# Service difficulty reports: N722EV

A list on [N722EV](https://openairdocs.org/aircraft/N722EV.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 7 · 314 reports

- [SDR SWIA202507210225](https://openairdocs.org/sdr/SWIA202507210225.md): Window Frame · cracked · Feb 25, 2025 · N722EV · Cndair CL6002C10 · Fuselage Main, Structure
  > COPILOTS UPPER WINDOW SUPPORT STRUCTURE HAS POSSIBLE CRACK (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW CO-PILOT WINDSHIELD POST UPPER FRAME P/N CC670-33470-4 IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-0
- [SDR SWIA2024061900517](https://openairdocs.org/sdr/SWIA2024061900517.md): Frame · corroded · May 17, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Frame
  > AFT BAGGAGE COMPARTMENT AT FS1000.00 STGR 20L HAS POSSIBLE CORROSION AS MARKED (C-CHECK RO 6/17/2024) REPAIRED CORROSION UNDER AFT CARGO AT APPX FS1000 & STG 20L REO 670-53-61-2265 REV -- DATE 2024-05-02. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA20240426](https://openairdocs.org/sdr/SWIA20240426.md): Skin · eroded · Apr 26, 2024 · N722EV · Cndair CL6002C10 · Trailing Edge Flaps
  > EROSION NOTED ON R/H INBD FLAP LOWER SKIN BETWEEN FLS15-FLS38 (MARKED (C-CHECK RO 6/17/2024) R/H I/B FLAP LWR SKIN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01. REF CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
- [SDR SWI2024F00513](https://openairdocs.org/sdr/SWI2024F00513.md): Channel · gouged · Apr 25, 2024 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERNAL CHANNEL FOR FWD ATG ANTENNA HAS GOUGES AROUND BOTH CONNECTOR HOLES (C-CHECK RO 6/17/2024) INTERNAL CHANNEL FOR FWD ATG ANTENNA GOUGES HAVE BEEN BLENDED EVALED OUT OF LIMITS, REPAIRED AND REINSTALLED PER CRJ 700 SRM 51-42-20-001-001-A01, EO NO: C
- [SDR SWI2024F00512](https://openairdocs.org/sdr/SWI2024F00512.md): Skin · scratched · Apr 25, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > SCRATCHES AND GOUGES ON DOUBLER WHERE AFT ATG ANTENNA MOUNTS (C-CHECK RO 6/17/2024) REMOVED MINOR SCRATCHES AND GOUGES FROM EXTERNAL ( CONTACT) SURFACE OF ATG AFT ANTENNA DOUBLER REF. CRJ700 SRM TASK 51-12-00-001-001-A01, WET INSTALLED NEW REPLACEMENT A
- [SDR SWI2024F00511](https://openairdocs.org/sdr/SWI2024F00511.md): Stand Off · cracked · Apr 25, 2024 · N722EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 6/17/2024) REMOVED CRACKED INBD "A" BRACKET STANDOFF AND INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANSCOWL REF MHIRJ GREO #670-54-21-971 REV (B) 2023-
- [SDR SWIA2024061900425](https://openairdocs.org/sdr/SWIA2024061900425.md): Skin · scratched · Apr 25, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DEEP SCRATCHES AND GOUGES ON DOUBLER WHERE FWD ATG ANTENNA MOUNTS (C-CHECK RO 6/17/2024) REMOVED MINOR SCRATCHES AND GOUGES FROM EXTERNAL ( CONTACT) SURFACE OF ATG FWD ANTENNA DOUBLER REF. CRJ700 SRM TASK 51-12-00-001-001-A01WITH NEW FABRICATED AND DRIL
- [SDR SWI2024F00515](https://openairdocs.org/sdr/SWI2024F00515.md): Floor Support · corroded · Apr 24, 2024 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL BETWEEN F.S. 1000 AND F.S. 985 HAS CORROSION (C-CHECK RO 6/17/2024) COMPLIED WITHALL STEPS OF REO 670-53-61-2263 REV-- DATED- 2024-04-30, FOR REPLACEMENT/REPAIR OF LH FLOOR SILL AT F.S. 985.00-1000.0 AND COMPLIED WITH SKYWEST TASK CARD 51-9
