# Service difficulty reports: N930EV

A list on [N930EV](https://openairdocs.org/aircraft/N930EV.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 · 151 reports

- [SDR SWI2025F01125](https://openairdocs.org/sdr/SWI2025F01125.md): Uplock · faulted · Sep 1, 2025 · N930EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE ON DEPARTURE FROM CHICAGO AFTER SELECTING GEAR UP. LEFT GEAR WAS UP. NOSE UP. RIGHT GEAR WAS DASHED. RAN QRH. ALL THREE GEAR DOWN AND LOCKED AFTER QRH. CONTINUED TO LAND AT MKE. (FLIGHT 5225 - FILED CLOSED) THIS DISCREPANCY WAS T
- [SDR SWIA2024123100029](https://openairdocs.org/sdr/SWIA2024123100029.md): A/C Pack · warning message · Dec 29, 2024 · N930EV · Cndair CL6002B19 · Cabin Cooling System
  > DURING CLIMB IN DEN LEFT PACK DID NOT COME ON AND WE GOT CABIN ALT CAUTION AND FOLLOWED WITH CBAIN ALT WARNING. (FLIGHT 5024 - FILED CLOSED) REF AML 1502615 FOR LH PACK DEFERRAL AND AML 1502517 FOR PASSENGER O2 MASKS DEPLOYED CORRECTIVE ACTION.
- [SDR SWIA2024123001407](https://openairdocs.org/sdr/SWIA2024123001407.md): A/C Pack · faulted · Dec 29, 2024 · N930EV · Cndair CL6002B19 · Cabin Cooling System
  > DURING CLIMB IN DEN LEFT PACK DID NOT COME ON AND WE GOT CABIN ALT CAUTION AND FOLLOWED WITH CBAIN ALT WARNING. (FLIGHT 5024 - FILED OPEN) REF AML 1502615 FOR LH PACK DEFERRAL AND AML 1502517 FOR PASSENGER O2 MASKS DEPLOYED CORRECTIVE ACTION.
- [SDR SWIA20240514313](https://openairdocs.org/sdr/SWIA20240514313.md): Floor Support · corroded · Mar 13, 2024 · N930EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESS FLOOR ANGLE FROM FS 501-FS 509 HAS SIGNS OF CORROSION (C-CHECK RO 5/13/2024) REPAIRED CORROSION DAMAGE AT FS 501-509 RH FLOOR SILL ANGLE IAW REO 601R-53-41-666 REV-C DATE 2012-11-06, CRJ200 SRM 51-12-00, SRM 51-25-06, AND SRM 51-25-16. NDT PERFORM
- [SDR SWIA20240305](https://openairdocs.org/sdr/SWIA20240305.md): Rivet · worn · Mar 5, 2024 · N930EV · Cndair CL6002B19 · Landing Gear Doors
  > LH MLG DOOR FWD SIDE HAS EXCESSIVE WEAR, EVALUATE (C-CHECK RO 5/13/2024) REPAIRED L/H MLG DOOR FWD SIDE IAW REO 601R-52-82-102 AND CRJ200 SRM 51-42-06 AND CRJ200 SRM 52-82-00 CRJ200 SRM, 51-25-06 AND CRJ200 SRM 51-40-11 AND CRJ200 SRM 51-24-36 AND CRJ200
- [SDR SWIA20240514304](https://openairdocs.org/sdr/SWIA20240514304.md): Rivet · damaged · Mar 4, 2024 · N930EV · Cndair CL6002B19 · Fuselage Structure (General)
  > NUTPLATE FASTENER HOLE ON STRAP AND UNDERLYING MATING SUB STRUCTURE AT FS 559.00 STR 17L FOUND TO HAVE OBLONG CONDITION (C-CHECK RO 5/13/2024) REPAIRED AND FABRICATED CONICAL WASHER P/N: 601R-53-41-3232 ON SUB STRUCTURE AT F.S 559.00 STR 17 LH IAW MHIRJ RE
- [SDR SWI202405140405](https://openairdocs.org/sdr/SWI202405140405.md): Unknown · corroded · Feb 27, 2024 · N930EV · Cndair CL6002B19 · Fuselage Structure (General)
