# Service difficulty reports: N752EV

A list on [N752EV](https://openairdocs.org/aircraft/N752EV.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 8 · 365 reports

- [SDR SWIA202507310001](https://openairdocs.org/sdr/SWIA202507310001.md): Window · cracked · Jul 30, 2025 · N752EV · Cndair CL6002C10 · Flight Compartment Windows
  > LEFT WINDOW SHATTERED CLIMBING THROUGH 26000 FT (FLIGHT 6444) REMOVED AND REPLACED CAPTAINS SIDE WINDOW IAW TASK CARD 56-220-1000-SKY. OPS CHECK OF WINDOW HEAT GOOD. LEAK CHECK GOOD. AIRCRAFT SAFE FOR RETURN TO SERVICE.
- [SDR SWIA20240904](https://openairdocs.org/sdr/SWIA20240904.md): Slat Track · cracked · Sep 4, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK CANISTER 1-3 SUPPORT BRACKET HAS SUSPECTED CRACKED UNDER FUEL PANEL 651AB (MARKED). REPAIRED RH SLAT TRACK CANISTER 1-3 SUPPORT BRACKET PER. GREO REO 670-57-42-577 REV: --. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWIA202411120805](https://openairdocs.org/sdr/SWIA202411120805.md): Floor Support · damaged · Aug 5, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF FLOOR BEAM RBL 9 AT APPROX FS855 - FS977 FOUND ELONAGTED HOLE AT CROSS BEAM FROM PREVIOUS REPAIR AT FS969. (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED FLOOR BEAM RBL 9 AT FS 969 IAW REO 670-53-51-300 REV. -- DATED 2024-08-07 ALL STEPS AT LO
- [SDR SWIA20240805](https://openairdocs.org/sdr/SWIA20240805.md): Floor Support · elongated · Aug 5, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF FLOOR BEAM RBL 9 AT APPROX FS855 - FS977 FOUND ELONAGTED HOLE AT CROSS BEAM FROM PREVIOUS REPAIR AT FS969. (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED FLOOR BEAM RBL 9 AT FS 969 IAW REO 670-53-51-300 REV. -- DATED 2024-08-07 ALL STEPS AT LOCA
- [SDR SWIA20240726](https://openairdocs.org/sdr/SWIA20240726.md): Hinge · out of limits · Jul 26, 2024 · N752EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > REPLACE PASSENGER DOOR HINGE (ON FUSELAGE SIDE) DUE TO 25 OUT OF 27 LUGS BEING OUT OF LIMITS. CAMP # 28592083. (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED AND INSTALLED 1EA NEW PAX DOOR HINGE, FUSELAGE SIDE PER CRJ700SRM 53-21-23-201-007-A01, CRJ700SRM 51-42-21
- [SDR SWI2024F01135](https://openairdocs.org/sdr/SWI2024F01135.md): Drag Angle · cracked · Jul 21, 2024 · N752EV · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > LH AFT DRAG ANGLE HAS POSSIBLE CRACK AT VERTICAL STABILIZER ROOT (MARKED). (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED THE L/H V-STAB AFT DRAG ANGLE PER CRJ700SRM 55-31-00-201-001-A01. SEE CONTINUATION FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002
- [SDR SWIA20240721](https://openairdocs.org/sdr/SWIA20240721.md): Drag Angle · cracked · Jul 21, 2024 · N752EV · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > RH AFT DRAG ANGLE HAS POSSIBLE CRACK AT VERTICAL STABILIZER ROOT (MARKED). (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED AFT DRAG ANGLE IN THE RH VERTICAL ROOT REF REO 670-55-31-176 REV -- DATED 2024-08-01, CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK C
- [SDR SWIA20241009721](https://openairdocs.org/sdr/SWIA20241009721.md): Drag Angle · cracked · Jul 21, 2024 · N752EV · Cndair CL6002C10 · Vertical Stabilizer
  > RH AFT DRAG ANGLE HAS POSSIBLE CRACK AT VERTICAL STABILIZER ROOT (MARKED). (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED AFT DRAG ANGLE IN THE RH VERTICAL ROOT REF REO 670-55-31-176 REV -- DATED 2024-08-01, CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CAR
- [SDR SWI2024F00956](https://openairdocs.org/sdr/SWI2024F00956.md): Drag Angle · cracked · Jul 21, 2024 · N752EV · Cndair CL6002C10 · Vertical Stabilizer
