# Service difficulty reports: N933EV A list on [N933EV](https://openairdocs.org/aircraft/N933EV.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 · 186 reports - [SDR SWIA2025102000908](https://openairdocs.org/sdr/SWIA2025102000908.md): Floor Support · corroded · Sep 8, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CORROSION FOUND ON RBL 27 FLOOR BEAM CAP BETWEEN FS 559 AND FS 559+10 (C-CHECK RO 10/19/2025)REMOVED CORRODED SECTION AND REPAIRED IAW REO 601R-53-41-3351 REV -- DATED 2025-09-24. COMPLETED TASK CARD 51-900-1003-SKY AND ATTCHED COMPLETED FOR 337. WEIGH CHANG - [SDR SWI2025F01447](https://openairdocs.org/sdr/SWI2025F01447.md): Floor Support · corroded · Sep 7, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR BEAM CAP RBL 27 FROM FS 559 TO FS 559+10 IS CORRODED (C-CHECK RO 10/19/2025)REPLACED RBL 27 FS 559+10 TO FS 569 FLOOR BEAM CAP IAW MHIRJ REO 601R-53-51-719 REV -- DATED 2025-08-25 & IAW SKYCARD 51-900-1003-SKY ATTACHED COMPLETED 337 AND NO WEIGHT CHAN - [SDR SWIA2025102000907](https://openairdocs.org/sdr/SWIA2025102000907.md): Floor Support · corroded · Sep 7, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR SUPPORT CAP RBL 27 BETWEEN FS 569 AND FS 610 IS CORRODED. REPLACED RBL 27 F.S 569 TOF.S 610 FLOOR BEAM CAP IAW MHIRJ REO 601R-53-61-8371 REV -- DATED 2025-08-25 REF CAMP #30628236 FOR WORK PERFORMED AND IAW SKY CARD 51-900-1003-SKY COMPLETED AND ATTACHE - [SDR SWIA20250905](https://openairdocs.org/sdr/SWIA20250905.md): Floor Support · corroded · Sep 5, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR SUPPORT CAP CORRODED FROM FS574 TO FS621. REPLACED FLOOR SUPPORT CAP FROM FS574 TO FS 621 IAW BOMBARDIER REO 601R-53-61-3778 REV-B DATED 2016-12-19 COMPLETED TASK CARD 51-900-1003-SKY. - [SDR SWIA202510200824](https://openairdocs.org/sdr/SWIA202510200824.md): Access Panel · corroded · Aug 24, 2025 · N933EV · Cndair CL6002B19 · Wing, Plate/Skin > CORROSION AROUND WING PLANK ACCESS 510AB. REMOVED CORROSION FROM 510AB LANDING AND FOUND WITHIN LIMITS OF REO 601R-57-21-030. COMPLETED TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE NOTED - [SDR SWI2025F01446](https://openairdocs.org/sdr/SWI2025F01446.md): Skin · corroded · Aug 20, 2025 · N933EV · Cndair CL6002B19 · Wing, Plate/Skin > CORROSION AROUND WING PLANK OF ACCESS 540BB (C-CHECK RO 10/19/2025)REMOVED CORROSION FROM 540BB LANDING IAW REO 601R-57-21-030 REV. L, DATED 2014-02-05 AND REO 601R-57-21-3969 REV -- DATED 2025-8-26. ATTACHED COMPLETED FORM 337 AND TASK CARD 51-900-1003-SKY - [SDR SWIA2025102000820](https://openairdocs.org/sdr/SWIA2025102000820.md): Access Panel · corroded · Aug 20, 2025 · N933EV · Cndair CL6002B19 · Wing, Plate/Skin > CORROSION FOUND ON PANEL 640BB FUEL TANK ACCESS PANEL LANDING. (C-CHECK RO 10/19/2025)REMOVED CORROSION FROM 640BB LANDING IAW REO 601R-57-21-030 REV. L, DATED 2014-02-05 AND REO 601R-57-21-3968 REV -- DATED 2025-8-25. ATTACHED COMPLETED FORM 337 AND TASK CA - [SDR