  > SIGNS OF CORROSION AT RH PRESS SILL FS515 (C-CHECK RO 5/13/2024) REMOVED CORROSION ON RH PRESS SILL FS515 IAW REO 601R-53-41-666. REV. -C. DATE: 2012-11-06. NDT PERFORMED BY BARON NDT, LLC, FAA CRS# 5NDR545D. REPORT # S031324-13. AND CRJ-200 SRM 51-21-06,
- [SDR SWIA20240514227](https://openairdocs.org/sdr/SWIA20240514227.md): Support · corroded · Feb 27, 2024 · N930EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SIGNS OF CORROSION AT RH PRESS SILL FS501 (C-CHECK RO 5/13/2024) REPAIRED CORROSION DAMAGE AT FS 501 RH FLOOR SILL PANEL IAW REO 601R-53-41-666 REV-C DATE 2012-11-06 CRJ200 SRM 51-25-06, AND SRM 51-25-16, SRM 51-21-11, SRM 51-21-06. NDT PERFORMED BY BARON
- [SDR SWI202405140404](https://openairdocs.org/sdr/SWI202405140404.md): Lock Fastener · corroded · Feb 22, 2024 · N930EV · Cndair CL6002B19 · Fuselage Structure (General)
  > SIGNS OF CORROSION ADN MISSING PAINT UNDER PRESSURE FLOOR PANEL LH SIDE IN AND/OR AROUND FASTENERS FS451BLENDED OUT CORROSION UNDER PRESSURE FLOOR PANEL AT FS451. BLENDS PERFORMED ARE WITHIN LIMITS. TREAETED, PRIMED, AND APPLIED TOPCOAT TO REPAIR AREA IAW BOM
- [SDR SWI202405140403](https://openairdocs.org/sdr/SWI202405140403.md): Nut · corroded · Feb 22, 2024 · N930EV · Cndair CL6002B19 · Fuselage Structure (General)
  > SIGNS OF CORROSION AND MISSING PAINTUNDER PRESSURE FLOOR PANEL SH SIDE IN AND/OR AROUND FASTENERS FS457 (C-CHECK RO 5/13/2024) REMOVED CORROSION UNDER PRESSURE FLOOR PANEL, LEFT SIDE F.S. 457. FOUND TO BE WITHIN LIMITS IAW BOMBARIDIER REO 601R-53-41-666 RE
- [SDR SWI202405140402](https://openairdocs.org/sdr/SWI202405140402.md): Unknown · corroded · Feb 22, 2024 · N930EV · Cndair CL6002B19 · Fuselage Structure (General)
  > SIGNS OF CORROSION ON MULTIPLE FASTENERS UNDER FLOOR PANEL RH SIDE IN AND/OR AROUND FASTENERS AT FS428 (C-CHECK RO 5/13/2024) REPAIRED CORROSION DAMAGE @ FS 428.00 R/H FLOOR SILL PANEL NUT PLATE IAW REO 601R53-41-666 REV-C DATE: 2012-11-06. NDT PERFORMED B
- [SDR SWI202405140401](https://openairdocs.org/sdr/SWI202405140401.md): Unknown · corroded · Feb 22, 2024 · N930EV · Cndair CL6002B19 · Fuselage Structure (General)
  > SIGNS OF CORROSION ON MULTIPLE FASTENERS UNDER FLOOR PANEL RH SIDE IN AND/OR AROUND FASTENERS FS457 (C-CHECK RO 5/13/2024) REPAIRED CORROSION DAMAGE AT FS 457 RH FLOOR SILL PANEL AROUND. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D REPORT # S030124-1
- [SDR SWIA20240514221](https://openairdocs.org/sdr/SWIA20240514221.md): Unknown · damaged · Feb 21, 2024 · N930EV · Cndair CL6002B19 · Fuselage Structure (General)
  > DAMAGED FASTENER HOLE AT FS559.00+5 LBL27 (C-CHECK RO 5/13/2024) PERFORMED REPAIR ON FS 559.00+5 LBL27 PER REO 60IR-53-41-3228. REV. -- DATE: 2024-04-08, REO 60IR-53-41-3228. REV--(P1) DATE: 2024-04-01 AND CRJ-200 SRM 53-00-00. CRJ-200 SRM 51-45-00. CRJ-20
