# Service difficulty reports: N932EV

A list on [N932EV](https://openairdocs.org/aircraft/N932EV.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 · 180 reports

- [SDR SWIA2026100477493](https://openairdocs.org/sdr/SWIA2026100477493.md): Steering Sys · faulted · Oct 4, 2026 · N932EV · Cndair CL6002B19 · Landing Gear Steering System
  > STEERING INOP CAUTION MESSAGE SHORTLY AFTER TAKEOFF FOLLOWED BY WOW INPUT CAUTION MESSAGE AND WOW OUTPUT FAIL STATUS MESSAGE FLIGHT 5819. SEE AML 2008047, CAMP 33164595 FOR INITIAL TROUBLESHOOTINGSEE CAMP 33164797, 33164844, 33165940, 33165964 FOR R & R, A
- [SDR SWIA2025F01326](https://openairdocs.org/sdr/SWIA2025F01326.md): Warning Message · false activation · Sep 22, 2025 · N932EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > WOW INPUT CAUTION MESSAGE SHORTLY AFTER TAKEOFF. (FLIGHT 5121 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30883122 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 30883945 AND CP 30883899 FOR MAINTENANCE PERFORMED. WOW INPUT CAUTION MESSAGE
- [SDR SWI2025F01323](https://openairdocs.org/sdr/SWI2025F01323.md): Warning Message · illuminated · Sep 22, 2025 · N932EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > WOW INPUT CAUTION MESSAGE SHORTLY AFTER TAKEOFF. (FLIGHT 5121)
- [SDR SWIA20250207201](https://openairdocs.org/sdr/SWIA20250207201.md): Warning Message · illuminated · Feb 1, 2025 · N932EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > D:GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF WHEN WE SELECTED LEG GEAR HANDLE UP. NOES GEAR DID NOT SEEM TO BE GOING UP. PERFORMED QRH, MESSAGED PERSISTED, RETURNED TO FIELD.C:DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. MX ACTIONS CW, PLACARDS IN
- [SDR SWIA2025011341228](https://openairdocs.org/sdr/SWIA2025011341228.md): Hinge Fitting · gouged · Dec 28, 2024 · N932EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > RH AILERON CENTER INBD HINGE FITTING WING SIDE IS GOUGED. (C-CHECK RO 1/13/2025) REMOVED DAMAGE FROM THE R/H AILERON CTR INBD HINGE FITTING AND REPAIRED PER REO 601R-57-51-1060 REV -- DATE 2024-12-31 BY REMOVING DAMAGE, NDT INSPECTING, ROTO-PEENING THE
- [SDR SWIA2025011341224](https://openairdocs.org/sdr/SWIA2025011341224.md): Structure · damaged · Dec 24, 2024 · N932EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LH WING OUTBD HINGEBOX AT WS220.00, THE INBD ATTACH LOBES ON THE WING HAVE TOOLING DAMAGE (MARKED) (C-CHECK RO 1/13/2025) REMOVED NOTED DAMAGE FROM LH WING OUTBD HINGEBOX AT WS220.00 INBD ATTACH LUGS ON THE WING SIDE. NDT INSPECTED NO DEFECTS NOTED ROT
- [SDR SWIA20250113221](https://openairdocs.org/sdr/SWIA20250113221.md): Attach Fitting · chafed · Dec 21, 2024 · N932EV · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > SCREW JACK ATTACH FITTINGS ON THE HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR R/H AND L/H UPPER FWD EDGES OF BOTH SCREW JACK FITTINGS TO HAVE CHAFE MARKS/BARE METAL. (MARKED) (C-CHECK RO 1/13/2025) BLENDED ON FORWARD UPPER INNER EDGE OF JACK SCREW/H
- [SDR SWIA20250113211](https://openairdocs.org/sdr/SWIA20250113211.md): Hinge · corroded · Dec 11, 2024 · N932EV · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL ON JOB HN00204794 CAMP #29239579, FOUND R/H ELEVATOR #1 HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BOTH BEARING BORES, AND THE BORE OF THE INBOARD HINGE HALF TO BE OVERSIZED. REPLACE HINGE FITTING ASSY. (C-CHECK
