# Service difficulty reports: N905EV

A list on [N905EV](https://openairdocs.org/aircraft/N905EV.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 6 · 293 reports

- [SDR SWIA2026071877602](https://openairdocs.org/sdr/SWIA2026071877602.md): Seat Track · corroded · Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 SEAT RAIL SCRATCHED AND CORRODED. INSTALLED A NEW SEAT RAIL IAW AMM 53-01-11-400-802.
- [SDR SWIA2026071877601](https://openairdocs.org/sdr/SWIA2026071877601.md): Seat Track · corroded · Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT RAIL SCRATCHED AND CORRODED. REMOVED AND REPLACED THE SEAT RAIL IAW AMM 53-01-11-400-802.
- [SDR SWIA2026071877600](https://openairdocs.org/sdr/SWIA2026071877600.md): Seat Track · corroded · Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL SCRATCHED AND CORRODED. INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11-400-802,
- [SDR SWIA2026071877599](https://openairdocs.org/sdr/SWIA2026071877599.md): Seat Track · corroded · Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT RAIL SCRATCHED AND CORRODED. REMOVED AND INSTALLED NEW SEAT RAIL, IAW AMM 53-01-11-400-802.
- [SDR SWIA2026071877598](https://openairdocs.org/sdr/SWIA2026071877598.md): Seat Track · scratched · Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT RAIL SCRATCHED AND CORRODED. INSTALLED NEW RBL9 SEAT RAIL IAW AMM 53-01-11-400-802
- [SDR SWIA2026071877597](https://openairdocs.org/sdr/SWIA2026071877597.md): Seat Track · scratched · Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL27 SEAT RAIL SCRATCHED AND CORRODED. INSTALLED NEW SEAT RAIL AT RBL27 IAW AMM 53-01-11-400-802.
- [SDR SWIA2026071877596](https://openairdocs.org/sdr/SWIA2026071877596.md): Seat Track · scratched · Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL27 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS559.078 TO 559. 093 REPLACED RBL 27 SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR SWIA20250502001](https://openairdocs.org/sdr/SWIA20250502001.md): Warning Message · illuminated · May 1, 2025 · N905EV · Cndair CL6002B19 · Stabilizer Position Indicating
  > DURING CLIMB THROUGH 3500 FEET RECEIVED A STAB TRIM RUNAWAY NOSE DOWN. RAN MEMORY ITEMS, QRC, QRH. RETURNED TO ORD. (FLIGHT 5852 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30068339 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 30070396
- [SDR SWIA2025041500014](https://openairdocs.org/sdr/SWIA2025041500014.md): Landing Gear · warning message · Apr 14, 2025 · N905EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > WHEN BRINGING THE GEAR DOWN RECEIVED A GEAR DISAGREE WARNING MESSAGE. NO GREEN LIGHT FOR THE GEAR. RAN QRH PROCEDURE AND GOT THE GEAR DOWN AND LOCKED. THREE GREEN LIGHT. MEL 32-30-1CAT A DUE TAC 40385 ODI SMOD APPROVAL FOR RTS CAT II DOWNGRADED (FLIGHT 5040
- [SDR SWIA2023050100020](https://openairdocs.org/sdr/SWIA2023050100020.md): Unknown · cracked · Apr 20, 2023 · N905EV · Cndair CL6002B19 · Landing Gear System
  > RIGHT M/L/G WHEEL WELL. BRAKE PRESSURE TRANSDUCER BRACKET CRACKED. (C-CHECK RO 4/26/2023) REMOVED CRACKED AND INSTALLED NEW BRAKE PRESSURE TRANSDUCER MOUNT BRACKET IN RH MLG WHEEL WELL - REF REO 601R-53-42-007, REV A, DATE 31-JAN-2006. OPERATIONAL AND
- [SDR SWIA2023050100019](https://openairdocs.org/sdr/SWIA2023050100019.md): Unknown · corroded · Apr 4, 2023 · N905EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > MULTIPLE SPOTS OF CORROSION NOTED ON RH FLOOR SILL FS473.15.00 TO FS499.00 (AREA MARKED) (C-CHECK RO 4/26/2023) REMOVED CORROSION ON RH FLOOR SILL BETWEEN FS473.15.00 TO FS499.00 REF CRJ200 SRM 51-21-06FOUND TO BE WITHIN LIMITS/RESTORED FINISH REF REO 6
