# Service difficulty reports: N759EV

A list on [N759EV](https://openairdocs.org/aircraft/N759EV.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 5 · 201 reports

- [SDR SWIA2026011375064](https://openairdocs.org/sdr/SWIA2026011375064.md): Frame · mechanic error · Jan 13, 2026 · N759EV · Cndair CL6002C10 · Fuselage Main, Frame
  > MISDRILLED HOLE ON THE REAR SPAR FRAME SECTOR FS797.00, AT LBL36. (FILED CLOSED)PERFORMED ALL STEPS PER REO 670-53-41-789 REV -- DATE 2026 JAN 23. NO OTHER DISCREPENCIES FOUND AT THIS TIME. SEE NDT REPORT ATTACHED.
- [SDR SWIA2026011400003](https://openairdocs.org/sdr/SWIA2026011400003.md): Frame · mechanic error · Jan 13, 2026 · N759EV · Cndair CL6002C10 · Fuselage Main, Frame
  > MISDRILLED HOLE ON THE REAR SPAR FRAME SECTOR FS797.00, AT LBL36. (OPEN)
- [SDR SWIA202511240180](https://openairdocs.org/sdr/SWIA202511240180.md): Stringer · damaged · Oct 18, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > WHILE PERFORMING REPAIR ON ELECTRICAL BAY FLOOR AT FS193.00 FOUND STGR.16R HAS ELONGATED HOLES. INSTALLED NEW STR. 16R AT FS193.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG#CC670-33030 REV-B. COMPLIED WITH REO 670-53-11-2201 REV -A DATE 2025-10-30 ALTERNATE
- [SDR SWIA20251124003](https://openairdocs.org/sdr/SWIA20251124003.md): Floor Support · corroded · Oct 3, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT RBL 9 HAS CORROSION APPROXIMATELY BETWEEN BS 501 TO BS 565. REPAIRED THE FLOOR SUPPORT IAW REO 670-53-31-1112 REV -. TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025112400929](https://openairdocs.org/sdr/SWIA2025112400929.md): Angle · bent · Sep 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE AT BS 1031, S18 FOUND BENT WITH A RIVET SHEARED. FOUND TO BE BENT AND CRACKED, REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 REVISION 38, AND DWG MM670-36023, REV B. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1
- [SDR SWIA2025112400924](https://openairdocs.org/sdr/SWIA2025112400924.md): Cleat · cracked · Sep 24, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BS 1015, S18 CLEAT APPEARS TO BE CRACKED. INSTALLED NEW CLEAT IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, REVISION 38, AND DWG MM670-36022, REV C. COMPLIED WITH SKYWEST TAK CARD 51-900-1002-SKY.
- [SDR SWIA202511240913](https://openairdocs.org/sdr/SWIA202511240913.md): Rib · worn · Sep 13, 2025 · N759EV · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT OTBD FLAP BUTE DOOR CAMS & RIB FITTINGS HAVE WEAR & ARE MUSHROOMED AT ALL 5 LOCATIONS. REPAIRED THE BUTE DOOR CAMS AND RIB FITTINGS, REPLACED OTBD MOST LOCATION IAW REO 670-57-53-008 REV -D, & DWG 601R14502, REV D, CHECKS GOOD. COMPLIED WITH SKYWEST
- [SDR SWI2025F01548](https://openairdocs.org/sdr/SWI2025F01548.md): Window Post · cracked · Sep 8, 2025 · N759EV · Cndair CL6002C10 · Flight Compartment Windows
  > POSSIBLE CRACK RIGHT WINDSHIELD POST. REMOVED CRACKED RT SIDE POST 601R33223-2 & REPLACED WITH NEW IAW SRM 51-42-21-001-001-A01 REV. 38 & DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.LEAK CHECKED GOOD.
