# Service difficulty reports: N906EV

A list on [N906EV](https://openairdocs.org/aircraft/N906EV.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 6 · 293 reports

- [SDR SWIA2026031975560](https://openairdocs.org/sdr/SWIA2026031975560.md): Retainer · gouged · Mar 19, 2026 · N906EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER AFT SEAL RETAINER IS GOUGED. REMOVED AND REPLACED THE CARGO DOOR UPPER AFT SEAL RETAINER IN REFERENCE WITH THE SRM 51-42-06.
- [SDR SWIA2026031975559](https://openairdocs.org/sdr/SWIA2026031975559.md): Track · cracked · Mar 19, 2026 · N906EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK ON FS 574.00, BOTTOM CHANNEL NEAR DOOR SURROUND IS CRACKED. REMOVED AND REPLACED THE CARGO DOOR FWD TRACK ON FS 574.00, BOTTOM CHANNEL NEAR DOOR SURROUND IN REFERENCE WITH THE SRM 51-42-06.
- [SDR SWIA2026031975558](https://openairdocs.org/sdr/SWIA2026031975558.md): Bracket · cracked · Mar 19, 2026 · N906EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD BALANCE SPRING BRACKET ASSEMBLY ON FS 574.00 NEAR STR 6L IS CRACKED. REMOVED AND REPLACED THE CARGO DOOR FWD BALANCE SPRING BRACKET ASSEMBLY ON FS 574.00 NEAR STR 6L IN REFERENCE WITH THE SRM 51-42-06.
- [SDR SWIA2026031975557](https://openairdocs.org/sdr/SWIA2026031975557.md): Track · damaged · Mar 19, 2026 · N906EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR TRACK ON FWD FACE OF FS 621.00 BULKHEAD IS DAMAGED FROM DOOR ROLLER. REMOVED AND REPLACED THE AFT CARGO DOOR TRACK ON FWD FACE OF FS 621.00 BULKHEAD IN REFERENCE WITH THE CRJ-200 SRM 51-42-06 AND SRM 51-42-21. PERFORMED EDDY CURRENT INSPECTION
- [SDR SWIA2026031875556](https://openairdocs.org/sdr/SWIA2026031875556.md): Bracket · cracked · Mar 18, 2026 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRANSFER FROM EAML 1842990: CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1842558 BRACKET IN AFT CARGO BAY INBOARD OF AFT CARGO DOOR FWD ROLLER TRACK FS574.00 BELOW AFT CARGO DOOR COUNTER BALANCE SPRING GROOVE PULLEY IS CRACKED APROX 2 INCHES LONG
- [SDR SWIA2025061305](https://openairdocs.org/sdr/SWIA2025061305.md): Windshield · cracked · Jun 5, 2025 · N906EV · Cndair CL6002B19 · Flight Compartment Windows
  > IN CRUISE NOTICED A BLACK PUFF ON RIGHT WINDSHIELD, THEN ORANGE GLOW, AND SPIDER WEBBING CRACK ON WINDSHIELD. SHORTLY AFTER R WINDOW HEAT CAUTION AND R WSHLD HEAT CAUTION. (FLIGHT 5945 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30276892 WITH
- [SDR SWI2025F00713](https://openairdocs.org/sdr/SWI2025F00713.md): Windshield · cracked · Jun 5, 2025 · N906EV · Cndair CL6002B19 · Flight Compartment Windows
  > IN CRUISE NOTICED A BLACK PUFF ON RIGHT WINDSHIELD, THEN ORANGE GLOW, AND SPIDER WEBBING CRACK ON WINDSHIELD. SHORTLY AFTER R WINDOW HEAT CAUTION AND R WSHLD HEAT CAUTION. (FLIGHT 5945 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20250102](https://openairdocs.org/sdr/SWIA20250102.md): Indicator · unreliable · Jan 2, 2025 · N906EV · Cndair CL6002B19 · Airspeed/Mach Indicator
