# Service difficulty reports: N723EV

A list on [N723EV](https://openairdocs.org/aircraft/N723EV.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 · 250 reports

- [SDR SWIA2026091477153](https://openairdocs.org/sdr/SWIA2026091477153.md): Windshield · failed · Sep 14, 2026 · N723EV · Cndair CL6002C11 · Flight Compartment Windows
  > FO FRONT WINDSHIELD SHATTERED, FLIGHT 5296. REMOVED AND REPLACED THE FOS WINDSHIELD IAW AMM 56-11-01 OPS CHECK GOOD. PLEASE REF EAML 1993078 FOR PRESSURIZATION AND LEAK CHECK.
- [SDR SWIA202507210416](https://openairdocs.org/sdr/SWIA202507210416.md): Frame · corroded · Apr 16, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS 1051.30 CORRODED BETWEEN STGR 27 AND STGR 25LH #29987334 (C-CHECK RO 07/18/2025)REPAIRED FRAME AT FS1051.30 BETWEEN STGR 27 AND STGR 25LH IAW REO 670-53-61-2500 REV -- 2025-05-26. COMPLIED WITH ALL STEPS OF REO 670-53-61-2500 REV -- 2025-05-26. CO
- [SDR SWIA202507210413](https://openairdocs.org/sdr/SWIA202507210413.md): Window Post · damaged · Apr 13, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT WINDSHIELD POST FITTING PN: GC212-0046-4, WHEN REMOVED FOUND FASTENERS HOLES PREVIOUSLY COUNTER SUNK, BUT REQUIRE PROTRUDING HEAD FASTENERS NOT FLUSH FASTENERS. REPLACE PARTS. REPLACED RH WINDSHIELD POST FITTING PN: GC212-0046-4 WITH NEW IAW SRM 51-42-2
- [SDR SWI2025F01014](https://openairdocs.org/sdr/SWI2025F01014.md): Cleat · corroded · Mar 17, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > (MX 29809807) CORROSION NOTED ON PAX DOOR CLEAT OF FORMER FS329.41 AND DD6 INTERCOSTAL (C-CHECK RO 07/18/2025)INSTALLED NEW PAX DOOR CLEAT OF FORMER FS329.41 AND DD6 INTERCOSTAL. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. LEAK CHECK GOOD
- [SDR SWI2025F01013](https://openairdocs.org/sdr/SWI2025F01013.md): Support Angle · corroded · Mar 17, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > (MX 29814919) CORROSION NOTED ON PAX DOOR FWD ANGLE SUPPORT. (C-CHECK RO 07/18/2025) INSTALLED NEW PAX DOOR FWD ANGLE SUPPORT P/N 601R318731-3. IAW. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKY
- [SDR SWIA20250721001](https://openairdocs.org/sdr/SWIA20250721001.md): Intercostal · corroded · Mar 17, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > (MX 29815563) CORROSION NOTED ON INTERCOSTAL FWD DD3 CLIP (C-CHECK RO 07/18/2025)REMOVED AND REPLACED PAX DOOR INTERCOSTAL FWD DD3 CLIP REF CRJ700 SRM 51-42-06-001-001-A01, AND DWG 601R31702 REV. N.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. ALL CHECKS G
- [SDR SWIA202507210317](https://openairdocs.org/sdr/SWIA202507210317.md): Frame · corroded · Mar 17, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON INBOARD UPPER FLANGE OF RBL9 AT FS 549. PERFORMED FLANGE REPAIR ON INBOARD UPPER FLANGE OF RBL9 AT FS 549 INSTALLED ANGLE (18), FILLER (23) AND SHIM (19) REF CRJ700 SRM 53-00-41-201-001-A01AND COMPLIED WITH ALL THE STEPS OF THE REO 670-53
- [SDR SWIA202507210315](https://openairdocs.org/sdr/SWIA202507210315.md): Floor Support · corroded · Mar 15, 2025 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RBL9 FLOOR BEAM BETWEEN FS847 AND FS863. (C-CHECK RO 07/18/2025)REMOVED AND REPLACED RBL9 FLOOR BEAM BETWEEN FS847 AND FS863 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-35920 REV. M ALL CHECKS GOOD
