# Service difficulty reports: N925EV

A list on [N925EV](https://openairdocs.org/aircraft/N925EV.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 4 · 191 reports

- [SDR SWIA2026020275115](https://openairdocs.org/sdr/SWIA2026020275115.md): Striker · damaged · Feb 2, 2026 · N925EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND DAMAGE ON AFT UPPER PAX DOOR SEAL STRIKER NEAR DOOR ROLLER. FOUND DENT DAMAGE. (W - 0.650 D- 0.20 W - 0.15) LOCATED ON THE AFT UPPER PAX DOOR SEAL STRIKER NEAR THE DOOR ROLLER. PER REO 601R-53-22-033 REV -D DATED 2014/02/17 PERFORMED TEMP REPAIR TYPE I
- [SDR SWIA20260108](https://openairdocs.org/sdr/SWIA20260108.md): Controller · malfunctioned · Jan 8, 2026 · N925EV · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > WING OVHT MESSAGE ON TAKE OFF. QRH PROCEDURE WAS CONDUCTED & MESSAGE CLEARED. NO FURTHER MESSAGES DURING FLIGHT. (FLIGHT 5125) TROUBLESHOT IAW FIM 30-10-00. INTERROGATED MDC, NO FAULTS OR HISTORY FOUND. PERFORMED GVI OF WIRING GOING TO LT WAI MSOV, LOOKED AT
- [SDR SWIA202505270024](https://openairdocs.org/sdr/SWIA202505270024.md): Landing Gear · warning message · May 24, 2025 · N925EV · Cndair CL6002B19 · Central Warning
  > GEAR DISAGREE WARNING ALONG WITH ASSOCIATED NOSE DOOR WARNING ON TAKEOFF. BOTH MAINS RETRACTED AND SHOWED UP BUT NOSE GEAR INDICATION SHOWED LINES. QRH RESOLVED ISSUE. RECEIVED 3 GREEN DN INDICATIONS. RTF (FLIGHT 5807 - FILED CLOSED)TROUBLESHOT GEAR DISAGR
- [SDR SWIA2025040329](https://openairdocs.org/sdr/SWIA2025040329.md): Terminal Block · smoke · Mar 29, 2025 · N925EV · Cndair CL6002B19 · Ice/Rain Protection System Wiring
  > SMOKE IN COCKPIT FROM CP SIDE WINDSHIELD HEAT. QRH RESOLVED ISSUE. (FLIGHT 5025 - FILED CLOSED)TROUBLESHOT COCKPIT SMOKE EVENT PER FIM 21-21-00 AND FOUND WHILE INSPECTING L/H WINDSHIELD WITH HEAT ON, FOUND LIGHT SMOKE COMING OUT BETWEEN L/H WINDSHIELD HEAT POW
- [SDR SWI2025F00404](https://openairdocs.org/sdr/SWI2025F00404.md): Heater · smoke · Mar 29, 2025 · N925EV · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > SMOKE IN COCKPIT FROM CP SIDE WINDSHIELD HEAT. QRH RESOLVED ISSUE. (FLIGHT 5025 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202502140002](https://openairdocs.org/sdr/SWIA202502140002.md): Wire Harness · damaged · Feb 12, 2025 · N925EV · Cndair CL6002B19 · Landing Gear System Wiring
  > ON DEPARTURE FROM DENVER RECEIVED A NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGES. MESSAGES CLEARED WITH QRH (FLIGHT 5083 - FILED CLOSED) ARRIVED AT A/C INTERROGATED PSEU AND BASED ON THE INPUT REASONABLENESS TABLE TABLE 103 IN FIM 32-60-05 IT APPEARS
- [SDR SWI202408190689](https://openairdocs.org/sdr/SWI202408190689.md): Selector Valve · faulted · Aug 17, 2024 · N925EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON GEAR EXTENSION ON FINAL. RAN QRH AND CYCLED THE GEAR TWICE NORMALLY WITH 30 SECOND DELAY. MESSAGE PERSISTED. QUICK CYCLED GEAR UNDER DIRECTION OF QRH AND THEN GOT THREE GEAR DOWN AND LOCKED. (FLIGHT 5391 - FILED CLOSED) THIS DISCREPANCY