- [SDR SWIA202501130059](https://openairdocs.org/sdr/SWIA202501130059.md): Access Panel · damaged · Dec 6, 2024 · N932EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT WING LOWER PLANK FUEL ACCESS HOLE FOR PANEL 550FB HAS FRETTING AS MARKED. (C-CHECK RO 1/13/2025) BLENDED OUT PITTING ON THE L/H WING LOWER PLANK FUEL ACCESS HOLE 550FB, OTBD LANDING REF BOMBARDIER REO 601R-57-21-030 REV-L, DATED 2014-02-05, DETAIL
- [SDR SWIA2020113206](https://openairdocs.org/sdr/SWIA2020113206.md): Access Panel · damaged · Dec 6, 2024 · N932EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER PLANK FUEL ACCESS HOLE FOR PANEL 540DB HAS FRETTING AS MARKED. (C-CHECK RO 1/13/2025) BLENDED OUT PITTING ON THE L/H WING LOWER PLANK FUEL ACCESS HOLE 540DB, OTBD LANDING REF BOMBARDIER REO 601R-57-21-030 REV-L, DATED 2014-02-05, DETAIL
- [SDR SWIA202501130100](https://openairdocs.org/sdr/SWIA202501130100.md): Strap · damaged · Nov 30, 2024 · N932EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT WING STRAP ON LOWER SKIN AT APPROXIMATELY WS65.75 AT MAIN LANDING GEAR LOWER TRUNNION STRAP HAS PITTING AND ENVIRONMENTAL DAMAGE AS MARKED (C-CHECK RO 1/13/2025) REMOVED CORROSION FROM THE R/H WING LWR SKIN AT WS65.75-WS80.50 PER CRJ200SRM 51-21-0
- [SDR SWIA2025011325](https://openairdocs.org/sdr/SWIA2025011325.md): Floorbeam · cracked · Nov 25, 2024 · N932EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FITTING ON RBL9 FLOORBEAM AT FS461 IS CRACKED (C-CHECK RO 1/13/2025) REMOVED AND INSTALLED 1EA NEW RBL9 FS461.00 FLOOR BEAM FITTING PER CRJ200SRM 51-42-06, CRJ200SRM 51-42-21, DWG 601R31118 REV L, AND DWG 601R31146 REV J. COMPLIED WITH SKYWEST TASK C
- [SDR SWIA2025011320](https://openairdocs.org/sdr/SWIA2025011320.md): Panel · eroded · Nov 20, 2024 · N932EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > PANEL 630JL HAS EROSION AND PITTING ALONG LENGTH OF LE 29183407 (C-CHECK RO 1/13/2025) BLENDED PITTING FROM AFFECTED AREA REF CRJ200 SRM 51-12-00. FOUND WITHIN LIMIT PER REO 601R-57-41-1181 REV -- DATED 2024-12-12 COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202501130058](https://openairdocs.org/sdr/SWIA202501130058.md): Hinge · damaged · Nov 18, 2024 · N932EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE (PAX DOOR SIDE) HAS OVERSIZED LOCKING PIN HOLE (C-CHECK RO 1/13/2025) COMPLIED WITH REO 601R-52-11-3030 REV. -- DATED 2024-11-23 ALL STEPS PAX DOOR HINGE LUG WALL THICKNESS IS GREATER THEN 0.100" TOOL # 10027TUC EXP. 31-AUG 2025, OPENED H
- [SDR SWIA2025011318](https://openairdocs.org/sdr/SWIA2025011318.md): Window Post · cracked · Nov 18, 2024 · N932EV · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT WINDSHIELD SIDE POST SUPPORT CRACKED (C-CHECK RO 1/13/2025) REMOVED AND INSTALLED 1EA NEW L/H WINDSHIELD SIDE POST SUPPORT ANGLE P/N 601R33235-3 PER CRJ200SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA202501130057](https://openairdocs.org/sdr/SWIA202501130057.md): Floor Support · corroded · Nov 17, 2024 · N932EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL27 FLOOR BEAM IS CORRODED ON INBD AND OTBD FLANGES FS582 €“ 598 (C-CHECK RO 1/13/2025) REPLACED LBL27 FLOOR BEAM FROM FS582 - FS598 REF CRJ200 SRM 53-00-43 AND REO # 601R-53-61-8256 REV:-- DATE: 24-11-21, COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA2025011316](https://openairdocs.org/sdr/SWIA2025011316.md): Post · cracked · Nov 16, 2024 · N932EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOTS SIDE POST LOWER OTBD BRACKET CRACKED (C-CHECK RO 1/13/2025) REMOVED PILOTS SIDE POST LOWER OTBD BRACKET REF. CRJ-200 SRM 51-42-06 INSTALLED NEW PILOT SIDE POST LOWER BRACKET P/N 601R34032-21S REF.CRJ-200 SRM 51-42-06 AND DRAWING 601R34032 REV.
