# Service difficulty reports: N713EV

A list on [N713EV](https://openairdocs.org/aircraft/N713EV.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 SWIA202504070002](https://openairdocs.org/sdr/SWIA202504070002.md): Landing Gear · faulted · Apr 2, 2025 · N713EV · Cndair CL6002C11 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING RECEIVED ON SELECTION OF GEAR HANDLE UP. MAIN GEAR REMAINED DOWN/GREEN, NOSE GEAR MAY HAVE HAD MOMENTARY TRANSIT INDICATION. SELECTED GEAR DOWN AND ALL REMAINED DOWN AND LOCKED. (FLIGHT 4290 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERR
- [SDR SWIA2025040300002](https://openairdocs.org/sdr/SWIA2025040300002.md): Warning Message · illuminated · Apr 2, 2025 · N713EV · Cndair CL6002C11 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING RECEIVED ON SELECTION OF GEAR HANDLE UP. MAIN GEAR REMAINED DOWN/GREEN, NOSE GEAR MAY HAVE HAD MOMENTARY TRANSIT INDICATION. SELECTED GEAR DOWN AND ALL REMAINED DOWN AND LOCKED. (FLIGHT 4290 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROG
- [SDR SWIA2024112500020](https://openairdocs.org/sdr/SWIA2024112500020.md): Skin · damaged · Nov 20, 2024 · N713EV · Cndair CL6002C11 · Trailing Edge Flaps
  > RH OTBD FLAP UNDER WING SKIN HAS CREASING DUE TO BIRD STRIKE DAMAGE. REPAIRED RH OTBD FLAP UNDER WING SKIN IAW SRM 57-53-01 TYPE 3 REPAIR.
- [SDR SWIA202411210001](https://openairdocs.org/sdr/SWIA202411210001.md): Skin · damaged · Nov 20, 2024 · N713EV · Cndair CL6002C11 · Trailing Edge Flaps
  > RH OTBD FLAP UNDER WING SKIN HAS CREASING DUE TO BIRD STRIKE DAMAGE. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024011800005](https://openairdocs.org/sdr/SWIA2024011800005.md): Windshield · delaminated · Jan 15, 2024 · N713EV · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT WINDSHIELD FOGGING ON EDGES ALL AROUND. (FLIGHT 3085 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27688183 WITH THE FOLLOWING CORRECTIVE ACTION: "FOUND RH WINDSHIELD TO HAVE DELAMINATION OUT OF LIMITS. REMOVED AND REPLACED RH WINDSHIELD IAW
- [SDR SWIA20231107010](https://openairdocs.org/sdr/SWIA20231107010.md): Unknown · corroded · Oct 10, 2023 · N713EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON FWD SIDE OF FRAME AT FS517, STGR 17L - 18L. (C-CHECK RO 11/10/2023) FS517 FRAME FOUND TO BE OUT OF LIMITS. MATERIAL IS MORE THEN 80% EXFOLIATED. REF CRJ700 SRM 53-31-06-101-002-A01. RECEIVED REO AND PERFORMED REPAIR TO LH FS517 FRAME SEG
- [SDR SWI2023F00474](https://openairdocs.org/sdr/SWI2023F00474.md): Unknown · corroded · Sep 21, 2023 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON LH WEB AT FS 280.00 (C-CHECK RO 11/10/2023) REMOVED AND REPLACED WITH NEW LH LOWER WEB AT FS 280.00 REF. CRJ 700 SRM 53-11-10-201-003-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWI2023F0000474](https://openairdocs.org/sdr/SWI2023F0000474.md): Unknown · corroded · Sep 21, 2023 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON LH WEB AT FS 280.00 (C-CHECK RO 11/10/2023) REMOVED AND REPLACED WITH NEW LH LOWER WEB AT FS 280.00 REF. CRJ 700 SRM 53-11-10-201-003-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWI2023F00470](https://openairdocs.org/sdr/SWI2023F00470.md): Unknown · corroded · Sep 18, 2023 · N713EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON R/H CROSSBEAM AT F.S 280.0 BULKHEAD (C-CHECK RO 11/10/2023) CORROSION AT R/H CROSSBEAM AT FS 280.0 IS OUT OF LIMITS. REMOVED AND INSTALLED NEW R/H CROSSBEAM AT FS 280.0 REF DWG CC670-34010 REV K, CRJ 700 SRM 51-42-13-001-001-A01, CRJ700