- [SDR SWIA2024060500004](https://openairdocs.org/sdr/SWIA2024060500004.md): Warning Message · false activation · Jun 4, 2024 · N925EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > D:DUE TO FLAPS FAIL CAUTION. FLAPS 0 LANDING, COMPLY WITH FULL FLAP EVAULATION PER AD 2009-06-12/09.C: FLAP FAILCAT A DUE WITHIN 10 CYCLES BY TAC 37720. SMOD APPROVAL REQIRED FOR RTS. FLAPS FAIL CAUTION. FLAPS 0 LANDING. (FLIGHT 4663) RESET AND OPERATED FL
- [SDR SWIA2024051000312](https://openairdocs.org/sdr/SWIA2024051000312.md): Vane · chafed · Mar 12, 2024 · N925EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBD FLAP VANE CHAFED AT WS104.099 (C-CHECK RO 5/9/2024) REPAIRED R/H I/B FLAP VANE L/E SKIN AT W.S. 104.099 IAW CRJ200 SRM 57-52-00 AND 57-52-00 REPAIR #1. NDT PERFORMED BY BARON NDT LLC CRS#: 5NDR545D REPORT#: S032524-1 DATED 25MAR2024. SEE REPORT FOR
- [SDR SWIA20240510229](https://openairdocs.org/sdr/SWIA20240510229.md): Skin · damaged · Feb 29, 2024 · N925EV · Cndair CL6002B19 · Elevator, Plate/Skin
  > LH ELEVATOR SKIN ABOVE HINGE #2 DAMAGED, EVAL (C-CHECK RO 5/9/2024) PERFORMED REPAIR AT L/H ELEVATOR SKIN ABOVE HINGE #2 IAW CRJ 200 REO 601R-55-21-591 REV -- DATE: 2024-03-15,SRM 55-20-00,SRM 51-24-36,SRM 51-12-00,SRM 51-25-06,SRM 51-25-16, PERFORMED NDT
- [SDR SWI2024F00399](https://openairdocs.org/sdr/SWI2024F00399.md): Shroud · damaged · Feb 27, 2024 · N925EV · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > LE SHROUD LH SIDE H STAB DAMAGED (C-CHECK RO 5/9/2024) REPAIRED LH SIDE HORIZONTAL STABILIZER LEADING EDGE SHROUD BETWEEN FSS31.999 TO FSS67.790 IAW REO 601R-55-11-757 REV -- DATE: 2024-04-25, CRJ 200 AMM 20-22-01, AMM 55-10-00, CRJ 200 SRM 51-42-06, SRM
- [SDR SWIA20240510227](https://openairdocs.org/sdr/SWIA20240510227.md): Shroud · damaged · Feb 27, 2024 · N925EV · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > LE SHROUD RH SIDE H STAB DAMAGED (C-CHECK RO 5/9/2024) REPAIRED RH SIDE HORIZONTAL STABILIZER OF THE LEADING EDGE SHROUD BETWEEN FSS 31.999 TO FSS 67.790 IAW MHIRJ REO 601R-55-11-757 REV -- DATE: 2024-04-25 AND IAW CRJ 200 AMM 20-22-01, AMM 55-10-00 AND
- [SDR SWIA2024051000030](https://openairdocs.org/sdr/SWIA2024051000030.md): Skin · dented · Jan 30, 2024 · N925EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > ADM N925EV-8460THERE IS A SCRATCH AND TWO DENTS ON THE UPPER FWD OF DOOR WHEN CLOSED, SCRATCH IS JUST THOUGH PAINT, MEASURING 26.75 IN FROM TOP OF DOOR, AND 4.75 IN FROM FWD EDGE. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVI
- [SDR SWIA2024010200030](https://openairdocs.org/sdr/SWIA2024010200030.md): Unknown · dented · Dec 30, 2023 · N925EV · Cndair CL6002B19 · Trailing Edge Flaps
  > FOUND DENT ON THE LEADING EDGE OF THE FLAP-VANE ON THE LEFT OB FLAP AT APPROX. F/STA 210.50 (FILED CLSOED) FOUND DENT AT LEFT WING O/B FLAP VANE F.S. 210.50 TO BE OUT OF LIMITS PER SRM 57-53-00 FIG 102 SHEET 3. NO DENTS PERMITTED. REF CP 27621022 FOR FURTHER
- [SDR SWI20240510398](https://openairdocs.org/sdr/SWI20240510398.md): Guide · eroded · Dec 1, 2023 · N925EV · Cndair CL6002B19 · Wing Structure
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA69883-601R-57-41-1124 925EV MXCODEID56613-PR - RH WING OUTBOARD LEADING EDGE (630KL) HAS EROSION. COMPLIED WITH TEMPORARY REPAIR PER REO601R-57-41-1124, REV--, DATED 2021-05-04. PERMANENT REPAIR DUE WITHIN 6000 FLT H