- [SDR SWI2025F00061](https://openairdocs.org/sdr/SWI2025F00061.md): Skin · chafed · Nov 16, 2024 · N932EV · Cndair CL6002B19 · Ailerons
  > RH AILERON LOWER INBOARD LEADING EDGE SKIN SHROUD CHAFFED (C-CHECK RO 1/13/2025) BLENDED CHAFE ON RH AILERON LOWER INBD LEADING LEADING EDGE SKIN SHROUD REF CRJ 200 SRM 51-12-00-00, FOUND TO BE OUT OF LIMITS PER AND REPLACED RH AILERON LOWER INBD LEADIN
- [SDR SWI2025F00060](https://openairdocs.org/sdr/SWI2025F00060.md): Floorbeam · corroded · Nov 16, 2024 · N932EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL9 FLOOR BEAM INBD FLANGE IS CORRODED AT FS409+96 (C-CHECK RO 1/13/2025) REMOVED AND REPLACED LBL9 FLOORBEAM CAP FS409 - FS409 +112 REF DWG NO. 601R31117 REV E AND REO NO. 601R-53-31-1316 REV -- DATED 2024-11-25 AND CRJ200 SRM51-42-21 REV 39 DATED MAR
- [SDR SWIA202501130056](https://openairdocs.org/sdr/SWIA202501130056.md): Channel · bent · Nov 15, 2024 · N932EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FS574.00 FRAME CENTER CHANNEL BENT TWO PLACES (C-CHECK RO 1/13/2025) REMOVED CENTER CHANNEL ON CARGO DOOR FS574.00 FRAME REF CRJ 200 SRM 51-42-06-00 AND INSTALLED NEW CENTER CHANNEL ON CARGO DOOR FS574.00 FRAME REF CRJ 200 SRM 51-42-06-00, DR
- [SDR SWIA202501130055](https://openairdocs.org/sdr/SWIA202501130055.md): Floor Support · corroded · Nov 15, 2024 · N932EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON RH PRESSURE FLOOR SILL PANEL FS409+128 €“ 559 (C-CHECK RO 1/13/2025) BLENDED AND EVALUATED RH PRESSURE FLOOR SILL PANEL AT FS 409+128 - 559 IN ACCORDANCE WITH REO 601R-53-41-666 REV -C DATE 2012-11-06 MATERIAL IS FOUND O
- [SDR SWIA202501130054](https://openairdocs.org/sdr/SWIA202501130054.md): Floor Support · corroded · Nov 15, 2024 · N932EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL FS409+128 €“ 559 (C-CHECK RO 1/13/2025) BLENDED 5EA SPOTS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL FS409+128 - 559 REF CRJ 200 SRM 51-21-06-00 EVALUATED BLEND AREAS 1 TO 4 ON LH PRESSURE F
- [SDR SWIA202501130053](https://openairdocs.org/sdr/SWIA202501130053.md): Track · gouged · Nov 15, 2024 · N932EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT TRACK GOUGED/ROLLER INDENTIONS WHERE UPPER ROLLERS TRAVEL TO END OF TRACK (C-CHECK RO 1/13/2025) REMOVED AND INSTALLED 1EA NEW CARGO DOOR AFT TRACK PER CRJ200SRM 51-42-06 AND DWG 601R35207 REV -W. ALL LEAK AND OPS CHECKS GOOD. COMPLIED WI
- [SDR SWIA2025011315](https://openairdocs.org/sdr/SWIA2025011315.md): Floor Support · corroded · Nov 15, 2024 · N932EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BOARD SUPPORT STRAP AT FS559 APPROX LBL 27-42 HAS CORROSION IN SEVERAL SPOTS (C-CHECK RO 1/13/2025) REMOVED AND INSTALLED NEW FLOORBOARD SUPPORT STRAP AT FS559 APPROX LBL 27-42 REF DRWG 601R31025 REV N, CRJ 200 SRM 51-42-06-00, AND CRJ 200 SRM 51-
