# Service difficulty reports: N929EV

A list on [N929EV](https://openairdocs.org/aircraft/N929EV.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 · 108 reports

- [SDR SWIA2026091877224](https://openairdocs.org/sdr/SWIA2026091877224.md): Bracket · bent · Sep 18, 2026 · N929EV · Cndair CL6002B19 · Entrance Stairs
  > MLG DISAGREE & NLG DOOR WARNING MESSAGE ON CLIMB OUT FROM DULLES. RAN QRH & MLG CAME BACK DOWN. DIVERTED BACK TO DULLES. MEL 32-30-1CAT A DUE ONE FLT DAY 091926, CAT II DOWNGRADED. ODI EVENT SMOD APROVAL REQUIRED FOR RTS, NLG DOOR WARNING WAS FIRST FOLLOWED
- [SDR SWIA2026031875522](https://openairdocs.org/sdr/SWIA2026031875522.md): Door · leaking · Mar 17, 2026 · N929EV · Cndair CL6002B19 · Service Doors
  > CAPT REPORTED AT 29K FT, GOT A LOUD SOUND AND FA SAID IT WAS COMING FROM SERVICE DOOR. CABIN PRESSURE BEGAN TO CLIMB AT 400 FPM. SOUND WENT AWAY AT 17K FT. AND PRESSURIZATION STARTED WORKING AGAIN. (FLIGHT 5321) CLEANED AND INSPECTED SERVICE DOOR SEAL IAW A
- [SDR SWIA20251223021](https://openairdocs.org/sdr/SWIA20251223021.md): Outflow Valve · obstructed · Dec 21, 2025 · N929EV · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > EMERGENCY DESCENT DUE TO RAPID DEPRESSURIZATION AT 33K FT. CALL FROM FA ABOUT A LOUD BANG FOLLOWED BY LOSS OF PRESSURIZATION. RAN QRC & QRH, LANDED WITHOUT ANY ISSUES. (FLIGHT 5053) DURING PRESSURIZATION OPS CHECKS FOUND ONCE 6.0 DELTA P IS REACHED RATE INDI
- [SDR SWIA2025122201](https://openairdocs.org/sdr/SWIA2025122201.md): Cabin Pressure · pressure loss · Dec 21, 2025 · N929EV · Cndair CL6002B19 · Cabin Pressure Control System
  > EMERGENCY DESCENT DUE TO RAPID DEPRESSURIZATION AT 33K FEET. GOT A CALL FROM FA ABOUT A LOUD BANG FOLLOWED BY LOSS OF PRESSURIZATION. RAN QRC AND QRH AND LANDED WITHOUT ANY ISSUES. (FLIGHT 5053 - FILED OPEN)
- [SDR SWIA2025100700914](https://openairdocs.org/sdr/SWIA2025100700914.md): Skin · ground damage · Sep 14, 2025 · N929EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR DAMAGE FROM LAV SERVICING TRUCK NEAR AFT POTABLE WATER PANEL: UPON INSPECTION, FOUND DAMAGE TO FUSELAGE STRUCTURE BETWEEN FS574 €“ FS589.00 AND BTW STR 17R-18R. IMPACT (LAVATORY CART) CAUSED DAMAGE TO MULTIPLE PARTS. REFER TO REO 601R-53-61-8383 TAB
- [SDR SWIA202506300027](https://openairdocs.org/sdr/SWIA202506300027.md): Retainer · bent · Jun 27, 2025 · N929EV · Cndair CL6002B19 · Passenger/Crew Doors
  > MCD LOWER SEAL RETAINER BENT NEAR AFT RADIUS. (FILED CLOSED)REMOVED AND REPLACED MCD LOWER CENTER AND LOWER AFT SEAL RETAINERS WITH REFERENCE TO REO 601R-51-11-915, REV. -- DATED 1/04/2006 AND SRM 51-42-06. COMPLETED 51-900-1003-SKY AND M-337. REFERENCE CP 303
- [SDR SWIA202503210001](https://openairdocs.org/sdr/SWIA202503210001.md): Steering Sys · inoperative · Mar 20, 2025 · N929EV · Cndair CL6002B19 · Landing Gear Steering System
  > STEERING INOP CAUTION MESSAGE AFTER TAKEOFF. RAN QRH MESSAGE PERSISTED. (FLIGHT 5452 - FILED CLOSED) T/S "STEERING INOP" CAUTION MESSAGE PER CRJ200 FIM 32-50-01, INSPECTED NOSE LANDING GEAR HYDRAULIC COMPARTMENT AND FOUND CONNECTOR PS1 FOR STEERING PRESS
