# Service difficulty reports: N909EV

A list on [N909EV](https://openairdocs.org/aircraft/N909EV.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 5 · 232 reports

- [SDR SWIA2026092777277](https://openairdocs.org/sdr/SWIA2026092777277.md): Switch · failed · Sep 27, 2026 · N909EV · Cndair CL6002B19 · Stabilizer Position Indicating
  > STAB TRIM CAUTION ON TAKEOFF AT FLAPS 8 RAN APPROPRIATE QRH, MESSAGE DID NOT CLEAR FLIGHT 6058 - FILED CLOSEDWHILE ATTEMPTING TO ENGAGE STAB TRIM CHANNELS 1 AND 2, FOUND THAT THE STAB TRIM CAUTION MESSAGE WOULD REPOPULATE AFTER A SECONDINTERROGATED MDC AND FOU
- [SDR SWIA2026071576650](https://openairdocs.org/sdr/SWIA2026071576650.md): Hinge Bracket · broken · Jul 15, 2026 · N909EV · Cndair CL6002B19 · Passenger/Crew Doors
  > OPERATIONS CALLED TO ADVISE THEY ARE HAVING DIFFICULTY OPERATING THE MCD. FLIGHT 4639. UPON INSPECTION FOUND PAX DOOR VENT FLAP AFT HINGE BRACKET BROKEN. REMOVED AND REPLACED PAX DOOR VENT FLAP AFT HINGE BRACKET WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH
- [SDR SWIA2026030975484](https://openairdocs.org/sdr/SWIA2026030975484.md): Landing Gear · warning message · Mar 9, 2026 · N909EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE. FIXED WITH QRH. (FLIGHT 6022). CP 31854923 FOR FUNCTION TEST OF THE GEAR EXTENSION/RETRACTION SYSTEM SEE CP 31854883 FOR INSPECTION OF NLG OLEO CENTERING SENSOR, HARNESS, AND BRACKET SEE CP 31854876 FOR CHECKING AND RIGGING AL
- [SDR SWIA2026012375095](https://openairdocs.org/sdr/SWIA2026012375095.md): Skin · dented · Jan 23, 2026 · N909EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN BETWEEN BS 409+80 - 409+96, S18 - 19L, PERMANENT REPAIR OF LT FUSELAGE SKIN IAW REO 601R-53-31-1363, REV CP 31597873 FOR STEP 1, CP 31599706 FOR STEP 2, 31596075 FOR STEP 3, 31599715 FOR STEP 4, 31596400 FOR STEP 5, 31599965 FOR STEPS 7
- [SDR SWIA2025060200522](https://openairdocs.org/sdr/SWIA2025060200522.md): Unknown · odor · May 22, 2025 · N909EV · Cndair CL6002B19 · Air Distribution System
  > DURING CRUISE AT FL320 GOT A STRONG BURNING SMELL FROM THE FLIGHT DECK VENTS. AT ONE POINT WE HAD A BURNING SMOKE SMELL. (FLIGHT 5021 - FILED CLOSED)MAY 23, 2025 STATION: CID--PREVIOUS TROUBLESHOOTING NOTED, TROUBLESHOT IN REFERENCE TO FIM 21-21-00, PERFOR
- [SDR SWI2025F00655](https://openairdocs.org/sdr/SWI2025F00655.md): Unknown · odor · May 22, 2025 · N909EV · Cndair CL6002B19 · Air Distribution System
  > DURING CRUISE AT FL320 GOT A STRONG BURNING SMELL FROM THE FLIGHT DECK VENTS. AT ONE POINT WE HAD A BURNING SMOKE SMELL. (FLIGHT 5021 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025051918](https://openairdocs.org/sdr/SWIA2025051918.md): Unknown · odor · May 18, 2025 · N909EV · Cndair CL6002B19 · Air Distribution System
  > STRONG BURNING SMELL DURING FLIGHT. NO SMOKE. NO INDICATION. FA COULD NOT SMELL IT. PARTIALLY DISSIPATED DURING FLIGHT THEN CAME BACK STRONGER. SMELL WENT AWAY DURING DECENT. REFERENCE AML 1607385, 1607510, 1607516 AND 1607525. (FLIGHT 5435) TROUBLESHOT BURNIN
- [SDR J6BA2025022006](https://openairdocs.org/sdr/J6BA2025022006.md): Fastener · missing · Feb 6, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BEAM JOINTS AT FS 409.00 TO FS 409.00 + 10 LBL 27.0, LBL 9.0, RBL 9.0, AND RBL 27.0 MISSING FASTENERS. (FILED CLOSED) COMPLIED WITH REO 601R-53-21-3722, REV--, DATED 2025-02-13 FOR DISPOSITION FOR MISSING FASTENERS TO FLOOR BEAM INSTALLATION BTW FS4