- [SDR SWIA2024061900424](https://openairdocs.org/sdr/SWIA2024061900424.md): Hinge Fitting · chafed · Apr 24, 2024 · N722EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LH WS264.00 OUTBOARD FLAP HINGE FITTING ATTACHMENT POINTS FOR ATTACHMENT BRACKET SH670-14508-1 IS CHAFED. (C-CHECK RO 6/17/2024) REPAIRED CHAFED DAMAGES ON LH WS264.00 OUTBOARD FLAP HINGE FITTING ATTACHMENT POINTS FOR ATTACHMENT BRACKET SH670-14508-1 PER
- [SDR SWIA2024061900423](https://openairdocs.org/sdr/SWIA2024061900423.md): Hinge · gouged · Apr 23, 2024 · N722EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER PIANO HINGE FUSELAGE SIDE, HINGE LAND AFT OF THE 27TH LUG GOUGED. (C-CHECK RO 6/17/2024) REMOVED AND INSTALLED NEW PAX DOOR HINGE ( FUSELAGE SIDE). REF: CRJ-700 SRM 53-21-23-201-010-A01 AND REO 670-53-21-2392 REV -- DATE 2024-04-30 ALL STEPS O
- [SDR SWI2024F00517](https://openairdocs.org/sdr/SWI2024F00517.md): Stringer · corroded · Apr 22, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R BETWEEN FS364-379 HAS AREAS OF CORROSION (C-CHECK RO 6/17/2024) REPAIRED STRINGER 23R BETWEEN FS364-379 REF CRJ700 SRM 53-00-03-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. CHECKS GOOD.
- [SDR SWI2024F00516](https://openairdocs.org/sdr/SWI2024F00516.md): Insert · broken · Apr 22, 2024 · N722EV · Cndair CL6002C10 · Engine Thrust Reverser
  > RH ENGINE UPPER INBOARD T/R NYLON INSERT BROKEN OFF (C-CHECK RO 6/17/2024) REMOVED RH ENGINE UPPER INBOARD T/R NYLON INSERT REF. CRJ700 AMM 78-33-05-960-801-A02,STEPS 1-4A,(1)-(5). REPAIRED ELONGATED SCREW HOLES FOR NYLON INSERT AND INSTALLED NEW RH ENGI
- [SDR SWIA2024061900422](https://openairdocs.org/sdr/SWIA2024061900422.md): Frame · corroded · Apr 22, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS379 STGR23R IS CORRODED (C-CHECK RO 6/17/2024) REMOVED CORROSION ON FRAME AT FS379 STGR23R. REF CRJ700 SRM 51-21-06-001-001-A01EVALUATED. ORIGINAL THICKNESS.063" MINIMUM REMAINING THICKNESS.040" TOTAL MATERIAL LOSS.023" MAXIMUM ALLOWED B
- [SDR SWI2024F00518](https://openairdocs.org/sdr/SWI2024F00518.md): Frame · corroded · Apr 21, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Frame
  > AFT SIDE OF SUB FRAME AT FS 535.0 CORRODED AT LOWER GUIDE FITTING (C-CHECK RO 6/17/2024) COMPLIED WITH MHIRJ REO 670-53-31-871 REV-- DATED 2024-05-08 IN REPAIRING OF THE LOWER GUIDE FITTING AT AFT SIDE OF SUB FRAME AT FS535.00. COMPLIED WITH TASK CARD 5
- [SDR SWIA2024061900421](https://openairdocs.org/sdr/SWIA2024061900421.md): Frame · corroded · Apr 21, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FWD SIDE OF SUB FRAME AT FS 578.0 CORRODED AT LOWER GUIDE FITTING (C-CHECK RO 6/17/2024) COMPLIED WITH MHIRJ REO 670-53-31-872 REV-- DATED 2024-04-30 IN REPAIRING OF THE LOWER GUIDE FITTING AT FWD SIDE OF SUB FRAME AT FS578.00 COMPLIED WITH TASK CARD 51-
- [SDR SWI2024F00510](https://openairdocs.org/sdr/SWI2024F00510.md): Bracket · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS533.00 STGR22L 23L. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED MACHINED BRACKET IN FWD CARGO, F.S. 533 STGR 22-23L, WITH NEW, REF CRJ 700 SRM 51-42-20-001-001-A01 REVISION 38: JUL 25/2020, CRJ
- [SDR SWI2024F00509](https://openairdocs.org/sdr/SWI2024F00509.md): Skin · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > AFT BAGGAGE BAY FS1031.00 STGR27L HAS CORROSION ON SKIN AS MARKED (C-CHECK RO 6/17/2024) REMOVED CORROSION ON AFT BAGGAGE BAY FS1031.00 STGR27L REF CRJ700 SRM 51-21-06-001-001-A01EVALUATED. ORIGINAKL THICKNESS.050" MINIMUM REMAINING THICKNESS.040" TOTA