- [SDR SWIA20240514218](https://openairdocs.org/sdr/SWIA20240514218.md): Unknown · chafed · Feb 18, 2024 · N930EV · Cndair CL6002B19 · Fuselage Structure (General)
  > DURING THE AUDIT OF 1C TASK CARD 53-280-300, INTERNAL ZONAL INSPECTION OF THE CARGO COMPARTMENT, IT WAS NOTED THAT THERE IS EVIDENCE OF MULTIPLE FASTENER CHAFES/CONTACT ON THE FWD SIDE OF THE FS 621 BULKHEAD. PLEASE INVESTIGATE AND REPAIR AS REQUIRED. (C-CH
- [SDR SWIA20240514205](https://openairdocs.org/sdr/SWIA20240514205.md): Vane · chafed · Feb 5, 2024 · N930EV · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H I/B FLAP VANE EXISTING REPAIR IN MIDDLE CHAFFED (C-CHECK RO 5/13/2024) REPAIRED R/H I/B FLAP VANE SKIN IAW CRJ200 SRM 57-52-00,57-52-00 REPAIR #1,51-21-11,51-25-06 AND 51-25-16 AMM 27-54-10.CALIBRATED TOOLS USED: DEPTH GUAGE AV-7277 CAL DUE: AUG 2024,
- [SDR SWIA202309280006](https://openairdocs.org/sdr/SWIA202309280006.md): Unknown · warning message · Sep 26, 2023 · N930EV · Cndair CL6002B19 · Landing Gear System
  > ON DEPARTURE WHILE SELECTING THE GEAR UP WE RECEIVED STEERING INOP (C) MSG. FOLLOWING THAT MSG WE GOT A GEAR DISAGREE (W) MSG AND A NOSE DOOR (W) MSG. NOSE DOOR (W) MSG WENT AWAY ON ITS OWN. NOSE GEAR WAS SHOWING DOWN ON EICAS WHEN THE HANDLE WAS IN THE UP POS
- [SDR SWIA20230927006](https://openairdocs.org/sdr/SWIA20230927006.md): Unknown · warning message · Sep 26, 2023 · N930EV · Cndair CL6002B19 · Landing Gear Door Actuator
  > ON DEPARTURE WHILE SELECTING THE GEAR UP WE RECEIVED STEERING INOP (C) MSG. FOLLOWING THAT MSG WE GOT A GEAR DISAGREE (W) MSG AND A NOSE DOOR (W) MSG. NOSE DOOR (W) MSG WENT AWAY ON ITS OWN. NOSE GEAR WAS SHOWING DOWN ON EICAS WHEN THE HANDLE WAS IN THE UP POS
- [SDR SWIA2023052319](https://openairdocs.org/sdr/SWIA2023052319.md): Unknown · unknown · May 19, 2023 · N930EV · Cndair CL6002B19 · Landing Gear Door Actuator
  > OVERSPED LANDING GEAR DURING RETRACTION ON GO-AROUND AT APPROX 220 KIAS. NOSE GEAR DID NOT INDICATE UP. ONCE BELOW 200 THE NOSE GEAR RETRACTED AND ALL GEAR INDICATED UP. TURNED HYD PUMPS 3B AND 2 ON PER QRH. GEAR LOWERED NORMALLY, INDICATED DN, AND NORMAL LAND
- [SDR SWIA202266349](https://openairdocs.org/sdr/SWIA202266349.md): None · faulty · Aug 23, 2022 · N930EV · Cndair CL6002B19 · Doors
  > L EMER DOOR CAUTION MESSAGE CONTINUOUSLY CAME ON, NO PRESSURIZATION ISSUE AND HAD GREEN DOOR INDICATOR (FLIGHT #6971 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25375145 WITH THE FOLLOWING CORRECTIVE ACTION: "LEFT OVERWING EMERGENCY EXIT DO
- [SDR SWIA202157113](https://openairdocs.org/sdr/SWIA202157113.md): Stiffener · cracked · Mar 28, 2021 · N930EV · Cndair CL6002B19 · Fuselage Main, Structure