  > FLIGHT CREW REPORTS: UNRELIABLE AIRSPEED JUST AFTER TAKEOFF. EFIS COMP MON WITH IAS AND ALT FLAGS. MACH TRIM AND STALL FAIL CAUTIONS ALSO APPEARED. FO'S SIDE AFFECTED WITH AIRSPEED RANGING FROM 80 KNOTS TO 180 KNOTS DIFFERENT AND ALTITUDE 2000' DIFFERENT. (
- [SDR SWIA20240830](https://openairdocs.org/sdr/SWIA20240830.md): Splice · corroded · Aug 30, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Structure
  > UNION SPLICE AT FS 559.00-RBL9 IS CORRODED. REMOVED CORROSION AT UNION SPLICE AT FS 559.00-RBL9 REF SRM 51-21-06EVALUATED. ORIGINAL THICKNESS UPPER SIDE 0.150" REF STANDAR CMS6798 REV--, MINIMUM THICKNESS MEASURED 0.030", MATERIAL LOSS 0.120" WAS FOUND OUT O
- [SDR SWIA2024111508024](https://openairdocs.org/sdr/SWIA2024111508024.md): Door Frame · chafed · Aug 24, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Structure
  > THE CARGO DOOR SURROUND LOWER AFT STOP FITTING IS CHAFFED. (C-CHECK RO 10/26/2024) (FILED CLOSED)COMPLIED WITH ALL STEPS OF MHIRJ REO 601R-53-61-8221, REV--, DATED 2024-09-04 IN THE REPAIR OF THE AFT CARGO DOOR SURROUND LOWER AFT STOP FITTING. SEE CONTINUATIO
- [SDR SWIA2024102824](https://openairdocs.org/sdr/SWIA2024102824.md): Stop Fitting · chafed · Aug 24, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Structure
  > THE CARGO DOOR SURROUND LOWER AFT STOP FITTING IS CHAFFED. (C-CHECK RO 10/26/2024) (FILED OPEN)COMPLIED WITH ALL STEPS OF MHIRJ REO 601R-53-61-8221, REV--, DATED 2024-09-04 IN THE REPAIR OF THE AFT CARGO DOOR SURROUND LOWER AFT STOP FITTING. SEE CONTINUATION
- [SDR SWIA20241115823](https://openairdocs.org/sdr/SWIA20241115823.md): Spar · gouged · Aug 23, 2024 · N906EV · Cndair CL6002B19 · Wing Spar
  > RH WING AFT SPAR AILERON HINGE FITTING #4 GOUGE ON LOWER OUTBOARD SIDE (C-CHECK RO 10/26/2024) (FILED CLOSED)COMPLIED WITH ALL STEPS OF MHIRJ REO 601R-57-51-1056 REV -- DATED 2024-09-09 IN THE REPAIR OF THE RH WING AFT SPAR AILERON HINGE FITTING #4 ON THE LOWE
- [SDR SWIA202411150023](https://openairdocs.org/sdr/SWIA202411150023.md): Spar · gouged · Aug 23, 2024 · N906EV · Cndair CL6002B19 · Wing Spar
  > LH WING AFT SPAR AILERON HINGE FITTING #3 GOUGE BETWEEN LUGS AND ON LOWER OUTBOARD SIDE (C-CHECK RO 10/26/2024) (FILED CLOSED)REPAIRED LH WING AFT SPAR AILERON HINGE FITTING #3 IAW REO 601R-57-51-1055 REV --, DATED 2024-09-07, SEE CONTINUATION CARD FOR FURTHER
- [SDR SWI2024F01065](https://openairdocs.org/sdr/SWI2024F01065.md): Hinge Fitting · gouged · Aug 23, 2024 · N906EV · Cndair CL6002B19 · Ailerons
  > RH WING AFT SPAR AILERON HINGE FITTING #2 GOUGE ON LOWER INBOARD AND OUTBOARD SIDE (C-CHECK RO 10/26/2024) (FILED OPEN)COMPLIED WITH ALL STEPS OF REO 601R-57-51-1057 REV -- DATED 2024-09-09 IN THE REPAIR OF THE RH WING AFT SPAR AILERON HINGE FITTINGS #2 AND #3
- [SDR SWI2024F01064](https://openairdocs.org/sdr/SWI2024F01064.md): Hinge Fitting · gouged · Aug 23, 2024 · N906EV · Cndair CL6002B19 · Ailerons
