# Service difficulty reports: N910EV

A list on [N910EV](https://openairdocs.org/aircraft/N910EV.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 4 · 152 reports

- [SDR SWIA2026100877555](https://openairdocs.org/sdr/SWIA2026100877555.md): Landing Gear · malfunctioned · Oct 8, 2026 · N910EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > NOSE GEAR DID NOT COME UP WHEN THE GEAR LEVER WAS SELECTED TO THE UP POSITION. RAN QRH, GEAR CAME DOWN. FLIGHT 5745. PERFORMED AN OPS CHECK OF NLG WOW 2 PROXIMITY SENSOR & CENTERED WOW PROXIMITY SENSOR IAW AMM 32-61-05, OPS CHKD GOOD. PERFORMED NLG GEAR S
- [SDR SWI2025F01846](https://openairdocs.org/sdr/SWI2025F01846.md): Floorbeam · cracked · Nov 4, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > TRANSVERSE FLOOR BEAM @ FS. 589 FOUND TO BE CRACKED IN MULTIPLE LOCATIONS WHERE AFT CARGO DOOR LOWER SILL SITS. REPAIRED TRANSVERSE BEAM AT FS 589.00 IAW MHIRJ REO 601R-53-61-8412 REV--. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUE CARD FOR WORK PE
- [SDR SWIA2025121901104](https://openairdocs.org/sdr/SWIA2025121901104.md): Door Sill · corroded · Nov 4, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Structure
  > AFT CARGO DOOR LOWER SILL, CORRODED IN MULTIPLE LOCATIONS AND BENT, EVAL REQUIRED. REMOVED AND REPLACED CARGO DOOR LOWER SILL IAW SRM 51-42-21, 51-40-11, 51-42-06, 51-42-13, REV. 39B, AND REO 601R-53-61-8412, REV--. COMPLETED TASK CARD 51-900-1003-SKY. R
- [SDR SWIA2025121901018](https://openairdocs.org/sdr/SWIA2025121901018.md): Spar · damaged · Oct 18, 2025 · N910EV · Cndair CL6002B19 · Ailerons
  > LEFT AILERON AFT SPAR MOST OUTBOARD BORES ARE OVERSIZED. REPAIRED R/H AILERON AFT SPAR MOST OTBD AND INBD BORE ON WING IAW GREO 601R-57-51-015 REV NC.
- [SDR SWIA2025121901015](https://openairdocs.org/sdr/SWIA2025121901015.md): Drain · misrepaired · Oct 15, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Structure
  > WHILE WORKING SB 601R-57-054 INADVERTENTLY REAMED SATELLITE HOLES FOR WATER DRAINS AT BL 0 ON LT & RT SIDES BETWEEN STRINGERS 14-15. REPAIRED SATELLITE HOLES FOR WATER DRAINS AT BL 0 ON LT AND RT SIDE BETWEEN STRS 14-15 IAW REO 601R-57-21-3982 REV -.
- [SDR SWIA2025121901006](https://openairdocs.org/sdr/SWIA2025121901006.md): Intercostal · corroded · Oct 6, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FOUND TO BE SEVERELY CORRODED ON MORE THAN ONE ELEMENT REQUIRING REPLACEMENT LOCATED AT BS 364, S25L - 25R. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR W
- [SDR SWIA202512190004](https://openairdocs.org/sdr/SWIA202512190004.md): Mount Bracket · damaged · Oct 4, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Structure
  > UPON INSTALLATION OF THE A/C POWER RECEPTACLE BRACKET MOUNT FOUND 1 EA FASTENER HOLE TO BE ELONGATED ON AFT O/B SIDE IN CORNER MARKED WITH RED TAPE. REPAIRED A/C POWER RECEPTACLE BRACKET MOUNT IAW MHIRJ REO 601R-53-11-4026 REV -. COMPLETED SKYCARD 51-900-100
- [SDR SWIA2025121900930](https://openairdocs.org/sdr/SWIA2025121900930.md): Intercostal · corroded · Sep 30, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTALS FOUND TO BE SEVERELY CORRODED ON MORE THAN ONE ELEMENT REQUIRING REPLACEMENT. REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-42-06, AND 51-42-21 06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202512190925](https://openairdocs.org/sdr/SWIA202512190925.md): Spar · damaged · Sep 25, 2025 · N910EV · Cndair CL6002B19 · Ailerons
  > R/H AILERON AFT SPAR MOST OUTBOARD BORES ARE OVERSIZED. REPAIRED R/H AILERON AFT SPAR MOST OTBD AND INBD BORE ON WING IAW GREO 601R-57-51-015 REV NC.