  > UPON ACCESS FOR BELL CRANK REPAIR FOUND UPPER STIFFENER AT WS 00 IN MLG WHEEL WELL TO BE CRACKED (C-CHECK RO 4/1/2021) UPPER STIFFENER LISTED IN DISCREPANCY IS LOCATED AT W.S. 48.30. REMOVED AND REPLACED UPPER STIFFENER IN R/H MLG WHEEL WELL, W.S. 48.30
- [SDR SWIA202157112](https://openairdocs.org/sdr/SWIA202157112.md): Bellcrank · abnormal · Mar 27, 2021 · N930EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > UPON INITIAL GEAR SWING LH BELLCRANK WAS CLOCKED INCORRECTLY CAUSING DAMAGE TO BELLCRANK AND SURROUNDING STRUCTURE (C-CHECK RO 4/1/2021) REPAIRED BELLCRANK AND SURROUNDING STRUCTURE IAW MHIRJ REO 601R-53-41-2887 REV -- DATED 2021-03-29. REFERENCE CONTINUA
- [SDR SWIA202157114](https://openairdocs.org/sdr/SWIA202157114.md): Bellcrank · abnormal · Mar 12, 2021 · N930EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > UPON INITIAL GEAR SWING LH AND RH BELLCRANKS WERE CLOCKED INCORRECTLY CAUSING THE BELLCRANKS TO BREAK AND SURROUNDING STRUCTURAL DAMAGE (C-CHECK RO 4/1/2021) REPAIRED LH & RH BELLCRANK AND SURROUNDING STRUCTURE IAW MHIRJ REO 601R-53-41-2888 REV -- DATED
- [SDR SWIA202157140](https://openairdocs.org/sdr/SWIA202157140.md): Fairing · chafed · Mar 8, 2021 · N930EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > L/H STUB FAIRING HAS CHAFING DAMAMGE AND INTERNAL BRACKET IS ALLOWING MOVEMENT. (C-CHECK RO 4/1/2021) INSTALLED NEW HARDWARE ON L/H STUB FAIRING TO CORRECT THE INTERNAL BRACKET AND LET THE STUB FAIRING FUNCTION CORRECTLY IAW CRJ 200 AMM 53-82-01-400-808.
- [SDR SWIA202157124](https://openairdocs.org/sdr/SWIA202157124.md): Floor Support · corroded · Feb 28, 2021 · N930EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR BEAM CAP HAS SEVERAL AREAS OF CORROSION BETWEEN F.S. 409.00 AND 409.00+128. (C-CHECK RO 4/1/2021) REPAIRED LBL 9 FLOOR BEAM CAP CORROSION BETWEEN F.S. 409.00 AND 409.00+128 IAW CRJ 200 SRM 53-00-43 AND REO 601R-53-31-1184 REV.-- DATED 2021-03-
- [SDR SWIA202157139](https://openairdocs.org/sdr/SWIA202157139.md): Nut · corroded · Feb 21, 2021 · N930EV · Cndair CL6002B19 · Wing, Attach Fittings
  > RH WING HINGE BOX ATTACHING HARDWARE NUTS FWD AND AFT AT WS 178, WS 220, AND WS 264 ARE CORRODED/ RUSTED AND REQUIRE REPLACEMENT. (C-CHECK RO 4/1/2021) REMOVED AND INSTALLED SERVICEABLE HARDWARE ON R/H FLAP HINGE BOX WS 178.00,WS 220.00AND WS 264.00 IAW C
- [SDR SWIA202157138](https://openairdocs.org/sdr/SWIA202157138.md): Nut · corroded · Feb 21, 2021 · N930EV · Cndair CL6002B19 · Wing, Attach Fittings
  > LH AFT HINGE BOX NUTS AT WS 264, FWD HINGE BOX NUT AT WS 220, AND FWD AND AFT HINGE BOX NUTS AT WS 178 ARE CORRODED/RUSTED AND REQUIRE REPLACMENT. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED LH AFT HINGE BOX NUTS AT WS 264, FWD HINGE BOX NUT AT WS 220, AND