- [SDR SWI2025F01040](https://openairdocs.org/sdr/SWI2025F01040.md): Intercostal · corroded · Mar 14, 2025 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ( MX 29796801) CORROSION NOTED ON INTERCOSTAL FWD DD7 CLIP (C-CHECK RO 07/18/2025)INSTALLED NEW INTERCOSTAL FWD DD7 CLIP. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWIA202507210314](https://openairdocs.org/sdr/SWIA202507210314.md): Intercostal · corroded · Mar 14, 2025 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ( MX 29796784) CORROSION NOTED ON INTERCOSTAL FWD DD1 CLIP (C-CHECK RO 07/18/2025)INSTALLED NEW INTERCOSTAL FWD DD1 CLIP. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWI2025F01027](https://openairdocs.org/sdr/SWI2025F01027.md): Former · corroded · Mar 13, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > (MX 29789716) PAX DOOR FORMER F/S 311.75 IS CORRODED AT DD1 AND DD6 LOCATION (C-CHECK RO 07/18/2025)REMOVED AND REPLACED PAX DOOR AFT FORMER FS. 311.75 AT DD1 AND DD6 LOCATION IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. AND DWG 6
- [SDR SWI2025F01026](https://openairdocs.org/sdr/SWI2025F01026.md): Floorbeam · corroded · Mar 13, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON INBOARD UPPER FLANGE ON FLOORBEAM LBL 9 AT FS 549 (C-CHECK RO 07/18/2025)COMPLIED WITH ALL STEPS OF REO 670-53-31-1022 REV-- DATE 2025-04-02, AND REO 670-53-31-1020 REV -- 2025-04-14 IN THE REPAIR ON INBD UPPER FLANGE ON FLOORBEAM LBL9 AT
- [SDR SWI2025F01025](https://openairdocs.org/sdr/SWI2025F01025.md): Intercostal · corroded · Mar 13, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > (MX 29789703) CORROSION NOTED AT PAX DOOR FWD INTERCOSTAL DD3 (C-CHECK RO 07/18/2025)INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD3. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. LEAK CHECK GOOD, COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01024](https://openairdocs.org/sdr/SWI2025F01024.md): Intercostal · corroded · Mar 13, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > (MX 29789709) CORROSION NOTED AT PAX DOOR FWD INTERCOSTAL DD2 (C-CHECK RO 07/18/2025)INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD2. IAW. CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA202507210313](https://openairdocs.org/sdr/SWIA202507210313.md): Angle · corroded · Mar 13, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > (MX 29789718) CORROSION NOTED AT PAX DOOR ANGLE BETWEEN FORMER FS. 327.963 AND FRAME FS. 327.763 LINE DD7A. (C-CHECK RO 07/18/2025)INSTALLED NEW PAX DOOR ANGLE P/N 601R317052-1, BETWEEN FORMER FS. 327.763 AND FRAME FS. 338.963 LINE DD7A. IAW. CRJ700 SRM 51
- [SDR SWIA2025072100312](https://openairdocs.org/sdr/SWIA2025072100312.md): Intercostal · cracked · Mar 12, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR SUSSPECTED CRACK ON AFT DD7 INTERCOSTAL. INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD7. IAW SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWI2025F01039](https://openairdocs.org/sdr/SWI2025F01039.md): Stringer · corroded · Mar 6, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R HAS CORROSION BETWEEN FS295 - FS310 (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW AVIONICS BAY STRINGER 24R BETWEEN FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH T
- [SDR SWIA202507210306](https://openairdocs.org/sdr/SWIA202507210306.md): Stringer · damaged · Mar 6, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF PREVIOUS REPAIR DOUBLER AT FS293 - FS312 BETWEEN 2" ABOVE STR 24R AND 2" BELOW STR 25R FOR ACCESS TO REPLACE STRINGER 25R (CAMP 29634791 JOB HN00220902) FOUND UNDERLYING SKIN DAMAGE (C-CHECK RO 07/18/2025)REPAIRED DAMAGED SKIN AT FS293 - FS312