SWIA20251020813](https://openairdocs.org/sdr/SWIA20251020813.md): Floor Support · corroded · Aug 13, 2025 · N933EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure > WHILE PERFORMING REINSPECT OF R/H PRESSURE FLOOR SILL, FOUND CORROSION AT PREVIOUS BLEND REPAIR AT APPROX. F.S. 530.50, R.B.L. 42.00 AROUND NUTPLATE LOCATION. (C-CHECK RO 10/19/2025)REMOVED CORROSION FROM RH FLOOR SILL AT FS 530 AND FOUND WITHIN LIMITS OF 601 - [SDR SWI2025F01449](https://openairdocs.org/sdr/SWI2025F01449.md): Floor Support · corroded · Aug 12, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > UPON REPEAT INSPECTION OF THE L/H FLOOR SILL FOUND ADDITIONAL CORROSION AT, FS 413, FS 480, AND FS 537 ON L/H FLOOR SILL (C-CHECK RO 10/19/2025)REPAIRED CORRSION ON LH FLOOR SILL AT FS 413, FS 480, AND FS 537 IAW REO 601R-53-41-666 REV C DATED 2012-11-06. CO - [SDR SWI2025F01448](https://openairdocs.org/sdr/SWI2025F01448.md): Frame · corroded · Aug 12, 2025 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > UPON REPEAT INSPECTION FOUND CORROSION ON PREVIOUS REPAIRED LOCATIONS, FS 439, FS 500. (C-CHECK RO 10/19/2025)REMOVED CORROSION ON LHS PREVIOUS REPAIRED LOCATIONS AT FS 439 AND FS 500 IAW BOMBARDIER REO # 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK - [SDR SWIA2025102000812](https://openairdocs.org/sdr/SWIA2025102000812.md): Floor Support · corroded · Aug 12, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > UPON REPEAT INSPECTION OF L/H FLOOR SILL FOUND CORROSION ON PREVIOUS REPAIRED LOCATIONS, FS 428, FS 518, AND 541 AROUND SCREW HOLES. (C-CHECK RO 10/19/2025)REMOVED CORROSION FROM LH FLOORSILL AT FS 428, 518, AND 541 AND FOUND IN LIMITS IAW REO 601R-53-41-666 - [SDR SWI2025F01445](https://openairdocs.org/sdr/SWI2025F01445.md): Floor Support · corroded · Aug 11, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > WHILE PERFORMING REINSPECT OF R/H PRESSURE FLOOR SILL. FOUND CORROSION AT PREVIOUSLY BLENDED LOCATION F.S. 475.00 SILL PANEL. AREA WAS PREVIOUSLY REPAIRED I.A.W. REO 601R-53-41-666 REV.C, DATED 2012-11-06. REFERENCE EXPRESSJET W/O: 390949, MACON AIR CENTER C/O - [SDR SWIA2025102000811](https://openairdocs.org/sdr/SWIA2025102000811.md): Floor Support · corroded · Aug 11, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > WHILE PERFORMING REINSPECT OF R/H PRESSURE FLOOR SILL, F.S. 409.00+128 TO F.S. 559.00, FOUND (2EA) PREVIOUS BLEND LOCATIONS THAT ARE CORRODED AROUND NUTPLATES. ONE DAMAGE LOCATION AT F.S. 535.00 APPROX. AND ONE DAMAGE LOCATION AT F.S. 555.00 APPROX. DAMAGE AT - [SDR SWI2025F01444](https://openairdocs.org/sdr/SWI2025F01444.md): Yoke · nicked · Aug 8, 2025 · N933EV · Cndair CL6002B19 · Engine Mount Section > RIGHT ENGINE FORWARD YOKE MOUNT HAS 2EA. NICKS ON THE FORWARD LOWER END. (C-CHECK RO 10/19/2025)REPAIRED RH ENG FWD YOKE MOUNT IAW REO 601R-71-21-005 REV F FATED 2019-02-20. COMPLETED TASK CARD 51-900-1003-SKY AND ATTCHED COMPLETED FORM 337. NO WEIGHT CHANGE - [SDR