# Service difficulty reports: N753EV

A list on [N753EV](https://openairdocs.org/aircraft/N753EV.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 · 282 reports

- [SDR SWIA202503270019](https://openairdocs.org/sdr/SWIA202503270019.md): Skin · dented · Mar 19, 2025 · N753EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND VERTICAL DENT ON AFT PART OF R/H FUSELAGE BELOW R/H ENGINE ASSY. DAMAGE LOCATION FOUND TO BE APPROXIMATELY 0.5" INCHES AFT OF THE AFT RIVET LINE OF FRAME 1051.3. DENT SPANS VERTICALLY APPROXIMATELY 6 INCHES AND INTERSECTS STGR 14R AT THE DENT MID-POINT.
- [SDR SWIA20241024](https://openairdocs.org/sdr/SWIA20241024.md): Roller · failed insp · Oct 24, 2024 · N753EV · Cndair CL6002C10 · Leading Edge Devices
  > LH ROLLER ON SLATS 3-2 FWD 1B FAILED INSPECTION (C-CHECK RO 12/24/2024) (FILED CLOSED)OK, TO INSTALL. PA. 911290REMOVED AND REPLACED LH ROLLER ON SLAT 3-2 FWD IB IAW CRJ 700 AMM 27-81-44.
- [SDR SWIA202412261024](https://openairdocs.org/sdr/SWIA202412261024.md): Roller · failed insp · Oct 24, 2024 · N753EV · Cndair CL6002C10 · Leading Edge Devices
  > LH ROLLER ON SLATS 3-2 FWD 1B FAILED INSPECTION (C-CHECK RO 12/24/2024) (FILED OPEN)OK, TO INSTALL. PA. 911290REMOVED AND REPLACED LH ROLLER ON SLAT 3-2 FWD IB IAW CRJ 700 AMM 27-81-44.
- [SDR SWIA202412301023](https://openairdocs.org/sdr/SWIA202412301023.md): Roller · out of limits · Oct 23, 2024 · N753EV · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK ROLLER 1-2 AFT OUTBD FLAT SPOT OUT OF LIMITS (C-CHECK RO 12/24/2024) (FILED CLOSED) OK TO INSTALL PA911290 REMOVED AND REPLACED RH SLAT TRACK ROLLER 1-2 AFT OUTBD IAW AMM 27-81-44.
- [SDR SWIA202412261023](https://openairdocs.org/sdr/SWIA202412261023.md): Slat Track · out of limits · Oct 23, 2024 · N753EV · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK ROLLER 1-2 AFT OUTBD FLAT SPOT OUT OF LIMITS (C-CHECK RO 12/24/2024) (FILED OPEN) OK TO INSTALL PA911290 REMOVED AND REPLACED RH SLAT TRACK ROLLER 1-2 AFT OUTBD IAW AMM 27-81-44.
- [SDR SWIA202501071014](https://openairdocs.org/sdr/SWIA202501071014.md): Floorbeam · cracked · Oct 14, 2024 · N753EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL 12 COCKPIT FLOORBEAM CRACKED, OTBD SIDE, AT 280 BEAM. (C-CHECK RO 12/24/2024) (FILED CLOSED)PERFORMED REPAIR ON RBL 12 COCKPIT FLOOR BEAM OTBD SIDE AT 280 BEAM PER REO 670-53-11-896. REV. AMM 20-70-00.
- [SDR SWIA202412261014](https://openairdocs.org/sdr/SWIA202412261014.md): Floorbeam · cracked · Oct 14, 2024 · N753EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL 12 COCKPIT FLOOR BEAM CRACKED, OTBD SIDE, AT 280 BEAM. (C-CHECK RO 12/24/2024) (FILED OPEN)PERFORMED REPAIR ON RBL 12 COCKPIT FLOOR BEAM OTBD SIDE AT 280 BEAM PER BOMBARDIER REO 670-53-11-896. REV. --. DATE: 2015-03-17. CRJ-700 AMM 20-70-00. NDT PERFORMED
- [SDR SWIA202053648](https://openairdocs.org/sdr/SWIA202053648.md): Attach Bracket · cracked · Oct 9, 2020 · N753EV · Cndair CL6002C10 · Wing Miscellaneous Structure
  > RT WING FLAP STUB FAIRING ATTACH BRACKET CRACKED. C-CHECK RO 10/22/2020. ORDERED AND RECEIVED A NEW RT STUB FAIRING ATTACH BRACKET. LOCATED AND DRILLED THE NEW BRACKET AND INSTALLED, REF CRJ 700 SRM.