- [SDR SWIA202157123](https://openairdocs.org/sdr/SWIA202157123.md): Trunnion · cracked · Feb 18, 2021 · N930EV · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LH MLG TRUNNION FASTENER HOLES AS FOLLOWS EACH HAS INDICATIONS,1" LONG AND 45% FSH IN LOCATION #4, AND 65% FSH IN LOCATIONS #8, & #13. FAILED NDT INSPECTION. (REFERENCE NDT REPORT & ATTACHMENTS FOR LOCATION). (C-CHECK RO 4/1/2021) REPAIRED LEFT HAND TRU
- [SDR SWIA202157122](https://openairdocs.org/sdr/SWIA202157122.md): Trunnion · failed · Feb 18, 2021 · N930EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RH MLG TRUNNION FASTENER HOLE #7 HAS AN INDICATION.1" LONG BY 40% FSH. FAILED NDT INSPECTION(REFERENCE NDT REPORT & ATTACHMENTS FOR LOCATION). (C-CHECK RO 4/1/2021) REPAIRED RIGHT HAND MLG TRUNNION FASTENER HOLE #14 IAW MHIRJ REO 601R-57-21-3428, REV -
- [SDR SWIA202157121](https://openairdocs.org/sdr/SWIA202157121.md): Trunnion · damaged · Feb 18, 2021 · N930EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > R/H TRUNNION AFT HOLE IN STRAP IS OVERSIZED. (C-CHECK RO 4/1/2021) REPAIRED RIGHT HAND MLG TRUNNION AFT HOLE LOCATION (#16) IAW MHIRJ REO 601R-57-21-3428, REV -- DATED 2021-02-26. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. FORM 337 AND MAJOR REPAIR
- [SDR SWIA202157120](https://openairdocs.org/sdr/SWIA202157120.md): Trunnion · damaged · Feb 18, 2021 · N930EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > L/H TRUNNION AFT HOLE IN STRAP IS OVERSIZED (C-CHECK RO 4/1/2021) REPAIRED LEFT HAND TRUNNION AFT HOLE IN STRAP (#14) IAW MHIRJ REO 601R-57-21-3427, REV -- DATED 2021-02-26. REFERENCE CONTINUE CARD FOR WORK PERFORMED. FORM 337 AND MAJOR REPAIR TASK CARD
- [SDR SWIA202157137](https://openairdocs.org/sdr/SWIA202157137.md): Nut · corroded · Feb 13, 2021 · N930EV · Cndair CL6002B19 · Ailerons
  > RH AILERON HINGE #4 ANIT ROTATION PLATE NUT AND WASHER CORRODED. (C-CHECK RO 4/1/2021) REMOVED AND INSTALLED NEW SERVICEABLE NUT AND WASHER ON R/H AILERON HINGE #4 ANTI ROTATION PLATE IAW CRJ 200 AMM 20-21-00-910-801.
- [SDR SWIA202157136](https://openairdocs.org/sdr/SWIA202157136.md): Plate · corroded · Feb 8, 2021 · N930EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORWARD ANCHOR FITTING SERATED PLATE IS CORRODED. (C-CHECK RO 4/1/2021) INSTALLED SERICABLE PAX DOOR ANCHOR FITTING I.A.W. CRJ-200 AMM TASK 52-11-17-400-804
- [SDR SWIA202157135](https://openairdocs.org/sdr/SWIA202157135.md): Plate · corroded · Feb 8, 2021 · N930EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT ANCHOR FITTING SERATED PLATE IS CORRODED. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING SERATED PLATE WITH SERVICABLE P/N: 600-38061-6 I.A.W CRJ-200 AMM TASK 52-11-17-400-804.
