C REMAINS IN - [SDR R61A201904130469](https://openairdocs.org/sdr/R61A201904130469.md): Spar · damaged · Apr 13, 2019 · N860RW · Emb ERJ170100SE · Wing Spar > DURING HEAVY CHECK MAINTENANCE FOUND RT WING T/E AT SPAR 3 HYD LINE FITTING HOLE IS ELONGATED THRU SPAR 3. REPAIRED RT WING T/E AT SPAR 3 HYD LINE FITTING HOLE THRU SPAR 3 AS MARKED BY REAMING AND INSTALLING FABRICATED BUSHING REF. SRM 57-50-05/REPAIR 01P. A/C - [SDR R61A2019042610423](https://openairdocs.org/sdr/R61A2019042610423.md): Fitting · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Main, Structure > WHILE AIRCRAFT WAS IN HEAVY CHECK, MAINTENANCE FOUND CORROSION ON RH INBD AFT WINDSCREEN TIE DOWN FITTING. MAINTENANCE REMOVED AND REPLACED RH INBD AFT WINDSCREEN TIE DOWN FITTING, REF SRM 51-40-08. THIS AIRCRAFT REMAINS IN HEAVY CHECK FOR DURATION OF THE CHEC - [SDR R61A201904260422](https://openairdocs.org/sdr/R61A201904260422.md): Seat Track · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage, Seat/Cargo Attach Fittings > *WHILE AIRCRAFT WAS IN HEAVY CHECK* MAINTENANCE FOUND LEVEL 2 CORROSION ON CENTER FUSELAGE III DRY AREA 53-23 LH SEAT TRACK FRAME 84. MAINTENANCE PERFORMED PERMANENT REPAIR BY FABRICATION AT LH SEAT TRACK FRAME 84 FILLER AND SPLICES REPAIR, REF: SRM 53-00-10/R - [SDR R61A201904260421](https://openairdocs.org/sdr/R61A201904260421.md): Angle · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK, MAINTENANCE FOUND HEATED DRAIN MAST ANGLES ARE CORRODED AFT OF FR87 BETWEEN STRG.27R AND 28R. MAINTENANCE REMOVED AND REPLACED 2EA HEATED DRAIN MAST INTERCOSTAL CLIPS (ANGLES) AFT OF FR87 BETWEEN STGR 27R-28R REF. EMB SRM 51-40-08. PNS R - [SDR R61A201904260420](https://openairdocs.org/sdr/R61A201904260420.md): Shear Panel · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION CENTER FUSELAGE III WET AREA 53-23 CENTER SHEAR PANEL. MAINTENANCE REMOVED AND REPLACED NEW CENTER FUSELAGE III WET AREA 53-23 CENTER SHEAR PANEL REF EMB SRM 51-40-08. - [SDR R61A201904250419](https://openairdocs.org/sdr/R61A201904250419.md): Frame Splice · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Main, Structure > IN HEAVY CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 CENTER SPLICE FRAME 90. MAINTENANCE REMOVED AND REPLACED CENTER SPLICE AT FRAME 90, REF EMB SRM 51-40-08. - [SDR R61A201904120418](https://openairdocs.org/sdr/R61A201904120418.md): Upper Sheet · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > IN HEAVY CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION STRUCTURAL CENTER FUSELAGE III DRY AREA 53-23 RH UPPER SHEET. MAINTENANCE REMOVED AND REPLACED RH UPPER SHEET. REF EMB SRM 51-40-08. - [SDR R61A201904250417](https://openairdocs.org/sdr/R61A201904250417.md): Crossbeam · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Main, Structure > IN HEAVY CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION ON BEAM BETWEEN RH INBD SEAT TRACK AND FUSELAGE. *MAJOR REPAIR* MAINTENANCE PERFORMED PERMANENT REPAIR BY FABRICATING L-ANGLE REPAIR ON CROSSBEAM AT FR84 IAW ETD2019-170-052642. - [SDR R61A2019041920396](https://openairdocs.org/sdr/R61A2019041920396.md): Floorbeam · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Main, Floor Beam > DURING HEAVY CHECK MAINTENANCE FOUND CORRODED FLOOR BOARD SUPPORT ANGLE FRM 80 STRG 26R-27R. INSTALLED NEW FLOOR BOARD SUPPORT ANGLE FRM 80 @ STRG 27R-28R, REF SRM 51-40-08. A/C REMAINS IN CHECK. - [SDR R61A2019041920395](https://openairdocs.org/sdr/R61A2019041920395.md): Shear Tie · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Internal Mounting Structure > DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FRM 84 STRG 28R-27R. REMOVED AND REPLACED CORRODED SHEAR CLIP FR 84, STRG 28R-27R. REF SRM 51- 40-08. SEE A/C REMAINS IN CHECK. - [SDR R61A2019041920394](https://openairdocs.org/sdr/R61A2019041920394.md): Shear Tie · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Internal Mounting Structure > DURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIP FRM 82 STRG 28R-27R. REMOVED AND REPLACED CORRODED SHEAR CLIP FR 82, STRG 28R-27R. REF SRM 51-40-08. A/C REMAINS IN CHECK. - [SDR R61A2019041920393](https://openairdocs.org/sdr/R61A2019041920393.md): Beam · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Main, Structure > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 