- [SDR SWIA2025112400908](https://openairdocs.org/sdr/SWIA2025112400908.md): Intercostal · corroded · Sep 8, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLEAT AT INTERCOSTAL DD4 AND FRAME FS313.56 ON PAX DOOR HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED PAX DOOR CLEAT AT INTERCOSTAL DD4 AND FRAME FS313.56. REF: SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH SKYWEST TAK CARD 51-900-1
- [SDR SWI2025F01549](https://openairdocs.org/sdr/SWI2025F01549.md): Aneroid · corroded · Sep 7, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > TWO CLIPS AT FS320.00 AND BOTTOM CHANNEL OF PAX DOOR HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED TWO CLIPS AT FS320.00 AND BOTTOM CHANNEL OF PAX DOOR. IAW SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N COMPLIED WITH SKYWEST TASK CARD 51-900-1002-
- [SDR SWIA202511240907](https://openairdocs.org/sdr/SWIA202511240907.md): Angle · corroded · Sep 7, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > TWO CLIPS AT FS338 AND BOTTOM CHANNEL OF PAX DOOR HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED TWO CLIPS AT FS338.00 AND BOTTOM CHANNEL OF PAX DOOR. IAW SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWI2025F01554](https://openairdocs.org/sdr/SWI2025F01554.md): Slat Track · damaged · Sep 1, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 3-2 SIDE ROLLER INBD AND OUTBD FWD DAMAGE. (C-CHECK RO 11/22/2025)INSTALLED NEW/SERVICEABLE RH WING SLAT TRACT 3-2 (I/B FWD, I/B AFT, O/B FWD AND O/B AFT) SIDE ROLLERS PER CRJ700 AMM 27-81-44-400-803-A01
- [SDR SWI2025F01553](https://openairdocs.org/sdr/SWI2025F01553.md): Slat Track · damaged · Sep 1, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 2-2 SIDE ROLLER INBD AND OUTBD AFT DAMAGE. (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED INBD AND OUTBD AFT SIDE ROLLERS FOR THE R/H WING 2-2 SLAT TRACK. REF CRJ700 AMM 27-81-44-400-802-A01
- [SDR SWI2025F01552](https://openairdocs.org/sdr/SWI2025F01552.md): Slat Track · damaged · Sep 1, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 1-2 SIDE ROLLER OUTBD AFT DAMAGE (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW OUTBD AND REPLACED THE INBD AFT SIDE ROLLERS FOR THE R/H WING 1-2 SLAT TRACK. REF CRJ700 AMM 27-81-44-400-801-A01
- [SDR SWI2025F01551](https://openairdocs.org/sdr/SWI2025F01551.md): Roller · failed insp · Sep 1, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 3-2 IB FWD, IB AFT, OB FWD, OB AFT SIDE ROLLERS FAILED INSPECTION. (S/N 00798) (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED 4 EA. NEW LH SLAT TRACK 3-2 IB FWD, IB AFT, OB FWD, OB AFT SIDE ROLLERS AS FOLLOWS. REF CRJ-700 AMM 27-81-44-400-803-A01
- [SDR SWI2025F01550](https://openairdocs.org/sdr/SWI2025F01550.md): Roller · failed insp · Sep 1, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 2-2 IB FWD, IB AFT, OB FWD, OB AFT SIDE ROLLERS FAILED INSPECTION. (S/N 00797) (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW 4EA SLAT-TRACK SIDE ROLLERS AT THE L/H 2-2 SLAT TRACK, WITH 4EA SERVICEABLE SIDE ROLLERS REF CRJ700 AMM 27-81-44-400-
- [SDR SWIA202511240901](https://openairdocs.org/sdr/SWIA202511240901.md): Roller · failed insp · Sep 1, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-2 INBD AFT AND OTBD AFT SIDE ROLLERS FAILED INSPECTION. REMOVED AND INSTALLED TWO NEW SLAT TRACKS 1-2 INBD AFT AND OTBD AFT SIDE ROLLERS. AMM 27-81-44-400-801-A01
- [SDR SWIA202511240830](https://openairdocs.org/sdr/SWIA202511240830.md): Canister · cracked · Aug 30, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK CANNISTER 1-3 ATTACH BRACKET INSIDE FUEL PANEL 651AB IS CRACKED. COMPLIED WITH REPAIR OF THE RH WING SLAT TRACK 1-3 CANNISTER ATTACH BRACKET REF REO 670-57-42-577 REV-- DATE: 2016-12-02. COMPLIED WITH ALL STEPS, COMPLIED WITH TASK CARD 51
