# Service difficulty reports: N720EV

A list on [N720EV](https://openairdocs.org/aircraft/N720EV.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 · 261 reports

- [SDR SWI2025F01519](https://openairdocs.org/sdr/SWI2025F01519.md): Unknown · smoke · Nov 1, 2025 · N720EV · Cndair CL6002C10 · Air Distribution System
  > DUE TO SMOKE FILLED CABIN ODI EVENT, MECHANICS RECOMENDED A COMP WASH DURING THE BORROSCOPE PROCEDURE. (FLIGHT 6512) TROUBLESHOT WRITE UP FOR CABIN SMOKE AND OR ELECTRICAL BURNING ODOR IAW FIM 21-21-00-810-806, FIM 21-22-00-810-806 AND FIM 79-30-00-810-821.
- [SDR SWI2025F01466](https://openairdocs.org/sdr/SWI2025F01466.md): Unknown · smoke · Nov 1, 2025 · N720EV · Cndair CL6002C10 · Air Distribution System
  > DUE TO SMOKE FILLED CABIN ODI EVENT, MECHANICS RECOMENDED A COMP WASH DURING THE BORROSCOPE PROCEDURE. (FLIGHT 6512) TROUBLESHOT WRITE UP FOR CABIN SMOKE AND OR ELECTRICAL BURNING SMELL IAW CRJ 700 FIM 21-21-00-810-806 AND FIM 21-22-00-810-806 AND FIM 79-30-0
- [SDR SWI2024F01214](https://openairdocs.org/sdr/SWI2024F01214.md): Fitting · damaged · Aug 22, 2024 · N720EV · Cndair CL6002C10 · Trailing Edge Flaps
  > L/H I/B FLAP- I/B WING LUG FITTING- CENTER INBOARD LUG IS DAMAGED (ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED CLOSED)EVALUATED AND REPAIRED DAMAGE ON LH INBD FLAP-INBD WING LUG FITTING-CENTER INBD LUG IAW CRJ700 SRM 57-21-27, 51-12-00. NDT PERFORMED BY BARON
- [SDR SWI2024F01213](https://openairdocs.org/sdr/SWI2024F01213.md): Fitting · damaged · Aug 22, 2024 · N720EV · Cndair CL6002C10 · Trailing Edge Flaps
  > L/H I/B FLAP- I/B WING LUG FITTING- CENTER OUTBOARD LUG IS DAMAGED-(ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED CLOSED)REPAIRED DAMAGE ON LH IB FLAP, IB WING LUG FITTING, CENTER OTBD LUG IAW CRJ700 SRM 51-21-27, SRM 51-12-00, AND REO 670-57-21-993 REV-- DATE
- [SDR SWI2024F01212](https://openairdocs.org/sdr/SWI2024F01212.md): Fitting · damaged · Aug 22, 2024 · N720EV · Cndair CL6002C10 · Trailing Edge Flaps
  > R/H I/B FLAP- IB WING LUG FITTING- CENTER OUTBOARD FITTING IS DAMAGED (ROLLED OVER METAL ON EDGE) (C-CHECK RO 10/28/2024) (FILED CLOSED)PERFORMED REPAIR ON R/H IB FLAP IB WING LUG FITTING CENTER OB FITTING PER MHIRJ REO 670-57-21-992. REV.--. DATE: 2024-09-16
- [SDR SWIA2024F01071](https://openairdocs.org/sdr/SWIA2024F01071.md): Lug · damaged · Aug 22, 2024 · N720EV · Cndair CL6002C10 · Trailing Edge Flaps
  > L/H I/B FLAP- I/B WING LUG FITTING- CENTER INBOARD LUG IS DAMAGED (ROLLED METAL) (C-CHECK RO 10/28/2024) (FILED OPEN)EVALUATED AND REPAIRED DAMAGE ON LH INBD FLAP-INBD WING LUG FITTING-CENTER INBD LUG IAW CRJ700 SRM 57-21-27, 51-12-00. NDT PERFORMED BY BARON N
- [SDR SWIA20241029822](https://openairdocs.org/sdr/SWIA20241029822.md): Lug · damaged · Aug 22, 2024 · N720EV · Cndair CL6002C10 · Trailing Edge Flaps
  > R/H I/B FLAP- IB WING LUG FITTING- CENTER OUTBOARD FITTING IS DAMAGED (ROLLED OVER METAL ON EDGE) (C-CHECK RO 10/28/2024) (FILED OPEN)PERFORMED REPAIR ON R/H IB FLAP IB WING LUG FITTING CENTER OB FITTING PER MHIRJ REO 670-57-21-992. REV.--. DATE: 2024-09-16 A