  > RH AFT DRAG ANGLE HAS POSSIBLE CRACK AT VERTICAL STABILIZER ROOT (MARKED). (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED AFT DRAG ANGLE IN THE RH VERTICAL ROOT REF REO 670-55-31-176 REV -- DATED 2024-08-01, CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CAR
- [SDR SWIA20240711](https://openairdocs.org/sdr/SWIA20240711.md): Spar · gouged · Jul 11, 2024 · N752EV · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB AFT SPAR - FITTING FOR RUDDER MIDDLE LOWER HINGE - UPR SURFACE GOUGED. REMOVED DAMAGE ON VERTICAL STAB AFT SPAR - FITTING FOR RUDDER MIDDLE LOWER HINGE - UPR SURFACE REF CRJ700 SRM 51-12-00-001-001-A01. V-STAB AFT SPAR, MID LOWER RUDDER HINGE FIT
- [SDR SWI2024F01134](https://openairdocs.org/sdr/SWI2024F01134.md): Frame · corroded · Jun 20, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 265.0 / LH STGR 26 TO RH STGR 26 IS CORRODED FLAGGED S/N:0659 (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED AND REPLACED STIFFENING ANGLE ON FRAME FS265 P/N CC670-34104-1 REF DWG CC670-34020 REV. B. AND DWG CC670-33025 REV. D REF. CRJ 700 SRM 51-42-06-0
- [SDR SWI2024F01133](https://openairdocs.org/sdr/SWI2024F01133.md): Intercostal · corroded · Jun 20, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UNDER COCKPIT FLOOR, FWD OF 280 FRAME. FWD JACKING POINT THE RH INTERCOSTAL IS CORRODED. FLAGGED S/N 0658 (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED FWD OF F/S 280 FRAME FWD JACKING POINT THE RH INTERCOSTAL IAW DWG CC670-32050 REV. NC AND REO 670-53-11
- [SDR SWI2024F01132](https://openairdocs.org/sdr/SWI2024F01132.md): Floorbeam · corroded · Jun 20, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > UNDER COCKPIT FLOOR, FWD OF 280 FRAME. FWD JACKING POINT THE LH INTERCOSTAL IS CORRODED. FLAGGED S/N 0657 (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED FWD OF F/S 280 FRAME FWD JACKING POINT THE L/H INTERCOSTAL IAW DWG CC670-32050 REV. NC AND REO 67
- [SDR SWIA202411040620](https://openairdocs.org/sdr/SWIA202411040620.md): Fitting · corroded · Jun 20, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD BAGGAGE BAY INTERNAL STRUCTURE MACHINED FITTING (LBL24) (SH670-33390-1) CORROSION AROUND SCREW HOLES (C-CHECK RO 10/7/2024) (FILED CLOSED) INSTALLED NEW FITTING IAW BOMBARDIER DRAWING SH670-33600 REV AD, CRJ700 SRM 51-42-22-001-001-A01 REV 38. DATE: J
- [SDR SWIA20240620](https://openairdocs.org/sdr/SWIA20240620.md): Skin · corroded · Jun 20, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION AROUND MULTIPLE RIVET HEADS ON EXTERNAL SKIN FS939.00 - FS992.00 BETWEEN STGR20R & 22L. (MARKED IN RED) 28413806 (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED CORROSION FROM FASTENER HOLES (6 PLACES), AND EVALUATED AS 'OUT-OF-LIMITS'. RECIEVED AND COMPL
- [SDR SWI2024F00978](https://openairdocs.org/sdr/SWI2024F00978.md): Frame · corroded · Jun 20, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 265.0 / LH STGR 26 TO RH STGR 26 IS CORRODED FLAGGED S/N:0659 (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED AND REPLACED STIFFENING ANGLE ON FRAME FS265 P/N CC670-34104-1 REF DWG CC670-34020 REV. B. AND DWG CC670-33025 REV. D REF. CRJ 700 SRM 51-42-06-001
- [SDR SWI2024F00977](https://openairdocs.org/sdr/SWI2024F00977.md): Floorbeam · corroded · Jun 20, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > UNDER COCKPIT FLOOR, FWD OF 280 FRAME. FWD JACKING POINT THE LH INTERCOSTAL IS CORRODED. FLAGGED S/N 0657 (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED FWD OF F/S 280 FRAME FWD JACKING POINT THE L/H INTERCOSTAL IAW DWG CC670-32050 REV. NC AND REO 670-