SWIA2025102000808](https://openairdocs.org/sdr/SWIA2025102000808.md): Floor Support · corroded · Aug 8, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOORBEAM CAP CORRODED FROM FS559+10 TO FS621 AT RBL 9. (C-CHECK RO 10/19/2025)REMOVED AND INSTALLED A NEWLY FABRICATED FLOORBEAM CAP FROM FS 559+10 TO FS 621 AT RBL 9 THAT WAS FABRICATED ON CAMP 30643261 IAW CRJ 200 SRM 51-42-21, 51-42-34, AND 51-25-16 COMP - [SDR SWI2025F01440](https://openairdocs.org/sdr/SWI2025F01440.md): Floor Support · corroded · Aug 7, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR BEAM CAP CORRODED FROM FS559+10 TO FS621 LBL27. (C-CHECK RO 10/19/2025)REMOVED AND INSTALLED NEW FABRICATED FLOOR BEAM CAP P/N 601R35031-267 IAW REO 601R-53-51-720 REV -- DATED 2025-08-25 AND TASK CARD 51-900-1003-SKY ATTACHED COMPLETED M-337 NO WEIGHT - [SDR SWI2025F01439](https://openairdocs.org/sdr/SWI2025F01439.md): Floor Support · corroded · Aug 7, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOORBEAM CAP CORRODED FS559 TO FS621 RBL 27. (C-CHECK RO 10/19/2025)REMOVED AND REPLACED TWO FLOOR BEAMS CAPS ONE FROM FS 559+10 TO FS569 IAW MHIRJ REO 601R-53-51-719 REV -- DATED 2025-08-25 OTHER BEAM CAP FROM FS 569 TO FS 610 IAW MHIRJ REO 601R-53-61-837 - [SDR SWI2025F01438](https://openairdocs.org/sdr/SWI2025F01438.md): Floor Support · corroded · Aug 7, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > L/H FLOOR SUPPORT CAP AT LBL 9 FROM FS 394 TO FS 409+128 IS CORRODED IN SEVERAL LOCATIONS.)REMOVED AND REPLACED LH FLOOR SUPPORT CAP AT LBL 9 FROM FS 394 TO FS 409+128 IAW CRJ 200 SRM 51-42-21, 51-42-22, AND 51-21-16, 51-42-34, 51-40-11, 51-24-36 AND 51-42-1 - [SDR SWIA2025102000807](https://openairdocs.org/sdr/SWIA2025102000807.md): Floor Support · corroded · Aug 7, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > 2 SCREW HOLES FROM FS 409+112 TO 409+128 HAVE CORROSION. (C-CHECK RO 10/19/2025)REPLACED LH FLOORSILL AT FS 409+112 - FS 409+128 IAW CRJ 200 SRM 51-42-06, 51-42-21 AND REO 601R-31-1347 REV -- DATED 2025-09-01. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED - [SDR SWI2025F01442](https://openairdocs.org/sdr/SWI2025F01442.md): Doubler · corroded · Aug 6, 2025 · N933EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin > AFT POTABLE WATER DRAIN DOUBLER CORRODED BETWEEN FS605 AND FS621 STGR 26L TO STGR 26R. (C-CHECK RO 10/19/2025)REMOVED AND REPLACED AFT POTABLE WATER DRAIN DOUBLER P/N 601R43216-9 IAW CRJ 200 SRM 51-42-06 & 51-45-00 & SKY 51-900-1003-SKY MAJOR REPAIR M-337 CO - [SDR SWI2025F01441](https://openairdocs.org/sdr/SWI2025F01441.md): Floor Support · corroded · Aug 6, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LBL9 FLOOR BEAM IS CORRODED AT MULTIPLE LOCATIONS BETWEEN F.S.409+128 TO F.S.559. (C-CHECK RO 10/19/2025)REPLACED LBL 9 FLOORBEAM CAP AT FS 409+128 - FS 559 IAW REO 601R-53-41-3346 REV A DATED 2025-08-21. ATTACHED COMPLETED FORM 337 AND TASK CARD 51-900-1003 - [SDR SWIA2025102000806](https://openairdocs.org/sdr/SWIA2025102000806.md): Floor