# Service difficulty reports: N915EV

A list on [N915EV](https://openairdocs.org/aircraft/N915EV.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 · 169 reports

- [SDR SWIA2026022575723](https://openairdocs.org/sdr/SWIA2026022575723.md): Former · corroded · Feb 25, 2026 · N915EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER MID FORMER F.S. 327.763 FOUND TO BE CORRODED (C-CHECK RO 04/16/2026)REMOVED AND INSTALLED NEW SERVICABLE PAX DOOR LOWER MID FORMER FS 327.763 IAW SRM 51-42-06, 51-42-21 51-40-11 AND SKY CARD 51-900-1003-SKY.
- [SDR SWIA2026022575715](https://openairdocs.org/sdr/SWIA2026022575715.md): Former · corroded · Feb 25, 2026 · N915EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER F.S. 313.56 FOUND TO BE CORRODED. REMOVED AND INSTALLED NEW PAX DOOR FORMER FS 313.56 P/N 601R318086-1 IAW CRJ 200 SRM 51-42-06,51-42-13, 51-40-11 AND SKYCARD 51-900-1003-SKY.
- [SDR SWIA2026021775719](https://openairdocs.org/sdr/SWIA2026021775719.md): Pressure Deck · corroded · Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT PRESSURE FLOOR SKIN IS CORRODED AT (1EA) LOCATION AT F.S. 529.00. REPAIRED LH PRESSURE FLOOR SKIN AT FS529.00 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06 06 COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026021775717](https://openairdocs.org/sdr/SWIA2026021775717.md): Pressure Deck · corroded · Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT PRESSURE FLOOR SKIN IS CORRODED AT (2EA) NUTPLATE LOCATIONS BETWEEN F.S. 499.00 AND F.S.513.00. (C-CHECK RO 04/16/2026)REPAIRED R/H PERESSURE FLOOR SKIN AT 2EA NUTPLATE LOCATIONS BETWEEN FS499.00 AND FS513.00 IAW REO 601R-53-41-666 REV-C DATED 2012-11
- [SDR SWIA2026021775708](https://openairdocs.org/sdr/SWIA2026021775708.md): Floor Skin · gouged · Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT PRESSURE FLOOR SKIN IS GOUGED AT (1EA) NUTPLATE LOCATION BETWEEN F.S. 424.00 AND F.S. 439.00. REPAIRED RH FLOOR SKIN GOUGE AT 1EA NUTPLATE LOACTION BETWEEN FS424.00 AND FS439.00 IAW REO 601R-53-41-3409 REV--. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026021775707](https://openairdocs.org/sdr/SWIA2026021775707.md): Pressure Deck · corroded · Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT PRESSURE FLOOR SKIN CORRODED AT ONE LOCATION BETWEEN BS 544 - 559. REPAIRED RT PRESSURE FLOOR SKIN IAW REO 601R-53-41-666, REV-C.
- [SDR SWIA2026021775705](https://openairdocs.org/sdr/SWIA2026021775705.md): Floor Skin · gouged · Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT PRESSURE FLOOR SKIN IS GOUGED AT ONE NUTPLATE LOCATION BTWN BS 513 & 529. REPAIRED RT PRESSURE FLOOR SKIN IAW REO 601R-53-41-3409 REV--. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026021175721](https://openairdocs.org/sdr/SWIA2026021175721.md): Hinge · damaged · Feb 11, 2026 · N915EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON THE PAX DOOR ROLL PIN HOLE IS ELONGATED. PERFORMED A MAJOR REPAIR TO THE PAX DOOR PIANO HINGE HALF (DOOR SIDE) BY INSTALLING A LARGER SPRING PIN IAW MHIRJ REO 601R-52-11-3094 REV-. COMPLETED SKYWEST RII MAJOR REPAIR TASK CARD 51-900-1003-SK
- [SDR SWIA2026021175704](https://openairdocs.org/sdr/SWIA2026021175704.md): Floor Support · corroded · Feb 11, 2026 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT CORRODED AT BS 559 FOUND TO BE OUT OF LIMITS IAW REO 601R-53-41-666, REV-C. REPAIRED RT FLOOR SUPPORT IAW REO 601R53-41-3408, REV -. 6 AND SKY CARD 51-900-1003-SKY.