- [SDR SWI2025F01036](https://openairdocs.org/sdr/SWI2025F01036.md): Web · cracked · Feb 19, 2025 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PREVIOUS REPAIR OF THE TRU BAY FLOOR SKIN AT THE ADG HYD PUMP HAS A CRACK IN THE RADIUS AROUND THE FS192.5 FRAME. (MARKED) (C-CHECK RO 07/18/2025)PERFORMED REPAIR OF TRU BAY DOOR FLOOR SKIN AT FS 193 RHS PER REO 670-53-11-509 REV E DATED 2018-02-08 ALL STEPS
- [SDR SWI2025F01035](https://openairdocs.org/sdr/SWI2025F01035.md): Fitting · cracked · Feb 19, 2025 · N723EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > LEFT PYLON SS DOUBLER HAS MULTIPLE CRACKS RADIATING FROM AROUND THE FITTING FOR THE ENGINE DRIVEN PUMP PRESSURE LINE, UNDER PANEL 412BB, 412BT & 412CT. (MARKED) (C-CHECK RO 07/18/2025)REMOVED AND REPLACED DOUBLER ON PYLON FIREWALL WEB WITH NEW P/N MM670-37001
- [SDR SWIA202507210219](https://openairdocs.org/sdr/SWIA202507210219.md): Web · cracked · Feb 19, 2025 · N723EV · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > LEFT PYLON SS WEB HAS MULTIPLE CRACKS RADIATING FROM AROUND THE FITTING FOR THE ENGINE DRIVEN PUMP PRESSURE LINE, UNDER PANEL 281AZ. (MARKED) (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW FIREWALL WEB ON LH ENGINE PYLON BETWEEN FS 1069 AND FS 1088 PER REF
- [SDR SWIA20250218](https://openairdocs.org/sdr/SWIA20250218.md): Attach Angle · corroded · Feb 18, 2025 · N723EV · Cndair CL6002C10 · Wing, Attach Fittings
  > SURFACE CORROSION ON LEFT REAR SPAR ATTACH ANGLE FOR TIRE BURST PANEL 542AZ (C-CHECK RO 07/18/2025)REPLACED LEFT REAR SPAR ATTACH ANGLE FOR TIRE BURST PANEL 542AZ REF. CRJ 700 SRM 51-42-21-001-001-A01 AND DWG # CC670-10320 REV: F. COMPLIED WITH ALL STEPS OF
- [SDR SWI2025F01043](https://openairdocs.org/sdr/SWI2025F01043.md): Stringer · corroded · Feb 14, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > AVIONICS BAY STRINGER 23R BETWEEN FS310 - FS319 IS CORRODED (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW AVIONICS BAY STRINGER 23R BETWEEN FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, DWG SH670-31630 REV K AND REO 670-53-2
- [SDR SWIA202507210214](https://openairdocs.org/sdr/SWIA202507210214.md): Stringer · corroded · Feb 14, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > AVIONICS BAY STRINGER 26L BETWEEN FS280- FS295 IS CORRODED (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW STRINGER 26L FROM FS280- FS333 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH TASK CA
- [SDR SWI2025F01034](https://openairdocs.org/sdr/SWI2025F01034.md): Frame · corroded · Feb 13, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME F/S 319 IS CORRODED AT STRG 27 (MX 29634776) (C-CHECK RO 07/18/2025)INSTALLED NEW LOWER FRAME SECTION FS319 BETWEEN STR 23R - STR 21L REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV KCOMPLIED WITH SKYWEST TASK C
- [SDR SWI2025F01033](https://openairdocs.org/sdr/SWI2025F01033.md): Intercostal · corroded · Feb 13, 2025 · N723EV · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION NOTED ON PAX DOOR INTERCOSTAL MID DD6 (MARKED) (C-CHECK RO 07/18/2025)REMOVED AND REPLACED PAX DOOR INTERCOSTAL MID DD6 REF CRJ700 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD.