- [SDR SWIA202053647](https://openairdocs.org/sdr/SWIA202053647.md): Support Bracket · corroded · Sep 30, 2020 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT BRACKET P/N SH670-41524-1 AT STGR 21R BETWEEN FS 349 AND FS 364. C-CHECK RO 10/22/2020. REMOVED AND REPLACED THE SUPPORT BRACKET AT STGR 21R BETWEEN FS 349 AND FS 364 WITH NEW, REF CRJ 700 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD F
- [SDR SWIA202053646](https://openairdocs.org/sdr/SWIA202053646.md): Stringer · corroded · Sep 30, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 21R BETWEEN FS 349-FS 364. C-CHECK RO 10/22/2020. REMOVED CORRODED STR 21R BETWEEN FS 349-364 AND REPLACED WITH NEW, REFERENCING DWG AND CRJ 700. LEAK TEST GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA202053645](https://openairdocs.org/sdr/SWIA202053645.md): Skin · dented · Sep 26, 2020 · N753EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LT INBOARD FLAP DENTED JUST INBOARD OF WS 54.55, MARKED. C-CHECK RO 10/22/2020. REPAIRED LT INBOARD FLAP LOWER SKIN DAMAGE, IAW CRJ700 SRM.
- [SDR SWIA202053644](https://openairdocs.org/sdr/SWIA202053644.md): Floorbeam · corroded · Sep 25, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > MAIN CABIN CROSSBEAM AT FS 549.00 FOUND CORROSION UNDER FLOORBEAM AT LBL 9. C-CHECK RO 10/22/2020. BLENDED CORROSION, WITHIN LIMITS, REF REO. ALL STEPS ACCOMPLISHED. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA202053643](https://openairdocs.org/sdr/SWIA202053643.md): Floorbeam · corroded · Sep 24, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280 RT CROSS BEAM HAS CORROSION. C-CHECK RO 10/22/2020. REMOVED CORRODED RT FS 280 CROSSBEAM AND REPLACED WITH NEW, REFERENCING DWG CRJ 700 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA202053642](https://openairdocs.org/sdr/SWIA202053642.md): Floorbeam · corroded · Sep 22, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION AT APPROX FS 549 LBL 9 INBOARD ON FLOORBEAM. C-CHECK RO 10/22/2020. REPAIRED DAMAGED FLOORBEAM AT FS 549 LBL 9, REF CRJ700 SRM.