- [SDR SWI20240510397](https://openairdocs.org/sdr/SWI20240510397.md): Skin · eroded · Dec 1, 2023 · N925EV · Cndair CL6002B19 · Wing, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA69059-601R-57-41-1120 N925EV MXCODEID56580-PR - RH WING CENTER LEADING EDGE PANEL (630JL) HAS EROSION. COMPLIED WITH REO 601R-57-41-1120, REV. --, 2021-04-26 IN ITS ENTIRETY (STEPS 1-5). THIS REPAIR IS VALID FOR 600
- [SDR SWIA202405101201](https://openairdocs.org/sdr/SWIA202405101201.md): Skin · damaged · Dec 1, 2023 · N925EV · Cndair CL6002B19 · Wing, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA69006-601R-57-41-1119 N925EV MXCODEID56249-PR - LH WING CENTER LEADING EDGE PANEL (530JL) HAS EROSION. REMOVED EROSION DAMAGE ON L/H WING CENTER LEADING EDGE PANEL 530JL REF CRJ 200 SRM 51-12-00. COMPLIED WITH REO 60
- [SDR SWIA202158214](https://openairdocs.org/sdr/SWIA202158214.md): Support Angle · corroded · Apr 21, 2021 · N925EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > LH FWD AVIONICS BAY DOOR SEAL RETAINER SUPPORT ANGLE HAS CORROSION. (C-CHECK RO 5/16/2021) VALUATE LH FWD AVIONICS BAY DOOR SEAL RETAINER SUPPORT ANGLE CORRECTIVE ACTION: LH FWD ANGLE IS 100% EXFOLIATED, FOUND TO BE OUT OF LIMITS. REF CRJ 200 SRM 52-00
- [SDR SWIA202158190](https://openairdocs.org/sdr/SWIA202158190.md): Cup · damaged · Apr 19, 2021 · N925EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UNDER FLOOR AFT HAND RAIL CUP REQUIRES REPLACEMENT. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED THE PAX DOOR AFT HANDRAIL CUP ASSY WITH 1EA. NEW PART REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, & BOMBARDIER DWG 601R31527 REV W. COMPLIED WIT
- [SDR SWIA202158189](https://openairdocs.org/sdr/SWIA202158189.md): Bulkhead Web · cracked · Apr 16, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS.621 PRESS BULKHEAD LWR WEB AFT STIFFENER LOCATED OUTBD OF LBL36 ABOVE FLOOR AT WL80 FOUND CRACKED. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED REPLACEMENT FS.621 PRESS. BULKHEAD WEB AFT SIDE STIFFENER P/N 601R36008-51 AT WL.79 OUTBD OF LBL36 PER
- [SDR SWIA202158188](https://openairdocs.org/sdr/SWIA202158188.md): Angle · cracked · Apr 13, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 RBL 9, INBOARD VERTICAL ANGLE APPEARS CRACKED AT TOP END. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED VERTICAL ANGLE UNDER FLOOR LEVEL AT FS.280 RBL.9 (INBD) REF REO 601R-53-11-171 REV.-D DATED 13 FEB 07 AND CRJ 200 SRM 51-42-21 AND COMPLIED WITH
- [SDR SWIA202158187](https://openairdocs.org/sdr/SWIA202158187.md): Angle · cracked · Apr 13, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 LBL 9, INBOARD VERTICAL ANGLE APPEARS CRACKED AT TOP END. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED VERTICAL ANGLE UNDER FLOOR LEVEL AT FS.280 LBL.9 (INBD) REF REO 601R-53-11-171 REV.-D DATED 13 FEB 07 AND CRJ 200 SRM 51-42-21 COMPLIED WITH 51-
- [SDR SWIA202158186](https://openairdocs.org/sdr/SWIA202158186.md): Frame · cracked · Apr 9, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Frame
  > *FS333 FRAME CRACKED BETWEEN STR1L AND STR2L (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED FRAME SECTOR 601R32004-41 REF. CRJ 200 SRM 51-42-06, CRJ-200-SRM 51-42-21. DRAWING 601R31522 REV AC AND DRAWING 601R31016 REV D. COMPILED WITH 51-900-1003-SKY AND