- [SDR SWIA2026021075714](https://openairdocs.org/sdr/SWIA2026021075714.md): Floor Support · corroded · Feb 10, 2026 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT IS CORRODED BETWEEN F.S. 461 TO F.S. 473, F.S. 529 TO F.S. 544 AND F.S. 544 TO F.S. 559. BLENDED OUT CORROSION AT FS461 TO FS473, FS529 TO FS544 AND FS544 TO FS559 PERFORMED NDT AND RESTORED REWORKED ARE IAW REO 601R-53-41-666 REV-C DATED
- [SDR SWIA2026021075713](https://openairdocs.org/sdr/SWIA2026021075713.md): Stringer · corroded · Feb 10, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 21L IS CORRODED BETWEEN FS 574 AND 589. REMOVED AND INSTALLED A SERVICABLE SECTION OF STRINGER 21L IAW SRM 53-00-03 REPAIR TYPE S6451, SRM 51-42-06, & REO 601R-53-61-8492 REV --.
- [SDR SWIA2026021075703](https://openairdocs.org/sdr/SWIA2026021075703.md): Frame · corroded · Feb 10, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 319 FRAME IS CORRODED BETWEEN STR 23L AND 22L. REMOVED AND REPLACED FRAME SECTOR AT FS319 BETWEEN STR 23L AND 21L IAW SRM 51-42-06 AND 51-42-21.
- [SDR SWIA2026020975710](https://openairdocs.org/sdr/SWIA2026020975710.md): Floorbeam · chafed · Feb 9, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FITTING ON FLOORBEAM RBL27 AT F.S.621 HAS 2EA. CHAFES. REMOVED AND REPLACED FITTING AT FLOORBEAM RBL27 FS621 IAW CRJ 200 SRM 51-42-22 AND REO 601R-53-61-3778 REV-B DATED 2016-12-19 FOR ALTERNATE FASTENERS COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026020875711](https://openairdocs.org/sdr/SWIA2026020875711.md): Skin · chafed · Feb 8, 2026 · N915EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WING PLANK ACCESS HOLE AT 510BB, AFT LANDING CHAFED(MARKED WITH TAPE). PERFORMED A MAJOR REPAIR BY BLENDING CORROSION ON LOWER WING PLANK ACCESS HOLE AT 510BB LANDING IAW REO 601R-57-21-030 REV L DATED 2014-02-05. COMPLETED SKYWEST TASK CARD 51-900-1
- [SDR SWIA2026020775722](https://openairdocs.org/sdr/SWIA2026020775722.md): Frame · corroded · Feb 7, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 349 FRAME IS CORRODED FROM STR 25L TO 25R ON THE FRONT AND BACK SIDE. REPAIRED BS 349 FRAME CORROSION FROM STR 25L TO 25R ON THE FRONT AND BACK SIDE IAW REO 601R-53-21-3798 REV --, AND SKY CARD 51-900-1003-SKY.
- [SDR SWIA2026020575712](https://openairdocs.org/sdr/SWIA2026020575712.md): Skin · dented · Feb 5, 2026 · N915EV · Cndair CL6002B19 · Trailing Edge Flaps
  > DENT ON BOTTOM SIDE OF LT INBOARD FLAP INBOARD SIDE. REPAIRED LT INBD FLAP BOTTOM INDB SIDE DENT IAW CRJ 200 SRM 57-52-00-02 REPAIR 3 COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026012975720](https://openairdocs.org/sdr/SWIA2026012975720.md): Window Post · dented · Jan 29, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST LOWER LH FITTING IS DENTED. (C-CHECK RO 04/16/2026)REMOVED AND REPLACED WINDSHIELD CENTER POST LH LOWER FITTING IAW SRM 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026012875716](https://openairdocs.org/sdr/SWIA2026012875716.md): Bracket · corroded · Jan 28, 2026 · N915EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR INNER STRUCTURE, LOWER FRAME SPLICE BRACKET IS CORRODED. REMOVED AND REPLACED SERVICE DOOR INNER STRUCTURE LOWER FRAME SPLICE BRACKET IAW CRJ 200 SRM 51-42-06 COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026012775718](https://openairdocs.org/sdr/SWIA2026012775718.md): Panel · damaged · Jan 27, 2026 · N915EV · Cndair CL6002B19 · Wing, Plate/Skin