- [SDR SWIA202411120820](https://openairdocs.org/sdr/SWIA202411120820.md): Floor Support · corroded · Aug 20, 2024 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH PRESSURE SILL AT FS773.50 HAS SIGNS OF CORROSION ON THE FLOOR ANGLE (C-CHECK RO 10/28/2024) (FILED CLOSED)REMOVED CORROSION AND EVALUATED AREA ON RH PRESSURE SILL AT FS773.50 THE FLOOR ANGLE, NOMINAL THICKNEES 0.125", MATERIAL REMAINING 0.124", FOUND WITHIN
- [SDR SWIA20241029820](https://openairdocs.org/sdr/SWIA20241029820.md): Floor Support · corroded · Aug 20, 2024 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH PRESSURE SILL AT FS773.50 HAS SIGNS OF CORROSION ON THE FLOOR ANGLE (C-CHECK RO 10/28/2024) (FILED OPEN)REMOVED CORROSION AND EVALUATED AREA ON RH PRESSURE SILL AT FS773.50 THE FLOOR ANGLE, NOMINAL THICKNEES 0.125", MATERIAL REMAINING 0.124", FOUND WITHIN L
- [SDR SWIA202411120810](https://openairdocs.org/sdr/SWIA202411120810.md): Drag Angle · cracked · Aug 10, 2024 · N720EV · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF THE VERTICAL STABILIZER RH SIDE IS CRACKED (C-CHECK RO 10/28/2024) (FILED CLOSED)PERFORMED REPAIR ON RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF VERTICAL STABILIZER RH SIDE PER BOMBARDIER REO 670-55-31-018. REV
- [SDR SWIA20241029810](https://openairdocs.org/sdr/SWIA20241029810.md): Drag Angle · cracked · Aug 10, 2024 · N720EV · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF THE VERTICAL STABILIZER RH SIDE IS CRACKED (C-CHECK RO 10/28/2024) (FILED OPEN)PERFORMED REPAIR ON RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF VERTICAL STABILIZER RH SIDE PER BOMBARDIER REO 670-55-31-018. REV.-
- [SDR SWIA202265391](https://openairdocs.org/sdr/SWIA202265391.md): None · cracked · Apr 18, 2022 · N720EV · Cndair CL6002C10 · Window/Windshield System
  > FO SIDE OUTER WINDSHIELD CRACKED AT CRUISE. (FLIGHT 3130 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24684700 WITH THE FOLLOWING CORRECTIVE ACTION: "REPLACED FO 'S WINDSHIELD IN REFERENCE TO CRJ700 AMM 56-11-01 AND COMPLIED WITH TASK CAR
- [SDR SWIA202162544](https://openairdocs.org/sdr/SWIA202162544.md): None · cracked · Nov 11, 2021 · N720EV · Cndair CL600* · Window/Windshield System
  > R WINDOW HEAT CAUTION MESSAGE. FOLLOWED QRH. ABOUT 10 MINUTES LATER THE RIGHT WINDOW HAD A CRACK IN IT. FOLLOWED THE QRH FOR CRACKED WINDOW. (FLIGHT 3074 - FILED CLOSED) REMOVED AND REPLACED RH SIDE WINDOW WITH SERVICEABLE UNIT PER AMM 56-11-01 AND SKYWE
- [SDR SWIA202160014](https://openairdocs.org/sdr/SWIA202160014.md): Buss Bar · failed · Aug 3, 2021 · N720EV · Cndair CL6002C10 · Hydraulic System, Main
  > CLIMBING, GOING TO 12,000 FT, RECEIVED A DUAL HYD SYS FAILURE OF SYSTEMS 1 & 3. PRESS ON BOTH SYS WAS 0, BOTH BRAKE READINGS WERE AT 0, FLUID QTY ON TAXI CHECK WAS 80/70/75 ON ALL 3 SYSTEMS. HYD TEMPS NORMAL. RAN QRH FOR COMBINED FAILURE HYD 1 LO PRESS & HYD 3
- [SDR SWIA202158730](https://openairdocs.org/sdr/SWIA202158730.md): Seal · leaking · Jun 11, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > MAIN CABIN DOOR AT ALT WAS MAKING A VERY LOUD SOUND CAUSING A RETURN TO FIELD. (FLIGHT 2953 - FILED CLOSED) FOUND LOWER FRWD. CORNER ON PAX DOOR SEAL TORN AND NOT SECURED TO DOOR SEAL TRACK. REMOVED AND REPLACED PAX DOOR SEAL WITH SERVICEABLE UNIT. PRES