Support · corroded · Aug 6, 2025 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RBL9 FLOOR BEAM IS CORRODED AT MULTIPLE LOCATIONS BETWEEN F.S.409+128 TO F.S.559. (C-CHECK RO 10/19/2025)REPLACED RBL 9 FLOOR BEAM CAP AT FS 409+128 - 559 IAW REO 601R-53-41-3348 REV -- DATED 2025-08-25. ATTACHED COMPLETED FORM 337 AND SKYWEST TASK CARD 51- - [SDR SWI2025F01443](https://openairdocs.org/sdr/SWI2025F01443.md): Door Frame · out of limits · Aug 5, 2025 · N933EV · Cndair CL6002B19 · Fuselage Main, Structure > FS409 RBL18 VERTICAL POST HAS INDICATIONS IN THE AFT RADIUS OF @WL69 AS FOLLOWS: INBD SIDE: 65% FSH BY.75" LONG, & OUTBD SIDE: 55% BY.3" LONG. FAILED NDT INSPECTION. (C-CHECK RO 10/19/2025)REMOVED AND REPLACED FS 409 RBL 18 POSTS INSTALLED NEW ONES P/N 601 - [SDR SWIA2025102000805](https://openairdocs.org/sdr/SWIA2025102000805.md): Door Frame · out of limits · Aug 5, 2025 · N933EV · Cndair CL6002B19 · Fuselage Main, Structure > FS409 BL0 VERTICAL POST HAS INDICATIONS IN THE AFT RADIUS OF @WL69 AS FOLLOWS: LH SIDE: 60% FSH BY.4" LONG, & RH SIDE: 70% BY.4" LONG. FAILED NDT INSPECTION. (C-CHECK RO 10/19/2025)REPLACED 409+128 POSTS AT BL0 IAW REO 601R-53-41-889 REV D DATED 2018, COMP - [SDR SWIA2025102000802](https://openairdocs.org/sdr/SWIA2025102000802.md): Landing · corroded · Aug 2, 2025 · N933EV · Cndair CL6002B19 · Wing, Plate/Skin > INDICATIONS NOTED AT LH WING ACCESS HOLE LANDING COMMON TO PANEL 550DB APPROX. 70% FULL SCREEN HEIGHT, FAILING NDT. INDICATION AREA MARKED ON A/C. (C-CHECK RO 10/19/2025)REMOVED CORROSION FROM 550DB LANDING IAW REO 601R-57-21-030 REV. L, DATED 2014-02-05 AN - [SDR SWIA2025102000801](https://openairdocs.org/sdr/SWIA2025102000801.md): Skin · corroded · Aug 1, 2025 · N933EV · Cndair CL6002B19 · Wing, Plate/Skin > CORROSION AROUND WING PLANK OF ACCESS 510AB. CORRECT LOCATION OF CORROSION IS AROUND ACCESS PANEL 610AB. REMOVED CORROSION AROUND WING PLANK ACCESS PANEL 610AB IAW BOMBARDIER REO 601R-57-21-030. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM - [SDR SWIA2025102000730](https://openairdocs.org/sdr/SWIA2025102000730.md): Skin · chafed · Jul 30, 2025 · N933EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin > L/H WING, LOWER WING PLANK HAS CHAFE DAMAGE FROM CONTACT WITH FLAP FAIRING 586AB. (C-CHECK RO 10/19/2025)REPAIRED LH WING LOWER PLANK CHAFE DAMAGE FROM CONTACT WIT FLAP FARIING 586AB IAW REO 601R-57-21-3961 REV--, DATED 2025-08-06 COMPLETED TASK CARD 51-900- - [SDR SWIA2025102000728](https://openairdocs.org/sdr/SWIA2025102000728.md): Skin · corroded · Jul 28, 2025 · N933EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin > MID. FUSELAGE SKIN UNDER FORWARD WING - TO - FUSELAGE FAIRING SEALANT BED HAS NUMEROUS AREAS OF CORROSION AROUND NUTPLATE HOLES. MARKED WITH TAPE. (C-CHECK RO 10/19/2025)REPAIRED FUSELAGE SKIN UNDER FORWARD WING TO FUSELAGE FAIRING SEALANT BED AROUND NUTPLATE - [SDR SWIA202305190015](https://openairdocs.org/sdr/SWIA202305190015.md): Unknown · smoke · May 18, 2023 · N933EV · Cndair CL6002B19 · Communications System > SELECTOR PANEL BELOW FLIGHT ATTENDANT INTERPHONE PUSHED IN BEYOND THE HOUSING, FLIGHT ATTENDANT NOTICED MOMENTARY MINOR SMOKE WHICH SHORTLY THEREAFTER DISSIPATED. (FLT 5787, FILED CLOSED)REMOVED AND REPLACED ATTENDANT INTERPHONE HANDSET IN REF WITH CRJ200 AMM - [SDR SWIA202305110001](https://openairdocs.org/sdr/SWIA202305110001.md): Unknown · damaged · May 10, 2023 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > COMPLY WITH REPAIR AUTHORIZATION: RA81748-601R-53-11-3816 N933EV,MXCODEID65355-PR - DAMAGED SCREW HOLE TO ACCESS DOOR SURROUND STRUCTURE FOR ACCESS PANEL 131AL INSTALLATION. COMPLIED WITH TEMPORARY DISPOSITION IAW REO 601R-53-11-3816 DATED: 2022-12-18 REV -- - [SDR SWIA20230214](https://openairdocs.org/sdr/SWIA20230214.md): None · warning message · Feb 14, 2023 · N933EV · Cndair CL6002B19 · Steering Unit > ON THE MISSED APPROACH, AFTER SELECTING GEAR UP, GOT A GEAR DISAGREE WARNING & NLG INDICATOR RED. RAN QRH PROCEDURE. GEAR SELECTED DOWN IAW CHECKLIST, GOT 3 GREEN INDICATORS. NO LIMITATIONS EXCEEDED. AIRCRAFT IS DOWNGRADED FROM CAT II STATUS. FOUND ASSOC - [SDR SWIA202265870](https://openairdocs.org/sdr/SWIA202265870.md): None · cracked · May 6, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > BATT RIB CHANNEL CRACKED AT LHS WS 53.60. (C-CHECK RO 6/1/2022) REPAIRED BATT RIB CHANNEL CRACK AT LHS WS 53.60.REF REO 601R-57-51-046 REV B DATED 2002-02-28.C/W 51-900-1003-SKY - [SDR SWIA202265869](https://openairdocs.org/sdr/SWIA202265869.md): None · cracked · May 6, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > BATT RIB FWD ANGLE CRACKED AT LHS WS48.30. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED DAMAGED ANGLE P/N 600-10204-27 REF CRJ200 SRM 51-42-21, 51-42-06, BOMBARDIER ENG DWG 600-10204 REV M COMPLIED WITH 51-900-1003 SKY - [SDR SWIA202265868](https://openairdocs.org/sdr/SWIA202265868.md): None · shifted · May 2, 2022 · N933EV · Cndair CL6002B19 · Landing Gear System > LH MLG TRUNNION AFT FORCE MATE BUSHING IS MIGRATED.010 THE PN FOR LH MLG TRUNNION IS 601R10068-1 (C-CHECK RO 6/1/2022) REPLACE LH MLG TRUNNION AFT BUSHING PER REO 601R-57-21-3588 REV --, DATED 2022-05-10. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WI - [SDR SWIA202265867](https://openairdocs.org/sdr/SWIA202265867.md): None · cracked · Apr 28, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > FRAME AT FS333 STRINGER 1L CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED FRAME SECTOR AT FS333 STRINGER 1L REF DWG 601R31016 REV C, DWG 601R31522 REV AC, DWG 601R32004 REV N. CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-42-21. COMPLIED WITH SKYWEST TASK - [SDR SWIA202265866](https://openairdocs.org/sdr/SWIA202265866.md): None · corroded · Apr 28, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > CORROSION FOUND AT FS 349.00 CROSSBEAM TOP CAP BETWEEN LBL27-LBL36. (C-CHECK RO 6/1/2022) REPAIRED CORROSION FOUND AT FS 349.00 