# Service difficulty reports: N928EV

A list on [N928EV](https://openairdocs.org/aircraft/N928EV.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 3 · 141 reports

- [SDR SWIA2026101077592](https://openairdocs.org/sdr/SWIA2026101077592.md): Floor Support · corroded · Oct 10, 2026 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MULTIPLE SPOTS OF CORROSION ON THE RT PRESSURE FLOOR SUPPORT BTWN BS 484 AND 513. BLENDED MULTIPLE SPOTS OF CORROSION ON THE RT PRESSURE FLOOR SILL BTWN BS 484 & 513 REF SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT IAW NDTM PART 4, 51-00-
- [SDR SWIA2026091677215](https://openairdocs.org/sdr/SWIA2026091677215.md): Retainer · damaged · Sep 16, 2026 · N928EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR BOTTOM SEAL RETAINER IS DAMAGED. REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM MIDDLE SEAL RETAINER IAW SRM 51-42-13 AND REO 601R-52-11-915 REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA20250312221](https://openairdocs.org/sdr/SWIA20250312221.md): Skin · damaged · Feb 21, 2025 · N928EV · Cndair CL6002B19 · Wing, Plate/Skin
  > TRANSFER FROM EAML 1541896: REF EAML 1539813 INSPECTED RT WING AND FOUND MULTIPLE AREAS OF DAMAGE TO THE RT WING TIP FAIRING AND RT WING NAV LIGHT ASSEMBLY. ALSO FOUND UNDERLYING INSTALLATION STRUCTURE DAMAGE AS LISTED IN REO 601R-57-00-201 TABLE 1, SHEET 6.
- [SDR SWIA2024020800004](https://openairdocs.org/sdr/SWIA2024020800004.md): Connector · not seated · Feb 4, 2024 · N928EV · Cndair CL6002B19 · Fire Protection System Wiring
  > RECEIVED A WING OVERHEAT WARNING MSG AND THEN ANTI ICE DUCT WARNING MSG ON CLIMB OUT FROM DEN, RAN QRH AND IT CLEARED BOTH MSGS. TURNED IT BACK ON AND GOT BOTH MSG AGAIN. DID NOT LAND OVERWEIGHT AND DID NOT DECLARE EMERGENCY. (FLIGHT 4663 FILED CLOSED)THIS DIS
- [SDR SWI2024F00109](https://openairdocs.org/sdr/SWI2024F00109.md): Warning Message · activated · Feb 4, 2024 · N928EV · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > WE RECEIVED A WING OVERHEAT WARNING MSG AND THEN ANTI ICE DUCT WARNING MSG ON CLIMB OUT FROM DEN, RAN QRH AND IT CLEARED BOTH MSGS. TURNED IT BACK ON AND GOT BOTH MSG AGAIN. DID NOT LAND OVERWEIGHT AND DID NOT DECLARE EMERGENCY. (FLIGHT 4663 FILED OPEN)THIS IS
- [SDR SWIA202266722](https://openairdocs.org/sdr/SWIA202266722.md): Track · cracked · Nov 1, 2022 · N928EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FORWARD TRACK LOWER BRACKET HAS A CRACK (FILED CLOSED) REPLACED CARGO DOOR FORWARD TRACK LOWER BRACKET IN REFERENCE TO CRJ 200 SRM 51-42-06
- [SDR SWIA202054416](https://openairdocs.org/sdr/SWIA202054416.md): Floor Support · corroded · Nov 20, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN FLOOR BEAM BETWEEN FS 473-FS 484, RBL 9 INBOARD FLANGE HAS CORROSION ON UPPER SURFACE. C-CHECK RO 11/24/2020. REPAIRED CABIN FLOOR BEAM BETWEEN FS 473-FS 484 RBL 9 INBOARD FLANGE CORROSION, IAW MHIRJ REO SKY CARD. W&B PROVIDED, FORM 337 IS ATTACHED.