- [SDR J6BA2025022005](https://openairdocs.org/sdr/J6BA2025022005.md): Floorbeam · damaged · Feb 5, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS 409.00 TO FS 409.00 + 37 AT RBL 9.0 BEYOND LIMITS OF REO 601R-53-00-005. (FILED CLOSED) PERFORMED REPAIR OF FLOOR BEAM FROM FS 409.00 TO FS 409.00 + 37 WITH REFERENCE TO REO 601R-53-00-027 REV "D" DATED 26-NOV-20
- [SDR J6BA202502060005](https://openairdocs.org/sdr/J6BA202502060005.md): Floor Support · damaged · Feb 5, 2025 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS 409.00 TO FS 409.00 + 37 AT RBL 9.0 BEYOND LIMITS OF REO 601R-53-00-005. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR J6BA202502200128](https://openairdocs.org/sdr/J6BA202502200128.md): Bulkhead · cracked · Jan 28, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD (FS621), INTERCOSTAL CRACKED INLINE WITH STINGER 14L. (FILED CLOSED) REMOVED AND REPLACED THE INTERCOSTAL INLINE WITH STINGER 14L ON THE AFT SIDE OF THE AFT PRESSURE BULKHEAD FS621.00. WORK DONE IN REFERENCE WITH THE CRJ-200 SRM 51-
- [SDR J6BA20250131028](https://openairdocs.org/sdr/J6BA20250131028.md): Intercostal · cracked · Jan 28, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD (FS621), INTERCOSTAL CRACKED INLINE WITH STINGER 14L. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR J6BA202502020127](https://openairdocs.org/sdr/J6BA202502020127.md): Mount Bracket · cracked · Jan 27, 2025 · N909EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT BALANCE SPRING MOUNTING BRACKET WITH REFERENCE TO CRJ-200 SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION OF FASTENER BORES THROUGH ENTIRE STACK UP
- [SDR J6BA2025013127](https://openairdocs.org/sdr/J6BA2025013127.md): Bracket · cracked · Jan 27, 2025 · N909EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET CRACKED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR J6B2025F00004](https://openairdocs.org/sdr/J6B2025F00004.md): Bracket · none · Jan 24, 2025 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 HAS BEEN REMOVED TO FOM (FILED CLOSED) INSTALLED THE PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 IN REFERENCE WITH THE CRJ-200 SRM 51-42-06. COMPLETED FORM
- [SDR J6BA20250220124](https://openairdocs.org/sdr/J6BA20250220124.md): Sill Drain · corroded · Jan 24, 2025 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES. (FILED CLOSED) BLENDED CORROSION ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS
- [SDR J6B2025F00002](https://openairdocs.org/sdr/J6B2025F00002.md): None · none · Jan 24, 2025 · N909EV · Cndair CL6002B19 · Standard Practices/Structures
  > PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 HAS BEEN REMOVED TO FOM (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR J6BA20250128024](https://openairdocs.org/sdr/J6BA20250128024.md): Door Frame · corroded · Jan 24, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION FOUND ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR J6BA202502200121](https://openairdocs.org/sdr/J6BA202502200121.md): Door Sill · corroded · Jan 21, 2025 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL LOWER ANGLE (REF SRM 53-21-23 ITEM 56B) CORRODED. (FILED CLOSED) REMOVED AND REPLACED THE PAX DOOR SILL LOWER ANGLE IN REFERENCE WITH THE CRJ-200 SRM 51-42-06, SRM 51-42-21, SRM 51-42-13 AND SRM 53-21-23. COMPLETED FORM M-337. COMPLIED WITH