- [SDR SWIA202158429](https://openairdocs.org/sdr/SWIA202158429.md): Skin · gouged · May 9, 2021 · N720EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > GOUGE ON EXTERIOR FUSELAGE SKIN BETWEEN STRINGER 2R & 4R AND FS1098 & FS1126 (C-CHECK RO 5/22/2021) GOUGE ON EXTERIOR FUSELAGE SKIN BETWEEN STRINGER 2R AND 4R AND FS1098.00 AND FS1126.00 WAS BLENDED, CHEMICAL CONVERSION COATING APLLIED AND PROTECTIVE FI
- [SDR SWIA202158447](https://openairdocs.org/sdr/SWIA202158447.md): Floor Support · corroded · Apr 11, 2021 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT ANGLE REF CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202158446](https://openairdocs.org/sdr/SWIA202158446.md): D-Ring · corroded · Apr 10, 2021 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD CARGO D RING MOUNT BRACKET AT FS 533 / STRINGRER 26-27L HAS CORROSION ON TOP (C-CHECK RO 5/22/2021) REMOVED AND REPLACED 1EA NEW FORWARD CARGO D RING MOUNT BRACKET P/N SH670-33389-1 AT FS 533/STRINGERS 26-27LH. REF CRJ-700 SRM 51-42-21-001-001-A
- [SDR SWIA202158428](https://openairdocs.org/sdr/SWIA202158428.md): Angle · corroded · Apr 9, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR F/S 321.0 CLIP HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR CLIP AT F.S. 321.0, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL6
- [SDR SWIA202158427](https://openairdocs.org/sdr/SWIA202158427.md): Stringer · corroded · Apr 8, 2021 · N720EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR27 HAS EVIDENCE OF CORROSION ON FUSELAGE SKIN FLANGE BETWEEN FS349 - FS333 (C-CHECK RO 5/22/2021) CORROSION REMOVED FROM STGR27, MATERIAL LOSS FOUND TO BE OUT OF LIMITS, STGR27 REPLACED FROM FS333-FS364 REF CRJ700 SRM 51-42-06-001-001-A01, COMPLIED
- [SDR SWIA202158426](https://openairdocs.org/sdr/SWIA202158426.md): Angle · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR F/S 320.0 CLIP HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR CLIP AT F.S. 320.0, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESS LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-
- [SDR SWIA202158425](https://openairdocs.org/sdr/SWIA202158425.md): Intercostal · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR FWD DD3 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR DD3 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (C
- [SDR SWIA202158424](https://openairdocs.org/sdr/SWIA202158424.md): Intercostal · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR MID DD6 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR MID DD6 INTERCOSTAL, REF CRJ 700 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TA
- [SDR SWIA202158423](https://openairdocs.org/sdr/SWIA202158423.md): Intercostal · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR MID DD4 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR DD4 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (C
- [SDR SWIA202158422](https://openairdocs.org/sdr/SWIA202158422.md): Intercostal · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID DD2 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) INSTALLED NEW PAX DOOR MID DD2 INTERCOSTAL REF. CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N / COMPLIED WITH TASK CARD 51-900-1002-SKY / SEE CONTINUATION FOR DETAIL