- [SDR SWIA202053684](https://openairdocs.org/sdr/SWIA202053684.md): Mount · corroded · Sep 19, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON FLOOR MOUNT FITTING AT NUTPLATE LOCATION, BETWEEN RBL 9 TO RBL 27, FS 280.00 TO FS 295.00. C-CHECK RO 10/22/2020. CORROSION 100% THROUGH FLOOR MOUNTING FITTING, REMOVED CORRODED FITTING FROM INTERCOSTALS BETWEEN FS 280.00-FS 295.00 APPROXIMATELY
- [SDR SWIA202053683](https://openairdocs.org/sdr/SWIA202053683.md): Mount · corroded · Sep 19, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON FLOOR MOUNT FITTING AT NUTPLATE LOCATION, BETWEEN LBL 27 TO LBL 36, FS 280.00 TO FS 295.00. C-CHECK RO 10/22/2020. CORROSION 100% THROUGH FLOOR MOUNTING FITTING, REMOVED CORRODED FITTING FROM INTERCOSTAL BETWEEN FS 280.00-FS 295.00 LBL 27-LBL 36
- [SDR SWIA202053682](https://openairdocs.org/sdr/SWIA202053682.md): Mount · corroded · Sep 19, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON FLOOR MOUNT FITTING AT NUTPLATE LOCATION, BETWEEN LBL 9 TO LBL 27, FS 280.00 TO FS 295.00. C-CHECK RO 10/22/2020. CORROSION 100% THROUGH FLOOR MOUNTING FITTING, REMOVED CORRODED FITTING FROM INTERCOSTALS BETWEEN FS 280.00-FS 295.00 LBL 9-LBL 27,
- [SDR SWIA202053681](https://openairdocs.org/sdr/SWIA202053681.md): Mount · corroded · Sep 19, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON FLOOR MOUNT FITTING AT NUTPLATE LOCATION, BETWEEN LBL 9 TO LBL 27 FS 310.00. C-CHECK RO 10/22/2020. CORROSION 100% THROUGH FLOOR MOUNTING FITTING, REMOVED CORRODED FITTING FROM FS 310.00 FLOOR SUPPORT POST, REF CRJ700 SRM. INSTALLED REPLACEMENT
- [SDR SWIA202053641](https://openairdocs.org/sdr/SWIA202053641.md): Stringer Splice · corroded · Sep 19, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 25R JOINT SPLICE AT FS 333.00 CORRODED. C-CHECK RO 10/22/2020. NO ALLOWABLE DAMAGE ON JOINT SPLICE. REMOVED AND INSTALLED NEW MAIN AVIONICS BAY STR 25R SPLICE AT FS 333.00, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK C
- [SDR SWIA202053640](https://openairdocs.org/sdr/SWIA202053640.md): Frame · corroded · Sep 18, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY FS 319.70 LOWER FRAME CORRODED BETWEEN STR 27 AND STR 26R. C-CHECK RO 10/22/2020. REMOVED CORRODED FS 319.70 FRAME BETWEEN STR 27 AND STR 26R AND REPLACED WITH NEW, REFERENCING CRJ 700 SRM. LEAK TEST GOOD. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA202053680](https://openairdocs.org/sdr/SWIA202053680.md): Doubler · corroded · Sep 17, 2020 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > THE GALLEY NR 1 HAS A CORRODED DOUBLER BEHIND THE FLOOR MOUNT FITTING (FOOT) AT THE INBOARD/AFT CORNER. C-CHECK RO 10/22/2020. REMOVED THE GALLEY NR 1 CORRODED DOUBLER BEHIND THE FLOOR MOUNT FITTING (FOOT) AT THE INBOARD/AFT CORNER REFERENCING ZODIAC AEROSPA
- [SDR SWIA202053639](https://openairdocs.org/sdr/SWIA202053639.md): Doubler · corroded · Sep 17, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > MAIN AVIONICS BAY TCAS ANTENNA DOUBLER CORRODED BETWEEN FS 295.00 AND FS 310.00. C-CHECK RO 10/22/2020. REMOVED CORRODED TCAS ANTENNA DOUBLER BETWEEN FS 295 TO FS 310 AND INSTALLED NEW, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD. COMP
- [SDR SWIA202053679](https://openairdocs.org/sdr/SWIA202053679.md): Channel · corroded · Sep 16, 2020 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON RT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) AT FS 581.00 TO FS 669.00. C-CHECK RO 10/22/2020. RECEIVED NEWLY FABRICATED RT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) FROM FS 581.00 TO FS 669.00. DRILLED AND LOCATED, REF CRJ700 SRM. INSTA
- [SDR SWIA202053678](https://openairdocs.org/sdr/SWIA202053678.md): Seat Track · corroded · Sep 16, 2020 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT FUSELAGE SIDE SEAT RAIL AT FS 581.00 TO FS 669.00. C-CHECK RO 10/22/2020. REPLACED RT FUSELAGE SIDE SEAT RAIL AT FS 581-FS 669, REF CRJ700 AMM. SEE CONTINUE CARD.