- [SDR SWI2025F01032](https://openairdocs.org/sdr/SWI2025F01032.md): Stringer Clip · corroded · Feb 13, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > STRINGER CLEAT AT 21R FS333 IS CORRODED (MX 29635322) (C-CHECK RO 07/18/2025)INSTALLED NEW STRINGER CEAT 21R AT FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-32600 REV AK. COMPLIED WITH SKYWEST TASK CARD 51
- [SDR SWI2025F01031](https://openairdocs.org/sdr/SWI2025F01031.md): Stringer · corroded · Feb 13, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRIGER 25R IS CORRODED BETWEEN F/S 280 AND F/S 295 (MX 29634791) (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW STRINGER 25R FROM FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH
- [SDR SWI2025F01030](https://openairdocs.org/sdr/SWI2025F01030.md): Window Post · cracked · Feb 13, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Structure
  > R/H WINDSHIELD POST IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW RH WINDSHIELD POST REF CRJ 700SRM 51-42-21-001-001-A01, DWG. CC670-33055 REV. F, AND REO 670-53-11-2126 REV. A. DATE: 2025-04-25. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE
- [SDR SWIA202507210213](https://openairdocs.org/sdr/SWIA202507210213.md): Cleat · corroded · Feb 13, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > STRINGER CLEAT AT 23R FS319 IS CORRODED (C-CHECK RO 07/18/2025)STRINGER CLEAT AT 23R FS319 IS FOUND TO BE OUT OF LIMITS 100% MATERIAL LOSS REFCRJ-700 SRM 53-21-03-101-002-A01REMOVED AND REPLACED STRINGER CLEAT P/N SH670-35625-1 AT 23R FS319 REF CRJ-700 SRM 51
- [SDR SWIA20250209](https://openairdocs.org/sdr/SWIA20250209.md): Hinge · gouged · Feb 9, 2025 · N723EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE ( FUSELAGE SIDE) AFT MOST LUG LAND IS GOUGED. HN00219949 (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE ON THE FUSELAGE SIDE REF CRJ 700 SRM 53-21-23-201-007-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 REV. 38 DATED JUL 25/
- [SDR SWIA202507210207](https://openairdocs.org/sdr/SWIA202507210207.md): Hinge · gouged · Feb 7, 2025 · N723EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE LUG NUMBER 1 AND 7 GOUGED (FROM FORWARD SIDE OF DOOR) (C-CHECK RO 07/18/2025)REMOVED AND REPLACED PASSENGER DOOR PIANO HINGE REF. CRJ700 SRM 52-11-01-201-002-A01, CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AN
- [SDR SWIA202507210205](https://openairdocs.org/sdr/SWIA202507210205.md): Skin · scratched · Feb 5, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FORWARD DRAIN MAST EXTERIOR SKIN PENETRATION FORWARD INBOARD FASTENER HOLE HAS MULTIPLE SCRATCHES AFT OF FS333.00 BETWEEN STGR25R - STGR24R (C-CHECK RO 07/18/2025)COMPLIED WITH REO 670-53-21-2588 REV -- DATED 2025-03-12 REPAIR FORWARD DRAIN MAST EXTERIOR SK
- [SDR SWI2025F01019](https://openairdocs.org/sdr/SWI2025F01019.md): Skin · debonded · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Ailerons
  > LH AILERON OUTBD EDGE CORNER. DISBONDED. (C-CHECK RO 07/18/2025)REMOVED AND REPLACED RUBBING BLOCK PN: CC670-13076-3 REF. CRJ 700 SRM 51-42-13-001-001-A01, INSTALLED NEW LH AILERON O/B RIB REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01
- [SDR SWI2025F01018](https://openairdocs.org/sdr/SWI2025F01018.md): Stand Off · cracked · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)INSTALLED NEW R/H UPPER TRANSCOWL I/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD
- [SDR SWI2025F01017](https://openairdocs.org/sdr/SWI2025F01017.md): Stand Off · cracked · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-9
- [SDR SWI2025F01016](https://openairdocs.org/sdr/SWI2025F01016.md): Stiffener · sheared · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > R/H LWR TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 07/18/2025)ON R/H LOWER TRANSCOWL, 3 EA. FASTENER HOLES COMMON TO ZED STIFFENER P/N CN624-2038-203 ON INNER SKIN FOUND TO BE CRACK FREE WITH NO DAMAGE NOTED. ENGINEERING REQUIRED FOR ALTERNATE METH
- [SDR SWI2025F01015](https://openairdocs.org/sdr/SWI2025F01015.md): Stand Off · cracked · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51