- [SDR SWIA202054443](https://openairdocs.org/sdr/SWIA202054443.md): Bonding Wire · corroded · Nov 12, 2020 · N928EV · Cndair CL6002B19 · Stabilizer System Wiring
  > RT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE IS CORRODED AND OUTBOARD HINGE BOLT AND ANTI ROTATION HARDWARE ARE CORRODED. C-CHECK RO 11/24/2020. REMOVE AND REPLACED CORRODED HARDWARE AT INBOARD HINGE BONDING WIRE AND OUTBOARD HINGE BOLT AND ANTI ROTATION
- [SDR SWIA202054442](https://openairdocs.org/sdr/SWIA202054442.md): Bonding Wire · corroded · Nov 12, 2020 · N928EV · Cndair CL6002B19 · Stabilizer System Wiring
  > LT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE IS CORRODED AND OUTBOARD HINGE BOLT AND ANTI ROTATION HARDWARE ARE CORRODED. C-CHECK RO 11/24/2020. REPLACED LT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE, OUTBOARD HINGE BOLT AND NUT AND ANTI ROTATION HARDWA
- [SDR SWIA202054441](https://openairdocs.org/sdr/SWIA202054441.md): Retainer · corroded · Nov 12, 2020 · N928EV · Cndair CL6002B19 · Ailerons
  > RT AILERON OUTBOARD HINGE BOLT RETAINER AND HARDWARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CORRODED RETAINER AND HARDWARE AT RT AILERON OUTBOARD HINGE (NR 4), IAW CRJ-200-AMM.
- [SDR SWIA202054446](https://openairdocs.org/sdr/SWIA202054446.md): Angle · damaged · Nov 10, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP P/N: 601R38891-1 AT FS 310 STGR 20L REQUIRES FABRICATION. C-CHECK RO 11/24/2020. FABRICATED NEW CLIP OUT OF MATERIAL S9144-4, IAW CRJ200 SRM AND DWG.
- [SDR SWIA202054445](https://openairdocs.org/sdr/SWIA202054445.md): Stop Fitting · chafed · Nov 7, 2020 · N928EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FUSELAGE FWD UPPER PIN STOP FITTING IS CHAFED. C-CHECK RO 11/24/2020. REMOVED AND INSTALLED SERVICEABLE PAX DOOR FUSEALAGE UPPER FWD STOP FITTING, IAW CRJ 200 AMM.
- [SDR SWIA202054440](https://openairdocs.org/sdr/SWIA202054440.md): Seat Track · corroded · Nov 3, 2020 · N928EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACKS AT FS 559+4-FS 559+86 WAS FOUND TO BE OUT LIMITS. REQUIRES FABRICATION. C-CHECK RO 11/24/2020. FABRICATED SEAT TRACK FOR LBL AND RBL 9 AT FS 559+4-559+86. REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.
- [SDR SWIA202054425](https://openairdocs.org/sdr/SWIA202054425.md): Angle · cracked · Oct 30, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP ANGLE BETWEEN FS 621 AND FS 625 AT LBL 45 WL 93 IS CRACKED. C-CHECK RO 11/24/2020. REMOVED CRACKED CLIP ANGLE AND REPLACED WITH A SERVICEABLE BETWEEN FS 621 AND FS 625 AT LBL 45 WL 93, IAW CRJ200 SRM. APPLIED PROTECTIVE FINISH, IAW CRJ200 SRM.
- [SDR SWIA202054424](https://openairdocs.org/sdr/SWIA202054424.md): Bracket · cracked · Oct 30, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP ANGLE BETWEEN FS 621 AND FS 625 AT RBL 45 WL 93 IS CRACKED. C-CHECK RO 11/24/2020. REMOVED CRACKED CLIP ANGLE AND REPLACED WITH A SERVICEABLE BETWEEN FS 621 AND FS 625 AT RBL 45 WL 93, IAW CRJ200 SRM. APPLIED PROTECTIVE FINISH, IAW CRJ200 SRM.
- [SDR SWIA202054415](https://openairdocs.org/sdr/SWIA202054415.md): Trunnion · damaged · Oct 30, 2020 · N928EV · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > WHILE WORKING SB601R-57-046 FOUND ONE HOLE TO BE OVERSIZED ON RT TRUNNION. C-CHECK RO 11/24/2020. REPAIRED OVERSIZED FASTENER HOLE ON RT MLG TUNNION, IAW MHIRJ REO. TASK CARD AND FORM M-337 COMPLETED, NO WEIGHT CHANGE.
- [SDR SWIA202054439](https://openairdocs.org/sdr/SWIA202054439.md): Seat Track · corroded · Oct 29, 2020 · N928EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK FS 399-FS 409+128 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LBL 9 FLOOR SEAT TRACK AT FS 339 TO FS 409+128, IAW CRJ200 AMM. SEE SONTINUATION CARD FOR DETAILS.
- [SDR SWIA202054438](https://openairdocs.org/sdr/SWIA202054438.md): Seat Track · corroded · Oct 29, 2020 · N928EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK FS 364-FS 399 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK AT RBL 9 FS 364-399. REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.
- [SDR SWIA202054437](https://openairdocs.org/sdr/SWIA202054437.md): Seat Track · corroded · Oct 29, 2020 · N928EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK FS 364-FS 399 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK AT LBL 9 BETWEEN FS 364-FS 399, IAW CRJ-200 AMM.