- [SDR SWI2024F00508](https://openairdocs.org/sdr/SWI2024F00508.md): Bracket · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS581.00 STGR27 - 26L. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED WITH NEW BRACKET P/N SH670-33389-2 AT FS581.00 STGR27 - 26L. REF. CRJ 700 SRM 51-45-00-001-001-A01, 51-42-21-001-001-A01, AND 51
- [SDR SWI2024F00507](https://openairdocs.org/sdr/SWI2024F00507.md): Plate · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE AFT JOINT PLATE IS CORRODED FS581.00 STGR25L. MARKED IN RED. (C-CHECK RO 6/17/2024) REMOVED CORROSION AT FORWARD BAGGAGE BAY DOOR AFTER JOINT PLATE REF. CRJ-700 SRM 51-21-06-001-001-A01ORIGINAL THICKNESS IS.0
- [SDR SWI2024F00506](https://openairdocs.org/sdr/SWI2024F00506.md): Frame · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FORWARD BAGGAGE BAY - CORROSION ON FRAME LOWER FLANGE. FORWARD AND AFT WEB FS661.00 STGR26R - STGR26L. (MARKED IN RED) (C-CHECK RO 6/17/2024) BLENDED CORROSION ON FRAME LOWER FLANGE, FORWARD, AND AFT WEB AT FS661.00 STGR26R - STGR26L IAW CRJ 700 SRM 51
- [SDR SWI2024F00505](https://openairdocs.org/sdr/SWI2024F00505.md): Frame · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FORWARD BAGGAGE BAY - CORROSION ON FRAME WEB AND LOWER FLANGE FS645.00 STGR26R - STGR26L. (MARKED IN RED) (C-CHECK RO 6/17/2024) BLENDED CORROSION ON FRAME WEB AND LOWER FLANGE AT FS645.00 STGR26R - STGR26L IAW CRJ 700 SRM 51-21-06-001-001-A01 RECEIVED
- [SDR SWI2024F00504](https://openairdocs.org/sdr/SWI2024F00504.md): Bracket · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS581.00 STGR22L - 23L. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND INSTALLED NEW BRACKET P/N SH670-33390-2 REF. CRJ 700 SRM 51-45-00-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND 51-42-28-
- [SDR SWI2024F00503](https://openairdocs.org/sdr/SWI2024F00503.md): Stop Fitting · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Galley Doors
  > GALLEY SERVICE DOOR HAS CORROSION AT THE LOWER DOOR STOP FITTINGS AND SILL AS MARKED (C-CHECK RO 6/17/2024) REPLACED LOWER SILL PN# SH670-31996-39 ON GALLEY SERVICE DOOR SURROUND. REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AN
- [SDR SWI2024F00502](https://openairdocs.org/sdr/SWI2024F00502.md): Bracket · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS533.00 STGR27. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED FORWARD BAGGAGE BAY BRACKET FS533.00 STGR27 (PN SH670-33389-1) PER CRJ700 SRMS 51-42-21-001-001-A01, 51-42-22-001-001-A01 AND DWG NO
- [SDR SWIA2024061900420](https://openairdocs.org/sdr/SWIA2024061900420.md): Bracket · corroded · Apr 20, 2024 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS549.00 - FS565.00 STGR25R - 24R. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED BRACKET BETWEEN F.S. 549 AND F.S. 565 STGR 25R-24R WITH NEW, PN SH670-33852-1, REF CRJ 700 SRM 51-42-06-001-001-A01,
- [SDR SWI2024F00514](https://openairdocs.org/sdr/SWI2024F00514.md): Floorbeam · corroded · Apr 19, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR SUPPORT ANGLE AT F.S 280.00 IS HEAVILY CORRODED ON TOP. (C-CHECK RO 6/17/2024) REMOVED CORRODED COCKPIT FLOOR SUPPORT ANGLE AT FS280.00 AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE AT FS280.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND CR