- [SDR J6BA20250128021](https://openairdocs.org/sdr/J6BA20250128021.md): Angle · corroded · Jan 21, 2025 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL LOWER ANGLE (REF SRM 53-21-23 ITEM 56B) CORRODED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR J6BA20250220115](https://openairdocs.org/sdr/J6BA20250220115.md): Floorbeam · corroded · Jan 15, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BEAM, FLOOR BOARD LANDING HAS SURFACE CORROSION BETWEEN FS 409.00 TO 409.00 +112 @ RBL 9.00. (FILED CLOSED) REMOVED CORROSION ON FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS409.00 TO FS409.00 + 112 @ RBL 9.0 WITH REFERENCE TO SRM 51-21-06. PERFORMED
- [SDR J6B2025F00003](https://openairdocs.org/sdr/J6B2025F00003.md): Retainer · gouged · Jan 15, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR UPPER AFT CORNER SEAL RETAINER GOUGED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR UPPER AFT CORNER SEAL RETAINER WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY. REFERENCE CHILD CAMP FOR LEAK
- [SDR J6BA2025012815](https://openairdocs.org/sdr/J6BA2025012815.md): Floor Support · corroded · Jan 15, 2025 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT FLOOR BOARD LANDING HAS SURFACE CORROSION BETWEEN FS 409.00 TO 409.00 +112 @ RBL 9.00.
- [SDR J6B2025F00001](https://openairdocs.org/sdr/J6B2025F00001.md): Retainer · gouged · Jan 15, 2025 · N909EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER AFT CORNER SEAL RETAINER GOUGED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR J6BA20250220114](https://openairdocs.org/sdr/J6BA20250220114.md): Pump · failed insp · Jan 14, 2025 · N909EV · Cndair CL6002B19 · Fuel Boost Pump
  > RH ELECTRIC BOOST PUMP SATELLITE HOLE # 9 ON LOWER AFT WING PLANK HAS TOO MUCH NOISE INDICATION DURING EDDY CURRENT OPEN HOLE INSPECTION. (FILED CLOSED) REPAIRED RH ELECTRIC BOOST PUMP SATELLITE HOLE #9 ON LOWER AFT WING PLANK WITH REFERENCE TO REO 601R
- [SDR J6B2025F00000](https://openairdocs.org/sdr/J6B2025F00000.md): Structure · failed insp · Jan 14, 2025 · N909EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RH ELECTRIC BOOST PUMP SATELLITE HOLE # 9 ON LOWER AFT WING PLANK HAS TOO MUCH NOISE INDICATION DURING EDDY CURRENT OPEN HOLE INSPECTION. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR J6BA20250220111](https://openairdocs.org/sdr/J6BA20250220111.md): Floor Support · corroded · Jan 11, 2025 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CABIN FLOOR SILL ASSY WL73.00 BETWEEN FS559.00 TO FS 559.00 + 16 AND BETWEEN RBL 41.75 (FILED CLOSED) COMPLIED WITH REO 601R-53-51-699 DATED: 2025-01-15 REV - - TEMPORARY DISPOSITION FOR BLENDED CORROSION DAMAGE TO FLOOR SILL STRUCTURE BT
- [SDR J6BA20250220109](https://openairdocs.org/sdr/J6BA20250220109.md): Pressure Deck · corroded · Jan 9, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION ON LH PRESSURE FLOOR ASSY WL73.00 BETWEEN FS409 + 128 -TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00. (FILED CLOSED) BLENDED CORROSION ON LH PRESSURE FLOOR SILL ASSY WL73.00 BETWEEN FS409 + 128 TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00 WITH
- [SDR J6BA202501170009](https://openairdocs.org/sdr/J6BA202501170009.md): Pressure Deck · corroded · Jan 9, 2025 · N909EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION ON LH PRESSURE FLOOR ASSY WL73.00 BETWEEN FS409 + 128 -TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00.