- [SDR SWIA202311070918](https://openairdocs.org/sdr/SWIA202311070918.md): Unknown · corroded · Sep 18, 2023 · N713EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON L/H CROSSBEAM AT F.S 280.0 BULKHEAD (C-CHECK RO 11/10/2023) REMOVED AND REPLACED LH FLOOR CROSS BEAM WITH NEW DUE TO OUT OF LIMIT CORROSION REF. CRJ 700 SRM 51-42-06-001-001-A01,CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-00
- [SDR SWI2023F00469](https://openairdocs.org/sdr/SWI2023F00469.md): Unknown · broken · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF BROKEN. (C-CHECK RO 11/10/2023) INSTALLED 1 EA. NEW STAND-OFF P/N 624-2082-201 ON L/H UPPER TRANS COWL REF. REO 670-54-21-971, REV. A, DATED 2017-05-11. COMPLIED WITH STEPS 1-3. COMPLIED WITH SKYCARD 51-900-100
- [SDR SWI2023F00468](https://openairdocs.org/sdr/SWI2023F00468.md): Unknown · cracked · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LOWER TRANSCOWL OUTBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 11/10/2023) REPLACED CRACKED O/B STAND-OFF ANGLE ("A" BRACKET) P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. A, 2017-05-11.C/W SKY CARD 51-900-1002-SKY
- [SDR SWI2023F00467](https://openairdocs.org/sdr/SWI2023F00467.md): Unknown · corroded · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Fuselage Main, Frame
  > *CORROSION NOTED ON FRAME 549 BETWEEN STRG25R-26L(MARKED), MX#27166285 (C-CHECK RO 11/10/2023) BLENDED CORROSION ON FRAME AT FS 549 BETWEEN STGR 25R - STGR 26L REF CRJ700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. RECEIVED REO AND PERFORMED REPAI
- [SDR SWI2023F00466](https://openairdocs.org/sdr/SWI2023F00466.md): Unknown · cracked · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 11/10/2023) REMOVED CRACKED STANDOFF, AND INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON R/H UPPER TRANSCOWL REF REO #670-54-21-971 REV (A) 2017-05-11 STEPS 1-3, AND CRJ
- [SDR SWI2023F00465](https://openairdocs.org/sdr/SWI2023F00465.md): Unknown · gouged · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *FWD BAG BAY THRESHOLD DOUBLER ASSY. GOUGED AT FWD AND AFT HINGE POINTS (MARKED), MX#27166428 (C-CHECK RO 11/10/2023) REMOVED DAMAGE ON FWD BAG BAY THRESHOLD DOUBLER ASSY. (INNER CLOSING SKIN) AT FWD AND AFT HINGE POINTS. REF. CRJ700 SRM 51-12-00-001-001-A
- [SDR SWI2023F00464](https://openairdocs.org/sdr/SWI2023F00464.md): Unknown · corroded · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Fuselage Main, Frame
  > *CORROSION NOTED ON FRAME 565BETWEEN STRG26R-26L(MARKED), MX#27166289 (C-CHECK RO 11/10/2023) BLENDED CORROSION ON FRAME AT FS 565 BETWEEN STGR 26L - STGR 26R REF CRJ700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR AT LOWER FRAME S
- [SDR SWI2023F00463](https://openairdocs.org/sdr/SWI2023F00463.md): Unknown · corroded · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR I/B MOUNTING ANGLE HAS CORROSION AT THE FWD LATCH FITTING (C-CHECK RO 11/10/2023) REMOVED AND REPLACED GALLEY SERVICE DOOR I/B MOUNTING ANGLE WITH NEW REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG #SH670-31950 REV.Y. COMPLIED WITH SKYWE