- [SDR SWIA202158185](https://openairdocs.org/sdr/SWIA202158185.md): Skin · chafed · Apr 5, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > * THE CENTER WING LOWER PLANK IS CHAFED AT 2 LOCATIONS ALONG ITS AFT END, JUST INBOARD OF LBL 45 AND JUST INBOARD OF RBL 45, BOTH LOCATIONS ARE BELOW THE AFT SPAR. (C-CHECK RO 5/16/2021) REPAIRED THE CENTER WING LOWER PLANK CHAFE AT 2 LOCATIONS ALONG I
- [SDR SWIA202158210](https://openairdocs.org/sdr/SWIA202158210.md): Hinge · gouged · Apr 3, 2021 · N925EV · Cndair CL6002B19 · Ailerons
  > *RIGHT WING, AILERON HINGE FITTING #3 (CENTER OTBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #3 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14
- [SDR SWIA202158209](https://openairdocs.org/sdr/SWIA202158209.md): Hinge · gouged · Apr 3, 2021 · N925EV · Cndair CL6002B19 · Ailerons
  > *RIGHT WING, AILERON HINGE FITTING #2 (CENTER INBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #2 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14
- [SDR SWIA202158208](https://openairdocs.org/sdr/SWIA202158208.md): Hinge · corroded · Apr 3, 2021 · N925EV · Cndair CL6002B19 · Ailerons
  > *RIGHT WING, AILERON HINGE FITTING #1 (MOST INBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #1 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14.
- [SDR SWIA202158207](https://openairdocs.org/sdr/SWIA202158207.md): Seat Track · corroded · Apr 2, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * CORROSION IN MULTIPLE SPOTS ON RBL9.00 FLOOR SEAT TRACK BETWEEN FS364.00 & FS394.00 (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW SEAT TRACK WITH RTV 157 ON FAYING SURFACE BETWEEN FS364 TO FS399 REF CRJ 200 AMM 53-01-11-400-802
- [SDR SWIA202158206](https://openairdocs.org/sdr/SWIA202158206.md): Seat Track · corroded · Apr 2, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * CORROSION IN MULTIPLE SPOTS ON LBL9.00 FLOOR SEAT TRACK BETWEEN FS364.00 & FS394.00 (C-CHECK RO 5/16/2021) REMOVED DISCREPANT SEAT TRACK REF CRJ 200 SRM 51-41-02, FABRICATED AND INSTALLED NEW LBL 9 SEAT TRACK BETWEEN FS364.00 & FS394.00, REF REO 601
- [SDR SWIA202158184](https://openairdocs.org/sdr/SWIA202158184.md): Frame · corroded · Apr 2, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Frame
  > * CORROSION ON FRAME 409+16 FORWARD SIDE AND ATTACH FLANGE BETWEEN STR26R AND STR26L. (C-CHECK RO 5/16/2021) REPAIRED FRAME 409+16 FORWARD SIDE AND ATTACH FLANGE BETWEEN STR25R AND STR25L REF CRJ-200-SRM 53-00-15. PREESURE CHECK GOOD AND COMPLIED WITH
- [SDR SWIA202158205](https://openairdocs.org/sdr/SWIA202158205.md): Web · corroded · Apr 1, 2021 · N925EV · Cndair CL6002B19 · Passenger/Crew Doors
  > * PASSENGER DOOR AFT WEB NEAR PULLEY BRACKET FOR SUPPORT WHEEL CABLE HAS CORROSION (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND REPLACED WITH NEW PAX DOOR AFT WEB REF CRJ 200 SRM 51-42-06 SEE CONTINUE CARD FO DETAILS
- [SDR SWIA202158204](https://openairdocs.org/sdr/SWIA202158204.md): Angle · corroded · Apr 1, 2021 · N925EV · Cndair CL6002B19 · Passenger/Crew Doors
  > * PASSENGER DOOR ANGLE ATTACHED TO INNER SKIN FOR PANEL 832AT HAS CORROSION (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND REPLACED PAX DOOR ANGLE ATTACHED TO INNER SKIN FOR PANEL 832AT REF. CRJ200 SRM 51-42-13.