CROSSBEAM TOP CAP BETWEEN LBL27-LBL36. REF DWG 601R38673 REV D, CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-06, AND CRJ200 SRM 51-4 - [SDR SWIA202265865](https://openairdocs.org/sdr/SWIA202265865.md): None · cracked · Apr 13, 2022 · N933EV · Cndair CL6002B19 · Fuselage Structure (General) > RH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL103.90 IS CRACKED. (MARKED) (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW SUPPORT ANGLE AT R/H WINDSHIELD POST AT FS236.75 AND WL103.90 REF CRJ200 SRM 51-42-06 AND DWG 601R34032 REV P. COMPLIED WI - [SDR SWIA202265864](https://openairdocs.org/sdr/SWIA202265864.md): None · cracked · Apr 13, 2022 · N933EV · Cndair CL6002B19 · Fuselage Structure (General) > LH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL103.90 IS CRACKED. (MARKED) (C-CHECK RO 6/1/2022) REPLACED LH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL 103.90 PER CRJ200 SRM 51-42-06 & DRAWING 601R34032 REV P. CHECKS GOOD. SEE CONTINUA - [SDR SWIA202265863](https://openairdocs.org/sdr/SWIA202265863.md): None · out of tolerance · Apr 9, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > WHILE COMPLYING WITH SB 601R-57-046 REV C PART E (LH) AND PART F (RH) O/S FASTENERS WERE FOUND AT HOLE #14 BOTH LH AND RH SIDE. (FASTENER TYPE IS HST411AG-10), (HOLE DIA. IS.3400") WITH NO DEFECTS NOTED. (C-CHECK RO 6/1/2022) REPAIRED HOLE #14 BOTH LHS - [SDR SWIA202265862](https://openairdocs.org/sdr/SWIA202265862.md): None · cracked · Apr 8, 2022 · N933EV · Cndair CL6002B19 · Doors > PAX DOOR HAS CRACK AT UPPER INTERCOSTAL INSIDE ACCESS PANEL LOCATION 832BR. (C-CHECK RO 6/1/2022) INSTALLED REPLACEMENT INTERCOSTAL P/N 601R31902-318 AT PAX DOOR INNER STRUCTURE BETWEEN FS.338 & FS.349 REF. CRJ200 SRM 51-42-06 & BOMBARD. DWG. 601R31702 - [SDR SWIA202265861](https://openairdocs.org/sdr/SWIA202265861.md): None · corroded · Apr 8, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > INTERNAL FUSELAGE FS 310.0 JUST AFT OF RBL 7.0 GALLEY MOUNT HAS CORROSION. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW MOUNT PLATE PN# 601R38669-121 REF DWG 601R38669 REV-N AND CRJ200 SRM 51-42-06. RESTORED FINISH. COMPLIED WITH TASK CARD 51-900-100 - [SDR SWIA202265860](https://openairdocs.org/sdr/SWIA202265860.md): None · corroded · Apr 8, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > INTERNAL FUSELAGE FS 310.0 JUST FWD AND INB OF LBL 27 WARDROBE MOUNT HAS CORROSION. (C-CHECK RO 6/1/2022) REMOVED INSTALLED NEW WARDROBE MOUNT PLATE P/N 601R38670-31 WITH NEW HARDWARE. FS310.00 FWD AND IN/BD OF LBL27 REF DWG 601R38670 REV T AND CRJ200 S - [SDR SWIA202265859](https://openairdocs.org/sdr/SWIA202265859.md): None · cracked · Apr 8, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > FS 280 RBL 9.0 OUT BOARD CLIP IS CRACKED (C-CHECK RO 6/1/2022) REMOVED AND REPLACED 1EA. CLIP AT FS 280.00 RBL 9 IAW CRJ 200 SRM 51-42-21. REVISION 38, DATED JUL10/2019. CRJ200 SRM 51-40-11 REVISION 38, DATED JUL10/2019, REO 