- [SDR SWI2023F00462](https://openairdocs.org/sdr/SWI2023F00462.md): Unknown · corroded · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *FWD BAG BAY FLOOR SUPPORT PLATE CORRODED BETWEEN STRG23L-22L AND AFT OF FRAME 581 (MARKED),MX#27166412 (C-CHECK RO 11/10/2023) BLENDED CORROSION ON FWD BAGGAGE BAY SUPPORT PLATE BETWEEN STGR 22L - STGR 23L AFT OF FRAME AT FS 581 REF CRJ700 SRM 51-21-06-00
- [SDR SWI2023F00461](https://openairdocs.org/sdr/SWI2023F00461.md): Unknown · corroded · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE FLOOR PANEL SUPPORT AT FS. 280.00 CROSSBEAM HAS CORROSION BETWEEN LBL9 AND RBL9. (C-CHECK RO 11/10/2023) REMOVED AND REPLACED ANGLE FLOOR PANEL SUPPORT AT FS. 280.00 BETWEEN LBL9 AND RBL9 WITH NEW REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-340
- [SDR SWIA202311070915](https://openairdocs.org/sdr/SWIA202311070915.md): Unknown · corroded · Sep 15, 2023 · N713EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *FWD BAG BAY SUPPORT PLATE CORRODED BETWEEN STRG22L-23L AND FWD OF FRAME 533 (MARKED), MX#27166390 (C-CHECK RO 11/10/2023) BLENDED CORROSION ON FWD BAGGAGE BAY SUPPORT PLATE BETWEEN STGR 22L - STGR 23L FWD OF FRAME AT FS 533 REF CRJ700 SRM 51-21-06-001-001
- [SDR SWIA202311070910](https://openairdocs.org/sdr/SWIA202311070910.md): Unknown · worn · Sep 10, 2023 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > R/H SLAT TRACK 3-1 HAS ABNORMAL WEAR ON UPPER AND LOWER SURFACE (MARKED) (C-CHECK RO 11/10/2023) REMOVED PITTING AT AREAS REF CRJ-700 SRM 51-12-00-001-001-A01. WITHIN LIMITS, REF REO 670-57-42-1440 DATE: 2023-09-22 REV --. COMPLIED WITH SKYWEST TASK CARD
- [SDR SWI2023F00471](https://openairdocs.org/sdr/SWI2023F00471.md): Unknown · chafed · Sep 9, 2023 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > *R/H SLAT TRACK 1-1 IS CHAFFED AT LOWER/OTBD SIDE AT ATTACHMENT POINT (MARKED), MX#27140153 (C-CHECK RO 11/10/2023) COMPLIED WITH ALL THE STEP OF REO 670-57-42-1437 REV-- DATED 2023-09-18,ENSURED BLEND OUT HAS SMOOTH CONTOUR, ENSURED COMPLETE DAMAGE REMOVA
- [SDR SWIA202311070909](https://openairdocs.org/sdr/SWIA202311070909.md): Unknown · worn · Sep 9, 2023 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > *R/H SLAT TRACK 1-2 HAS ABNORMAL WEAR ON UPPER AND LOWER SURFACE, MX#27140154 (C-CHECK RO 11/10/2023) REMOVED PITTING AT AREAS REF CRJ-700 SRM 51-12-00-001-001-A01. COMPLIED WITH REO 670-57-42-1026 REV-A DATED 2023-09-22. COMPLIED WITH SKYWEST TASK CARD 51
- [SDR SWI2023F00475](https://openairdocs.org/sdr/SWI2023F00475.md): Unknown · cracked · Sep 6, 2023 · N713EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD EQUIPMENT COMPARTMENT LH DOOR LANDING POSSIBLE CRACK AT AFT LATCH CUT-OUT (C-CHECK RO 11/10/2023) REMOVED L/H SIDE FWD EQUIPMENT COMPARTMENT DOOR LANDING REF CRJ 700 SRM 51-42-06-001-001-A01 AND WET INSTALLED NEW L/H SIDE FWD EQUIPMENT COMPARTMENT
- [SDR SWIA202311070906](https://openairdocs.org/sdr/SWIA202311070906.md): Unknown · cracked · Sep 6, 2023 · N713EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD EQUIPMENT COMPARTMENT RH DOOR LANDING POSSIBLE CRACK AT AFT LATCH CUT-OUT (C-CHECK RO 11/10/2023) REMOVED AND WET INSTALLED NEW RH DOOR LANDING FROM UPPER ELECTRIC BAY ACCESS DOOR FROM FS169 TO FS193 REF CRJ 700 SRM 51-42-06-001-001-A01, DWG NO CC6