- [SDR SWIA202158421](https://openairdocs.org/sdr/SWIA202158421.md): Cleat · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CLEAT HAS CORROSION COMOM TO AFT DD6 INTERCOSTAL (C-CHECK RO 5/22/2021) REMOVED AND INSTALLED NEW PAX DOOR CLEAT COMMON TO AFT DD6 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N AND RESTORED FINISH ALL FAST
- [SDR SWIA202158420](https://openairdocs.org/sdr/SWIA202158420.md): Intercostal · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD5 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT DD5 INTERCOSTAL REF. CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N / COMPLIED WITH TASK CARD 51-900-1002-SKY / SEE CONTINUATION FOR
- [SDR SWIA202158419](https://openairdocs.org/sdr/SWIA202158419.md): Intercostal · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR AFT DD4 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR DD3 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (C
- [SDR SWIA202158418](https://openairdocs.org/sdr/SWIA202158418.md): Intercostal · corroded · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD2 INTERCOSTAL HAS CORROSION (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT DD2 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SK
- [SDR SWIA202158417](https://openairdocs.org/sdr/SWIA202158417.md): Intercostal · dented · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD1 INTERCOSTAL HAS DEEP DENT ON UPPER FLANGE RADIUS (C-CHECK RO 5/22/2021) INSTALLED NEW PAX DOOR DD1 INTERCOSTAL REF. CRJ700 SRM 51-40-11-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N / COMPLIED WITH TASK CARD 51-900-1002-SKY / SEE CONT
- [SDR SWIA202158416](https://openairdocs.org/sdr/SWIA202158416.md): Intercostal · dented · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD1 INTERCOSTAL HAS DEEP DENT ON UPPER FLANGE RADIUS (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT DD1 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST T
- [SDR SWIA202158415](https://openairdocs.org/sdr/SWIA202158415.md): Intercostal · dented · Apr 4, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD7 INTERCOSTAL HAS DEEP DENT ON UPPER FLANGE RADIUS (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT DD7 INTERCOSTAL, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST T
- [SDR SWIA202158413](https://openairdocs.org/sdr/SWIA202158413.md): Former · cracked · Apr 3, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER IS CRACK (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT FORMER, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTUR
- [SDR SWIA202158412](https://openairdocs.org/sdr/SWIA202158412.md): Intercostal · corroded · Apr 2, 2021 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR FRAME F/S 313..56 BETWEEN DD4 AND DD5 INTERCOSTAL IS CORRODED (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR FRAME F.S. 313.56, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWES
- [SDR SWIA202158411](https://openairdocs.org/sdr/SWIA202158411.md): Stringer · corroded · Apr 1, 2021 · N720EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *STINGER 27 HAS EVIDENCE OF CORROSION ON FUSELAGE SKIN FLANGE BETWEEN FRAMES FS 310 AND FS 319. (C-CHECK RO 5/22/2021) CORROSION REMOVED AT STGR27, MATERIAL LOSS FOUND TO BE OUT OF LIMITS, STGR27 REPLACED BETWEEN FS310-FS333 REF DWG SH670-31635 REV NC A
- [SDR SWIA202158410](https://openairdocs.org/sdr/SWIA202158410.md): Slat Track · worn · Mar 31, 2021 · N720EV · Cndair CL6002C10 · Leading Edge Devices
  > *LEFT WING #3 LEADING EDGE SLAT €“ 3-1 DRIVEN SLAT TRACK HAS WEAR DAMAGE 4 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED WEAR DAMAGE ON LH SLAT TRACK 3-1. REF CRJ700 SRM 51-12-00-001-001-A01. EVAL NO DAMAGE ALLOWED. NDT DEFECT FREE. RECEIVED AND C
- [SDR SWIA202158409](https://openairdocs.org/sdr/SWIA202158409.md): Slat Track · worn · Mar 31, 2021 · N720EV · Cndair CL6002C10 · Leading Edge Devices
  > *LEFT WING #2 LEADING EDGE SLAT €“ 2-3 DRIVEN SLAT TRACK HAS WEAR DAMAGE 4 AREAS. (MARKED) (C-CHECK RO 5/22/2021) REMOVED DAMAGE FROM LH SLAT TRACK 2-3.REWORKED AREA FOUND TO BE WITHIN LIMITS REF REO 670-57-42-1049 REV-- DATED 2021-04-08. ALL CHECKS G
- [SDR SWIA202158408](https://openairdocs.org/sdr/SWIA202158408.md): Support · corroded · Mar 30, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER SUPPORT ANGLE IS CORRODED (C-CHECK RO 5/22/2021) REMOVED AND REPLACED PAX DOOR AFT FORMER SUPPORT ANGLE, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV -N, PRESSURE LEAK CHECK GOOD / COMPLIED WITH SKYWEST TASK CARD 51-90
- [SDR SWIA202158445](https://openairdocs.org/sdr/SWIA202158445.md): Tension Tie · corroded · Mar 28, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER TENSION TIE HAS CORRODED HARDWARE (C-CHECK RO 5/22/2021) REMOVED AND REPLACED CORRODED HARDWARE PAX DOOR LOWER TENSION TIE IAW CRJ 700 AMM 52-11-19-400-801 A01. OPS TEST PREFORMED IN JOB: 71011585 OP: 130 CAMP: 22522934 / TUC 4964 S/N 252
- [SDR SWIA202158444](https://openairdocs.org/sdr/SWIA202158444.md): Tension Tie · corroded · Mar 28, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR UPPER TENSION TIE HAS CORRODED HARDWARE (C-CHECK RO 5/22/2021) REMOVED AND REPLACED CORRODED HARDWARE PAX DOOR UPPER TENSION TIE IAW CRJ 700 AMM 52-11-19-400-801-A01. OPS TEST PREFORMED IN JOB: 71011585 OP: 130 CAMP: 22522934 / TUC 4964 S/N 252
- [SDR SWIA202158443](https://openairdocs.org/sdr/SWIA202158443.md): Retainer · corroded · Mar 27, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT SEAL RETAINER HAS CORROSION AT FASTENERS (C-CHECK RO 5/22/2021) REPLACED CORRODED FASTENERS ON PAX DOOR AFT SEAL RETAINER IAW CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202158442](https://openairdocs.org/sdr/SWIA202158442.md): Retainer · corroded · Mar 27, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD SEAL RETAINER HAS CORROSION AT FASTENERS (C-CHECK RO 5/22/2021) REPLACED CORRODED FASTENERS ON PAX DOOR FWD SEAL RETAINER IAW CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202158441](https://openairdocs.org/sdr/SWIA202158441.md): Retainer · corroded · Mar 27, 2021 · N720EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR UPPER SEAL RETAINER HAS CORROSION AT FASTENERS (C-CHECK RO 5/22/2021) REPLACED CORRODED