- [SDR SWI2024F00976](https://openairdocs.org/sdr/SWI2024F00976.md): Fitting · corroded · Jun 20, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY INTERNAL STRUCTURE MACHINED FITTING (LBL24) (SH670-33390-1) CORROSION AROUND SCREW HOLES (C-CHECK RO 10/7/2024) (FILED OPEN) INSTALLED NEW FITTING IAW BOMBARDIER DRAWING SH670-33600 REV AD, CRJ700 SRM 51-42-22-001-001-A01 REV 38. DATE: JUL
- [SDR SWIA202411040618](https://openairdocs.org/sdr/SWIA202411040618.md): Skin · dented · Jun 18, 2024 · N752EV · Cndair CL6002C10 · Wing, Plate/Skin
  > RH WING ON UNDERSIDE OB AREA NEAR WINGLET APROX. BETWEEN FS.370.25 AND FS.398.93 HAS MULTIPLE DENTS ON EXTERIOR SKIN (MARKED). (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED RIGHT-HAND WING UNDERSIDE SKIN BETWEEN FS370.25 AND FS398.93 TO PROVIDE ACCESS TO DENTS.
- [SDR SWIA202410096018](https://openairdocs.org/sdr/SWIA202410096018.md): Skin · dented · Jun 18, 2024 · N752EV · Cndair CL6002C10 · Wing, Plate/Skin
  > RH WING ON UNDERSIDE OB AREA NEAR WINGLET APROX. BETWEEN FS.370.25 AND FS.398.93 HAS MULTIPLE DENTS ON EXTERIOR SKIN (MARKED). (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED RIGHT-HAND WING UNDERSIDE SKIN BETWEEN FS370.25 AND FS398.93 TO PROVIDE ACCESS TO DENTS. R
- [SDR SWIA20240618](https://openairdocs.org/sdr/SWIA20240618.md): Roll Pin · migrated · Jun 18, 2024 · N752EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE, DOOR SIDE, ROLL PIN IS MIGRATED AND CHAFING INTO LAND 27, FUSELAGE SIDE. (C-CHECK RO 10/7/2024) (FILED OPEN)PAX DOOR HINGE (DOOR SIDE) FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IRT CRJ700 SRM 52-11-01-201-002-A01, COMPLIED WITH 51-9
- [SDR SWI2024F01113](https://openairdocs.org/sdr/SWI2024F01113.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-1 HAS PITTING IN 2 AREAS ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED PITTING ON THE LH SLAT TRACK 3-1 REF REO 670-57-42-1639 REV -- DATED 2024-07-24. SEE CONTINUATION FOR DETAILS. COMPLIED WITH 51-900-1
- [SDR SWI2024F01112](https://openairdocs.org/sdr/SWI2024F01112.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-3 HAS PITTING IN 3 AREAS,1 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED SLAT TRACK 2-3 HAS PITTING IN 3 AREAS REF REO 670-57-42-1648 REV -- DATE 2024-07-31. COMPLIED WITH 51-900-
- [SDR SWI2024F01111](https://openairdocs.org/sdr/SWI2024F01111.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 HAS PITTING IN 4 AREAS, 2 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED DAMAGE ON LEFT SLAT TRACK 2-2 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REPAIRED THE
- [SDR SWI2024F01110](https://openairdocs.org/sdr/SWI2024F01110.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-1 HAS PITTING IN 4 AREAS, 2 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED DAMAGE ON LEFT SLAT TRACK 2-1 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. SLAT TRACK 2
- [SDR SWI2024F01109](https://openairdocs.org/sdr/SWI2024F01109.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-3 HAS PITTING IN 3 AREAS, 2 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED LEFT SLAT TRACK 1-3 HAS PITTING IN 3 AREAS REF REO 670-57-42-1643 REV -- DATE 2024-07-25. COMPLIED WITH 5
- [SDR SWI2024F01121](https://openairdocs.org/sdr/SWI2024F01121.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-2 HAS PITTING IN 3 AREAS,1 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED DAMAGE ON LH SLAT TRACK 1-2 - REF CRJ700 SRM 51-21-06-001-001-A01. REPAIRED LEFT SLAT TRACK 1-2 - REO 670-5
- [SDR SWI2024F01120](https://openairdocs.org/sdr/SWI2024F01120.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-2 HAS PITTING IN 1 AREA ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 3-2, LOWER SURFACE - REF CRJ700 SRM 51-21-06-001-001-A01. SLAT TRACK REPAIRED PER REO 670-57-42-16