- [SDR SWI2023F00473](https://openairdocs.org/sdr/SWI2023F00473.md): Unknown · cracked · Sep 5, 2023 · N713EV · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER TO FUSELAGE ATTACHMENT RH AFT DRAG ANGLE POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW RH AFT DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED WITH
- [SDR SWI2023F00472](https://openairdocs.org/sdr/SWI2023F00472.md): Unknown · cracked · Sep 5, 2023 · N713EV · Cndair CL6002C10 · Vertical Stabilizer
  > VERTICAL STABILIZER TO FUSELAGE ATTACHMENT RH FORWARD DRAG ANGLE POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW RH FWD DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED
- [SDR SWIA202311070905](https://openairdocs.org/sdr/SWIA202311070905.md): Unknown · cracked · Sep 5, 2023 · N713EV · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER TO FUSELAGE ATTACHMENT LH FORWARD DRAG ANGLE DOUBLER POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW LH FWD DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF CRJ700 SRM 55-31-00-201-001-A01 AND ALL STEP
- [SDR SWIA202157765](https://openairdocs.org/sdr/SWIA202157765.md): Skin · dented · Mar 27, 2021 · N713EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND DENT ON LH EXTERNAL SKIN AT FS501.00 BETWEEN STGR 19L AND STGR 20L. (C-CHECK RO 4/22/2021) COMPLIED WITH DENT REPAIR AT LH EXTERNAL SKIN FS501.00 BETWEEN STGR 19L AND STGR 20L REF-CRJ-700 REO 670-53-31-629 REV -- DATED 2021-04-08 & REO 670-51-00-0
- [SDR SWIA202157764](https://openairdocs.org/sdr/SWIA202157764.md): Doubler · chafed · Mar 12, 2021 · N713EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LH PYLON HYDRAULIC EDP PRESSURE LINE FIREWALL FITTING IS LOOSE AND CHAFING ON DOUBLER AND RIVETS. (C-CHECK RO 4/22/2021) REMOVED AND REPLACED WEB AND DOUBLER AT LH PYLON FIREWALL REF-CRJ-700 SRM 51-42-06-001-001 A01 AND DWG MM670-37001 REV AB. / COMPLI
- [SDR SWIA202157763](https://openairdocs.org/sdr/SWIA202157763.md): Frame · corroded · Mar 8, 2021 · N713EV · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S.319.70 FRAME SECTION FROM STGR18LTO STGR21L IS CORRODED. (C-CHECK RO 4/22/2021) REMOVED AND INSTALLED NEW FRAME SECTION FS319.70 FROM STGR18L TO STGR21L REF-CRJ-700 SRM 51-42-06-001-001 A01, SRM 51-42-21-001-001 A01 AND DWG SH670-31810 REV Y. LEAK C
- [SDR SWIA202157761](https://openairdocs.org/sdr/SWIA202157761.md): Striker · damaged · Mar 6, 2021 · N713EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LWR SEAL STRIKER'S FWD HOLE IS EXTREMELY ELONGATED. (C-CHECK RO 4/22/2021) REMOVED DAMAGED PAX DOOR LOWER SEAL STRIKER AND INSTALLED NEW PAX DOOR LOWER SEAL STRIKER P/N:SH670-31886-3S REF CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-31810
- [SDR SWIA202157760](https://openairdocs.org/sdr/SWIA202157760.md): Frame · corroded · Mar 6, 2021 · N713EV · Cndair CL6002C10 · Fuselage Main, Frame
  > RBL 9 BETWEEN F.S. 856.00 (SECTION AFT OF JOINT) AND F.S. 879.00 IS CORRODED BEYOND LIMITS AND REQUIRES REPAIR. (C-CHECK RO 4/22/2021) COMPLIED WITH RBL9 FLOOR BEAM FLANGE REPAIR BETWEEN FS863.00-FS879.00 REF-CRJ-700 SRM 53-00-41-201-001 A01 AND COMPLIE