- [SDR SWIA2025121900917](https://openairdocs.org/sdr/SWIA2025121900917.md): Floor Support · corroded · Sep 17, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SUPPORT IS CORRODED AT BS 549. REPAIRED THE CORROSION ON THE LT PRESSURE FLOOR SUPPORT AT FS 549 IAW REO 601R-53-41-666, REV C, AND SKY CARD 51-900-1003-SKY.
- [SDR SWI2025F01836](https://openairdocs.org/sdr/SWI2025F01836.md): Intercostal · corroded · Sep 15, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD7A FWD INTERCOSTAL FOUND TO BE CORRODED. REQUIRES REPLACEMENT. REPLACED PAX DOOR DD7A FWD INTERCOSTAL IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2025F01835](https://openairdocs.org/sdr/SWI2025F01835.md): Intercostal · corroded · Sep 15, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 MID CORRODED. REQUIRES REPLACEMENT. REMOVED AND REPLACED THE PAX DOOR MID INTERCOSTAL DD3 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2025121900915](https://openairdocs.org/sdr/SWIA2025121900915.md): Intercostal · corroded · Sep 15, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD2 MID FOUND TO BE CORRODED. REQUIRES REPLACEMENT. REMOVED AND REPLACED THE PAX DOOR MID INTERCOSTAL DD2 IAW SRM 51-42-06 AND 51-42-21, COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. CONTINUATION CARD FOR WORK PERF
- [SDR SWIA202512190911](https://openairdocs.org/sdr/SWIA202512190911.md): Former · corroded · Sep 11, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID FORMER, FS329.41 BETWEEN DD5 AND DD6 FOUND TO BE CORRODED REQUIRED REPLACEMENT. REPLACED PAX DOOR MID FORMER AT FS329.41 IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202512190909](https://openairdocs.org/sdr/SWIA202512190909.md): Rib · cracked · Sep 9, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > RIGHT MLG BATTERY RIB IS CRACKED AT WS 53.60 FWD O/B SIDE. REMOVED AND REPLACED RT BATTERY RIB AT WS 53.60 IAW SRM 51-42-06 AND 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2025F01845](https://openairdocs.org/sdr/SWI2025F01845.md): Drip Tray · damaged · Sep 8, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DRIP TRAY AT LBL 27, FS 409 IS DAMAGED. REPAIRED DRIP TRAY AND MOUNTING STRUCTURE IAW MHIRJ REO 601R-53-31-1351 REV-, AND REO 601R-53-31-1353, REV-. COMPLETED TASK CARD 51-900-1003-SKY. REF CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2025F01844](https://openairdocs.org/sdr/SWI2025F01844.md): Frame · corroded · Sep 8, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 319 FRAME IS CORRODED BETWEEN S18L AND 20L. REMOVED AND REPLACED THE STUB FRAME AT IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2025F01843](https://openairdocs.org/sdr/SWI2025F01843.md): Skin · cracked · Sep 8, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RIGHT FORWARD FUSELAGE SKIN IS CRACKED AT THE AFT LATCH CUTOUT OF THE TRU DOOR. REPLACED RT FORWARD FUSELAGE SKIN IAW SRM 51-42-06, 51-42-13, AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025121900908](https://openairdocs.org/sdr/SWIA2025121900908.md): Skin · cracked · Sep 8, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT FORWARD FUSELAGE SKIN IS CRACKED AT THE AFT LATCH CUTOUT OF THE TRU DOOR. REPLACED LT FORWARD FUSELAGE SKIN IAW SRM 51-42-06, 51-42-13, & 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWI2025F01834](https://openairdocs.org/sdr/SWI2025F01834.md): Door Sill · corroded · Sep 6, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR LOWER SILL FLOOR SUPPORT ANGLE IAW SRM 51-42-06, 51-42-13, AND 51-42-13. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2025F01833](https://openairdocs.org/sdr/SWI2025F01833.md): Floorbeam · cracked · Sep 6, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 CROSSBEAM LBL9 IB ANGLE IS CRACKED. (C-CHECK RO 12/17/2025)FABRICATED 1 EA CLAP AT FS 280 CROSSBEAM LBL 9IAW CRJ 200 SRM 51-40-06, 51-40-11, 51-25-00, 51-42-22 AND 51-42-21 REV. 39B, DATED 06-NOV-11. REFERENCING REO 601R-53-11-171 REV D DATED 13 FEB 0