- [SDR SWIA20230412003](https://openairdocs.org/sdr/SWIA20230412003.md): Heating Element · warning message · Apr 12, 2023 · N909EV · Cndair CL6002B19 · Pneumatic Indicating System
  > IN CRUISE TO DEN RECEIVED L/H 14TH STAGE DUCT WARNING FOLLOWED QRH TO LAND AT NEAREST SUITIBLE AIRPORT (FLIGHT 4741 FILED CLOSED)UPON ARRIVAL TO AIRCRAFT FOUND 14TH STAGE DUCT WARNING TO BE HARD FAULTED AND PYLON LOOP SECTION OF A/ICE PAGE OF THE EICAS TO BE I
- [SDR SWIA202265389](https://openairdocs.org/sdr/SWIA202265389.md): Flap System · failed · Apr 18, 2022 · N909EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > D: FLAP FAIL CAUTION FLAPS STUCK AT 8 OUT OF RNO ON FLAP RETRACT / C: MCI / CAT: "A" DUE IN 10 FC FROM TAC 37285 (DUE AT TAC 37295) / FLAP FAIL CAUTION FLAPS STUCK AT 8 OUT OF RNO ON FLAP RETRACT (FLIGHT 5998 - FILED CLOSED) APR 18, 2022 STATION: SFO--R
- [SDR SWIA202265137](https://openairdocs.org/sdr/SWIA202265137.md): None · cracked · Mar 21, 2022 · N909EV · Cndair CL6002B19 · Fuselage Structure (General)
  > THE BRAKET OUTBOARD OF THE FORWARD LOWER ROLLER TRACK FOR THE CARGO DOOR IS CRACKING FROM TWO RIVET HEADS. (FILED - CLOSED) REMOVED AND REPLACED DAMAGED BRACKET O/B OF THE FWD LOWER ROLLER TRACK FOR THE CARGO DOOR IN REFERENCE TO CRJ200 SRM 51-42-21.
- [SDR SWIA202264096](https://openairdocs.org/sdr/SWIA202264096.md): None · worn · Jan 31, 2022 · N909EV · Cndair CL6002B19 · Powerplant System
  > RH ENGINE AFT MOUNT THRUST FITTING APPEARS TO BE WORN (FILED CLOSED) REMOVED AND REPLACED THE RH ENGINE AFT THRUST FITTING IN REFERENCE TO AMM: 71-22-01. / TORQUE WRENCH INFO: / S/N: 1021102692 DUE: 7/2022
- [SDR SWIA202264095](https://openairdocs.org/sdr/SWIA202264095.md): None · failed · Jan 30, 2022 · N909EV · Cndair CL6002B19 · Powerplant System
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: NDT ENG MOUNT SHAFT - ENGINE MOUNT THRUST SHAFT DUE NDT INSPECTION. REMOVE AND REPLACE ENGINE THRUST MOUNT SHAFT IN REFERENCE TO AMM 71-00-00 AND 71-430-603 AND 71-440-603. SEND TO VENDOR FOR COMPLIANCE OF NDT (MRB 71-21
- [SDR SWIA202161239](https://openairdocs.org/sdr/SWIA202161239.md): None · failed · Sep 27, 2021 · N909EV · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR DISAGREE WARNING MESSAGE ON TAKEOFF OUT OF RNO WHEN SELECTING GEAR UP. NOSE WHEEL DOOR WARNING MESSAGE AND NOSE WHEEL STEERING INOP CAUTION ASSOCIATED. COMPLIED WITH QRH GEAR DOWN THREE GREEN AFTERWARDS. (FLIGHT 5899 - FILED CLOSED) INTERROGATED PSE
- [SDR SWIA2021072859784](https://openairdocs.org/sdr/SWIA2021072859784.md): Floor Support · broken · Jul 14, 2021 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL FROM FS559+80 TO FS574 HAS MULTIPLE BROKEN NUTPLATES. REPLACEMENT REQUIRED. (C-CHECK RO 7/24/2021) REPLACED 13EA NUTPLATES ON LH FLOOR SILL BETWEEN FS559+80 AND FS574 IAW CRJ200 SRM 51-45-00. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2021072859783](https://openairdocs.org/sdr/SWIA2021072859783.md): Pcu · out of rig · Jun 30, 2021 · N909EV · Cndair CL6002B19 · Drag Control System