- [SDR SWIA202054436](https://openairdocs.org/sdr/SWIA202054436.md): Floor Support · corroded · Oct 29, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BOLT DOUBLER AT FS 308 LBL 20 IS CORRODED. C-CHECK RO 11/24/2020. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW CRJ 200 SRM. REMOVED AND REPLACED FLOOR SUPPORT BOLT DOUBLER AT FS 308, IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR WO
- [SDR SWIA202054435](https://openairdocs.org/sdr/SWIA202054435.md): Floor Support · corroded · Oct 29, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 288 LBL 37 IS CORRODED. C-CHECK RO 11/24/2020. REPLACED FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 288 LBL 37. REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.
- [SDR SWIA202054417](https://openairdocs.org/sdr/SWIA202054417.md): Intercostal · corroded · Oct 29, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STGR 20L INTERCOSTAL IS CORRODED BETWEEN FS 310 AND FS 319. C-CHECK RO 11/24/2020. REMOVED AND REPLACED STGR 20L INTERCOSTAL BETWEEN FS 310 AND FS 319, IAW CRJ 200 SRM. CW SKY CARD NO WEIGHT CHANGES M-337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR DET
- [SDR SWIA202054414](https://openairdocs.org/sdr/SWIA202054414.md): Floorbeam · corroded · Oct 29, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 349 FLOOR CROSSBEAM IS CORRODED AT RBL 41. C-CHECK RO 11/24/2020. REPAIRED FLOOR SUPPORT CROSSBEAM AT FS 349 RBL 41, IAW BOMBARDIER REO. COMPLETED TASK CARD AND FORM 337, NO WEIGHT CHANGE.
- [SDR SWIA202054434](https://openairdocs.org/sdr/SWIA202054434.md): Seat Track · corroded · Oct 28, 2020 · N928EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS 559+4-559+86 LBL 9 AND RBL 9 FLOOR SEAT TRACKS HAVE MULTIPLE AREAS OF CORROSION AROUND SCREW HOLES. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK AT FS 559+4-559+86 LBL 9 AND RBL 9. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202054433](https://openairdocs.org/sdr/SWIA202054433.md): Strap · corroded · Oct 28, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 559 RBL 27-36 FLOOR BEAM STRAP IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FLOOR BEAM STRAP AT FS 559 RBL 27 TO 36, IAW CRJ-200 SRM.
- [SDR SWIA202054432](https://openairdocs.org/sdr/SWIA202054432.md): Strap · corroded · Oct 28, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 559 LBL 27 TO 36 FLOOR BEAM STRAP IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT FLOOR BEAM STRAP AT FS 559 LBL 27 TO 36, IAW CRJ-200 SRM.
- [SDR SWIA202054420](https://openairdocs.org/sdr/SWIA202054420.md): Door Sill · corroded · Oct 28, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL HAS SEVERAL AREAS OF CORROSION AROUND SCREW HOLES. C-CHECK RO 11/24/2020. REPAIRED CARGO DOOR SILL, IAW BOMBARDIER REO AND SKY CARD NO WEIGHT CHANGE WAS REQUIRED, M337 FORM HAS BEEN SUBMITTED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WO
- [SDR SWIA202054431](https://openairdocs.org/sdr/SWIA202054431.md): Bolt · corroded · Oct 27, 2020 · N928EV · Cndair CL6002B19 · Spoilers
  > LT SPOILERON HINGE BOLT RETENSION ANGLE ATTACH HARDWARE CORRODED AND REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT SPOILERON HINGE BOLT RETENTION ANGLE ATTACHMENT HARDWARE WITH SERVICEABLE HARDWARE, IAW CRJ 200 AMM, SRM.
- [SDR SWIA202054430](https://openairdocs.org/sdr/SWIA202054430.md): Screw · corroded · Oct 27, 2020 · N928EV · Cndair CL6002B19 · Ailerons
  > RT FLIGHT SPOILER HINGE BOLT NUT RETENTION ANGLE HARDWARE CORRODED AND REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RT FLIGHT SPOILER HINGE BOLT RETENTION ANGLE HARDWARE WITH SERVICEABLE HARDWARE, IAW CRJ 200 AMM AND SRM.