- [SDR SWIA2024061900419](https://openairdocs.org/sdr/SWIA2024061900419.md): Floorbeam · cracked · Apr 19, 2024 · N722EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280.00 CROSSBEAM ANGLE CRACKED AT LBL9 AS MARKED (C-CHECK RO 6/17/2024) REMOVED CRACKED CROSSBEAM ANGLE AT FS280.00 LBL9 AND INSTALLED NEW CROSSBEAM ANGLE FS280.00 AT LBL9. REF CRJ700 SRM 51-42-21-001-001-A01 & DWG CC670-34099 REV -- AND COMPLIED WITH
- [SDR SWIA2024061900418](https://openairdocs.org/sdr/SWIA2024061900418.md): Angle · cracked · Apr 18, 2024 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT COMPARTMENT - FS1098.20 STGR24R INBOARD CLIP IS CRACKED. (MARKED) (C-CHECK RO 6/17/2024) REMOVED FROM FS1098.20 STGR24R CRACKED INBOARD CLIP REF.CRJ-700 SRM 51-42-06-001-001-A01 INSTALLED NEW CLIP REF.CRJ-700 DRAWING MM670-35012 REV. G AND
- [SDR SWIA2024061900417](https://openairdocs.org/sdr/SWIA2024061900417.md): Fitting · scratched · Apr 17, 2024 · N722EV · Cndair CL6002C10 · Fuselage, Landing Gear Attach Fittings
  > DURING AUDIT OF 1C TASK CARD 32-740-101, (DETAILED INSPECTION OF THE RIGHT MAIN LANDING GEAR (MLG) ATTACHMENT POINTS), FOUND THE SIDE STAY FITTING HAS SEVERAL SCRATCHES ON FACE, O/B SIDE. (C-CHECK RO 6/17/2024) BLENDED AND MEASURED 3 EA BLEND SCRATCHES
- [SDR SWI2024F00501](https://openairdocs.org/sdr/SWI2024F00501.md): Slider · gouged · Apr 16, 2024 · N722EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD SLIDER IS GOUGED (C-CHECK RO 6/17/2024) COMPLIED WITH REO 670-54-21-1631, REV. --, 2024-05-02 ALL STEPS FOR REPAIR TO R/H UPPER TRANSCOWL INBD SLIDER. COMPLIED WITH MAJOR REPAIR FORM 337. COMPLIED WITH SKYWEST TASK CARD 51-900-1
- [SDR SWI2024F00500](https://openairdocs.org/sdr/SWI2024F00500.md): Stand Off · cracked · Apr 16, 2024 · N722EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD " A " BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) REPLACED I/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 M-337 & SKYCARD 51-900-1002-SKY.
- [SDR SWI2024F00499](https://openairdocs.org/sdr/SWI2024F00499.md): Stand Off · cracked · Apr 16, 2024 · N722EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) INSTALLED 1 EA. NEW STANDOFF P/N CN624-2082-201 ON R/H UPPER TRANS COWL (OTBD.). REF. MHIRJ REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3. COMPLIED WITH MA
- [SDR SWI2024F00498](https://openairdocs.org/sdr/SWI2024F00498.md): Stand Off · cracked · Apr 16, 2024 · N722EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) REMOVED AND REPLACED INBD STAND-OFF P/N CN624-2082-201 ON L/H LOWER TRANSCOWL REF. REO 670-54-21-971 REV. B, 2023-11-28 AND CRJ 700 SRM 51-42-28-001-001-A01. COMPLIED WITH SK
- [SDR SWI2024F00497](https://openairdocs.org/sdr/SWI2024F00497.md): Stand Off · cracked · Apr 16, 2024 · N722EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) INSTALLED 1 EA. NEW STANDOFF P/N CN624-2082-201 ON R/H UPPER TRANS COWL (OTBD.). REF. MHIRJ REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3. COMPLIED WITH MAJ
- [SDR SWIA2024061900416](https://openairdocs.org/sdr/SWIA2024061900416.md): Stand Off · cracked · Apr 16, 2024 · N722EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL OTBD A BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-1128. COMPLIED WITH M-337 & SKYCARD 51-900-1002-SKY.