- [SDR SWIA202053677](https://openairdocs.org/sdr/SWIA202053677.md): Seat Track · corroded · Sep 16, 2020 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT FUSELAGE SIDE SEAT RAIL FROM FS 675.00 TO FS 713.00. C-CHECK RO 10/22/2020. REMOVED AND REPLACED WITH NEW THE RT SEAT TRACK AT FS 675-713 CRJ 700 AMM. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053676](https://openairdocs.org/sdr/SWIA202053676.md): Channel · corroded · Sep 16, 2020 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON LT FUSELAGE SIDE SEAT RAIL RETAINER (U CHANNEL) AT FS 752.00. C-CHECK RO 10/22/2020. REPLACED SEAT RAIL RETAINER WITH NEW (PN SH670-37557-3), REF CRJ700 AMM.
- [SDR SWIA202053656](https://openairdocs.org/sdr/SWIA202053656.md): Seat Track · corroded · Sep 16, 2020 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT FUSELAGE SIDE SEAT RAIL FROM FS 785.00 TO FS 855.00. C-CHECK RO 10/22/2020. REPLACED RT FUSELAGE SIDE SEAT RAIL FROM FS 785.00 TO FS 855, REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA202053675](https://openairdocs.org/sdr/SWIA202053675.md): Bracket · corroded · Sep 15, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON MACHINED BRACKET (FLOOR MOUNT PLATE) AT APPROXIMATELY FS 533 STGR 27. C-CHECK RO 10/22/2020. REMOVED CORROSION ON MACHINED BRACKET (FLOOR MOUNT PLATE) AT APPROXIMATELY FS 533 STGR 27, REF CRJ700 SRM. ORIGINAL MATERIAL THICKNESS IS 0.240,? REF D
- [SDR SWIA202053638](https://openairdocs.org/sdr/SWIA202053638.md): Stringer · corroded · Sep 15, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON JOINT STRAP AT FS 333.00 STGR 21R. C-CHECK RO 10/22/2020. REMOVED CORROSION ON JOINT STRAP AT FS 333.00 STGR 21R, REF CRJ 700 SRM. ORIGINAL MATERIAL IS.063, MATERIAL REMOVED IS.027, MATERIAL REMAINING.036, OUT OF LIMITS. PERFORMED REPAIR, R
- [SDR SWIA202053637](https://openairdocs.org/sdr/SWIA202053637.md): Stringer · corroded · Sep 15, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER JOINT PIECE AT STGR 21R FS 333.00. C-CHECK RO 10/22/2020. REMOVED CORROSION ON STRINGER JOINT PIECE AT STGR 21R FS 333.00, REF CRJ 700 SRM. MATERIAL REMOVED IS.016, MATERIAL REMAINING.047, ORIGINAL MATERIAL IS.063, OUT OF LIMT
- [SDR SWIA202053636](https://openairdocs.org/sdr/SWIA202053636.md): Stringer · corroded · Sep 10, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER JOINT PIECE AT STGR 22R FS 333.00. C-CHECK RO 10/22/2020. REMOVED AND REPLACED STRINGER JOINT PIECE AT STGR 22R FS 333.00, REF CRJ700 SRM AND DW. NO LEAKS NOTED.
- [SDR SWIA202053635](https://openairdocs.org/sdr/SWIA202053635.md): Plate · corroded · Sep 9, 2020 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON GROUND PLATES AT FS 319.00 STGR 21R. C-CHECK RO 10/22/2020. REMOVED AND REPLACED GROUND PLATES AT FS 319.00 STGR 21R, REF CRJ700 SRM AND DWG. COMPLETED FORM M-337. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053634](https://openairdocs.org/sdr/SWIA202053634.md): Stringer Clip · corroded · Sep 9, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON CLIP AT FS 310.00 STGR 20R. C-CHECK RO 10/22/2020. CLIP AT FS 310 STGR 20R CORRODED BEYOND LIMIT. REMOVED AND REPLACED, REF CRJ700 SRM AND DWG. COMPLIED WITH SKYWEST TASK CARD "STRUCTURAL MAJOR REPAIR" (RII).