- [SDR SWIA202054444](https://openairdocs.org/sdr/SWIA202054444.md): Pressure Blkhd · damaged · Oct 26, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD HAS CHAFED RIVET HEAD AT RBL 18 AT APPROXIMATELY WL 82. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FS 621 BULKHEAD RIVET AT RBL 18 AT APPROXIMATELY WL 82, IAW CRJ 200 SRM. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202054429](https://openairdocs.org/sdr/SWIA202054429.md): Angle · corroded · Oct 26, 2020 · N928EV · Cndair CL6002B19 · Spoilers
  > RT SPOILERON BOLT RETENTION ANGLES ATTACH HARDWARE CORRODED/RUSTED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED THE ATTACHMENT HARDWARE ON THE RT SPOILERON RETENTION ANGLE WITH SERVICEABLE ATTACHMENT HARDWARE, IAW CRJ 200 AMM, SRM.
- [SDR SWIA202054423](https://openairdocs.org/sdr/SWIA202054423.md): Angle · cracked · Oct 26, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 484.00 INTERCOSTAL CLIPS ARE CRACKED AT LBL 27.00 AND LBL 36.00. C-CHECK RO 11/24/2020. REMOVED, FABRICATED, AND INSTALLED CLIPS AT FS 484 INTERCOSTAL AT LBL 27 AND LBL 36, IAW CRJ 200 SRM AND REO. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202054422](https://openairdocs.org/sdr/SWIA202054422.md): Tee Fitting · cracked · Oct 26, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RBL 9.00 HAS A CRACKED "T" FITTING ON THE INBOARD SIDE OF BEAM AT FS 461.00. C-CHECK RO 11/24/2020. REMOVED AND REPLACED "T" FITTING AT FS 461.00, IAW CRJ 200 SRM.
- [SDR SWIA202054421](https://openairdocs.org/sdr/SWIA202054421.md): Angle · cracked · Oct 26, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484.00 INTERCOSTAL CLIP IS CRACKED AT RBL 36.00. C-CHECK RO 11/24/2020. REMOVED CRACKED CLIP AT FS 484 RBL 36, FABRICATED, LOCATED, DRILLED AND INSTALLED REPLACEMENT CLIP IAW REO.
- [SDR SWIA202054428](https://openairdocs.org/sdr/SWIA202054428.md): Seat Track · corroded · Oct 23, 2020 · N928EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT TRACK FS 364-409+16 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. LT SIDE SEAT TRACK FS 364-409+16 SEGMENT IS CORRODED. REMOVED SEAT TRACK, LOCATED DRILLED COUNTERSUNKED AND INSTALLED NEW SIDE SEAT RAIL REFERENCE CONTINUATION CARD FOR THE WORK PE
- [SDR SWIA202054419](https://openairdocs.org/sdr/SWIA202054419.md): Floorbeam · cracked · Oct 22, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOOR CROSSBEAM IS CRACKED AT LBL 12 AND RBL 12. C-CHECK RO 11/24/2020. REPAIRED IAW GREO. COMPLETED TASK CARD AND ATTACHED 337. WEIGHT CHANGE OF 1.25 LBS AT FS 280.
- [SDR SWIA202054418](https://openairdocs.org/sdr/SWIA202054418.md): Frame · corroded · Oct 22, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333 FRAME IS CORRODED BETWEEN STGR 26L AND STGR 25R. C-CHECK RO 11/24/2020. INSTALLED SERVICEABLE 333 LOWER FRAME BETWEEN STR 26L AND 25R, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337, NO WEIGHT CHANGE. REFERENCE CONTINUATION CAR
- [SDR SWIA202054411](https://openairdocs.org/sdr/SWIA202054411.md): Frame · corroded · Oct 22, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605 FRAME IS CORRODED BETWEEN STGR 20L AND STGR 18R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FS 605 FRAME BETWEEN STGR 20L AND 20R, IAW CRJ 200 SRM AND SKY CARD. NO WEIGHT CHANGE AND M377 FORM HAS BEEN COMPLETED. REF ATTACHED CONTINUATION CARD FOR D
- [SDR SWIA202054410](https://openairdocs.org/sdr/SWIA202054410.md): Frame · corroded · Oct 22, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 589 FRAME IS CORRODED BETWEEN STGR 20L AND STRG 18R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FS 589 FRAME BETWEEN STGR 20L AND STGR 20R, IAW CRJ 200 SRM AND ATTACHED SKY CARD NO WEIGHT CHANGE FORM 337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR D
- [SDR SWIA202054427](https://openairdocs.org/sdr/SWIA202054427.md): Bolt · corroded · Oct 19, 2020 · N928EV · Cndair CL6002B19 · Ailerons