- [SDR SWI2025F01023](https://openairdocs.org/sdr/SWI2025F01023.md): Stand Off · cracked · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED CRACKED INBD "A" STANDOFF FROM L/H LOWER TRANSCOWL AND INSTALLED 1 EA NEW INBD STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANSCOWL REF GREO #670-54-21-971 REV (-B) 2023-11-2
- [SDR SWI2025F01022](https://openairdocs.org/sdr/SWI2025F01022.md): Channel · corroded · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT WATER DRAIN MAST CHANNEL (C-CHECK RO 07/18/2025)INSTALLED AFT DRAIN MAST CHANNEL REF SRM 51-42-06-001-001-A01,DWG:MM670-43200 REV NC. PRESSURE CHECK AND OPS CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01021](https://openairdocs.org/sdr/SWI2025F01021.md): Stand Off · cracked · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED CRACKED OUTBD "A" STANDOFF FROM L/H LOWER TRANSCOWL AND INSTALLED 1 EA NEW OUTBD STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANSCOWL REF GREO #670-54-21-971 REV (-B) 2023-11
- [SDR SWI2025F01020](https://openairdocs.org/sdr/SWI2025F01020.md): Stand Off · cracked · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900
- [SDR SWI20250721015](https://openairdocs.org/sdr/SWI20250721015.md): Stand Off · cracked · Feb 4, 2025 · N723EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51
- [SDR SWI2025F01012](https://openairdocs.org/sdr/SWI2025F01012.md): Fitting · crushed · Feb 3, 2025 · N723EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE-BAY DOOR, AFT CROTCH FITTING SMASHED, INBOARD SIDE OF FITTING, HN00218513 (C-CHECK RO 07/18/2025)COMPLIED WITH REO 670-53-61-2481 REV --, DATED 2025-03-19 STEPS 1-7. REF CRJ700 SRM 51-12-00-001-001-A01 REV.38 DATED JUL/25/2020. COMPLIED WITH
- [SDR SWI2025F01011](https://openairdocs.org/sdr/SWI2025F01011.md): Door Sill · chafed · Feb 3, 2025 · N723EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING AUDIT OF 1C TASK CARD 53-280-507 (DETAILED INSPECTION OF THE EXTERNAL FACE OF THE SILL, EDGE FRAMES, AND DOOR FITTINGS AROUND THE AFT BAGGAGE-BAY DOOR CUTOUT EXCEPT THE AREA UNDER THE PROTECTOR PLATE), FOUND CHAFFING ON THE LOWER FWD EDGE FRAME OF AFT C
- [SDR SWI2025F01010](https://openairdocs.org/sdr/SWI2025F01010.md): Fitting · crushed · Feb 3, 2025 · N723EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE-BAY DOOR, FORWARD CROTCH FITTING SMASHED, INBOARD SIDE OF FITTING, HN00218512 (C-CHECK RO 07/18/2025)REMOVED DAMAGE ON AFT BAGGAGE-BAY DOOR, FORWARD CROTCH FITTING, INBOARD SIDE OF FITTING. REF CRJ700 SRM 51-12-00-001-001-A01 AND PERFORMED REPAI
- [SDR SWI2025F01009](https://openairdocs.org/sdr/SWI2025F01009.md): Stringer · corroded · Feb 3, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR25R BETWEEN FS 319.7 AND FS333.0 AS MARKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED WITH NEW STRINGER SPLICE P/N SH670-32429-4 AT STR 25R FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV EPERFORMED PRESSURE LEAK CHECKREF
- [SDR SWI2025F01008](https://openairdocs.org/sdr/SWI2025F01008.md): Frame · corroded · Feb 3, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FS 310.0 FORWARD FLANGE BETWEEN STGR27 AND STGR26R AS MARKED (C-CHECK RO 07/18/2025)REMOVED AND REPLACED WITH NEW LOWER FRAME SECTION P/N SH670-31354-3 AND FRAME SPLICES AT FS310 FROM STR 25R TO STR 25L REF CRJ-700 SRM 53-00-06-201-006-A01 COM
- [SDR SWI2025F01007](https://openairdocs.org/sdr/SWI2025F01007.md): Stop · worn · Feb 3, 2025 · N723EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE-BAY DOOR, FORWARD LOWER STOP FITTING WORN, HN00218516 (C-CHECK RO 07/18/2025)REMOVED DAMAGE ON AFT BAGGAGE-BAY DOOR, FORWARD LOWER STOP FITTING. REF CRJ700 SRM 51-12-00-001-001-A01. AND REPAIRED PER REO 670-53-61-2481 REV --, DATED 2025-03-19.
- [SDR SWI2025F01006](https://openairdocs.org/sdr/SWI2025F01006.md): Skin · corroded · Feb 3, 2025 · N723EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN BETWEEN FS295.0 AND FS310. STGR27 AND STGR26R AS MARKED (C-CHECK RO 07/18/2025)REPAIRED CORROSION ON SKIN BETWEEN FS295.0 AND FS310. STGR27 AND STGR26R IAW REO 670-53-21-2585 REV -- DATED 2025-03-18. COMPLIED WITH ALL STEPS OF REO 670-53-2

Next page: https://openairdocs.org/aircraft/N723EV/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 = 'N723EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N723EV/reports

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