- [SDR SWIA2025011600013](https://openairdocs.org/sdr/SWIA2025011600013.md): Intercostal · damaged · Jan 13, 2025 · N929EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 IS DAMAGED. THIS HAS BEEN DEEMED A MAJOR REPAIR AND REQUIRES AN M-337 (FILED CLOSED) DUPLICATE WRITE UP. SEE ML 29460469 FOR MAJOR REPAIR - DUE TO BIRD
- [SDR SWIA202501131022](https://openairdocs.org/sdr/SWIA202501131022.md): Intercostal · damaged · Jan 13, 2025 · N929EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 IS DAMAGED. THIS HAS BEEN DEEMED A MAJOR REPAIR AND REQUIRES AN M-337 (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202501160011](https://openairdocs.org/sdr/SWIA202501160011.md): Seal · damaged · Jan 11, 2025 · N929EV · Cndair CL6002B19 · Fuselage Structure (General)
  > TRANSFER FROM EAML 1506706: TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 P/N: 600-33011-68, REF, AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REF IS DAMAGED. DAMAGE IS A DENT: 1.00€? L X 0.250€? W X 0
- [SDR SWIA2025011300050](https://openairdocs.org/sdr/SWIA2025011300050.md): Intercostal · dented · Jan 11, 2025 · N929EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRANSFER FROM EAML 1506706: TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 P/N: 600-33011-68, REF, AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REF IS DAMAGED. DAMAGE IS A DENT: 1.00€? L X 0.250€? W X 0
- [SDR SWIA202501061229](https://openairdocs.org/sdr/SWIA202501061229.md): Skin · cracked · Dec 29, 2024 · N929EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NOSE SKIN BETWEEN FS169.00-193.00 IS CRACKED (FILED CLOSED) REPLACED NOSE SKIN BETWEEN FS169.00-193.00 IN REFERENCE TO CRJ 200 SRM 51-42-06
- [SDR SWIA2024070800006](https://openairdocs.org/sdr/SWIA2024070800006.md): Proximity Sensor · faulted · Jul 6, 2024 · N929EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. NOSE WHEEL DID NOT COME UP. (FLIGHT 5378 - FILED CLOSED) PLEASE REFERENCE AML 1384104 PLEASE REFERENCE AML 1384105 PLEASE REFERENCE AML 1384107 PLEASE REFERENCE AML 1384108UPON COMPLETION OF REMOVAL AND REP
- [SDR SWIA20240402](https://openairdocs.org/sdr/SWIA20240402.md): None · none · Apr 2, 2024 · N929EV · Cndair CL6002B19 · Standard Practices/Structures
  > CLASSIFICATION OF MAJOR/MINOR DAMAGE REQUIRED PER GMM 3.25 AND 3.26MCI TYPE: SERVICEABLE / NEEDS ATTENTION (FILED CLOSED)APR 04, 2024 STATION: ATW--DAMAGE REQUIRES MAJOR REPAIR IAW 3.26 APR 10, 2024 STATION: MKE -- REFERENCE AML 1324409. DAMAGE WAS PREVIOUSL
- [SDR SWIA202404050002](https://openairdocs.org/sdr/SWIA202404050002.md): Unknown · damaged · Apr 2, 2024 · N929EV · Cndair CL6002B19 · Standard Practices/Structures
  > CLASSIFICATION OF MAJOR/MINOR DAMAGE REQUIRED PER GMM 3.25 AND 3.26MCI TYPE: SERVICEABLE / NEEDS ATTENTION (FILED OPEN)APR 04, 2024 STATION: ATW--DAMAGE REQUIRES MAJOR REPAIR IAW 3.26
- [SDR SWIA20231157018](https://openairdocs.org/sdr/SWIA20231157018.md): Unknown · dented · Oct 18, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT DAMAGE FOUND TO RH SIDE OF THE FUSELAGE, BELOW THE FORWARD EDGE OF THE RH ENGINE, AND IN THE PRESSURE VESSEL. THE DENT IS LOCATED ON THE FUSELAGE BETWEEN FS574.00 AND FS589.00 AND BETWEEN WL 97.50 AND WL 79.50. DENT MEASURES 15€? IN WIDTH BY 12 13/16€