- [SDR SWIA202158183](https://openairdocs.org/sdr/SWIA202158183.md): Floorbeam · corroded · Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * CORROSION ON FS280.00 BEAM BETWEEN RBL9.00 & LBL9.00 (MARKED WITH ORANGE STREAMER) (C-CHECK RO 5/16/2021) REMOVED CORROSION ON FS280 BEAM BETWEEN RBL9 & LBL9, REF CRJ 200 SRM 51-21-06, FWD ANGLE IS OUT OF LIMITS PER REF CRJ 200 SRM 53-00-00, AFT ANGLE
- [SDR SWIA202158182](https://openairdocs.org/sdr/SWIA202158182.md): Floorbeam · corroded · Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * CORROSION ON FLOOR SUPPORT ANGLE AT FS621 OUTBOARD OF LBL27. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT FS621 OUTBOARD OF LBL27 REF REO 601R-53-61-117 REV -E DATED 2018-01-15, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRES
- [SDR SWIA202158181](https://openairdocs.org/sdr/SWIA202158181.md): Tie Down · corroded · Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * CORROSION ON PLATES FOR CARGO NET TIE DOWNS BETWEEN FS574 AND FS621. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FWD, MID, AND AFT TIE DOWN PLATES FLOOR SUPPORTS. IAW CRJ200 SRM 51-42-06, 51-45-00, AND BOMBARDIER INC. CANADAIR ENGINEER DWG NO. 601R3
- [SDR SWIA202158180](https://openairdocs.org/sdr/SWIA202158180.md): Frame · cracked · Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Frame
  > * FS605 FRAME LOWER FLANGE CRACKED AT STR24L. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW LOWER FRAME SECTOR, 4(EA) SPLICES AND 2(EA) SUPPORT CLIPS OF FS605 REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG601R36026 REV.AF. COMPLIED WITH 51-9
- [SDR SWIA202158179](https://openairdocs.org/sdr/SWIA202158179.md): Cargo Track · cracked · Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * BRACKET ON BOTTOM OF CARGO TRACK SUPPORT AT FS621 CRACKED. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED 1EA. NEW SUPPORT BRACKET FOR CARGO DOOR TRACK, LOCATED AT BOTTOM OF DOOR SUPPORT TRACK AT FS621 REF. BOMBARDIER DWG#601R35050 REV Y. & SRM 51-42-
- [SDR SWIA202158178](https://openairdocs.org/sdr/SWIA202158178.md): Floor Support · corroded · Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * LH PRESSURE FLOOR SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REPAIRED LH PRESSURE FLOOR SILL REF REO 601R-53-41-2901 REV-- DATED 2021-04-16 AND REO 601R-53-41-666 REV C DATED 2012-11-06. PRESSURE CHECK GOOD AND COMPLIED WITH 51
- [SDR SWIA202158203](https://openairdocs.org/sdr/SWIA202158203.md): Hinge · corroded · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Spoilers
  > RH SPOILERON INBD AND OTBD HINGE POINT COVER PLATE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED INBD AND OTBD HINGE POINT COVER PLATE HARDWARE REF CRJ 200 AMM 27-64-01-400-801
- [SDR SWIA202158202](https://openairdocs.org/sdr/SWIA202158202.md): Hinge · corroded · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Spoilers
  > RH FLIGHT SPOILER INBD AND MIDDLE HINGE POINT HARDWARE AND INBD COVER PLATE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FLIGHT SPOILER INBD AND MIDDLE HINGE POINT HARDWARE & INBD COVER PLATE HARDWARE REF CRJ200 AMM 27-64-05-400-801
- [SDR SWIA202158201](https://openairdocs.org/sdr/SWIA202158201.md): Attach Fitting · corroded · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Spoilers
  > RH OTBD GROUND SPOILER INBD, MIDDLE, OTBD AND PCU CONNECT HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACE CORRODED HARDWARE WITH NEW HARDWARE ON RH OTBD GROUND SPOILER AT INBD, MIDDLE, OTBD, AND PCU ATTATCHING POINTS. REF CRJ 200 AMM 27-65-
- [SDR SWIA202158200](https://openairdocs.org/sdr/SWIA202158200.md): Hinge · corroded · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Spoilers