- [SDR SWIA202053633](https://openairdocs.org/sdr/SWIA202053633.md): Skin · chafed · Sep 8, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE EXTERNAL SKIN AT APPROXIMATEY FS 985.0 STGR 27 HAS 3 CHAFED AREAS, MARKED. C-CHECK RO 10/22/2020. BLENDED 3 CHAFED AREAS AFT FUSELAGE EXTERNAL SKIN AT APPROXIMATELY FS 985.0 STGR 27, REF REO. AREAS NR 1 & NR 2 ORIGINAL THICKNESS.118, NR 1 MATE
- [SDR SWIA202053632](https://openairdocs.org/sdr/SWIA202053632.md): Fitting · corroded · Sep 6, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > PAX DOOR SILL FWD CLOSING FITTING HAS EVIDENCE OF CORROSION. C-CHECK RO 10/22/2020. PAX DOOR SILL FWD CLOSING FITTING HAS 100% MATERIAL LOSS DUE TO PITTING CORROSION. REMOVED AND INSTALLED NEW PAX DOOR SILL FWD CLOSING FITTING, REF CRJ 700. COMPLETED FORM
- [SDR SWIA202053674](https://openairdocs.org/sdr/SWIA202053674.md): Angle · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE BETWEEN FS 533.00 TO FS 517.00 STGR 27 TO 26L. C-CHECK RO 10/22/2020. REMOVED CORRODED ANGLE AT FS 333-FS 517 STR 27-26L AND REPLACED WITH NEW REFERENCING CRJ 700 SRM. OPERATIONAL, BONDING, AND LEAK TESTS GOOD.
- [SDR SWIA202053673](https://openairdocs.org/sdr/SWIA202053673.md): Frame · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 549.00 BETWEEN STGR 27 AT STGR 26L FWD SIDE. C-CHECK RO 10/22/2020. COMPLIED WITH MHI RJ REO-ALL STEPS ACCOMPLISHED.
- [SDR SWIA202053672](https://openairdocs.org/sdr/SWIA202053672.md): Bracket · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON MACHINED BRACKET (FLOOR MOUNT PLATE) BETWEEN FS 549.00 TO FS 565.00, STGR 25R TO STGR 24R. C-CHECK RO 10/22/2020. REMOVED CORRODED MACHINED BRACKET BETWEEN FS 549-565 STR 25R-STR 24R AND REPLACED WITH NEW REFERENCING CRJ 700 SRM. LEAK TEST GOOD
- [SDR SWIA202053631](https://openairdocs.org/sdr/SWIA202053631.md): Intercostal · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON SGTR 21L ATTACHED INTERCOSTAL BETWEEN FS 349.00-FS 333.00. C-CHECK RO 10/22/2020. INSTALLED NEW INTERCOSTAL BETWEEN FS 333.00 AND FS 349.00 AT STR 21L, REF DWG AND CRJ700 SRM. RESTORED FINISH, REF CRJ700 SRM 51. APPLIED FILLET SEALENT, REF CRJ
- [SDR SWIA202053630](https://openairdocs.org/sdr/SWIA202053630.md): Stringer Clip · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON ATTACHING CLIP FOR STGR 19L FS 295.00. C-CHECK RO 10/22/2020. REMOVED CORRODED STR19L CLIP AT FS 295 AND REPLACED WITH NEW REFERENCING DWG AND CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.
- [SDR SWIA202053629](https://openairdocs.org/sdr/SWIA202053629.md): Stringer · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 21R BETWEEN FS 319.00-FS 333.00. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEW STRINGER JOINT AND ANGLE AT STR 21R FS 333, REF CRJ 700 SRM AND DWG. REMOVED AND INSTALLED NEW STRINGER 21R BETWEEN FS 280-FS 333, REF REO. NO LEAKS NOTED.
- [SDR SWIA202053628](https://openairdocs.org/sdr/SWIA202053628.md): Stringer · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 20R BETWEEN FS 295.00 TO FS 310.00. C-CHECK RO 10/22/2020. REPAIRED STR 20R BETWEEN FS 295-FS 310, REFERENCING CRJ 700 SRM DWG. LEAK TEST GOOD. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.