  > RH SPOILERON I/B AND O/B PCUS OUT OF RIG. TRAILING EDGE SURFACE EXCEEDS 0.120 ABOVE THE FLAP SURFACE. (C-CHECK RO 7/24/2021) REMOVED, REPLACED, AND RIGGED RH SPOILERON IB PCU AND RIGGED RH SPOILERON OB PCU IAW CRJJ 200 AMMS 27-62-01-830-801 & 27-62-01-
- [SDR SWIA202159773](https://openairdocs.org/sdr/SWIA202159773.md): Skin · dented · May 27, 2021 · N909EV · Cndair CL6002B19 · Elevator, Plate/Skin
  > FOUND DENT ON L/H ELEVATOR LOWER SKIN. (C-CHECK RO 7/24/2021) REPAIRED LH ELEVATOR LOWER SKIN IAW CRJ200 SRM 55-20-00 REV. 38, DATED 07/10/20419. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. WEIGHT CHANGE 0.5 LBS. SEE C
- [SDR SWIA2021072859771](https://openairdocs.org/sdr/SWIA2021072859771.md): Skin · chafed · May 3, 2021 · N909EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK AT WS 45 IS CHAFED AT THE AFT EDGE ALONG WITH TWO FASTENER HEADS. (C-CHECK RO 7/24/2021) RIGHT LOWER WING PLANK AT WS 45 IS CHAFED AT THE AFT EDGE ALONG WITH TWO FASTENER HEADS WAS REPAIRED IAW BOMBARDIER REO 601R-57-21-880 REV-D
- [SDR SWIA2021072859770](https://openairdocs.org/sdr/SWIA2021072859770.md): Hinge · chafed · Apr 22, 2021 · N909EV · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H OUTBOARD FLAP OUTBOARD HNIGE BOX HAS CHAFE/GOUGE DAMAGE AT THE AFT ATTACHMENT POINT (C-CHECK RO 7/24/2021) REPAIRED R/H OUTBOARD FLAP OUTBOARD HNIGE BOX AT W.S 264.00 CHAFE/GOUGE DAMAGE AT THE AFT ATTACHMENT POINT IAW MHIRJ REO 601R-57-21-3466 REV--
- [SDR SWIA2021072859785](https://openairdocs.org/sdr/SWIA2021072859785.md): Skin · corroded · Apr 13, 2021 · N909EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN ACCESS HOLE AT PANEL 640AT CUTOUT HAS SEVERAL AREAS OF MINOR CORROSION AROUND CUTOUT. (C-CHECK RO 7/24/2021) REPAIRED RH WING UPPER SKIN IAW REO 601R-57-21-3464 REV -- DATED 2021-04-29 BOND CHECK GOOD. SEE CONTINUATION CARD FOR DE
- [SDR SWIA202159769](https://openairdocs.org/sdr/SWIA202159769.md): Closeout Panel · corroded · Apr 13, 2021 · N909EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR LOWER CLOSE OUT FWD AND AFT LOWER PANS ARE HEAVILY CORRODED (C-CHECK RO 7/24/2021) REMOVED AND REPLACED SERVICE DOOR LOWER CLOSE OUT FWD AND AFT LOWER PANS IAW CRJ 200 SRM 51-42-06, 51-42-21,51-42-10 AND SNIEO 60138304S05 AND S06. FORM 33
- [SDR SWIA2021072859786](https://openairdocs.org/sdr/SWIA2021072859786.md): Skin · corroded · Apr 12, 2021 · N909EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING UPPER SKIN ACCESS HOLE AT PANEL 540AT CUTOUT HAS MINOR CORROSION IN SEVERAL AREAS AROUND CUTOUT. (C-CHECK RO 7/24/2021) REMOVED CROSSION FROM PANELS 540AT, 540BT, AND 540 CT PANEL LANDING IAW CRJ 200 SRM 51-21-06. COMPLIED WITH MHIRJ REO 601R-