- [SDR SWIA2025121900906](https://openairdocs.org/sdr/SWIA2025121900906.md): Floor Support · corroded · Sep 6, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SUPPORT TOP INBD FLANGE IS CORRODED FROM BS 409+5 TO BS 409+118. REMOVED AND REPLACED THE FLOOR SUPPORT CAP AT RBL9 FROM FS409+5-409+118 IAW SRM 51-42-06, 51-42-21, AND REO 601R-53-31-1350, REV-- DATED 2025-09-25. REF CONTINUATION CARD FOR ALL WOR
- [SDR SWIA202512190905](https://openairdocs.org/sdr/SWIA202512190905.md): Fitting · cracked · Sep 5, 2025 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 460.00 FITTING IS CRACKED ON THE OTBD SIDE OF LBL 9, FLOORBEAM. REMOVED AND INSTALLED SERVICEABLE FITTING AT BS 460 IAW REO 601R-53-41-3353, REV-. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2025F01847](https://openairdocs.org/sdr/SWI2025F01847.md): Angle · cracked · Sep 2, 2025 · N910EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT WING, BATTERY RIB AT WS 53.60 ANGLE ON INBD SIDE OF WEB IS CRACKED AND WEB IS CRACKED AS WELL. REMOVED AND REPLACED LT WING BATTERY RIB IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202512190902](https://openairdocs.org/sdr/SWIA202512190902.md): Angle · cracked · Sep 2, 2025 · N910EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT WING, BATTERY RIB AT WS 48.30 ANGLE IS CRACKED. REMOVED AND REPLACED THE LT UPPER BATTERY RIB ANGLE IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202512190831](https://openairdocs.org/sdr/SWIA202512190831.md): Post · failed insp · Aug 31, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Structure
  > BS 409+128 BL 0 VERTICAL POST RT & LT SIDES HAS INDICATIONS.3" LONG BY 100% FSH IN THE AFT RADIUS AT WL69. FAILED NDT INSPECTION. REMOVED AND REPLACED BS 409+128 BL 0 VERTICAL POST IAW REO 601R-53-41-889 REV-D, COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE
- [SDR SWIA202512190829](https://openairdocs.org/sdr/SWIA202512190829.md): Skin · misaligned · Aug 29, 2025 · N910EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR INNER SKIN HAS SEVERAL JO-BOLTS THAT ARE NOT PROPERLY INSTALLED. REPAIRED OVERSIZED HOLES AND INSTALLED FASTENERS IAW REO 601R-52-41-537 REV--. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWI2025F01842](https://openairdocs.org/sdr/SWI2025F01842.md): Intercostal · corroded · Aug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD 6 BETWEEN FS 320.163 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR MID INTERCOSTAL DD6 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2025F01841](https://openairdocs.org/sdr/SWI2025F01841.md): Intercostal · corroded · Aug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD 1 BETWEEN FS 323.361 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 MID BETWEEN FS323.61 AND FS336.961 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK
- [SDR SWI2025F01840](https://openairdocs.org/sdr/SWI2025F01840.md): Former · corroded · Aug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER IS CORRODED ON THE INSIDE. REMOVED AND REPLACED PAX DOOR AFT FORMER IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWI2025F01839](https://openairdocs.org/sdr/SWI2025F01839.md): Former · corroded · Aug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER IS CORRODED ON THE INSIDE. REMOVED AND REPLACED PAX DOOR FWD FORMER IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWI2025F01838](https://openairdocs.org/sdr/SWI2025F01838.md): Intercostal · corroded · Aug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD 1A BETWEEN FS 323.361 AND FS 336.961 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A IAW CRJ 200 SRM 51-42-06, 51-42-21 AND 51-42-11 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE. REF