  > FAILED NDT. FOUND 70% FSH INDICATIONS ON AFT SIDE OF WS185.5 PANEL 650BB ACCESS HOLE. REPAIRED WING LOWER PLANK ACCESS DOOR AT PNL 650BB IAW REO 601R-57-21-030 REV L DATED 2014-02-05 AND REO 601R-57-21-4033 REV. -- DATED 20206-02-09. COMPLETED TASK CARD 51-9
- [SDR SWIA2026011675709](https://openairdocs.org/sdr/SWIA2026011675709.md): Skin · corroded · Jan 16, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN AT AFT LAV SERVICING POINT IS CORRODED BETWEEN FS559+80 AND FS559+112 BETWEEN STGR20R AND STGR24R. REPAIRED EXTERNAL SKIN AT AFT LAV SERVICING POINT BETWEEN FS559+80 AND FS559+112 BETWEEN STGR20R AND STGR24R IAW MHIRJ REO 601R-53-51-729
- [SDR SWIA2026041775706](https://openairdocs.org/sdr/SWIA2026041775706.md): Doubler · corroded · Jan 16, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN DOUBLER AT THE LAV SERVICING POINT IS CORRODED. REPAIRED EXTERNAL SKIN DOUBLER AT LAV SERVICING POINT IAW REO 601R-53-51-729 REV--. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA20250424011](https://openairdocs.org/sdr/SWIA20250424011.md): Warning Message · illuminated · Apr 11, 2025 · N915EV · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > CREW DIVERTED TO PIT DUE TO ANTI ICE DUCT WARNING MSSG. (FLIGHT 5113 - FILED CLOSED) APR 15, 2025 STATION: PIT--PLEASE REFERENCE AML 1582914, PLEASE REFERENCE AML 1582036 PLEASE REFERENCE AML 1582037 FOR MAINTENANCE COMPLIED WITH. TROUBLESHOT ANTI ICE
- [SDR SWI2025F00446](https://openairdocs.org/sdr/SWI2025F00446.md): Warning Message · activated · Apr 11, 2025 · N915EV · Cndair CL6002B19 · Fire Protection System
  > CREW DIVERTED TO PIT DUE TO ANTI ICE DUCT WARNING MSSG. (FLIGHT 5113 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20250226004](https://openairdocs.org/sdr/SWIA20250226004.md): Windshield · cracked · Feb 24, 2025 · N915EV · Cndair CL6002B19 · Flight Compartment Windows
  > WINDSHIELD CRACKED IN FLIGHT. QRH EXECUTED AND DIVERTED TO KCOS (FLIGHT 5213 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29693854 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED LEFT WINDSHEILD IAW AMM 56-11-00 AND TASK CARD
- [SDR SWIA202403180016](https://openairdocs.org/sdr/SWIA202403180016.md): Oxygen Bottle · low pressure · Mar 16, 2024 · N915EV · Cndair CL6002B19 · Crew Oxygen System
  > OXY LO PRESS DURING CRUISE. (FLIGHT 4634 FILED CLOSED)SERVICED CREW O2 TO PROPER LEVEL REF CRJ200 AMM 12-16-35. MCI IS ALREADY IN PLACE FOR TROUBLESHOOTING ON CREW O2 SYSTEM AND A POTENTIAL LEAK.
- [SDR SWIA202266930](https://openairdocs.org/sdr/SWIA202266930.md): Structure · damaged · Nov 9, 2022 · N915EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > FOUND HOLE IN UNDERLYING STRUCTURE IN THE FOOTPRINT OF PANEL 594UB TO BE DAMAGED REPAIRED THE STRUCTURE IAW REO 601R-57-51-1003, REV-.
- [SDR SWIA202266929](https://openairdocs.org/sdr/SWIA202266929.md): Skin · corroded · Oct 24, 2022 · N915EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > VHF ANTENNA CUT OUT AT F.S. 455.8 STGR 0 AFT O/B DOME NUTPLATE HAS A HOLE CORRODED. COMPLIED WITH REO 601R-53-41-3091 REV-. MAJOR REPAIR.
- [SDR SWIA202266928](https://openairdocs.org/sdr/SWIA202266928.md): Hinge · gouged · Oct 24, 2022 · N915EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE LUGS ON FUSELAGE SIDE ARE GOUGED AT MID HINGE. REMOVED AND REPLACED THE DOOR HINGE IAW SRM 53-21-23.