- [SDR SWI2025F01547](https://openairdocs.org/sdr/SWI2025F01547.md): Intercostal · corroded · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERTCOSTAL DD2 FS338.00 - FS347.25 IS CORRODED (C-CHECK RO 11/22/2025)INSTALLED NEW PAX DOOR INTERTCOSTAL DD2 FS338.00 - FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N, COMPLIED WITH SKY CARD 51-900-1002-SKY, LEAK CHEC
- [SDR SWI2025F01546](https://openairdocs.org/sdr/SWI2025F01546.md): Mount · damaged · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FWD ATG ANTENNA MOUNT ON EXTERIOR SKIN HAS MULTIPLE TOOLING MARKS BETWEEN FS581.00 - FS597.00 BETWEEN STGR 25R - STGR24R AS MARKED (C-CHECK RO 11/22/2025)EVALUATED. NO FOUND ALLOWABLE DAMAGE ON CRJ700 SDS. REMOVED DOUBLER AT FWD ATG ANTENNA MOUNT REF CRJ700
- [SDR SWI2025F01545](https://openairdocs.org/sdr/SWI2025F01545.md): Former · corroded · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER FS347.25 IS CORRODED (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV N, COMPLIED WITH SKY CARD 51-900-1002-SK
- [SDR SWI2025F01544](https://openairdocs.org/sdr/SWI2025F01544.md): Slat Track · cracked · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 1-3 CANNISTER ATTACH BRACKET, INSIDE FUEL PANEL 551AB, POSSIBLY CRACKED (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REPAIR OF THE LH WING SLAT TRACK 1-3 CANNISTER ATTACH BRACKET REF REO 670-57-42-577 REV-- DATE: 2016-12-02. COMPLIED WIT
- [SDR SWI2025F01543](https://openairdocs.org/sdr/SWI2025F01543.md): Cleat · corroded · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CLEAT @ FS327.763 AND DD7A IS CORRODED (C-CHECK RO 11/22/2025)REMOVED AND REPLACED PAX DOOR CLEAT @ FS327.763 AND DD7A. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01558](https://openairdocs.org/sdr/SWI2025F01558.md): Cleat · corroded · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLEAT AT BS 320 AND DD3 IS CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT IAW SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01557](https://openairdocs.org/sdr/SWI2025F01557.md): Cleat · corroded · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLEAT, BS 323.00 AND DD1 IS CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT IAW SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01556](https://openairdocs.org/sdr/SWI2025F01556.md): Cleat · corroded · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLEAT, BS 323 AND DD1A IS CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT IAW SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01555](https://openairdocs.org/sdr/SWI2025F01555.md): Door Frame · corroded · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FRAME BS FS313.56, DD4 AND DD5 IS CORRODED. INSTALLED NEW PAX DOOR FRAME IAW SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N, COMPLIED WITH SKY CARD 51-900-1002-SKY, LEAK CHECKED GOOD
- [SDR SWIA202511240829](https://openairdocs.org/sdr/SWIA202511240829.md): Angle · corroded · Aug 29, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE AT FS327.763 - FS338.00 IS CORRODED. REMOVED AND REPLACED PAX DOOR ANGLE AT DD7A FS327.763 - FS338.00. REF: SRM 51-42-21-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F010560](https://openairdocs.org/sdr/SWI2025F010560.md): Hinge · damaged · Aug 28, 2025 · N759EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE, FUSELAGE SIDE, FWD 2EA LUGS HAVE IMPACT DAMAGE ON THE UPPER AREA (MARKED) (C-CHECK RO 11/22/2025)REMOVED GOUGE ON PAX DOOR HINGE, FUSELAGE SIDE, FWD 2 EA IAW CRJ 700 SRM 53-21-23-201-010-A01 TYPE I REPAIR ANS CRJ-700-SRM-51-12-00-001-001-A01.