- [SDR SWIA202512190827](https://openairdocs.org/sdr/SWIA202512190827.md): Intercostal · corroded · Aug 27, 2025 · N910EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL BETWEEN FS 320.163 AND FS 329.130 IS CORRODED. REMOVED AND REPLACED PAX DOOR MID INTERCOSTAL DD4 IAW CRJ 200 SRM 51-42-06 AND 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE. REFERENCE CONTI
- [SDR SWIA202512190826](https://openairdocs.org/sdr/SWIA202512190826.md): Skin · dented · Aug 26, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS FROM BS 589 - 621 BETWEEN S22R AND 27R. REPAIRED THE DENTS IAW 601R-53-61-8395, REV-. COMPLETED TASK CARD 51-900-1003-SKY. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWI2025F01837](https://openairdocs.org/sdr/SWI2025F01837.md): Skin · chafed · Aug 23, 2025 · N910EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK CHAFED ON TRAILING EDGE AT LWS 45.0 FROM CONTACT WITH PANEL 193AB. REPAIRED THE LT LOWER WING PLANK ON TRAILING EDGE IAW REO 601R-57-21-880, REV-D. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. COMPLETED AND ATTACHED MAJOR REP
- [SDR SWIA2025121900823](https://openairdocs.org/sdr/SWIA2025121900823.md): Skin · chafed · Aug 23, 2025 · N910EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK CHAFED ON TRAILING EDGE AT RWS 45.0 FROM CONTACT WITH PANEL 193AB. REPAIRED THE RT LOWER WING PLANK IAW REO 601R-57-21-880 REV-D. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. REFERENCE CONTINUATION CARD FOR WOR
- [SDR SWIA2025121900703](https://openairdocs.org/sdr/SWIA2025121900703.md): Door Frame · corroded · Jul 3, 2025 · N910EV · Cndair CL6002B19 · Fuselage Main, Structure
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA93189-601R-53-61-8212 MXCODEID77004-PR - FRAME FS574.00 AT CARGO DOOR FWD OPENING HAS CORROSION AT APPROX. WL 75.00. BLENDED CORROSION ON FRAME BS 574 AT CARGO DOOR FWD OPENING AT WL 75 IAW SRM 51-21-06 AND COMPLIED W
- [SDR SWI2025F00525](https://openairdocs.org/sdr/SWI2025F00525.md): Engine · faulted · Apr 12, 2025 · N910EV · Cndair CL6002B19 · Engine Oil Quantity
  > MASTER WARNING LH OIL PRESSURE ON CLIMB OUT, THEN N1 AND N2 AND ITT SPOOLED DOWN ON ITS OWN TO ZERO. RAN QRH ATTEMPTED RESTART TWICE - BOTH TIMES FAILED. COMING OUT OF XWA DIVERTED TO RAP. DECLARED AN EMERGENCY. NO EXTERNAL DAMAGE NOTED ON WALKAROUND POSTFLI
- [SDR SWIA20250414003](https://openairdocs.org/sdr/SWIA20250414003.md): Oil System · leaking · Apr 12, 2025 · N910EV · Cndair CL6002B19 · Turbine Engine Oil System
  > MASTER WARNING LH OIL PRESSURE ON CLIMB OUT, THEN N1 AND N2 AND ITT SPOOLED DOWN ON ITS OWN TO ZERO. RAN QRH ATTEMPTED RESTART TWICE - BOTH TIMES FAILED. COMING OUT OF XWA DIVERTED TO RAP. DECLARED AN EMERGENCY. NO EXTERNAL DAMAGE NOTED ON WALKAROUND POSTFLI
- [SDR SWIA2024082600010](https://openairdocs.org/sdr/SWIA2024082600010.md): Frame · corroded · Aug 10, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS574.00 AT CARGO DOOR FWD OPENING HAS CORROSION AT APPROX. WL75.00. (FILED - CLOSED)BLENDED CORROSION ON FRAME FS574.00 AT CARGO DOOR FWD OPENING AT APPROX WL75.00 WITH REFERENCE TO SRM 51-21-06 AND COMPLIED WITH REO 601R-53-61-8212 REV "--" DATED 2024-
- [SDR SWIA2024082673001](https://openairdocs.org/sdr/SWIA2024082673001.md): Frame Angle · corroded · Jul 31, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME ANGLE AT FS 605.00 BETWEEN STGR 18R AND 19R (FILED - CLOSED)REMOVED CORROSION FROM FRAME ANGLE AT FS 605.00 BETWEEN STGR 18R AND 19R WITH REFERENCE TO SRM 51-21-06 AND DISCOVERED CRACK. REPAIRED FRAME ANGLE AT FS 605.00 WITH REFERENCE TO RE