- [SDR SWIA202053627](https://openairdocs.org/sdr/SWIA202053627.md): Stringer · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 20R ATTACHED INTERCOSTAL BETWEEN FS 310.00 TO FS 349.00. C-CHECK RO 10/22/2020. REPLACED INTERCOSTAL BETWEEN FS 310-FS 349 ON STRINGER 20R, REF DRAWING AND CRJ700 SRM. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA202053626](https://openairdocs.org/sdr/SWIA202053626.md): Stringer · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 25 BETWEEN FS 319.00-FS 333.00, MARKED. C-CHECK RO 10/22/2020. REMOVED CORRODED STR 25R BETWEEN FS 280 AND FS 333 AND REPLACED WITH NEW REFERENCING DWG CRJ 700 SRM. LEAK TEST GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA202053625](https://openairdocs.org/sdr/SWIA202053625.md): Frame · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 310.00 BETWEEN STGR 26R-STGR 24L, AREAS MARKED ON FRONT AND AFT SIDES. C-CHECK RO 10/22/2020. REMOVED CORROSION ON FRAME FS 310.00 BETWEEN STGR 26R-STGR 24L, REF CRJ 700 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. REMOVED CORRODED L
- [SDR SWIA202053624](https://openairdocs.org/sdr/SWIA202053624.md): Frame · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 295.00 BETWEEN STGR 26R-20L ON MULTIPLE AREAS, FRONT AND AFT SIDES, AREAS MARKED. C-CHECK RO 10/22/2020. REMOVED AND INSTALLED NEW FRAME SECTION REINFORCING ANGLE FROM STR 20L TO STR 25R, REF REO DWG, CRJ 700 SRM. NO LEAKS NOTED.
- [SDR SWIA202053623](https://openairdocs.org/sdr/SWIA202053623.md): Stringer · corroded · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRG 27 AT APPROXIMATELY FS 283.00, MARKED. C-CHECK RO 10/22/2020. REMOVED CORROSION ON STR 27 AT FS 283.00, REF CRJ700 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW STR 27 FROM FS 280 TO FS 298, REF CRJ700 SRM AND DWG. NO LEAKS
- [SDR SWIA202053622](https://openairdocs.org/sdr/SWIA202053622.md): Slat Track · worn · Sep 5, 2020 · N753EV · Cndair CL6002C10 · Trailing Edge Flaps
  > RT SLAT TRACK 3-3 HAS MULTIPLE WEAR MARKS ON ITS UPPER AND LOWER ROLLING SURFACES. C-CHECK RO 10/22/2020. REPAIRED RT SLAT TRACK 3-3, REFERENCING REO CRJ 700 SRM CRJ 700 AMM AND DWG. OPERATIONAL TEST GOOD. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWES
- [SDR SWIA202053621](https://openairdocs.org/sdr/SWIA202053621.md): Bracket · corroded · Sep 4, 2020 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > SERVICE DOOR SILL THRESHOLD BRACKETS AT APPROXIMATELY FS 321 AND FS 338 HAVE EVIDENCE OF CORROSION. C-CHECK RO 10/22/2020. INSTALLED 4 EA BRACKETS AND 4 EA ANGLES, REF CRJ 700 SRM AND DWG. COMPLIED WITH SKY CARD.
- [SDR SWIA202053620](https://openairdocs.org/sdr/SWIA202053620.md): Slat Track · worn · Sep 4, 2020 · N753EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LT WING SLAT TRACK 3-3 HAS MULTIPLE WEAR MARKS ON UPPER AND LOWER ROLLER CONTACT SURFACES. C-CHECK RO 10/22/2020. REPAIRED LT WING SLAT TRACK 3-3 WEAR MARKS, IAW REO CRJ700 SRM CRJ700 AMM. OPERATIONS CHECK GOOD AT THIS TIME.

Next page: https://openairdocs.org/aircraft/N753EV/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 = 'N753EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N753EV/reports

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