- [SDR SWIA2023050327](https://openairdocs.org/sdr/SWIA2023050327.md): Unknown · dented · Mar 27, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS NOTED ON EXTERIOR SKIN BELOW CARGO DOOR CUTOUT (MARKED) (C-CHECK RO 4/30/2023) COMPLIED WITH DISPOSITION FOR DENTS AND BLEND TO FUSELAGE SKIN BETWEEN FS605 - FS621 AND STR 18L - STR 19L REF REO 601R-53-61-8000 REV -- 2023-04-12. COMPLIED
- [SDR SWIA202305030032](https://openairdocs.org/sdr/SWIA202305030032.md): Unknown · cracked · Mar 22, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS.280 HAS A CRACKED CLIP ON THE INBD SIDE OF LBL 9 (MARKED) (C-CHECK RO 4/30/2023) REMOVED CRACKED CLIP, FS 280 LBL9 INBD SIDE AND INSTALLED NEW CLIP PER DWG#601R31113 REV AD AND CRJ 200 SRM 51-42-21. SEE CONTINUATION CARD FOR DETAILS. M-337 AND SKYWE
- [SDR SWIA202305030030](https://openairdocs.org/sdr/SWIA202305030030.md): Unknown · cracked · Mar 20, 2023 · N929EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > L/ WING WS 48.3 UPPER FWD BATT ANGLE CRACKED. (C-CHECK RO 4/30/2023) REPLACED L/ WING WS 48.3 UPPER FWD BATT ANGLE WITH NEW PN 600-10204-27 PO# T60652 REF CRJ 200 SRM 51-42-06 AND BOMBARDIER DWG 600-10204 REV M.COMPLIED WITH SKY CARD 51-900-1003 SKY
- [SDR SWIA202305030029](https://openairdocs.org/sdr/SWIA202305030029.md): Unknown · chafed · Mar 20, 2023 · N929EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LH APRON SKIN CHAFED BY WING P SEAL. (C-CHECK RO 4/30/2023) COMPLIED WITH REPAIR TO LH APRON SKIN AS PER REO 601R-53-41-115 REV -A DATE 2005-07-20. M337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.
- [SDR SWIA202305030028](https://openairdocs.org/sdr/SWIA202305030028.md): Unknown · unknown · Mar 17, 2023 · N929EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > LH REPLACEMENT TRUNNION REQUIRES SERVICE BULLETIN 601R-57-048 REV C DATED 06/06/2013 RE-INCORPORATION. (C-CHECK RO 4/30/2023) COMPLIED WITH ALL STEPS OF FINAL REO 601R-57-21-3728 REV -- DATED 2023-04-05 ON LH REPLACEMENT TRUNNION. M-337 AND SKYWEST TASK
- [SDR SWIA202305030027](https://openairdocs.org/sdr/SWIA202305030027.md): Unknown · cracked · Mar 13, 2023 · N929EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > LH MLG TRUNNION REQUIRES REPLACEMENT DUE TO FINDING CRACKED HOLES (C-CHECK RO 4/30/2023) REMOVED OLD LH TRUNNION AND STEEL STRAP AND INSTALLED NEW LH TRUNNION AND STEEL STRAP REF REO 601R-57-21-3714 REV -- DATED 2023-04-05 AND BOMBARDIER RIL #3690 REV
- [SDR SWIA202305030026](https://openairdocs.org/sdr/SWIA202305030026.md): Unknown · corroded · Mar 9, 2023 · N929EV · Cndair CL6002B19 · Wing, Center Box
  > RH WING LOWER WING PLANK ACCESS HOLE 610AB HAS CORROSION.FLAGGED (C-CHECK RO 4/30/2023) REPAIRED RH WING LOWER WING PLANK ACCESS HOLE 610AB REF REO 601R-57-21-3717 REV-- DATED: 2023-03-23 AND SRM 51-21-06. SEE CONTINUE CARD FOR DETAILS. M-337 AND SKYWE
- [SDR SWIA202305030025](https://openairdocs.org/sdr/SWIA202305030025.md): Unknown · cracked · Mar 9, 2023 · N929EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > L/H MLG WHEEL WELL - TRUNION RIB BRACKET (BAT) HAS SUSPECTED CRACK - WS 48 (C-CHECK RO 4/30/2023) REPLACED L/H MLG WHEEL WELL - TRUNION RIB BRACKET (BAT) WITH NEW PN 600-10389-1 REF CRJ 200 SRM 51-42-21 AND BOMBARDIER DWG 600-10204 REV M. COMPLIED WITH