- [SDR SWI2024F01119](https://openairdocs.org/sdr/SWI2024F01119.md): Striker · bent · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SURROUND STRUCTURE SEAL STRIKER BENT AT FORWARD LOWER CENT ROLLER ASSY (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIR OF PAX DOOR SURROUND SEAL STRIKER AT LOWER CENT ROLLER ASSY AREA ACCOMPLISHED PER REF CRJ 700 SRM 53-21-23-201-006-A01. ALL LEAK A
- [SDR SWI2024F01118](https://openairdocs.org/sdr/SWI2024F01118.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 HAS PITTING IN 3 AREAS, 2 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) 28399060 (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 2-2, UPPER AND LOWER SURFACE - REF CRJ700 SRM 51-21-06-001-
- [SDR SWI2024F01117](https://openairdocs.org/sdr/SWI2024F01117.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-1 HAS PITTING IN 2AREAS, 1 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED DAMAGE ON RIGHT SLAT TRACK 2-1 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REMOVED SLA
- [SDR SWI2024F01116](https://openairdocs.org/sdr/SWI2024F01116.md): Fitting · gouged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE FORWARD HANDRAIL FITTING GOUGED (C-CHECK RO 10/7/2024) (FILED CLOSED)BLENDED FITTING AND FOUND OUT OF LIMITS. REPLACED WITH NEW FITTING REF. CRJ700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670-31810 REV AE. COMPLIED WITH
- [SDR SWI2024F01115](https://openairdocs.org/sdr/SWI2024F01115.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-3 HAS PITTING IN 2 AREAS ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED DAMAGE ON RIGHT SLAT TRACK 1-3 ON LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REPAIR ACCOMPLISHED PER COMPLIED WITH REO 670-57
- [SDR SWI2024F01114](https://openairdocs.org/sdr/SWI2024F01114.md): Seat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SLAT TRACK 1-2 HAS PITTING IN 1 AREA ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 1-2, UPPER AND LOWER SURFACE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1640 REV. -- D
- [SDR SWIA20240617](https://openairdocs.org/sdr/SWIA20240617.md): Skin · chafed · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)CHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27 FOUND TO BE OUT OF ALLOWABLE LIMITS DU
- [SDR SWI2024F01017](https://openairdocs.org/sdr/SWI2024F01017.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-1 HAS PITTING IN 2 AREAS ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED PITTING ON THE LH SLAT TRACK 3-1 REF REO 670-57-42-1639 REV -- DATED 2024-07-24. SEE CONTINUATION FOR DETAILS. COMPLIED WITH 51-900-100
- [SDR SWI2024F01016](https://openairdocs.org/sdr/SWI2024F01016.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-3 HAS PITTING IN 3 AREAS,1 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED SLAT TRACK 2-3 HAS PITTING IN 3 AREAS REF REO 670-57-42-1648 REV -- DATE 2024-07-31. COMPLIED WITH 51-900-10
- [SDR SWI2024F01015](https://openairdocs.org/sdr/SWI2024F01015.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 HAS PITTING IN 4 AREAS, 2 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LEFT SLAT TRACK 2-2 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REPAIRED THE L
- [SDR SWI2024F01014](https://openairdocs.org/sdr/SWI2024F01014.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-1 HAS PITTING IN 4 AREAS, 2 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LEFT SLAT TRACK 2-1 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. SLAT TRACK 2-1