- [SDR SWIA2023050100018](https://openairdocs.org/sdr/SWIA2023050100018.md): Unknown · dented · Mar 30, 2023 · N905EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CREASED/DENT DAMAGE FOUND ON UPPER FUSELAGE SKIN 3.5" AFT OF 31.875% BETWEEN STR 4R-5R (C-CHECK RO 4/26/2023) COMPLIED WITH REPAIR ON UPPER FUSELAGE SKIN 3.5" AFT OF 31.875% BET. STR 4R-5R REF REO 601R-53-71-222 REV A DATED 2023-04-08, COMPLIED WITH S
- [SDR SWIA2023050100017](https://openairdocs.org/sdr/SWIA2023050100017.md): Unknown · cracked · Mar 28, 2023 · N905EV · Cndair CL6002B19 · Fuselage Floor Panel
  > RH FLOOR BEAM FS484.00 RBL 27 CLIP IS CRACKED (INBD CLIP) (C-CHECK RO 4/26/2023) REMOVED AND REPLACED FLOOR BEAM CLIP AT FS 484.0, RBL 27. REF. REO 601R-53-41-059 REV. -C DATED 2020-03-11. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STR
- [SDR SWIA2023050100016](https://openairdocs.org/sdr/SWIA2023050100016.md): Unknown · cracked · Mar 28, 2023 · N905EV · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT SIDE. FLOOR BEAM OUTBOARD CLIP AT FS 484.0 IS CRACKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED LEFT SIDE FLOOR BEAM OUTBOARD CLIP AT FS484.0. REF. REO 601R-53-41-059 REV. -C DATED 2020-03-11.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL60
- [SDR SWIA2023050100014](https://openairdocs.org/sdr/SWIA2023050100014.md): Unknown · unknown · Mar 27, 2023 · N905EV · Cndair CL6002B19 · Fuselage, Stabilizer Attach Fittings
  > UPON REMOVAL ON THE RIGHT STAB TIP FOUND HOLE THE FLANGE UPPER SIDE WHERE THE NUTPLATE WAS. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW SPLICE P/N 600-23037-22. REF: DWG 600-23037, REV: L, DWG 600-23026, REV: T, CRJ200 SRM 51-42-06, CRJ200 SRM 51-
- [SDR SWIA2023050100013](https://openairdocs.org/sdr/SWIA2023050100013.md): Unknown · gouged · Mar 23, 2023 · N905EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > EXISTING DOUBLER AT AFT SIDE FS.280 BULKHEAD RBL12 WL93.50 IS GOUGED AND DENTED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED DOUBLER AT AFT SIDE FS.280 BULKHEAD RBL12 WL93.50 WITH NEW REF. CRJ 200 SRM 51-42-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1
- [SDR SWIA2023050100012](https://openairdocs.org/sdr/SWIA2023050100012.md): Unknown · punctured · Mar 23, 2023 · N905EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS.280 BULKHEAD HAS A PUNCTURE AT RBL14 WL87.50. (C-CHECK RO 4/26/2023) PERFORMED DOUBLER REPAIR AT FS280 BULKHEAD AT RBL14 WL87.50 REF REO 601R-53-11-3850 REV-- DATED 2023-04-03. COMPLIED WITH TASK 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS ON WORK
- [SDR SWIA2023050100011](https://openairdocs.org/sdr/SWIA2023050100011.md): Unknown · corroded · Mar 23, 2023 · N905EV · Cndair CL6002B19 · Fuel Storage
  > * FUEL CELL ACCESS PANEL LANDING AT 540BB HAS CORROSION 2 PLCS, MARKED. (C-CHECK RO 4/26/2023) REMOVED CORROSION ON FUEL CELL ACCESS PANEL LANDING AT 540BB REF CRJ 200 SRM 51-21-06. FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-57-21-
- [SDR SWIA2023050100010](https://openairdocs.org/sdr/SWIA2023050100010.md): Unknown · corroded · Mar 22, 2023 · N905EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FUSELAGE DOOR SURROUND ANGLE IS CORRODED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED FUSELAGE PAX DOOR ANGLE REF CRJ 200 SRM 51-42-06, SRM 51-42-13, SRM 51-42-21 AND DWG 601R31527 REV AM. REMOVED AND INSTALLED FWD AND NEW AFT HANDRAIL FITTING IAW CRJ 2