- [SDR SWIA202157759](https://openairdocs.org/sdr/SWIA202157759.md): Stringer · damaged · Mar 5, 2021 · N713EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 19L AT F.S. 1051 HAS A MISSDRILLED HOLE AT STGR CLIP LOCATION. (C-CHECK RO 4/22/2021) REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 19L FROM FS977 TO FS1060 IAW CRJ700 SRM 53-00-03-201-001-A01 FIGURE 53-00-03-991-805 AND CRJ700 SRM 51-42-21-001-
- [SDR SWIA202157780](https://openairdocs.org/sdr/SWIA202157780.md): Stop · worn · Mar 3, 2021 · N713EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE BAY DOOR TRACK STOPS WORN BEYOND LIMITS (C-CHECK RO 4/22/2021) ORDERED AND RECEIVED 4 NEW AFT BAGGAGE DOOR TRACK STOPS. INSTALLED ON JOB 71008165 OP 53 CAMP 22340237
- [SDR SWIA202157758](https://openairdocs.org/sdr/SWIA202157758.md): Beam · corroded · Mar 3, 2021 · N713EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON LBL9 BEAM IN THE PAD UP AREA BETWEEN F.S. 863 AND F.S. 879. (C-CHECK RO 4/22/2021) REPAIRED DAMAGED LBL9 BEAM LOCATED BETWEEN FS863 & FS879 IAW CRJ 700 SRM 53-00-41-201-001-A01 & DWG SH670-37383 REV C, COMPLIED WITH TASK CARD 51-900-1
- [SDR SWIA202157757](https://openairdocs.org/sdr/SWIA202157757.md): Former · corroded · Mar 3, 2021 · N713EV · Cndair CL6002C10 · Fuselage Main, Frame
  > DURING OF REMOVAL OF INNER SKIN FOUND FWD FORMER FS 311.75 PN 601R318024-3 IS CORRODED AT UPPER TENSION ROD CUT OUT. (C-CHECK RO 4/22/2021) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER FS311.75 REF-CRJ-700 SRM 51-42-06-001-001 A01 AND DWG 601R318031
- [SDR SWIA202157756](https://openairdocs.org/sdr/SWIA202157756.md): Hinge · gouged · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > THE PASSENGER DOOR HINGE HALF, FUSELAGE SIDE, HAS SCRATCHES/GOUGES ON ALL LUG LANDS, AND THE FWD 5 LUGS HAVE SCRATCHES/GOUGES. (C-CHECK RO 4/22/2021) REMOVED AND INSTALLED NEW PAX DOOR FUSELAGE HINGE REF-CRJ-700 SRM 53-21-23-201-007 A01 AND DWG SH670-31
- [SDR SWIA202157755](https://openairdocs.org/sdr/SWIA202157755.md): Hinge · gouged · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > THE PASSENGER DOOR HINGE HALF, DOOR SIDE, HAS CRATCHES/GOUGES ON ALL LUGS, AND AN ELONGATED SLOTTED TUBULAR SPRING PIN HOLE ON ITS AFT LUG. (C-CHECK RO 4/22/2021) REMOVED DAMAGE AS REQUIRED FROM THE OUTER SURFACE OF EACH LUG ON THE PASSENGER DOOR SIDE
- [SDR SWIA202157754](https://openairdocs.org/sdr/SWIA202157754.md): Skin · dented · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Trailing Edge Flaps
  > * LH INBD FLAP LOWER SKIN HAS 2 DENTS (MARKED) (C-CHECK RO 4/22/2021) NDT DENTS DEFECT FREE. EVAL INBD DENT IS WITHIN LIMITS. EVAL OTBD DENT IS OUT OF LIMITS. RECEIVED ENGINEERING DISPOSITION TO REPAIR SKIN FOR LH I/B FLAP LWR SKIN. REPAIRED DAMAGE
- [SDR SWIA202157753](https://openairdocs.org/sdr/SWIA202157753.md): Slat Track · corroded · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 3-2 CORRODED (C-CHECK RO 4/22/2021) COMPLIED WITH REO 670-57-42-1028 REV -- DATED 2021-03-09 AND CARD 51-900-1002-SKY
- [SDR SWIA202157752](https://openairdocs.org/sdr/SWIA202157752.md): Slat Track · corroded · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 2-2 CORRODED (C-CHECK RO 4/22/2021) REMOVED CORROSION ON RH SLAT TRACK 2-2 AND COMPLIED WITH THE TEMPORARY DISPOSITION OF REF REO 670-57-42-1031 REV -- DATED 2021-03-11 AND COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. / REINSPECTION RE