- [SDR SWIA202157125](https://openairdocs.org/sdr/SWIA202157125.md): Anchor Fitting · corroded · Feb 8, 2021 · N930EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT ANCHOR FITTING IS CORRODED IN (2) LOCATIONS AND IS CRACKED ON THE AFT SIDE. (C-CHECK RO 4/1/2021) INSTALLED SERICABLE PAX DOOR ANCHR FITTING AND STOP PLATE COVER I.A.W. CRJ-200 AMM TASK 52-11-17-400-804
- [SDR SWIA202157119](https://openairdocs.org/sdr/SWIA202157119.md): Splice Angle · cracked · Feb 8, 2021 · N930EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L IS CRACKED AT F.S. 280.00. (C-CHECK RO 4/1/2021) ON INVESTIGATION FOUND NO DAMAGE TO THE STRINGER 3L. FOUND SPLICE ANGLES INBOARD AND OUTBOARD TO BE CRACKED. REMOVED AND REPLACED SPLICE ANGLES IAW CRJ 200 SRM 51-42-21 AND 51-42-06. NO CHANGE T
- [SDR SWIA202157118](https://openairdocs.org/sdr/SWIA202157118.md): Floor Support · corroded · Feb 8, 2021 · N930EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL IS CORRODED AROUND (1) FASTENER, LOCATED (2) FASTENERS OUTBOARD OF BLEND #18 AS CALLED OUT IN REO 601R-53-41-2442 REV.--, DATED 2019-02-18. (C-CHECK RO 4/1/2021) BLENDED OUT CORROSION ON L/H PRESSURE SILL AROUND 1 FASTNER LOCATED 2
- [SDR SWIA202157110](https://openairdocs.org/sdr/SWIA202157110.md): Floor Support · corroded · Feb 8, 2021 · N930EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL IS CORRODED AROUND (1) FASTENER LOCATED FORWARD OF THE FASTENER CALLED OUT AT LOCATION #12 OF REO 601R-53-41-2442 REV.--, DATED 2019-02-18. (C-CHECK RO 4/1/2021) REPAIRED IAW REO 601R-53-41-666 REV C DATED 11/6/2012 DISPOSITION 1.2
- [SDR SWIA202157141](https://openairdocs.org/sdr/SWIA202157141.md): Seat Track · damaged · Feb 7, 2021 · N930EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH CABIN FLOOR SEAT RAIL AT LBL9 BETWEEN F.S. 409.00+64 AND F.S. 409.00+128 REQUIRES FABRICATION. (C-CHECK RO 4/1/2021) FABRICATED, LOCATED AND DRILLED SEAT TRACK ON LH CABIN FLOOR AT LBL9 BETWEEN FS 409+64 AND FS 409+128 IAW: CRJ200-SRM-51-40-11
- [SDR SWIA202157134](https://openairdocs.org/sdr/SWIA202157134.md): Attach Bolt · corroded · Feb 4, 2021 · N930EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RH WING VANE PANEL 695BB BOLT KEEPER ATTACH BOLTS ARE CORRODED (C-CHECK RO 4/1/2021) REMOVED AND REPLACED RH WING VANE PANEL 695BB BOLT KEEPER ATTACH BOLTS (4 BOLTS) IAW CRJ 200 AMM 27-54-05-000/400-801.
- [SDR SWIA202157133](https://openairdocs.org/sdr/SWIA202157133.md): Attach Bolt · corroded · Feb 4, 2021 · N930EV · Cndair CL6002B19 · Wing, Attach Fittings
  > RH WING MULTI-FUNCTIONAL SPOILER INBOARD / OUTBOARD ACTUATORS LOWER ATTACH HARDWARE IS CORRODED (C-CHECK RO 4/1/2021) REMOVED AND REPLACED RH WING MULTI-FUNCTIONAL SPOILER INBOARD/ OUTBOARD ACTUATOR'S LOWER ATTACH HARDWARE IAW CRJ 200 AMM 27-62-01-000/400
- [SDR SWIA202157132](https://openairdocs.org/sdr/SWIA202157132.md): Nut · corroded · Feb 4, 2021 · N930EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LH WING VANE PANEL 595BB LH OUTBOARD ATTACH NUT IS CORRODED (C-CHECK RO 4/1/2021) REMOVED AND REPLACED LH WING VANE PANEL 595BB LH OUTBOARD ATTACH NUT FROM HINGE BOX ASSEMBLY AT W.S220.00 IAW CRJ200 AMM REF: 57-21-35-000-802 AND 57-21-35-400-802. TORQUE W
- [SDR SWIA202157131](https://openairdocs.org/sdr/SWIA202157131.md): Attach Bolt · corroded · Feb 4, 2021 · N930EV · Cndair CL6002B19 · Wing, Attach Fittings
  > LH WING AILERON POSITION INDICATOR UNDER PANEL 598BB HAS ATTACH HARDWARE IS CORRODED (C-CHECK RO 4/1/2021) REMOVED AND REPLACED HARDWARE ON LH WING AILERON POSITION INDICATOR UNDER PANEL 598BB AS REQUIRED IAW CRJ 200 AMM 27-15-15-000/400-801. REFFERENCE