- [SDR SWIA202305010009](https://openairdocs.org/sdr/SWIA202305010009.md): Unknown · corroded · Mar 22, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)
  > PASSENGER DOOR. FWD DOOR STAIRS HANDLE ARM CUT-OUT CORRODED ON THE FLOOR SUPPORT ANGLE. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW PAX FWD CUT STAIR HANDLE ARM CUT OUT IAW CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV. AM. COMPLIED WITH SKYWEST TASK
- [SDR SWIA2023050100024](https://openairdocs.org/sdr/SWIA2023050100024.md): Unknown · corroded · Mar 20, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)
  > R/H SIDE SEAT RAIL FROM APPROXIMATELY FS449.85 TO FS499.00 HAS NUMEROUS SPOTS OF CORROSION AND CHAFING, MARKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED R/H SIDE SEAT RAIL FROM APPROXIMATELY FS449.85 TO FS499.00. REF. CRJ200 AMM 53-01-11-400-802
- [SDR SWIA2023050100008](https://openairdocs.org/sdr/SWIA2023050100008.md): Unknown · corroded · Mar 20, 2023 · N905EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PASSENGER DOOR. AFT DOOR STAIRS HANDLE ARM CUT-OUT CORRODED ON THE FLOOR SUPPORT ANGLE. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW AFT DOOR STAIR CUP IAW CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV. AM. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-
- [SDR SWIA2023050100023](https://openairdocs.org/sdr/SWIA2023050100023.md): Unknown · corroded · Mar 19, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)
  > R/H SIDE SEAT RAIL FROM FS409.00+16 TO FS409+112 HAS NUMEROUS SPOTS OF CORROSION AND CHAFING, MARKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED R/H SIDE SEAT RAIL FROM FS409.00+16 TO FS409+112. REF. CRJ200 AMM 53-01-11-400-802
- [SDR SWIA2023050100007](https://openairdocs.org/sdr/SWIA2023050100007.md): Unknown · corroded · Mar 18, 2023 · N905EV · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT HAND FLOOR SUPPORT BEAM CAP RBL9R, HAS NUMEROUS SPOTS OF CORROSIION AND WEAR, FROM FS409.0 TO FS409.0+112. (CORROSION SPOTS MARKED WITHIN RED GREASE PENCIL). (C-CHECK RO 4/26/2023) BLENDED OUT CORROSION ON RBL 9 FLOOR BEAM CAP FROM FS 409 TO 409+1
- [SDR SWIA2023050100006](https://openairdocs.org/sdr/SWIA2023050100006.md): Unknown · corroded · Mar 17, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)
  > R/H PRESSURE FLOOR SILL. ONE (1) SPOT OF CORRORION AT FS518.0 (C-CHECK RO 4/26/2023) REMOVED CORROSION FROM RH PRESSURE FLOOR SILL AT FS518.00 REF. CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR IAW ALL STEPS OF REO 601R-53-41-3143 RE
- [SDR SWIA2023050131301](https://openairdocs.org/sdr/SWIA2023050131301.md): Unknown · chafed · Mar 13, 2023 · N905EV · Cndair CL6002B19 · Wing Structure
  > *R/H WING INBOARD FLAP VANE SKIN LEADING EDGE IS CHAFED AT THE INBOARD. (C-CHECK RO 4/26/2023) REMOVED DAMAGED RH IB FLAP VANE INBOARD LEADING EDGE SKIN AND INSTALLED A NEW VANE SKIN 601R14303-54 REF CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. COM
- [SDR SWIA2023050100003](https://openairdocs.org/sdr/SWIA2023050100003.md): Unknown · gouged · Mar 13, 2023 · N905EV · Cndair CL6002B19 · Fuselage Floor Panel
  > *CARGO DOOR INTERIOR SURROUND AFT TRACK ASSY GOUGED/WORN OUTBOARD TRACK UPPER AND INBOARD TRACK UPPER SIDE (MARKED) (C-CHECK RO 4/26/2023) REMOVED DAMAGED AND INSTALLED NEW AFT CARGO DOOR AFT TRACK IAW CRJ200 SRM 51-42-06 REV. 39 ISSUED 03/10/21, SRM 5
- [SDR SWIA2023050100002](https://openairdocs.org/sdr/SWIA2023050100002.md): Unknown · dented · Mar 13, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)