- [SDR SWIA202501130052](https://openairdocs.org/sdr/SWIA202501130052.md): Doubler · corroded · Nov 14, 2024 · N932EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON THE FORWARD AND AFT END OF THE LAVATORY SERVICE POINT EXTERIOR SKIN DOUBLER STGR23R. (C-CHECK RO 1/13/2025) EVALUATED CORROSION ON THE FORWARD AND AFT END OF THE LAVATORY SERVICE POINT EXTERIOR SKIN DOUBLER, REPAIRED BY COMPLYING WITH REO #
- [SDR SWIA202501130051](https://openairdocs.org/sdr/SWIA202501130051.md): Skin · damaged · Nov 14, 2024 · N932EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DAMAGE ON EXTERNAL SKIN FS605.00 - 621.00 STGR23R -STGR24R (MARKED) (C-CHECK RO 1/13/2025) REPAIRED DAMAGED SKIN REF FS605 - FS621 BETWEEN STR23R - STR24R REF REO NO. 601R-53-61-8255 REV -- DATED 2024-12-03. COMPLIED WITHSKYWEST TASK CARD 51-900-1003-S
- [SDR SWIA2025011314](https://openairdocs.org/sdr/SWIA2025011314.md): Skin · bent · Nov 14, 2024 · N932EV · Cndair CL6002B19 · Rudder, Plate/Skin
  > RUDDER LEADING EDGE SKIN BENT AT LOWER RH HINGE CUT-OUT (C-CHECK RO 1/13/2025) DURING DRESS-BACK OF BENT SKIN OF THE R/H LWR L/E OF THE RUDDER, THE SKIN CRACKED. REMOVED AND INSTALLED 1EA NEW SKIN (P/N CC670-22035-5) PER CRJ200SRM 51-42-06 AND DWG 601R2
- [SDR SWIA202501130000](https://openairdocs.org/sdr/SWIA202501130000.md): Flange · chafed · Nov 13, 2024 · N932EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > UPON REMOVAL OF L/H AILERON, FOUND UPPER FLANGE CHAFED. TRANS#29145960 (C-CHECK RO 1/13/2025) REMOVED L/H AILERON'S OLD UPPER SKIN SHROUD PN# CC670-13052-3 AND INSTALLED NEW L/H AILERON UPPER SKIN SHROUD PN# CC670-13052-3 IAW CRJ200 SRM 51-42-21-00, CRJ
- [SDR SWIA20250113004](https://openairdocs.org/sdr/SWIA20250113004.md): Isolation Valve · chafed · Oct 4, 2024 · N932EV · Cndair CL6002B19 · Empennage Structure
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA74078-601R-53-61-7737 932EV MXCODEID59444-PR - FOUND SMALL CHAFE DAMAGE ON WINTERIZATION BEHIND THE 10TH STAGE ISOLATION VALVE ON THE FS 621 BULKHEAD VERTICAL STIFFENER AT BL 0.00. COMPLIED WITH REO 601R-53-61-7737 REV
- [SDR SWIA202401100009](https://openairdocs.org/sdr/SWIA202401100009.md): Unknown · warning message · Jan 9, 2024 · N932EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > WARNING MSG. GEAR DISAGREE RIGHT AFTER TAKE OFF. QRH COMPLETED. (FLIGHT 5309 FILED CLOSED) PLEASE REFERENCE AML 1276504 FOR TROUBLESHOOTING AND PICTURE OF ICE IN THE GEAR BAY.THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27662193 WITH THE FOLLOWING CORRECTIV
- [SDR SWIA202265926](https://openairdocs.org/sdr/SWIA202265926.md): None · cracked · Jun 13, 2022 · N932EV · Cndair CL6002B19 · Window/Windshield System
  > RH WINDOW SHATTERED DURING CRUISE. (FLIGHT 5176 - FILED CLOSED) REMOVED AND REPLACED RH SIDE WINDOW REF CRJ200 AMM 56-12-01. OPS CHECK AND LEAK CHECK GOOD.