- [SDR SWIA2023050308](https://openairdocs.org/sdr/SWIA2023050308.md): Unknown · corroded · Mar 8, 2023 · N929EV · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > R/H FLOOR SEAT RAIL FROM FS409.0+128 TO FS559.0 HAS SEVERAL SPOTS OF CORROSION (MARKED WITH RED GREASE PENCIL.) (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED NEW RH FLOOR SEAT RAIL PN 20276-288-0-0A BETWEEN FS 409.00 +128 AND FS 559.00 PER CRJ 200 AMM 53
- [SDR SWIA202305030024](https://openairdocs.org/sdr/SWIA202305030024.md): Unknown · cracked · Mar 8, 2023 · N929EV · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > DURING WORKING ON SB 601R-57-046 REV C DATED 12/20/012, FOUND 4 CRACKED HOLES AT.3310" AND ONE NO CRACKED OVERSIZED HOLE (.3410") ON RIGHT WING (AS MARKED) (C-CHECK RO 4/30/2023) COMPLIED WITH REO 601R-57-21-3715 REV -- DATED 2023-03-18 FOR REPAIR 4
- [SDR SWIA202305030023](https://openairdocs.org/sdr/SWIA202305030023.md): Unknown · dented · Mar 8, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL AFT DD1 UPPER FLANGE HAS DENT. (C-CHECK RO 4/30/2023) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL AT DD1 REF BOMBARDIER DWG 601R31702 REV-N, CRJ 200 AND SRM 51-42-06. PRESSURE C
- [SDR SWIA202305030022](https://openairdocs.org/sdr/SWIA202305030022.md): Unknown · corroded · Mar 8, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL MID DD3 HAS CORROSION BETWEEN FRAMES FS320-FS338 (C-CHECK RO 4/30/2023) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL AT DD3 REF BOMBARDIER DWG 601R31702 REV-N, AND CRJ 200 SRM 51
- [SDR SWIA202305030021](https://openairdocs.org/sdr/SWIA202305030021.md): Unknown · corroded · Mar 8, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL MID DD4 HAS CORROSION BETWEEN FRAMES FS320-FS338 (C-CHECK RO 4/30/2023) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL AT DD4 REF BOMBARDIER DWG 601R31702 REV-N, CRJ 200 SRM 51-42-06 AND CR
- [SDR SWIA20230503008](https://openairdocs.org/sdr/SWIA20230503008.md): Unknown · corroded · Mar 8, 2023 · N929EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL MID DD6 HAS CORROSION BETWEEN FRAMES FS320-FS338 (C-CHECK RO 4/30/2023) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL AT DD6 REF BOMBARDIER DWG 601R31702 REV-N, CRJ 200 SRM 51-42-
- [SDR SWIA2023050307](https://openairdocs.org/sdr/SWIA2023050307.md): Unknown · cracked · Mar 7, 2023 · N929EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK NOTED AT L/H SIDE OF TRU BAY FLOOR BETWEEN FRAME 193 AND THE BRAKE ACCUMULATOR GAUGES (MARKED) (C-CHECK RO 4/30/2023) REPAIRED LH TRU BAY FLOOR BETWEEN FRAME 193 AND THE BRAKE ACCUMULATOR GAUGES PER REO 601R-53-11-111 REV NC DATE 98-MAR-18, SRM 51
- [SDR SWIA2023050305](https://openairdocs.org/sdr/SWIA2023050305.md): Unknown · corroded · Mar 5, 2023 · N929EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/H PRESSURE FLOOR SILL PANEL FS 409+128 - FS559.00 HAS MULTIPLE AREA'S OF CORROSION AROUND SCREW HOLES. CIRCLED WITH A GREASE PENCIL. (C-CHECK RO 4/30/2023) REPAIRED MULITPLE AREAS OF CORROSION AROUND THE SCREW HOLES ON THE RH PRESSURE FLOOR SILL PAN
- [SDR SWIA2023030504](https://openairdocs.org/sdr/SWIA2023030504.md): Unknown · damaged · Mar 4, 2023 · N929EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR BEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD LBL9 HAS AN ERRANT HOLE THRU THE INBOARD FLANGE FS617.25. (MARKED IN RED) (C-CHECK RO 4/30/2023) COMPLIED WITH ALL STEPS OF REO 601R-53-61-7989 REV-- DATE:2023-04-03. COMPLIED WITH TASK CARD 51-900-100