  > RT AILERON INBOARD PCU HARDWARE IS CORRODED INBOARD. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RT INBOARD AILERON PCU MOUNTING BOLTS, IAW CRJ 200 AMM AND REMOVED THE UNSERVICEABLE HARDWARE FOR THE RT INBOARD AILERON PUC OUTPUT LINK AND PLACED SERVICEABLE H
- [SDR SWIA202054412](https://openairdocs.org/sdr/SWIA202054412.md): Skin · corroded · Oct 19, 2020 · N928EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FOR WING TO FUSELAGE FAIRINGS 191BB AND 192BB ATTACHMENT AREA IS CORRODED. C-CHECK RO 11/24/2020. REPAIRED FUSELAGE SKIN AT THE WING TO FUSELAGE FAIRINGS 191BB AND 192BB, IAW MHIRJ REO. COMPLETED TASK CARD AND ATTACHED FORM 337, DTA IS DUE WIT
- [SDR SWIA202052792](https://openairdocs.org/sdr/SWIA202052792.md): Intercostal · corroded · Sep 29, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING PAX DOOR HINGE REPLACEMENT FOUND CORROSION ON INTERCOSTAL AT STGR 21 BETWEEN STA 333.00 & STA 349.00. FILED CLOSED RO 9/4/2020. REMOVED AND REPLACED WITH SERVICEABLE INTERCOSTAL P/N 601R31527-19 AT STGR 21 LT BETWEEN STA 333.00 & STA 349.00, REF DWG,
- [SDR SWIA2020090852310](https://openairdocs.org/sdr/SWIA2020090852310.md): Hinge · worn · Aug 16, 2020 · N928EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR FUSELAGE SIDE HINGE WORN TO LIMITS. CAUSING ALIGNMENT PROBLEM FOR PAX DOOR, FILED CLOSED. REMOVED AND REPLACED PAX DOOR HINGE (AIRFRAME SIDE), REFERENCE APPLICABLE STEPS IN SRM. SEE CP 21388140 & CP 21384976 FOR FURTHER MAINTENANCE.
- [SDR SWIA202054426](https://openairdocs.org/sdr/SWIA202054426.md): Bolt · corroded · Jul 13, 2020 · N928EV · Cndair CL6002B19 · Ailerons
  > REMOVE & REINSTALL RT AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON, IAW AMM. COMPLY WITH TASK CARD. C-CHECK RO 11/24/2020. REMOVED & REINSTALLED RT AILERON TO PERFORM REPLACMENT
- [SDR SWIA202054413](https://openairdocs.org/sdr/SWIA202054413.md): Angle · weak · Jul 13, 2020 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT. C-CHECK RO 11/24/2020. COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT, REF ATTACHED CARD. W&B PRO
- [SDR SWIA2018113045312](https://openairdocs.org/sdr/SWIA2018113045312.md): Door Sill · corroded · Nov 16, 2018 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SERVICE DOOR SILL FLOOR PROTECTOR PLATE AROUND UPPER FASTENER HOLES. (C-CHECK) RO: 11/29/2018. REPLACED SERVICE DOOR FLOOR PROTECTOR PLATE REF SRM 51-40-11.
- [SDR SWIA2018113045314](https://openairdocs.org/sdr/SWIA2018113045314.md): Hinge · gouged · Oct 31, 2018 · N928EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE FUSELAGE SIDE AFT LANDING GOUGED. (C-CHECK) RO: 11/29/2018. REPAIRED PAX DOOR FUSELAGE SIDE HINGE REF REO 601R-53-21-3036.
- [SDR SWIA2018113045313](https://openairdocs.org/sdr/SWIA2018113045313.md): Door Sill · corroded · Oct 31, 2018 · N928EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL JUST INSIDE DOOR CUTOUT HAS CORROSION. (C-CHECK) RO: 11/29/2018. REMOVED AND INSTALLED NEW CARGO DOOR SILL REF REO 601R-53-61-1574.
- [SDR SWIA2018113045309](https://openairdocs.org/sdr/SWIA2018113045309.md): Stop Fitting · corroded · Oct 31, 2018 · N928EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR STOP FITTINGS (2 EA) HAVE CORROSION. (C-CHECK) RO: 11/29/2018. REMOVED AND INSTALLED NEW CARGO DOOR STOP FITTINGS WITH NEW HARDWARE REF SRM 51-41-02.
- [SDR SWIA2018113045308](https://openairdocs.org/sdr/SWIA2018113045308.md): Panel · chafed · Oct 31, 2018 · N928EV · Cndair CL6002B19 · Ailerons
  > RT AILERON PANEL 699BB IS CHAFED (C-CHECK) RO: 11/29/2018. BLENDED CHAFED TO A SMOOTH CONTOUR REF REO 601R-57-61-661.

Next page: https://openairdocs.org/aircraft/N928EV/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 = 'N928EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N928EV/reports

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