  > *DENTS IN BOTTOM DOUBLER BELOW AND AFT OF GROUND AIR CONDITIONING CONNECTION PNL 172BR (MARKED) (C-CHECK RO 4/26/2023) REPAIRED DAMAGED AREA COMMON TO LOWER FUSELAGE SKIN APPROXIMATELY BETWEEN FS574 & FS621 AND STRG26L TO STRG20R IAW REO 601R-53-61-799
- [SDR SWIA2023050100311](https://openairdocs.org/sdr/SWIA2023050100311.md): Unknown · chafed · Mar 11, 2023 · N905EV · Cndair CL6002B19 · Wing Structure
  > * L/H AILERON UPPER LEADING EDGE SKIN IS CHAFED, MARKED. (C-CHECK RO 4/26/2023) BLENDED DAMAGE ON LH AILERON UPPER LEADING EDGE REF REO 601R-57-60-013, REV -A, DATED 2013-08-05.FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW LH AILERON UPPER L
- [SDR SWIA2021112262663](https://openairdocs.org/sdr/SWIA2021112262663.md): Transmitter · failed · Nov 19, 2021 · N905EV · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > UNCOMMANDED FLAP EXTENSION IN FLIGHT WITH ASSOCIATED FLAPS DEGRADED STATUS MESSAGE. FLAPS EVENTUALLY STOWED AT 0 DEGREES OF EXTENSION. COMPLIED WITH FLAP TWIST QRH PROCEDURE. PERIODIC HYD 2B AND HYB 3B CAUTION MESSAGES. MESSAGES CLEARED WITH QRH PROCEDURE. (F
- [SDR SWIA2020031049246](https://openairdocs.org/sdr/SWIA2020031049246.md): Bracket · broken · Mar 3, 2020 · N905EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR AFT SURROUND PANEL 232EZ LOWER BRACKET IS BROKEN WHERE MARKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED AFT LOWER BRACKET COMMON TO SERVICE DOOR SURROUND PANEL 232EZ AND FS349 FRAME, PN 601R40170-25 PO 7632-00009/155, REFERENCE CRJ200 SRM.
- [SDR SWIA2020031049185](https://openairdocs.org/sdr/SWIA2020031049185.md): Mount Bracket · cracked · Feb 21, 2020 · N905EV · Cndair CL6002B19 · Aerodynamic Fairings
  > RH STUB FAIRING FWD MOUNTING BRACKET CRACKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED WITH NEW RH STUB FAIRING FWD MOUNTING BRACKET REF CRJ200 SRM.
- [SDR SWIA2020031049165](https://openairdocs.org/sdr/SWIA2020031049165.md): Floorbeam · damaged · Feb 20, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BEAM CAP AT LBL9 FS409.00+96 TO 409.00+112 FOUND TO BE OUT OF LIMITS ON CAMP # 20320140. PERFORM A SPLICE REPAIR. (C CHECK) RO 3/7/2020 PERFORMED FLOOR BEAM CAP SPLICE REPAIR FROM FS409.00+96 TO 409.00+112 LBL9. REF CRJ-200 SRM REPAIR NO. 2 AND BOMBARDIER
- [SDR SWIA2020031049163](https://openairdocs.org/sdr/SWIA2020031049163.md): Floorbeam · damaged · Feb 20, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BEAM CAP AT LBL9 FS409.00 TO 409.00+48 FOUND TO BE OUT OF LIMITS ON CAMP # 20320140. PERFORM A SPLICE REPAIR. (C CHECK) RO 3/7/2020 PERFORMED FLOOR BEAM CAP SPLICE REPAIR FROM FS409.00 TO 409.00+48 LBL9. REF CRJ-200 SRM, REPAIR NO. 2 AND BOMBARDIER REO. CO
- [SDR SWIA2020031049230](https://openairdocs.org/sdr/SWIA2020031049230.md): Plate · corroded · Feb 18, 2020 · N905EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT ANCHOR FITTING SERRATED PLATE, AIRCRAFT SIDE THAT ATTACHES TO FS349 FRAME, CORRODED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED WITH NEW PAX DOOR AFT ANCHOR FITTING SERRATED PLATE, AIRCRAFT SIDE THAT ATTACHES TO FS349 FRAME, PN 600-38061-6, RE
- [SDR SWIA2020031049161](https://openairdocs.org/sdr/SWIA2020031049161.md): Angle · cracked · Feb 14, 2020 · N905EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > F.S. 280, RBL 9 O/B ANGLE CRACKED IN RADIUS AT TOP OF ANGLE. (C CHECK) RO 3/7/2020 REMOVED CRACKED ANGLE AT FS 280.0 RBL 9.0 O/B SIDE AND INSTALLED NEW ANGLE,REF BOMBARDIER REO.