- [SDR SWIA2023050302](https://openairdocs.org/sdr/SWIA2023050302.md): Unknown · cracked · Mar 2, 2023 · N929EV · Cndair CL6002B19 · Passenger/Crew Doors
  > *SUSPECTED CRACK AT PAX DOOR AFT FORMER BETWEEN DD6-DD5 (MARKED) (C-CHECK RO 4/30/2023) SUSPECTED CRACK CONFIRMED. REMOVED AND REPLACED WITH NEW PAX DOOR AFT FORMER REF BOMBARDIER DWG 601R31702 REV-N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESS
- [SDR SWIA2023030521](https://openairdocs.org/sdr/SWIA2023030521.md): Unknown · cracked · Mar 2, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CLIP ON INTERCOSTAL IS CRACKED, FS621.00 - FS625 STGR14L. (MARKED) (C-CHECK RO 4/30/2023) REMOVED DAMAGED AND INSTALLED NEWLY DRILLED ANGLE ATTACHING TO INTERCOSTAL ATFS621.00 - FS625 STGR14L REF CRJ200 SRM 51-42-21 AND DWG 601-35012 REV-D. M337 AND SKY
- [SDR SWIA20230503011](https://openairdocs.org/sdr/SWIA20230503011.md): Unknown · cracked · Mar 1, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Structure
  > L/H SIDE LEFT WINDSHIELD SIDE SIDEPOST SUPPORT STRUCTURE HAS SUSPECT CRACK AT RADIUS. (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED NEW REPLACEMENT L/H SIDE LEFT WINDSHIELD SIDEPOST SUPPORT ANGLE.REF CRJ200 SRM 51-42-06,SRM 51-42-13 DWG:601R34032 REV-V.
- [SDR SWIA202305030004](https://openairdocs.org/sdr/SWIA202305030004.md): Unknown · cracked · Feb 28, 2023 · N929EV · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H SIDE WINDSHIELD SIDE POST AFT LOWER CLIP IS CRACKED AT RADIUS. (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED NEW AFT LOWER CLIP PART NUMBER 601R33235-4 AT RH SIDE WINDSHIELD REF. CRJ200 SRM 51-42-21. DRW NO.601R33007 REV-U. COMPLIED WITH TASK CARD 51
- [SDR SWIA20230503228](https://openairdocs.org/sdr/SWIA20230503228.md): Unknown · cracked · Feb 28, 2023 · N929EV · Cndair CL6002B19 · Nacelle/Pylon Structure
  > EVALUATE POSSIBLE CRACK ON LEFT ENG. PYLON CANTED RIB. (MARKED) (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED 1 EA NEW LOWER DRAG BRACE ON LH ENGINE PYLON PN 601-37030-1 PER CRJ 200 SRM 51-42-21 AND DWG # 601-37003 REV T. SEE CONTINUATION FOR FURTHER DET
- [SDR SWIA202205030002](https://openairdocs.org/sdr/SWIA202205030002.md): Unknown · damaged · May 3, 2022 · N929EV · Cndair CL6002B19 · Fuselage Main, Frame
  > COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK RO 4/30/2023) COMPLIED WITH REO 601R-53-41-1116 REV-C, 2017-03-09, REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00
- [SDR SWIA202205030001](https://openairdocs.org/sdr/SWIA202205030001.md): Unknown · cracked · May 3, 2022 · N929EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA74501-601R-53-11-2381 929EV-PR1 - LEFT NOSE ELECTRONIC BAY ACCESS DOOR AFT LATCH CUT-OUT HAS A CRACK. COMPLIED WITH TEMP REPAIR ON LEFT NOSE ELECTRONIC BAY ACCESS DOOR AFT LATCH CUT-OUT IN REFERENCE TO REO 601R-53-11-
- [SDR SWIA202155628](https://openairdocs.org/sdr/SWIA202155628.md): Pcu · out of tolerance · Jan 22, 2021 · N929EV · Cndair CL6002B19 · Drag Control Actuator