- [SDR SWI2024F01013](https://openairdocs.org/sdr/SWI2024F01013.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-3 HAS PITTING IN 3 AREAS, 2 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED LEFT SLAT TRACK 1-3 HAS PITTING IN 3 AREAS REF REO 670-57-42-1643 REV -- DATE 2024-07-25. COMPLIED WITH 51-
- [SDR SWI2024F01012](https://openairdocs.org/sdr/SWI2024F01012.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-2 HAS PITTING IN 3 AREAS,1 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LH SLAT TRACK 1-2 - REF CRJ700 SRM 51-21-06-001-001-A01. REPAIRED LEFT SLAT TRACK 1-2 - REO 670-57-
- [SDR SWI2024F01011](https://openairdocs.org/sdr/SWI2024F01011.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-2 HAS PITTING IN 1 AREA ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 3-2, LOWER SURFACE - REF CRJ700 SRM 51-21-06-001-001-A01. SLAT TRACK REPAIRED PER REO 670-57-42-1638
- [SDR SWI2024F01010](https://openairdocs.org/sdr/SWI2024F01010.md): Striker · bent · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SURROUND STRUCTURE SEAL STRIKER BENT AT FORWARD LOWER CENT ROLLER ASSY (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIR OF PAX DOOR SURROUND SEAL STRIKER AT LOWER CENT ROLLER ASSY AREA ACCOMPLISHED PER REF CRJ 700 SRM 53-21-23-201-006-A01. ALL LEAK AND
- [SDR SWI2024F01009](https://openairdocs.org/sdr/SWI2024F01009.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 HAS PITTING IN 3 AREAS, 2 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) 28399060 (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 2-2, UPPER AND LOWER SURFACE - REF CRJ700 SRM 51-21-06-001-00
- [SDR SWI2024F01008](https://openairdocs.org/sdr/SWI2024F01008.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-1 HAS PITTING IN 2AREAS, 1 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON RIGHT SLAT TRACK 2-1 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REMOVED SLAT
- [SDR SWI2024F01007](https://openairdocs.org/sdr/SWI2024F01007.md): Fitting · gouged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SURROUND STRUCTURE FORWARD HANDRAIL FITTING GOUGED (C-CHECK RO 10/7/2024) (FILED OPEN)BLENDED FITTING AND FOUND OUT OF LIMITS. REPLACED WITH NEW FITTING REF. CRJ700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670-31810 REV AE. COMPLIED WITH AL
- [SDR SWI2024F01006](https://openairdocs.org/sdr/SWI2024F01006.md): Fitting · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-3 HAS PITTING IN 2 AREAS ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON RIGHT SLAT TRACK 1-3 ON LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REPAIR ACCOMPLISHED PER COMPLIED WITH REO 670-57-4
- [SDR SWI2024F01005](https://openairdocs.org/sdr/SWI2024F01005.md): Fitting · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-2 HAS PITTING IN 1 AREA ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 1-2, UPPER AND LOWER SURFACE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1640 REV. -- DAT
- [SDR SWI2024F01004](https://openairdocs.org/sdr/SWI2024F01004.md): Skin · chafed · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)CHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27 FOUND TO BE OUT OF ALLOWABLE LIMITS DU
- [SDR SWI2024F01003](https://openairdocs.org/sdr/SWI2024F01003.md): Slat Track · damaged · Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-1 HAS PITTING IN 2 AREAS ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED PITTING ON THE LH SLAT TRACK 3-1 REF REO 670-57-42-1639 REV -- DATED 2024-07-24. SEE CONTINUATION FOR DETAILS. COMPLIED WITH 51-900-100

Next page: https://openairdocs.org/aircraft/N752EV/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 = 'N752EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N752EV/reports

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