- [SDR SWIA202266927](https://openairdocs.org/sdr/SWIA202266927.md): Floor Support · corroded · Oct 15, 2022 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT BETWEEN BS 409+128 & 559 FOUND CORRODED AT MULTIPLE LOCATIONS. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-666, REV -C. MAJOR REPAIR.
- [SDR SWIA202266926](https://openairdocs.org/sdr/SWIA202266926.md): Floor Support · corroded · Oct 14, 2022 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT BETWEEN BS 409+128 & 559. FOUND CORRODED AT MULTIPLE LOCATIONS. COMPLIED WITH REO 601R-53-41-666 REV -C. MAJOR REPAIR.
- [SDR SWIA202266925](https://openairdocs.org/sdr/SWIA202266925.md): Stringer · cracked · Oct 13, 2022 · N915EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED, BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03. MAJOR REPAIR.
- [SDR SWIA202266924](https://openairdocs.org/sdr/SWIA202266924.md): Pan · corroded · Oct 12, 2022 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER PAN IS CORRODED FORWARD AND AFT SIDES. REMOVED LOWER AFT SERVICE DOOR PAN IAW CRJ 200 SRM 51-42-06. INSTALLED SERVICEABLE LOWER AFT SERVICE DOOR PAN IAW CRJ 200 SRM 51-42-06. MAJOR REPAIR.
- [SDR SWIA202266923](https://openairdocs.org/sdr/SWIA202266923.md): Landing · corroded · Oct 12, 2022 · N915EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT WING PLANK HAS SEVERAL AREAS OF CORROSION AROUND FUEL PANEL 540BB OPENING. REPAIRED THE WING PANEL LANDING IAW 601R-57-21-0030 REV-, MAJOR REPAIR TASK CARD 51-900-1003-SKY.
- [SDR SWIA202266922](https://openairdocs.org/sdr/SWIA202266922.md): Floor Support · corroded · Oct 8, 2022 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT UPPER CAP INBD FLANGE HAD MULTIPLE AREAS OF CORROSION BETWEEN BS 409 - 409+112. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO 601R-53-31-1248 REV-. MAJOR REPAIR.
- [SDR SWIA202266921](https://openairdocs.org/sdr/SWIA202266921.md): Floor Support · corroded · Oct 8, 2022 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT UPPER CAP WAS FOUND CORRODED BS 409+123 - 424. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-3085, REV-.
- [SDR SWIA202266920](https://openairdocs.org/sdr/SWIA202266920.md): Floor Support · corroded · Oct 8, 2022 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SUPPORT UPPER CAP FOUND CORRODED BETWEEN BS 409+123 TO 424. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-3087, REV -.
- [SDR SWIA202266919](https://openairdocs.org/sdr/SWIA202266919.md): Frame · corroded · Oct 8, 2022 · N915EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR F.S.310 IS CORRODED AT STRINGER 27L. REMOVED THE FRAME SECTION, REINFORCMENT STRAP, AND SPLICES IAW SRM 51-42-21 AND 51-42-06. INSTALLED A FRAME NEW SECTION IAW SRM 51-42-21 AND 51-42-06. MAJOR REPAIR.
- [SDR SWIA202266918](https://openairdocs.org/sdr/SWIA202266918.md): Frame · cracked · Oct 4, 2022 · N915EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 718 FRAME IS CRACKED BETWEEN STGR 11R AND 12R. REPAIRED THE FRAME IAW REO 601R-53-61-193, REV A, AND SRM 51-42-06 REV-39.
- [SDR SWIA202266917](https://openairdocs.org/sdr/SWIA202266917.md): Frame · cracked · Oct 4, 2022 · N915EV · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 718 FRAME FOUND CRACKED BETWEEN STRINGERS 11L & 12L. REPAIRED THE FRAME IAW REO 601R-53-61-193, REV A.
- [SDR SWIA202266916](https://openairdocs.org/sdr/SWIA202266916.md): Skin · chafed · Oct 3, 2022 · N915EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER SKIN IS CHAFED ALONG BL 45 WHERE FAIRING CONTACTS SKIN. REPAIRED THE SKIN IAW REO 601R-57-21-880, REV-D.