- [SDR SWIA2020031049159](https://openairdocs.org/sdr/SWIA2020031049159.md): Angle · cracked · Feb 12, 2020 · N905EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > F.S. 280, LBL 9 O/B ANGLE CRACKED IN RADIUS AT TOP OF ANGLE. (C CHECK) RO 3/7/2020 REMOVED CRACKED ANGLE FROM FS 280.0 LBL 9.0 AND INSTALLED NEW ANGLE,REF BOMBARDIER REO.
- [SDR SWIA2020031049158](https://openairdocs.org/sdr/SWIA2020031049158.md): Skin · gouged · Feb 12, 2020 · N905EV · Cndair CL6002B19 · Rudder, Plate/Skin
  > *RUDDER HAS GOUGE ON LH SKIN BETWEEN LOWER AND MIDDLE HINGE. ( MARKED) (C CHECK) RO 3/7/2020 CUT AWAY DAMAGE ON RUDDER LH SKIN AND INSTALLED REPAIR TO LHS RUDDER SKIN BETWEEN R.S. 85.07 AND R.S. 90.32 IN REF REO. COMPLIED WITH SKYWEST TASK CARD. SEE CONTI
- [SDR SWIA2020031049241](https://openairdocs.org/sdr/SWIA2020031049241.md): Skin Panel · broken · Feb 6, 2020 · N905EV · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > WHILE INSPECTING PANEL 326BL FOR DISBONDED TEFLON STIPS FOR JOB 2763291 OP 82 MX TRANS. 20282016 FOUND PANEL TO BE UNSERVICABLE DUE TO BROKEN OFF SECTION OF PANEL (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PANEL 326BL OUTER SKIN P/N:600-21134-45 REF. SRM.
- [SDR SWIA2020031049176](https://openairdocs.org/sdr/SWIA2020031049176.md): Skin · cracked · Feb 6, 2020 · N905EV · Cndair CL6002B19 · Wing, Plate/Skin
  > COMPLY WITH SB 601R-57-037 REV E DATED 3/5/2009 ( WINGS - LOWER WING PLANK - MODIFICATION OF THE LEFT AND RIGHT WINGS IN AREA OF THE REAR SPAR AT WS148.019) PART'S A AND B (C CHECK) RO 3/7/2020 SERVICE BULLETIN, WINGS --- LOWER WING PLANK --- MODIFICATION
- [SDR SWIA2020031049184](https://openairdocs.org/sdr/SWIA2020031049184.md): Window · cracked · Feb 4, 2020 · N905EV · Cndair CL6002B19 · Passenger Compartment Windows
  > R/H WINDOW #4 (4CD) IS CRACKED AND CHIPPED ON THE OUTER WINDOW PANE, FWD LEADING EDGE. REQUIRES REPLACEMENT (C CHECK) RO 3/7/2020 REMOVED AND REPLACED THE PASSENGER WINDOW #4 @ (4CD). REF CRJ200 AMM. PRESSURE CHECKS GOOD.
- [SDR SWIA2020031049248](https://openairdocs.org/sdr/SWIA2020031049248.md): Bracket · cracked · Feb 3, 2020 · N905EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > CONNECTING BRACKET/BRIDGE FOR CANOE PANEL 697AB IS CRACKED. (C CHECK) RO 3/7/2020 INSTALLED NEW CONNECTING BRACKET TO CANOE PANEL # 697AB AS REQUIRED PER REF: CRJ200 SRM.