- [SDR SWI202408260781](https://openairdocs.org/sdr/SWI202408260781.md): Floor Support · corroded · Jul 29, 2024 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL HAS SURFACE CORROSION LOCATED AT APPROX. FS 555.00, 513.00 AND 447.00. (FILED - CLOSED)BLENDED AND REPAIRED ALL OF THE CORROSION AREAS ON THE RH PRESSURE FLOOR SILL FROM APPROX FS409 + 128 TO FS559.00 PER REO 601R-53-41-666 DATED: 2012-
- [SDR SWIA2024082672009](https://openairdocs.org/sdr/SWIA2024082672009.md): Floor Support · corroded · Jul 29, 2024 · N910EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL HAS NUMEROUS AREAS OF CORROSION LOCATED @ APPROX. FS460-465, 470.00-474.00, 485.5, 506.00, 513.00 AND 530.50. (FILED - CLOSED)BLENDED AND REPAIRED ALL OF THE CORROSION AREAS ON THE LH PRESSURE FLOOR SILL FROM APPROX FS409 + 128 TO FS559
- [SDR SWIA2024082672800](https://openairdocs.org/sdr/SWIA2024082672800.md): Track · cracked · Jul 28, 2024 · N910EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FORWARD TRACK LOWER CHANNEL CRACKED. (FILED - CLOSED)REMOVED AND REPLACED THE CARGO DOOR FORWARD TRACK LOWER CHANNEL WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
- [SDR SWIA2024082600724](https://openairdocs.org/sdr/SWIA2024082600724.md): Stiffener · cracked · Jul 24, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK INDICATION LOCATED FS409 + 128 BL0.00 ON VERTICAL BEAM/STIFFENER, FORWARD LEFT ANGLE AFT FACE, PROPAGATING OUTBOARD/AIRCRAFT LEFT FROM UPPER LEFT FASTENER (REFERENCE SRM 53-41-19 ITEM 6, FIGURE 1, SHEET 1 AND 3). (FILED - CLOSED)COMPLIED WITH REO 601R-53
- [SDR SWI202408260778](https://openairdocs.org/sdr/SWI202408260778.md): Pressure Blkhd · cracked · Jul 22, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14L, CLIP/ANGLE CRACKED. (FILED - CLOSED)REMOVED AND REPLACED CLIP/ANGLE ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGE
- [SDR SWI202408260777](https://openairdocs.org/sdr/SWI202408260777.md): Pressure Blkhd · cracked · Jul 22, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED - CLOSED)REMOVED AND REPLACED CLIP/ANGLE ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGE
- [SDR SWIA2024082600722](https://openairdocs.org/sdr/SWIA2024082600722.md): Pressure Blkhd · gouged · Jul 22, 2024 · N910EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD (FS621.00) FWD FACE HAS RIVET HEAD DAMAGE AND GOUGES ON DOUBLERS, LOCATED APPROX. LBL 18.00, 27.50, RBL 36.20, 27.50, 18.00 @ WL 87.50 AND WL 94.50. (FILED - CLOSED)UPON FURTHER INSPECTION FOUND 6 GOUGES LOCATED FS 621 BULKHEAD TOP DOUBL
- [SDR SWIA202162173](https://openairdocs.org/sdr/SWIA202162173.md): None · none · Oct 25, 2021 · N910EV · Cndair CL6002B19 · Fuselage Structure (General)
  > TRANSFER FROM EAML 763411: QTY 07 MIS-DRILLED HOLES RH H/STAB LOWER SKIN O/B RIB NO 9. REF REO601R-55-11-699 DATED 2021-10-22 REV -- (FLIGHT 5459 - FILED CLOSED) REPAIRED MIS-DRILLED HOLES IN RH HORZONTAL STAB LOWER SKIN BETWEEN RIB #7 - RIB #9 AND F/SPAR
- [SDR SWIA2021081260114](https://openairdocs.org/sdr/SWIA2021081260114.md): Engine · failed · Aug 7, 2021 · N910EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FAILURE AFTER DEPARTING KBIS THROUGH 7000€™. PERFORMED QRC, QRH PROCEDURES, RETURNED TO KBIS. (FLIGHT 5729 - FILED CLOSED) REF AML 703489 FOR CORRECTIVE. MORE INFORMATION WAS ADDED TO AML 703489 BUT BOTH ARE THE SAME DISCREPANCY. THIS DISCRE

Next page: https://openairdocs.org/aircraft/N910EV/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 = 'N910EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N910EV/reports

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