- [SDR SWIA2024061900414](https://openairdocs.org/sdr/SWIA2024061900414.md): Skin · gouged · Apr 14, 2024 · N722EV · Cndair CL6002C10 · Ailerons
  > RIGHT WING AILERON UPPER SKIN LEADING EDGE GOUGED AT APPROXIMATELY WS339.00 AS MARKED (C-CHECK RO 6/17/2024) BLENDED GOUGE DAMAGE ON RH WING AILERON UPPER LEADING EDGE AT WS339.00 IAW CRJ700 SRM 51-12-00-001-001-A01 FOUND OUT OF LIMITS PER CRJ 700 SRM 57
- [SDR SWI2024F00496](https://openairdocs.org/sdr/SWI2024F00496.md): Skin · gouged · Apr 7, 2024 · N722EV · Cndair CL6002C10 · Leading Edge Devices
  > LH INBD SLAT UNDERSIDE GOUGED AT APPROX LOC. WS128 TRAILING EDGE (C-CHECK RO 6/17/2024) REPAIRED GOUGE AT UNDERSIDE OF THE LH INBD SLAT AT APROX WS128 TRAILING EDGE REF MHIRJ REO 670-57-42-909 REV B DATED 2024-04-24. COMPLIED WITH TASK CARD 51-900-1002
- [SDR SWIA2024061900407](https://openairdocs.org/sdr/SWIA2024061900407.md): Skin · dented · Apr 7, 2024 · N722EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LH INBD FLAP LOWER SKIN HAS A CLUSTER OF SMALL DENTS ON INBD SIDE (C-CHECK RO 6/17/2024) L/H I/B FLAP LOWER SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
- [SDR SWIA2024061900406](https://openairdocs.org/sdr/SWIA2024061900406.md): Panel · corroded · Apr 6, 2024 · N722EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR PANEL 832DR HAS CORROSION AROUND FASTENER HOLES. (MX-TRANS #28049752) (C-CHECK RO 6/17/2024) ORIGINAL MATERIAL THICKNESS 0.05" AS PER CRJ700 SRM 52-11-32-001-001-A01. DAMAGES MUST BE AT MINIMUM 1.5 D FROM ANY FASTENER, OUT OF LIMITS AS PER CRJ70
- [SDR SWIA2024061903110](https://openairdocs.org/sdr/SWIA2024061903110.md): Floorbeam · cracked · Jan 10, 2023 · N722EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > TRANSFER FROM EAML 1061692: TRANSFERRED FROM CAMP 25898012. COCKPIT FLOOR BEAM RBL12, SUSPECT CRACK IN RADIUS OF THE AFT VERTICAL FLANGE WHERE IT ATTACHES TO THE FWD SIDE FS280 BEAM/WEB. (C-CHECK RO 6/17/2024) REPAIRED CRACKED RBL 12 COCKPIT FLOOR BEAM
- [SDR SWIA20250521105](https://openairdocs.org/sdr/SWIA20250521105.md): Not Reported · damaged · Jan 5, 2023 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DAMAGE DETERMINED TO BE OUTSIDE SRM LIMITS, DETERMINED TO BE MAJOR REPAIR. (FILED CLOSED)TRANSFERRED TO AML 1061696 FOR FERRY FLIGHT.