- [SDR SWIA202266915](https://openairdocs.org/sdr/SWIA202266915.md): Skin · chafed · Oct 3, 2022 · N915EV · Cndair CL6002B19 · Wing, Plate/Skin
  > L/H WING LOWER SKIN IS CHAFED FROM BL 0 TO LBL. 45. REPAIRED THE SKIN IAW REO 601R-57-21-880 REV-D.
- [SDR SWIA202266914](https://openairdocs.org/sdr/SWIA202266914.md): Structure · damaged · Oct 2, 2022 · N915EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > FOUND ONE ELONGATED SCREW HOLE ON PANEL 572AL THROUGH INTO STRUCTURE. REPAIRED THE STRUCTURE IAW REO 601R-57-31-1403 REV-.
- [SDR SWIA202266913](https://openairdocs.org/sdr/SWIA202266913.md): Skin · damaged · Sep 30, 2022 · N915EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SHANK UNDER PANEL 192BB. REPAIRED FUSELAGE SKIN UNDER PANEL 192BB IAW REO 601R-53-31-1246 REV -.
- [SDR SWIA202265957](https://openairdocs.org/sdr/SWIA202265957.md): None · failed · Jun 21, 2022 · N915EV · Cndair CL6002B19 · Landing Gear Door Actuator
  > ON T/O WE RECEIVED A NOSE GEAR DISAGREE WITH NOSE GEAR DOWN AND GEAR LEVER UP ALSO RECEIVED A CAUTION WOW OUTPUT AND NOSE STEERING INOP CAUTION MSG ASSOCIATED WITH THE MASTER WARNING RAN QRH AND RECEIVED 3 GREEN ON GEAR INDICATION (FLIGHT 5367 - FILED CLOS
- [SDR SWIA202156554](https://openairdocs.org/sdr/SWIA202156554.md): Stop Fitting · cracked · Feb 27, 2021 · N915EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR CUTOUT, UPPER/FWD STOP-FITTING IS CRACKED FILED CLOSED REMOVED AND REPLACED PASSENGER DOOR CUTOUT UPPER FORWARD STOP FITTING REFERENCING APPLICABLE STEPS OF CRJ200 SRM 51-42-20.
- [SDR SWIA2019091246307](https://openairdocs.org/sdr/SWIA2019091246307.md): Door Sill · corroded · Aug 5, 2019 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL AND SILL ANGLE ARE CORRODED BETWEEN FS 484 TO FS 499. (C-CHECK) RO: 09/12/2019 REPAIRED LT PRESSURE FLOOR SILL AND ANGLE IAW REO.
- [SDR SWIA2019091246306](https://openairdocs.org/sdr/SWIA2019091246306.md): Frame · cracked · Aug 2, 2019 · N915EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CRACKED AT FS333.00 BETWEEN STR 0 AND STR 2L. (C-CHECK) RO: 09/12/2019 REMOVED AND REPLACED FS 333 TOP FRAME SECTOR P/N: 601R32004-41 IAW SRM.
- [SDR SWIA2019091246305](https://openairdocs.org/sdr/SWIA2019091246305.md): Frame · corroded · Aug 2, 2019 · N915EV · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER FRAME SECTOR FS 574.00 CORRODED BETWEEN STR 25L TO 25R. (C-CHECK) RO: 09/12/2019 REPLACED LOWER FS 574 FRAME SECTOR IAW SRM.
- [SDR SWIA2019091246304](https://openairdocs.org/sdr/SWIA2019091246304.md): Strap · corroded · Aug 2, 2019 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRAP AT FS 559.00 LBL 27.0 TO LBL 45.0 FLOOR LEVEL IS CORRODED ON UPPER SURFACE. (C-CHECK) RO: 09/12/2019 REMOVED & REPLACED LT 559.00 LBL UPPER SURFACE STRAP P/N 601R31025-29 IAW SRM.
- [SDR SWIA2019091246303](https://openairdocs.org/sdr/SWIA2019091246303.md): Intercostal · corroded · Aug 2, 2019 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS DOOR SURROUND STRUCTURE, INTERCOSTAL CORRODED AT STR 27R BETWEEN FS349.00 AND FS364.00. (C-CHECK) RO: 09/12/2019 INSTALLED INTERCOSTAL BETWEEN FS349.00 AND FS364.00 AT STR 27R IAW SRM.

Next page: https://openairdocs.org/aircraft/N915EV/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 = 'N915EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N915EV/reports

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