  > LT INBOARD FLIGHT SPLR PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 2P1CN-A PINS: 11A/12A WAS FOUND TO BE OUT OF RANGE (1.007 K OHMS). REMOVED AND REPLACED LT INBOARD FLIGHT SPOILER PCU, IAW CRJ 200 AMM 27-62-01 REF CP 22194277-1 FOR LEAK CHECK. REF CP 22194
- [SDR SWIA202155627](https://openairdocs.org/sdr/SWIA202155627.md): Pcu · out of tolerance · Jan 22, 2021 · N929EV · Cndair CL6002B19 · Drag Control Actuator
  > LT INBOARD SPOILERON PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 2P1CN-B PINS: 1A/2A WAS FOUND TO BE OUT OF RANGE (1.015 K OHMS). REMOVED AND REPLACED LT INBOARD SPOILERON PCU, PER AMM 27-62-01 REF CP 22193782 FOR LEAK CHECK REF CP 22193864 FOR OPERATIONS CH
- [SDR SWIA2019061145972](https://openairdocs.org/sdr/SWIA2019061145972.md): Skin · damaged · May 30, 2019 · N929EV · Cndair CL6002B19 · Elevator, Plate/Skin
  > RH ELEVATOR SKIN UPPER I/B THERE ARE TOOLING MARKS AROUND FASTENERS. (C-CHECK) RO: 06/09/2019 REPAIRED RH ELEVATOR UPPER INBD SKIN IAW REO.
- [SDR SWIA2019061145971](https://openairdocs.org/sdr/SWIA2019061145971.md): Post · cracked · May 8, 2019 · N929EV · Cndair CL6002B19 · Fuselage Main, Structure
  > 6EA FS409+128 VERT POSTS HAVE CRACK INDICATIONS NOTED IN THE AFT RADIUS AT WL69,. ALL 6 INDICATION FAILED NDT. (C-CHECK) REMOVED AND REPLACED 6EA FS409+128 VERT POSTS IAW REO.
- [SDR SWIA2017041843217](https://openairdocs.org/sdr/SWIA2017041843217.md): Strap · corroded · Apr 1, 2017 · N929EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STRAP AT BS 559, LBL 40. REMOVED AND REPLACED THE STRAP IAW SRM.
- [SDR SWIA2017041843216](https://openairdocs.org/sdr/SWIA2017041843216.md): Floorbeam · corroded · Mar 31, 2017 · N929EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > COCKPIT FLOORBEAM AT BS 280, BTW LBL 11 - RBL 11 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM.
- [SDR SWIA201541158](https://openairdocs.org/sdr/SWIA201541158.md): Vane · chafed · Apr 20, 2015 · N929EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE, CENTER L/E CHAFED BEYOND LIMTS. R & R LT INBD FLAP VANE CENTER L/E REF SRM.
- [SDR SWIA201541157](https://openairdocs.org/sdr/SWIA201541157.md): Vane · chafed · Apr 20, 2015 · N929EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE, CENTER L/E CHAFED BEYOND LIMITS. R & R RT INBD FLAP VANE CENTER L/E REF SRM. COMPLETED M337.
- [SDR SWIA201541156](https://openairdocs.org/sdr/SWIA201541156.md): Bulkhead · unknown · Apr 20, 2015 · N929EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > ACCOMPLISHED REO TO RT SIDE BS 559, PRESSURE BULKHEAD, ACCOMPLISHED REO TO THE RT SIDE BS 559, PRESSURE BULKHEAD. COMPLIED WITH ST 51-900-1003, ATTACHED BTAC FROM M-210B FOR WORK PERFORMED.
- [SDR SWIA201541155](https://openairdocs.org/sdr/SWIA201541155.md): Bulkhead · unknown · Apr 20, 2015 · N929EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > ACCOMPLISH REO TO LT SIDE FS 559 PRESSURE BULKHEAD, ACCOMPLISHED REO TO LT SIDE BS 559, PRESSURE BULKHEAD. COMPLIED WITH ST 51-900-1003, ATTACHED BTAC M-210B FOR WORK PERFORMED.

Next page: https://openairdocs.org/aircraft/N929EV/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 = 'N929EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N929EV/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.