- [SDR SWIA202157751](https://openairdocs.org/sdr/SWIA202157751.md): Slat Track · corroded · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > * RH SLAT TRACK 1-2 CORRODED (C-CHECK RO 4/22/2021) AFTER BLENDED AREAS RH SLAT TRACK 1-2 ARE FOUND WITHIN TOLERANCE LIMITS REF-CRJ-700 REO 670-57-42-1026 REV -- DATED 2021-03-09, OPS/CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. / COMPLIED WITH TASK 5
- [SDR SWIA202157750](https://openairdocs.org/sdr/SWIA202157750.md): Slat Track · corroded · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > * RH SLAT TRACK 1-1 HAS WEAR MARKS AND IS CORRODED (C-CHECK RO 4/22/2021) AFTER BLENDED AREAS RH SLAT TRACK 1-1 ARE FOUND WITHIN TOLERANCE LIMITS REF-CRJ-700 REO 670-57-42-1025 REV -- DATED 2021-03-09, OPS/CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202157749](https://openairdocs.org/sdr/SWIA202157749.md): Slat Track · corroded · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 3-2 CORRODED (C-CHECK RO 4/22/2021) COMPLIED WITH REO 670-57-42-1024REV-- DATED2021-03-08 AND CARD 51-900-1002-SKY OPS CHECK GOOD AT THIS TIME
- [SDR SWIA202157748](https://openairdocs.org/sdr/SWIA202157748.md): Slat Track · corroded · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 2-2 CORRODED (C-CHECK RO 4/22/2021) AFTER BLENDED AREAS LH SLAT TRACK 2-2 ARE FOUND WITHIN TOLERANCE LIMITS REF-CRJ-700 REO 670-57-42-1023 REV -- DATED 2021-03-08, OPS/CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. / COMPLIED WITH TASK 51-
- [SDR SWIA202157747](https://openairdocs.org/sdr/SWIA202157747.md): Slat Track · corroded · Feb 23, 2021 · N713EV · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 1-2 CORRODED (C-CHECK RO 4/22/2021) AFTER BLENDED AREAS LH SLAT TRACK 1-2 ARE FOUND WITHIN TOLERANCE LIMITS REF-CRJ-700 REO 670-57-42-1022 REV -- DATED 2021-03-08, OPS/CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. / COMPLIED WITH TASK 51-
- [SDR SWIA202157779](https://openairdocs.org/sdr/SWIA202157779.md): Seat Track · corroded · Feb 21, 2021 · N713EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > * THE PASSENGER CABIN SEAT RAIL ON RBL 9 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 394 AND APPROX. FS 469. (C-CHECK RO 4/22/2021) INSTALLED NEW SEAT RAIL AT RBL 9.0 FROM FS394.00-FS469.00 P/N SH670-32159-1 REF C
- [SDR SWIA202157778](https://openairdocs.org/sdr/SWIA202157778.md): Seat Track · corroded · Feb 21, 2021 · N713EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE PASSENGER CABIN SEAT RAIL ON LBL 9 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 394 AND APPROX. FS 469. (C-CHECK RO 4/22/2021) FABRICATED AND INSTALLED NEW LBL9 SEAT TRACK P/N SH670-32249-1 FROM FS394 TO FS469
- [SDR SWIA202157777](https://openairdocs.org/sdr/SWIA202157777.md): Seat Track · corroded · Feb 21, 2021 · N713EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE PASSENGER CABIN SEAT RAIL ON LBL 27 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 394 AND APPROX. FS 469. (C-CHECK RO 4/22/2021) REPLACED SEAT TRACK FROM FS394-FS485 LBL 27 WITH NEW REF CRJ-700 AMM 53-00-49-400-

Next page: https://openairdocs.org/aircraft/N713EV/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 = 'N713EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N713EV/reports

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