- [SDR SWIA202265641](https://openairdocs.org/sdr/SWIA202265641.md): None · cut · Feb 6, 2022 · N932EV · Cndair CL6002B19 · Fuselage Structure (General)
  > DURING MOVEMENT OF THE AIRCRAFT, THE AIRCRAFT MADE CONTACT WITH A GROUND AIR UNIT ON THE RH SIDE BELOW THE CVR CUT DECAL. ( FILED- CLOSED) DAMAGE REPAIRED AS STATED IN MHIRJ SOW PER REO 601R-53-71-213 REV - DATED 5-13-22. REFERENCE CP 24703005 FOR EDDY C
- [SDR SWIA202264093](https://openairdocs.org/sdr/SWIA202264093.md): None · dented · Jan 31, 2022 · N932EV · Cndair CL6002B19 · Aileron Tabs
  > TRANSFER FROM EAML 835555: CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 835345 DENT FOUND ON RIGHT OUTBOARD FLAP TRAILING EDGE 18 INCHES FROM FLAP INBOARD EDGE. (FILED CLOSED) REMOVED AND REPLACED RH OUTBOARD FLAP IN REF TO TASK CARD 27-900-10
- [SDR SWIA202161645](https://openairdocs.org/sdr/SWIA202161645.md): None · corroded · Sep 20, 2021 · N932EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > REO 601R-53-41-2967 REV -- DATED 2021-09-18 REQ'S COMPLETION FOR CORROSION AT RBL 9 FLOOR BEAM BETWEEN FS 409+128- FS 559 (C-CHECK RO 10/07/2021) VERIFIED ALL STEPS OF REO 601R-53-41-2967 REV--, DATED 2021-09-18 HAVE BEEN COMPLIED WITH. REFERENCE CAMP # 2
- [SDR SWIA202161644](https://openairdocs.org/sdr/SWIA202161644.md): None · corroded · Sep 14, 2021 · N932EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RBL 9.00, FLOOR BEAM FLANGE ON INBOARD SIDE OF BEAM IS CORRODED AT APPROX. (28 EA) LOCATIONS AROUND NUTPLATE HOLES AND WHERE FLANGE MEETS SEAT TRACK BETWEEN F.S. 409.00+128 AND F.S. 559.00. (C-CHECK RO 10/07/2021) REPAIRED RBL 9.00, FLOOR BEAM FLANGE ON I
- [SDR SWIA202161643](https://openairdocs.org/sdr/SWIA202161643.md): None · corroded · Sep 14, 2021 · N932EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LBL 9.00, FLOOR BEAM FLANGE ON INBOARD SIDE OF BEAM IS CORRODED AT APPROX. (30 EA) LOCATIONS AROUND NUTPLATE HOLES AND WHERE FLANGE MEETS SEAT TRACK BETWEEN F.S. 409.00+128 AND F.S. 559.00. (C-CHECK RO 10/07/2021) REPAIRED LBL 9.00 FLOOR BEAM FLANGE ON IN
- [SDR SWIA202161642](https://openairdocs.org/sdr/SWIA202161642.md): None · corroded · Sep 14, 2021 · N932EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION AROUND SCREW HOLE ON FLOOR BEAM I/B FLANGE LBL 9 BETWEEN FS. 409.00 AND 409.00+16. (CENTER FLOOR BOARD SUPPORT STRUCTURE) (C-CHECK RO 10/07/2021) REPAIRED CORROSION AROUND SCREW HOLE ON FLOOR BEAM I/B FLANGE LBL 9 BETWEEN FS. 409.00 AND 409.00+
- [SDR SWIA202161693](https://openairdocs.org/sdr/SWIA202161693.md): None · bent · Sep 3, 2021 · N932EV · Cndair CL6002B19 · Aileron Tabs