- [SDR SWIA202157130](https://openairdocs.org/sdr/SWIA202157130.md): Seat Track · corroded · Feb 3, 2021 · N930EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH CABIN SIDE SEAT RAILS ARE CORRODED BETWEEN F.S. 424.00 AND F.S. 559.00+32. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED WITH NEW R/H CABIN SIDE SEAT RAILS BETWEEN FS 424 AND FS 559.00+32 IAW CRJ 200 AMM 53-01-11-400-802
- [SDR SWIA202157129](https://openairdocs.org/sdr/SWIA202157129.md): Seat Track · corroded · Feb 3, 2021 · N930EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH CABIN FLOOR SEAT RAIL AT RBL9 IS CORRODED BETWEEN F.S. 409.00+96 AND F.S. 409.00+112. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED R/H CABIN FLOOR SEAT RAIL AT RBL 9 BETWEEN F.S. 399 AND 409+126 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802. REFE
- [SDR SWIA202157128](https://openairdocs.org/sdr/SWIA202157128.md): Seat Track · corroded · Feb 3, 2021 · N930EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH CABIN FLOOR SEAT RAIL AT LBL9 IS CORRODED BETWEEN F.S. 409.00+64 AND F.S. 409.00+128. (C-CHECK RO 4/1/2021) INSTALLED SERVICEABLE LH CABIN FLOOR SEAT RAIL AT LBL 9 BETWEEN FS409.00+64 AND FS409.00+128 IAW CRJ 200 AMM 53-01-11-400-802
- [SDR SWIA202157117](https://openairdocs.org/sdr/SWIA202157117.md): Post · cracked · Feb 3, 2021 · N930EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FUSELAGE FS409+128 VERTICAL POST AT RBL18 HAS AN INDICATION.2" LONG BY 60% FSH IN THE AFT RADIUS OF THE INBD SIDE @ WL69. FAILED NDT INSPECTION. (C-CHECK RO 4/1/2021) REMOVED AND INSTALLED NEW SERVICEABLE VERTICAL POST AT RBL 18 IAW REO 601R-53-41-889 R
- [SDR SWIA202157108](https://openairdocs.org/sdr/SWIA202157108.md): Post · cracked · Feb 3, 2021 · N930EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FUSELAGE FS409+128 VERTICAL POST AT BL0 HAS AN INDICATION.2" LONG BY 80% FSH IN THE AFT RADIUS OF BOTH THE RH & LH SIDES @WL69. FAILED NDT INSPECTION. (C-CHECK RO 4/1/2021) FUSELAGE FS409+128 VERTICAL POST AT BL0 WAS REMOVED AND A NEW POST INSTALLED IA
- [SDR SWIA202157126](https://openairdocs.org/sdr/SWIA202157126.md): Intercostal · cracked · Feb 2, 2021 · N930EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > APU INLET DOOR ACTUATOR INTERCOSTAL AT F.S. 654.50 STGR 4L IS CRACKED AT BOTTOM FWD CORNER. (C-CHECK RO 4/1/2021) REPAIRED DAMAGE ON THE APU INLET DOOR ACTUATOR INTERCOSTAL AT F.S. 654.50 STGR 4L IAW MHIRJ REO 601R-53-62-300 REV -- DATED 2021-02-23. REFE
- [SDR SWIA202157127](https://openairdocs.org/sdr/SWIA202157127.md): Retainer · corroded · Jan 29, 2021 · N930EV · Cndair CL6002B19 · Emergency Exits
  > CREW ESCAPE HATCH SEAL RETAINER ATTACHING HARDWARE IS CORRODED AT 10EA. LOCATIONS. (MARKED WITH RED GREASE PENCIL) (C-CHECK RO 4/1/2021) REMOVED AND REPLACED CREW ESCAPE HATCH RETAINER HARDWARE IAW CRJ 200 AMM 52-22-07-000/400-802
- [SDR SWIA202157116](https://openairdocs.org/sdr/SWIA202157116.md): Retainer · corroded · Jan 25, 2021 · N930EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS DOOR SEAL RETAINER IS CORRODED AROUND ENTIRE DOOR. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED MAIN AVIONICS SEAL RETAINER IAW CRJ 200 SRM 51-42-06 REFERENCE CONTINUATION CARD FOR WORK PERFORMED

Next page: https://openairdocs.org/aircraft/N930EV/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 = 'N930EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N930EV/reports

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