  > RH INBD GROUND SPOILER OTBD HINGE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED HARDWARE ON RH INBD GROUND SPOILER OTBD HINGE REF CRJ 200 AMM 27-65-01-000-801
- [SDR SWIA202158177](https://openairdocs.org/sdr/SWIA202158177.md): Seat Track · corroded · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE SEAT RAIL SUPPORT BEAM FS424 TO FS513 RBL9.0 / 783161$M255 (C-CHECK RO 5/16/2021) REPAIRED SEAT RAIL PER MHIRJ REO 601R-53-41-2907, REV --, DATED 2021-05-07 AND COMPLIED WITH ALL STEPS OF THE REO. SEE CONTIUATION CARD FOR FURTHER DETAI
- [SDR SWIA202158176](https://openairdocs.org/sdr/SWIA202158176.md): Seat Track · corroded · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE SEAT RAIL SUPPORT BEAM FS409+118 TO FS559-10 LBL9.0 (C-CHECK RO 5/16/2021) / REMOVED CORROSION ON THE SEAT RAIL SUPPORT BEAM FROM FS409+118 TO FS559+10 LBL9, & FOUND TO BE OUT OF LIMITS PER REF REO 601R-53-00-005, REV -B, DATE 2011-01-
- [SDR SWIA202158175](https://openairdocs.org/sdr/SWIA202158175.md): Skin · damaged · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Wing, Plate/Skin
  > WHILE COMPLYING WITH SB 601R-57-046 REV C ( PART A) LHS 1EA O/S FASTENER FOUND INSTALLED IN HOLE #14. FASTENER TYPE IS (HST411-10, HOLE DIA. IS.340". (C-CHECK RO 5/16/2021) REPAIRED L/H SIDE 1 EA OVERSIZE FASTENER HOLE IN WING PLANK ASSY ( STEEL STRA
- [SDR SWIA202158174](https://openairdocs.org/sdr/SWIA202158174.md): Floor Support · corroded · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RH PRESSURE FLOOR SILL ANGLE CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REMOVED CORROSION FROM R/H PRESSURE FLOOR SILL ANGLE AT MULTIPLE LOCATIONS REF REO 601R-53-41-666, REV -C, 2012-11-06 AND REO 601R-53-41-2902 REV-- DATED: 2021-04
- [SDR SWIA202158173](https://openairdocs.org/sdr/SWIA202158173.md): Floor Support · corroded · Mar 31, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RH PRESSURE FLOOR SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REPAIRED RH PRESSURE FLOOR SILL REF REO 601R-53-41-2902 REV-- DATED: 2021-04-16 AND REO 601R-53-41-666 REV. €“C DATE 2012-11-06.. PRESSURE CHECK GOOD AND COMPLIED WI
- [SDR SWIA202158199](https://openairdocs.org/sdr/SWIA202158199.md): Seat Track · corroded · Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * THE CABIN FLOOR SEAT RAIL/TRACK ON RBL 9.0 BETWEEN FS 409+128 AND FS 559 HAS MULTIPLE SPOTS OF CORROSION, SCRATCHES AND NICKS. (C-CHECK RO 5/16/2021) REMOVED THE CORROSION AND OTHER DAMAGE FROM THE SEAT TRACK, FS409+126 TO FS559+4 RBL9.0 PART # 601R3
- [SDR SWIA202158198](https://openairdocs.org/sdr/SWIA202158198.md): Seat Track · corroded · Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * THE CABIN FLOOR SEAT RAIL/TRACK ON LBL 9.0 BETWEEN FS 409+128 AND FS 559 HAS MULTIPLE SPOTS OF CORROSION, SCRATCHES AND NICKS. (C-CHECK RO 5/16/2021) REMOVED THE CORROSION AND OTHER DAMAGE FROM THE SEAT TRACK, FS409+126 TO FS559+4 LBL9.0 PART # 601R31
- [SDR SWIA202158197](https://openairdocs.org/sdr/SWIA202158197.md): Floorbeam · corroded · Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * THE LBL 9.0 FLOOR BEAM ATTACHMENT TO THE FS 621 BULKHEAD'S SEAT TRACK HAS CORROSION AROUND ITS SCREW HOLES. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW CARGO TIE-DOWN TRACK AT LBL9 APPROX. FS621 REF CRJ200 AMM 53-00-49-000-801 & 53-00-49-400-80

Next page: https://openairdocs.org/aircraft/N925EV/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 = 'N925EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N925EV/reports

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