  > R/H OUTBOARD FLAP MIDDLE HINGE ARM LOWER OUTBOARD BOLT RETAINER IS BENT (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RH OB FLAP MIDDLE HINGE ARM LOWER OB BOLT RETAINER IAW CRJ-200 SRM 51-42-20
- [SDR SWIA202161641](https://openairdocs.org/sdr/SWIA202161641.md): None · damaged · Aug 30, 2021 · N932EV · Cndair CL6002B19 · Aircraft Fuel System
  > RH WING FUEL DRAIN HOLE AT WS148.019 FWD FASTENER HOLE HAS VISUAL DAMAGE IN THE UPPER SIDE EGDE OF THE BORE INSIDE THE FUEL TANK. (C-CHECK RO 10/07/2021) REPAIRED RH WING FUEL DRAIN HOLE AT WS 148.019 FWD FASTENER HOLE IAW REO 601R-57-21-3513 REV. -- DA
- [SDR SWIA202161640](https://openairdocs.org/sdr/SWIA202161640.md): None · damaged · Aug 23, 2021 · N932EV · Cndair CL6002B19 · Main Landing Gear
  > FOUND RH MLG TRUNNION FASTENER HOLE # 17 HAS INDICATION NOTED.100 LONG 70%FSH O/B TO I/B DIRECTION TOWARDS MLG FAILED NDT INSPECTION (C-CHECK RO 10/07/2021) REPAIRED THE RH MLG TRUNNION FASTENER HOLE # 17 IAW MHIRJ REO 601R-57-21-3511 REV -- DATED 2021-0
- [SDR SWIA202161639](https://openairdocs.org/sdr/SWIA202161639.md): None · damaged · Aug 23, 2021 · N932EV · Cndair CL6002B19 · Main Landing Gear
  > FOUND RH MLG TRUNNION FASTENER HOLE # 20 HAS INDICATION NOTED.100 LONG 70%FSH O/B TO I/B DIRECTION TOWARDS MLG FAILED NDT INSPECTION (C-CHECK RO 10/07/2021) REPAIRED THE RH MLG TRUNNION FASTENER HOLE # 20 IAW MHIRJ REO 601R-57-21-3511 REV -- DATED 2021-
- [SDR SWIA202161638](https://openairdocs.org/sdr/SWIA202161638.md): Stiffener · cracked · Aug 20, 2021 · N932EV · Cndair CL6002B19 · Fuselage Main, Keel
  > CRACK FOUND AT LOWER AFT CORNER OF RBL 18 POST AT F.S. 559+112 (C-CHECK RO 10/07/2021) UPON FURTHER INVESTIGATION FOUND POST TO BE LOCATED AT RBL 18 AT FS 409+128. REMOVED AND REPLACED POST IAW REO 601R-53-41-889 REV B DATED 2017/03/06. COMPLETED TASK CAR
- [SDR SWIA202161683](https://openairdocs.org/sdr/SWIA202161683.md): None · damaged · Aug 19, 2021 · N932EV · Cndair CL6002B19 · Elevator Structure
  > L/H ELEVATOR SYSTEM 2 & 3 PCU'S FAIL BEARING BACKLASH. (C-CHECK RO 10/07/2021) REPLACED L/H ELEVATOR BEARINGS AND BUSHINGS IAW CRJ 200 AMM 20-26-00-910-804 AND 20-26-00-910-808. BACKLASH GOOD AFTER RE-ACCOMPLISHING. REF CONTINUATION CARD FOR DETAILS OF
- [SDR SWIA202161637](https://openairdocs.org/sdr/SWIA202161637.md): None · corroded · Aug 19, 2021 · N932EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 349.00 HAS CORROSION AT STGR 27 ON AFT SIDE (C-CHECK RO 10/07/2021) REMOVED AND REPLACED FS 349 FRAME SEGMENT BETWEEN STR 23L AND 23R IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WE
- [SDR SWIA202161636](https://openairdocs.org/sdr/SWIA202161636.md): Stiffener · damaged · Aug 11, 2021 · N932EV · Cndair CL6002B19 · Fuselage Main, Keel