LH BEAM Y=-10.748". FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER FOR LH BEAM BETWEEN FRAMES 87-88 REFER SRM 53-23-10. APPLIED SURFACE PROTECTION TO AREA PER SRM 51 - [SDR R61A2019041920392](https://openairdocs.org/sdr/R61A2019041920392.md): Shear Tie · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Internal Mounting Structure > DURING HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP CORRODED AT FR 86 BETWEEN STRG 27R AND 26R. REMOVED AND REPLACED NEW SHEAR CLIP AT FR 86 BETWEEN STRG 28R AND 27R REF. SRM51-- 40-08. A/C REMAINS IN CHECK. - [SDR R61A2019041920391](https://openairdocs.org/sdr/R61A2019041920391.md): Shear Tie · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Internal Mounting Structure > DURING HEAVY CHECK MAINTENANCE FOUND SHEAR CLIP CORRODED AT FR 85 BETWEEN STRG 27R AND 26R. REMOVED AND REPLACED NEW SHEAR CLIP AT FR 85 BETWEEN STRG 28R AND 27R REF. SRM51-- 40-08. A/C REMAINS IN CHECK. - [SDR R61A2019041920390](https://openairdocs.org/sdr/R61A2019041920390.md): Gusset · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH CENTER GUSSET FRAME 90.REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 RH GUSSET PLATE FRAME 90. REF EMB SRM 51-40-08. A/C REMAINS IN CHECK. - [SDR R61A2019041920389](https://openairdocs.org/sdr/R61A2019041920389.md): Support · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH AFT PANEL SUPPORT. REMOVED AND REPLACED STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 R/H AFT PANEL SUPPORT. REF: SRM 51-40-08. A/C REMAINS IN CHECK. - [SDR R61A2019041920388](https://openairdocs.org/sdr/R61A2019041920388.md): Shear Plate · corroded · Apr 12, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH SHEAR PLATE. REMOVED AND REPLACED STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH SHEAR PLATE REF. EMB SRM 51-40-08. A/C REMAINS IN CHECK. - [SDR R61A2019042511416](https://openairdocs.org/sdr/R61A2019042511416.md): Angle · cracked · Apr 11, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > IN HEAVY CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION ON PANEL 1441FR 3 LOWER ANGLES. MAINTENANCE REMOVED AND REPLACED 3EA ANGLES TO PANEL 1441FR. REF SRM 51-40-08, AMM 20-10-01. PN 170-10065-002, 170-10064-002, AND 170-10063-004. - [SDR R61A2019042011340](https://openairdocs.org/sdr/R61A2019042011340.md): Angle · corroded · Apr 11, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > DURING HEAVY CHECK MAINTENANCE FOUND CORROSION LOWER 3 ANGLE ON PANEL 1431DL. REMOVED AND REPLACED DAMAGED ANGLES (3EA.) ON PANEL #1431DL, REF EMB SRM 51-40-08 AND AMM 20-10-01. A/C REMAINS IN CHECK. - [SDR R61A2019041910387](https://openairdocs.org/sdr/R61A2019041910387.md): Crossbeam · corroded · Apr 11, 2019 · N860RW · Emb ERJ170100SE · Fuselage Main, Structure > DURING HEAVY CHECK MAINTENANCE FOUND FRAME 11 FLOOR CROSSBEAM HAS CORROSION. PERFORMED PERMANENT REPAIR BY BLEND OUT ON CROSSBEAM FR11 IN ACCORDANCE WITH REF ETD 2019-170-051756 REV A. A/C REMAINS IN CHECK. - [SDR R61A2019041980386](https://openairdocs.org/sdr/R61A2019041980386.md): Floor Support · corroded · Apr 8, 2019 · N860RW · Emb ERJ170100SE · Fuselage Miscellaneous Structure > DURING HEAVY CHECK MAINTENANCE FOUND RH OUTBOARD FLOOR SILL HAS SEVERAL AREAS OF CORROSION AT FR 12-14. REMOVED AND REPLACED RH OUTBOARD FLOOR SILL AT FR 12-14 REF. SRM 51-40-08. A/C REMAINS IN CHECK. - [SDR R61A201810111016](https://openairdocs.org/sdr/R61A201810111016.md): Connector · unsecure · Oct 11, 2018 · N860RW · Emb ERJ170100SE · Flight Control System Wiring > SLAT FAIL IN FLIGHT. FLAPS DEPLOYED TO "2" MAX BRAKE TEMP ON LANDING 290 C ON RIGHT MAIN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND LT OUTBOARD SLAT SKEW SENSOR CONNECTOR OFF. RE-SECURED CONNECTOR ON LT OB SKEW SENSOR IAW AMM 27-83-01. - [SDR UHLA201612080527](https://openairdocs.org/sdr/UHLA201612080527.md): Floorbeam · corroded · Dec 8, 2016 · N860RW · Emb ERJ170100SE · Fuselage Main, Floor Beam > CENTER COCKPIT FLOORBEAM AT FRAME 11 CORRODED. PERFORMED A PERMANENT REPAIR IAW ETD2016-170-109522. Next page: https://openairdocs.org/aircraft/N860RW/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 = 'N860RW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N860RW/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.