601R-53-11-926 REV-B DATED - [SDR SWIA202265858](https://openairdocs.org/sdr/SWIA202265858.md): None · cracked · Apr 8, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > FS 280 RBL 9.0 INBOARD CLIP IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED 1EA. CLIP AT FS 280.00 RBL 9 IAW CRJ 200 SRM 51-42-21. REVISION 38, DATED JUL10/2019, REO 601R-53-11-926 REV-B DATED 2006-05-10. COMPLIED WITH SKYWEST TASK CARD 51-900- - [SDR SWIA202265857](https://openairdocs.org/sdr/SWIA202265857.md): None · cracked · Apr 7, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > FS 280 LBL 9.0 OUT BOARD CLIP IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED NEW FS280 LBL9 OTBD CLIP REF PREVIOUSLY INCORPERATED REO 601R-53-11-171, REV -D, DATED 13-FEB-07. COMPLIED WITH TASK CARD 51-900-1003-SK - [SDR SWIA202265856](https://openairdocs.org/sdr/SWIA202265856.md): None · cracked · Apr 7, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > FS 280.0 LBL9.0 INBOARD CLIP IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED NEW FS280 LBL9 INBD CLIP REF PREVIOUSLY INCORPERATED REO 601R-53-11-171, REV -D, DATED 13-FEB-07. COMPLIED WITH TASK CARD 51-900-1003-SKY - [SDR SWIA202265855](https://openairdocs.org/sdr/SWIA202265855.md): None · cracked · Apr 7, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Frame > L/H SIDE LBL 27.0 AT FS 484.0 INBOARD CLIP IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED THE CLIP AT LBL 27, FS484.00 AND REPLACED WITH NEW IAW CRJ200 51-42-06, AND CRJ200 SRM 51-42-21 AND DWG 601R31171 REV-B. COMPLIED WITH TASK CARD 51-900-1003-SKY. - [SDR SWIA202265854](https://openairdocs.org/sdr/SWIA202265854.md): None · cracked · Apr 7, 2022 · N933EV · Cndair CL6002B19 · Fuselage Structure (General) > AFT EQUIPTMENT BAY R/H SIDE FS 625 CLIP AT STR 14R IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW FS625 STGR14R CLIP REF DWG 601-35012 REV-B AND CRJ 200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS. - [SDR SWIA202265852](https://openairdocs.org/sdr/SWIA202265852.md): None · cracked · Apr 7, 2022 · N933EV · Cndair CL6002B19 · Fuselage Main, Keel > L/H SIDE FS 625 CLIP IS CRACKED AT STR 15L (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW FS625 STGR15L CLIP REF DWG 601-35012 REV-B, CRJ200 SRM 51-42-21 AND CRJ 200 SRM 51-42-06. RESTORED FINISH. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE C - [SDR SWIA202265851](https://openairdocs.org/sdr/SWIA202265851.md): None · cracked · Apr 7, 2022 · N933EV · Cndair CL6002B19 · Fuselage Structure (General) > AFT EQUIPTMENT BAY L/H SIDE FS 625 CLIP AT STR 14 IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW FS625 STGR14L CLIP REF DWG 601-35012 REV-B AND CRJ 200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS. Next page: https://openairdocs.org/aircraft/N933EV/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 = 'N933EV' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N933EV/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.