- [SDR SWI2025F01561](https://openairdocs.org/sdr/SWI2025F01561.md): Hinge · damaged · Aug 28, 2025 · N759EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE, DOOR SIDE, THE FIRST LUG BORE HAS IMPACT DAMAGE/OVAL SHAPED NO THE FORWARD SIDE (MARKED) (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW PAX DOOR HINGE HALF. REF: CRJ-700 SRM 52-11-01-201-002-A01 AND DRAWING 601R31702 REV N, COMPLIED WITH SK
- [SDR SWI2025F01564](https://openairdocs.org/sdr/SWI2025F01564.md): Stiffener · loose · Aug 27, 2025 · N759EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL Z STIFFENER RIVETS ARE PULLED LOOSE (C-CHECK RO 11/22/2025)WET INSTALLED "Z" STIFFENER, -1 (REPAIR DOUBLER), -2 (SHIM), -3 (FILLER), AND -4 (EXTERNAL DOUBLER) TO R/H UPPER TRANSCOWL REF. MHIRJ REO 670-54-21-1759 REV. (--) DATED: 2025-09-0
- [SDR SWI2025F01563](https://openairdocs.org/sdr/SWI2025F01563.md): Stiffener · sheared · Aug 27, 2025 · N759EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 11/22/2025)REPAIRED R/H LOWER TRANSCOWL INNER SKIN AT SHEARED RIVETS COMMON TO ZED STIFFENER, REF. REO 670-54-21-1760, REV. --, 2025-09-15. COMPLIED WITH 51-900-1002 SKY
- [SDR SWI2025F01562](https://openairdocs.org/sdr/SWI2025F01562.md): Transcowl · cracked · Aug 27, 2025 · N759EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/22/2025)INSTALLED NEW I/B "A" BRACKET (PN CN624-2082-S1501) INTO L/H UPPER TRANSCOWL REF REO# 670-54-21-971, REV B, DATED 11/28/23. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED W/SK
- [SDR SWIA202511240827](https://openairdocs.org/sdr/SWIA202511240827.md): Transcowl · loose · Aug 27, 2025 · N759EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL Z STIFFENER RIVETS ARE LOOSE (C-CHECK RO 11/22/2025)REPAIRED LOOSE RIVETS ON THE "Z" STIFFENER AND CRACK TO THE PERFORATED SKIN OF THE L/H LOWER TRANSCOWL. ALL STEPS OF REO 670-54-21-1763 REV -- DATED 2025-09-10 AND REO 670-54-51-1763 REV
- [SDR SWI2025F01542](https://openairdocs.org/sdr/SWI2025F01542.md): Intercostal · corroded · Aug 26, 2025 · N759EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1 HAS CORROSION ON UNDERSIDE OF FLANGE CENTER OF DOOR (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1 FS323.00 -FS335.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 6
- [SDR SWI2025F01541](https://openairdocs.org/sdr/SWI2025F01541.md): Intercostal · corroded · Aug 26, 2025 · N759EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 HAS CORROSION MULTIPLE AREAS BOTH SIDES (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 FS320.00 -FS338.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV N
- [SDR SWI2025F01540](https://openairdocs.org/sdr/SWI2025F01540.md): Floor Support · corroded · Aug 26, 2025 · N759EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR BEAM LBL9.0 FWD OF FS685.00 IS CORRODED (C-CHECK RO 11/22/2025)REPAIRED FLOOR BEAM LBL9.0 BETWEEN FS613.0 - FS685.50 REF REO 670-53-31-1095 REV -A DATE 2025-11-06 DISPOSITION A TO C AND CRJ 700 SRM 53-00-41-201-001-A01. COMPLIED WITH ALL STEPS OF TASK
- [SDR SWI2025F01539](https://openairdocs.org/sdr/SWI2025F01539.md): Intercostal · corroded · Aug 26, 2025 · N759EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1A HAS CORROSION ON UNDERSIDE OF FLANGE CENTER OF DOOR (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1A FS323.00 -FS335.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING
- [SDR SWIA2025112400826](https://openairdocs.org/sdr/SWIA2025112400826.md): Intercostal · corroded · Aug 26, 2025 · N759EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 HAS CORROSION MULTIPLE AREAS BOTH SIDES (C-CHECK RO 11/22/2025)REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 FS320.00 - FS338.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV
- [SDR SWI2025F01569](https://openairdocs.org/sdr/SWI2025F01569.md): Slat Track · worn · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 3-3 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2203 REV-- DATED 2025-09-12 PERFORMED OPERATIONAL TEST OF THE FLAPS AND SLAT SYSTEM CRJ700 AMM 27-50-00-710-801-A02 TEST OK AT THIS MOMENTCOM
- [SDR SWI2025F01568](https://openairdocs.org/sdr/SWI2025F01568.md): Slat Track · corroded · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 3-2 HAS CORROSION IN MULTIPLE SPOTS, INCLUDING O/B SIDE. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2199 REV-- DATED 2025-06-12PERFORMED OPERATIONAL TEST OF THE FLAPS AND SLAT SYSTEM CRJ700 AMM 27-50-00-710-801-A02 TEST OK
- [SDR SWI2025F01567](https://openairdocs.org/sdr/SWI2025F01567.md): Slat Track · worn · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 3-1 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025) COMPLIED WITH REO 670-57-42-2200 REV-- DATED 2025-09-12 PERFORMED OPERATIONAL TEST OF THE FLAPS AND SLAT SYSTEM CRJ700 AMM 27-50-00-710-801-A02 TEST OK AT THIS MOMENT
- [SDR SWI2025F01566](https://openairdocs.org/sdr/SWI2025F01566.md): Slat Track · worn · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 2-2 HAS WEAR MARKS AND PITTING IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2210 REV-- DATED 2025-09-15. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 51-9
- [SDR SWI2025F01565](https://openairdocs.org/sdr/SWI2025F01565.md): Slat Track · worn · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 3-1 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2208 REV -- DATED 2025-09-15. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 27-900-1009-SK
- [SDR SWI2025F01579](https://openairdocs.org/sdr/SWI2025F01579.md): Slat Track · damaged · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 2-2 HAS PITTING IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2202 REV -- DATED 2025-09-12. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01578](https://openairdocs.org/sdr/SWI2025F01578.md): Slat Track · worn · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 1-1 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2197 REV-- DATED 2025-09-12 PERFORMED OPERATIONAL TEST OF THE FLAPS AND SLAT SYSTEM CRJ700 AMM 27-50-00-710-801-A02 TEST OK AT THIS MOMENTCO
- [SDR SWI2025F01577](https://openairdocs.org/sdr/SWI2025F01577.md): Slat Track · corroded · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 1-1 HAS PITTING AND CORROSION, INCLUDING I/B AND O/B SIDES. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2206 REV -- DATED 2025-09-15. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TAS
- [SDR SWI2025F01576](https://openairdocs.org/sdr/SWI2025F01576.md): Slat Track · worn · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 1-2 HAS WEAR MARKS AND PITTING IN MULTIPLE SPOTS, INCLUDING I/B AND O/B SIDES. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2207 REV-- DATED 2025-09-15. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLI
- [SDR SWI2025F01575](https://openairdocs.org/sdr/SWI2025F01575.md): Slat Track · corroded · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 2-3 HAS CORROSION ON THE INBOARD SIDE. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2212 REV -- DATED 2025-09-16. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 27-900-1009-SK
- [SDR SWI2025F01574](https://openairdocs.org/sdr/SWI2025F01574.md): Slat Track · worn · Aug 25, 2025 · N759EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 1-1 HAS WEAR MARKS IN MULTIPLE SPOTS. (MARKED) (C-CHECK RO 11/22/2025)COMPLIED WITH REO 670-57-42-2206 REV -- DATED 2025-09-15. OPS TEST GOOD AT THIS TIME PER CRJ700 AMM 27-50-00-710-801-A02. COMPLIED WITH SKYWEST TASK CARD 27-900-1009-SKY

Next page: https://openairdocs.org/aircraft/N759EV/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 = 'N759EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N759EV/reports

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