  > FUSELAGE FS409+128 LBL18 INBD VERTICAL POST HAS AN INDICATION.2" LONG BY 50% FSH IN THE AFT RADIUS @WL69. FAILED NDT INSPECTION. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED VERTICAL POSTS AT LBL 18 AT FS 409+128 IAW REO 601R-53-41-889 REV B DATED 2017/
- [SDR SWIA202161682](https://openairdocs.org/sdr/SWIA202161682.md): None · corroded · Aug 10, 2021 · N932EV · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > RH ELEVATOR, HINGES #1, #BL24.5, #2 AND #3, HAVE CORRODED HARDWARE (INCLUDING BUSHINGS) ON THE STOP BRACKET AND ANTI-ROTATION DEVICE. (C-CHECK RO 10/07/2021) INSTALLED NEW HARDWARE DURING ELEVATOR INSTALL IAW CRJ 200 AMM 27-34-01-400-801. REFERENCE CAMP#
- [SDR SWIA202161663](https://openairdocs.org/sdr/SWIA202161663.md): None · chafed · Aug 10, 2021 · N932EV · Cndair CL6002B19 · Fuselage Structure (General)
  > CARGO COMPARTMENT ANGLE GOUGED AND CHAFED AT APPROX FS559+96 AND STGR15. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED CARGO COMPARTMENT ANGLE P/N 601R31006-35 AT APPROX FS559+96 IAW CRJ 200 SRM 51-42-06 REF CP # 2339006-1 FOR FABRICATION OF THE ANGLE REF
- [SDR SWIA202161662](https://openairdocs.org/sdr/SWIA202161662.md): Angle · cracked · Aug 10, 2021 · N932EV · Cndair CL6002B19 · Doors
  > CARGO DOOR SURROUND STRUCTURE, ANGLE ON LOWER SIDE OF BEAM MEMBER CRACKED AT FS621 (C-CHECK RO 10/07/2021) REMOVED AND REPLACED ANGLE AT CARGO DOOR SURROND STRUCTURE ON LOWER SIDE OF BEAM AT FS 621 WITH NEW SERVICEABLE PN 601R35050-109 IAW CRJ 200 SRM 51-
- [SDR SWIA202161661](https://openairdocs.org/sdr/SWIA202161661.md): Seat Track · corroded · Aug 9, 2021 · N932EV · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH FLOOR SEAT TRACK CORRODED AT LBL9.00 BETWEEN FS409 TO FS409+128 (C-CHECK RO 10/07/2021) UPON FURTHER INVESTIGATION FOUND L/H FLOOR SEAT TRACK AT LBL 9.00 BETWEEN F.S. 409.00 TO F.S. 409.00+128 TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-21-49. REMOVED AND I
- [SDR SWIA202161660](https://openairdocs.org/sdr/SWIA202161660.md): Seat Track · corroded · Aug 9, 2021 · N932EV · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RH FLOOR SEAT TRACK CORRODED AT RBL9.00 BETWEEN FS409 TO FS409+128 (C-CHECK RO 10/07/2021) REMOVED RH FLOOR SEAT TRACK CORRODED AT RBL9.00 BETWEEN FS409 TO FS409+128 AND INSTALLED NEW SERVICABLE IN IT'S PLACE IAW CRJ200 AMM 53-01-11-400-802. REFERENCE CON

Next page: https://openairdocs.org/aircraft/N932EV/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 = 'N932EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N932EV/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.