- [SDR SWIA2023010967083](https://openairdocs.org/sdr/SWIA2023010967083.md): Not Reported · damaged · Jan 5, 2023 · N722EV · Cndair CL6002C10 · Fuselage Structure (General)
  > DAMAGE DETERMINED TO BE OUTSIDE SRM LIMITS, DETERMINED TO BE MAJOR REPAIR. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2022010967021](https://openairdocs.org/sdr/SWIA2022010967021.md): Skin · dented · Dec 20, 2022 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DINGS AT FS 1031.00, STGR22RH JUST AFT OF LP AIR GROUND AIR CONNECTION DOOR REPAIR OF FUSELAGE SKIN AT FS 1031.00, STGR22RH JUST AFT OF LP AIR GROUND AIR CONNECTION DOOR DONE IN REFERENCE TO REO 670-53-61-2108 REV:- DATE; 2023-01-01
- [SDR SWIA2022122267021](https://openairdocs.org/sdr/SWIA2022122267021.md): Skin · dented · Dec 20, 2022 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1031.00, S22R JUST AFT OF LP AIR GROUND AIR CONNECTION DOOR. OPEN
- [SDR SWIA202158127](https://openairdocs.org/sdr/SWIA202158127.md): Engine · odor · May 9, 2021 · N722EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > AT 200€™ ON CLIMB OUT RECEIVED SMOKE AFT LAV WARNING MESSAGE, FOLLOWED BY AFT FLIGHT ATTENDANT EMERGENCY CALL CONFIRMING LIGHT SMOKE FROM THE LAV. RETURNED TO FIELD WHILE COMPLYING WITH QRH PROCEDURE OF OPENING APPLICABLE CIRCUIT BREAKERS. UPON LANDING FLIGHT
- [SDR SWIA2020072751454](https://openairdocs.org/sdr/SWIA2020072751454.md): Seat Track · malfunctioned · Jul 16, 2020 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > MOST AFT (LH INBD) SEAT TRACK REQUIRES REPLACEMENT DUE TO SEAT 17AB NOT LOCKING DOWN PROPERLY. REMOVED AND REPLACED AFT (LH INBD) SEAT TRACK WITH NEWLY FABRICATED ONE REF CRJ700 AMM
- [SDR SWIA2020072751462](https://openairdocs.org/sdr/SWIA2020072751462.md): Floor Panel · cracked · Jul 13, 2020 · N722EV · Cndair CL6002C10 · Fuselage Floor Panel
  > CABIN FLOOR BOARD PANEL 241CLF IS CRACKED. FLOORBOARD 241CLF INSTALLED ON JOB 71012790 OP 7015 CAMP 21083713
- [SDR SWIA2020072751461](https://openairdocs.org/sdr/SWIA2020072751461.md): Angle · cracked · Jul 6, 2020 · N722EV · Cndair CL6002C10 · Passenger/Crew Doors
  > CRACK FOUND ON PASSENGER DOOR INNER HANDLE HOUSING ASSY INNER ANGLE P/N# 601R318072-1. (C-CHECK) RO 7/23/2020 REMOVED, DRILLED,LOCATED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INNER HANDLE HOUSING ASSY INNER ANGLE REF CRJ700 SRM.
- [SDR SWIA2020072751453](https://openairdocs.org/sdr/SWIA2020072751453.md): Angle · damaged · Jul 3, 2020 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > IN THE AVIONICS BAY, BELOW FLOORBOARD, FOUND A CLIP WITH AN EXISTING ELONGATED HOLE, AT FS349.0 COMMON TO STR27L (C-CHECK) RO 7/23/2020 REMOVED AND REPLACED CLIP FS349 COMMON TO STR 27L REF CRJ 700 SRM AND DWG. COMPLIED WITH SKY CARD.
- [SDR SWIA2020072751452](https://openairdocs.org/sdr/SWIA2020072751452.md): Intercostal · cracked · Jun 24, 2020 · N722EV · Cndair CL6002C10 · Passenger/Crew Doors
  > CRACK FOUND ON PASSENGER DOOR INTERCOSTAL DD7 P/N# 601R318825-1. (C-CHECK) RO 7/23/2020 REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD7 REF MHIRJ DRAWING AND CRJ700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N722EV/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 = 'N722EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N722EV/reports

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