- [SDR SWIA2020031049153](https://openairdocs.org/sdr/SWIA2020031049153.md): Seat Track · corroded · Jan 24, 2020 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9.00 FROM FS409.00 TO FS409.00+112HAS MULTIPLE LOCATIONS OF PITTED CORROSION (C CHECK) RO 3/7/2020 BLENDED OUT CORROSION ON SEAT TRACK LBL9.0 AT FS409.00 TO FS409.00+112. REF. CRJ200 SRM. EVALUATED BLEND AS OUT-OF-LIMITS. REMOVED SEAT TRAC
- [SDR SWIA2020031049228](https://openairdocs.org/sdr/SWIA2020031049228.md): Frame · corroded · Jan 23, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Frame
  > *FRAME 513.00 HAS HEAVY CORROSION PITTING FROM APPROXIMATELY STGR 4RH €“ STGR 7RH (MARKED) (C CHECK) RO 3/7/2020 BLENDED OUT CRROSION ON FS 513 FRAME RH AT STRINGER 4R TO 7R AND FOUND ACCEPTABLE TO ENGINEERING REF REO.
- [SDR SWIA2020031049150](https://openairdocs.org/sdr/SWIA2020031049150.md): Stringer · corroded · Jan 23, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *BETWEEN FS333.00 AND FS349.00 / STGR. 27 REPAIR IS CORRODED. FLAGGED (C CHECK) RO 3/7/2020 NO ALLOWABLE DAMAGE ALLOWED ON REPAIR PARTS FS333.00 AND FS349.00 / STGR. 27 REPAIR REF CRJ200 SRM. REMOVED BAD REPAIR PARTS FS333.00 AND FS349.00 / STGR. 27 REF CR
- [SDR SWIA2020031049148](https://openairdocs.org/sdr/SWIA2020031049148.md): Stringer · cracked · Jan 23, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *FWD CABIN - APPROX. FS. 333.00 RIGHT HAND STGR 1 THE FRAME IS CRACKED (MARKED) (C CHECK) RO 3/7/2020 REMOVED FS 333.00 FRAME TO FOM REF CRJ200 SRM. INSTALLED NEW FS 333.0 FRAME REF CRJ200 SRM AND DRW. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETA
- [SDR SWIA2020031049245](https://openairdocs.org/sdr/SWIA2020031049245.md): Guide · broken · Jan 22, 2020 · N905EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > *ALL 4 OF THE AVIONICS BAY DOOR GUIDES ON THE SURROUND (2EA FWD AND 2EA AFT) ARE BROKEN (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED ALL FOUR (2EA. FWD AND 2EA. AFT) NEW AVIONICS BAY DOOR GUIDES REF BOMBARDIER CRJ-200 CMM. SEE CONTINUATION CARD FO
- [SDR SWIA2020031049225](https://openairdocs.org/sdr/SWIA2020031049225.md): Damper · corroded · Jan 22, 2020 · N905EV · Cndair CL6002B19 · Elevator Control System
  > *RH ELEV CENTER HINGE INBD FLUTTER DAMPER CORRODED HARDWARE AT ELEV ATTACH POINT (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED RH ELEVATOR INBD AND OTBD FLUTTER DAMPER CORRODED HARDWARE REF. CRJ-200 AMM. PERFORMED OPERATIONAL TEST OF THE ELEVATOR CO
- [SDR SWIA2020031049146](https://openairdocs.org/sdr/SWIA2020031049146.md): Cleat · cracked · Jan 22, 2020 · N905EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FWD CABIN - FS. 280 BULKHEAD LEFT HAND STGR 3 - STRINGER TO FRAME CLEAT HAS SIGNS OF A CRACK (MARKED). (C CHECK) RO 3/7/2020 REMOVED AND REPLACED CRACKED CLEAT AT FS. 280 BULKHEAD LEFT HAND STGR 3 WITH NEW REF. CRJ 200 SRM AND BOMBARDIER DWG.
- [SDR SWIA2020031049144](https://openairdocs.org/sdr/SWIA2020031049144.md): Attach Fitting · cracked · Jan 22, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > WINDSHIELD CENTER POST LOWER LH & RH ATTACH FITTINGS CRACKED IN RADIUS. MARKED IN RED. (C CHECK) RO 3/7/2020 REMOVED CRACKED ATTACH FITTINGS AND INSTALLED NEW ATTACH FITTINGS 2EA. IN THE WINDSHIELD CENTER POST REF BOMBARDIER DWG AND CRJ 200 SRM. SEE CONTIN

Next page: https://openairdocs.org/aircraft/N905EV/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 = 'N905EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N905EV/reports

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