FASTENERS ON PAX DOOR UPPER SEAL RETAINER IAW CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202158440](https://openairdocs.org/sdr/SWIA202158440.md): Seat Track · corroded · Mar 27, 2021 · N720EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE SPOTS OF CORROSION ON SEAT RAIL AT LBL 27 FROM FS477.40-FS693.00 (C-CHECK RO 5/22/2021) 2EA SEAT RAILS P/N SH670-33426-1 AND SH670-33463-1 WERE REMOVED AND REPLACED BY NEW ONES P/N SH670-33426-1 AND SH670-33463-1 IAW CRJ700 AMM 53-00-49-400-801
- [SDR SWIA202158407](https://openairdocs.org/sdr/SWIA202158407.md): Crossbeam · corroded · Mar 27, 2021 · N720EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION AT THREE LOCATIONS ON FS549.00 CROSSBEAM BETWEEN RBL9.0 AND LBL9.0 (C-CHECK RO 5/22/2021) REMOVED CORROSION. REF CRJ700 SRM 51-21-06-001-001. NDT DEFECT FREE. EVAL OUT OF LIMITS AS NO DAMAGE ALLOWED AT LOCATION. RECEIVED AND REPAIRED DAMA
- [SDR SWIA202158406](https://openairdocs.org/sdr/SWIA202158406.md): Floor Support · corroded · Mar 27, 2021 · N720EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * CORROSION ON RH FLOOR SILL AROUND ALL SCREW HOLES AND AFT END FS661.00 TO FS693.00 (MARKED WITH ORANGE STREAMER) (C-CHECK RO 5/22/2021) REMOVED OLD DAMAGED FLOOR SILL AT FS 661-693 AND INSTALLED A NEW SILL IAWDWG SH670-32170 REV V AND CRJ-700 SRM 51-4
- [SDR SWIA202158439](https://openairdocs.org/sdr/SWIA202158439.md): Seat Track · corroded · Mar 26, 2021 · N720EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE SPOTS OF CORROSION ON SEAT RAIL AT LBL 9 FROM FS477.40-FS693.00 (C-CHECK RO 5/22/2021) REMOVED AND REPLACED SEAT TRACK RAIL AT LBL 9 FROM FS477.40 TO FS693.00 REF CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17
- [SDR SWIA202158438](https://openairdocs.org/sdr/SWIA202158438.md): Seat Track · corroded · Mar 26, 2021 · N720EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *MULTIPLE SPOTS OF CORROSION ON SEAT RAIL AT RBL 9 FROM FS477.40-FS693.00 (C-CHECK RO 5/22/2021) REMOVED AND REPLACED WITH NEW SEAT TRACK RAIL AT RBL9 FROM FS477.40 TO FS693.00 REF CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17
- [SDR SWIA202158437](https://openairdocs.org/sdr/SWIA202158437.md): Seat Track · corroded · Mar 26, 2021 · N720EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *MULTIPLE SPOTS OF CORROSION ON R/H SIDE SEAT RAILS FROM FS669.40-FS989.00 (C-CHECK RO 5/22/2021) 6 EA CORRODED R/H SIDE SEAT RAILS FROM FS669.40 TO FS989.00 WERE REMOVED AND REPLACED BY NEW ONES IAW CRJ700 AMM 53-00-49-400-801-A03.
- [SDR SWIA202158436](https://openairdocs.org/sdr/SWIA202158436.md): Seat Track · corroded · Mar 26, 2021 · N720EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *MULTIPLE SPOTS OF CORROSION ON L/H SIDE SEAT RAILS FROM FS669.40-989.00 (C-CHECK RO 5/22/2021) REMOVED AND REPLACED SIDE SEAT TRACKS ON L/H FS669.40-989.00 REF CRJ700 AMM 53-00-49-000-801-A17 & 53-00-49-400-801-A17. SEE CONTINUE CARD FOR DETAILS.

Next page: https://openairdocs.org/aircraft/N720EV/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 = 'N720EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N720EV/reports

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