- [SDR SWIA2021072859768](https://openairdocs.org/sdr/SWIA2021072859768.md): Fitting · cracked · Apr 11, 2021 · N909EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. (C-CHECK RO 7/24/2021) REMOVED AND REPLACED CO-PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING IAW CRJ 200 SRM- 51-42-21, 51-40-11 AND DWG 601R33007. COMPLETED TASK CARD 51-900-1003-SKY AND ATT
- [SDR SWIA2021072859767](https://openairdocs.org/sdr/SWIA2021072859767.md): Fitting · cracked · Apr 11, 2021 · N909EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. (C-CHECK RO 7/24/2021) REMOVED AND REPLACED PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING IAW CRJ 200 SRM- 51-42-21, 51-40-11 AND DWG 601R33007. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED
- [SDR SWIA2021072859782](https://openairdocs.org/sdr/SWIA2021072859782.md): Angle · cracked · Apr 9, 2021 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH UPPER OBLIQUE ANGLE CRACKED AT FS621.00 TO FS625.00 RBL45 STRGR 14R AND WL97.5 (C-CHECK RO 7/24/2021) REMOVED AND REPLACED RH UPPER OBLIQUE ANGLE AT FS621.00 TO FS625.00 RBL45 STRG14R AND WL97.5 IAW CRJ200 SRM 51-42-21
- [SDR SWIA2021072859781](https://openairdocs.org/sdr/SWIA2021072859781.md): Angle · cracked · Apr 9, 2021 · N909EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH UPPER OBLIQUE ANGLE CRACKED AT FS621.00 TO FS625.00 LBL45 STRGR 14L AND WL97.5 (C-CHECK RO 7/24/2021) REMOVED AND REPLACED LH UPPER OBLIQUE ANGLE AT FS621,00 TO 625.00 LBL45 STRG14L AND WL97.5 IAW CRJ200 SRM 51-42-21
- [SDR SWIA2021072859780](https://openairdocs.org/sdr/SWIA2021072859780.md): Structure · damaged · Apr 8, 2021 · N909EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > BAGGAGE DOOR AFT UPPER "TEE" IMPACT DAMAGE @ FS621.0 (C-CHECK RO 7/24/2021) REMOVED AND REPLACED AFT UPPER T FITTING IAW CRJ 200 AMM 52-31-00-820-801 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
- [SDR SWIA2021072859779](https://openairdocs.org/sdr/SWIA2021072859779.md): Seat Track · gouged · Apr 8, 2021 · N909EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL RIGHT SIDE FORWARD OF FS409.0 +128 NINE PLACES GOUGED (C-CHECK RO 7/24/2021) SEAT RAIL RIGHT SIDE FORWARD OF FS409.0 +128 NINE PLACES GOUGED, FOUND TO BE OUT OF LIMITS. REFERENCE CAMP# 22737342 FOR FABRICATION AND INSTALL OF NEW SEAT RAIL
- [SDR SWIA2021072859766](https://openairdocs.org/sdr/SWIA2021072859766.md): Hinge Arm · damaged · Apr 8, 2021 · N909EV · Cndair CL6002B19 · Trailing Edge Flaps
  > L/H OUTBOARD FLAP HINGE ARM AT FLAP ATTACH POINT IS DAMGAGED ON INNER FLANGE FROM COUNTER SUNK SCREW BEING LEFT IN HINGE ARM AREA. (C-CHECK RO 7/24/2021) REPAIRED LH OUTBOARD FLAP OB HINGE ARE AT WS 264.00 IAW MHIRJ REO 601R-57-21-3468 DATED 2021-05-02

Next page: https://openairdocs.org/aircraft/N909EV/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 = 'N909EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N909EV/reports

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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.