  > RH WING AFT SPAR AILERON HINGE FITTING #4 GOUGE ON LOWER OUTBOARD SIDE (C-CHECK RO 10/26/2024) (FILED OPEN)COMPLIED WITH ALL STEPS OF MHIRJ REO 601R-57-51-1056 REV -- DATED 2024-09-09 IN THE REPAIR OF THE RH WING AFT SPAR AILERON HINGE FITTING #4 ON THE LOWER
- [SDR SWI2024F01063](https://openairdocs.org/sdr/SWI2024F01063.md): Hinge Fitting · gouged · Aug 23, 2024 · N906EV · Cndair CL6002B19 · Ailerons
  > LH WING AFT SPAR AILERON HINGE FITTING #3 GOUGE BETWEEN LUGS AND ON LOWER OUTBOARD SIDE (C-CHECK RO 10/26/2024) (FILED OPEN)REPAIRED LH WING AFT SPAR AILERON HINGE FITTING #3 IAW REO 601R-57-51-1055 REV --, DATED 2024-09-07, SEE CONTINUATION CARD FOR FURTHER D
- [SDR SWIA2024102823](https://openairdocs.org/sdr/SWIA2024102823.md): Hinge Fitting · gouged · Aug 23, 2024 · N906EV · Cndair CL6002B19 · Ailerons
  > LH WING AFT SPAR AILERON HINGE FITTING #2 OUTBOARD LUG GOUGED (C-CHECK RO 10/26/2024) (FILED OPEN)REPAIRED LH WING AFT SPAR AILERON HINGE FITTING #2 OUTBOARD LUG AS PER REO 601R-57-51-1053 REV--, 2024-09-01. SEE CONTINUATION CARD FOR FURTHER DETAILS. AND COMP
- [SDR SWIA20241115822](https://openairdocs.org/sdr/SWIA20241115822.md): Hinge Fitting · worn · Aug 22, 2024 · N906EV · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF BEARING ON L/H ELEVATOR I/B HINGE FITTING P/N 600-24043-1, FOUND BEARING BORE TO BE PITTED AND WORN. I/B HINGE FITTING REQUIRES REPLACEMENT. (C-CHECK RO 10/26/2024) (FILED CLOSED)INSTALLED 1 EA. NEW L/H ELEVATOR INBD HINGE FITTING ASSY. P/N 600
- [SDR SWIA2024102822](https://openairdocs.org/sdr/SWIA2024102822.md): Hinge Fitting · worn · Aug 22, 2024 · N906EV · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL OF BEARING ON L/H ELEVATOR I/B HINGE FITTING P/N 600-24043-1, FOUND BEARING BORE TO BE PITTED AND WORN. I/B HINGE FITTING REQUIRES REPLACEMENT. (C-CHECK RO 10/26/2024) (FILED OPEN)INSTALLED 1 EA. NEW L/H ELEVATOR INBD HINGE FITTING ASSY. P/N 600-2
- [SDR SWI2024F01262](https://openairdocs.org/sdr/SWI2024F01262.md): Hinge Fitting · worn · Aug 21, 2024 · N906EV · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > DURING REMOVAL OF BEARING ON R/H ELEVATOR I/B HINGE FITTING PN 600-24043-1, FOUND BEARING BORES TO BE PITTED AND WORN. I/B HINGE FITTING REQUIRES REPLACEMENT. (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND REPLACED 1 EA. HINGE FITTING ASSEMBLY P/N 600-24043
- [SDR SWI2024F01261](https://openairdocs.org/sdr/SWI2024F01261.md): Striker · damaged · Aug 21, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SEAL STRIKER DAMAGED IN FORWARD AND AFT CORNERS AS MARKED (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND INSTALLED NEW SERVICE DOOR LOWER STRIKER SEALS ON THE AFT AND FWD SIDES REF CRJ 200 SRM 51-42-06 AND DWG 601R38340 REV. B. COMPLIED W
- [SDR SWIA2024111510821](https://openairdocs.org/sdr/SWIA2024111510821.md): Gusset · gouged · Aug 21, 2024 · N906EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR GUSSET AT FS310.0 STGR10R GOUGED AS MARKED (FILED CLOSED)REMOVED DAMAGED SERVICE DOOR GUSSET & INSTALLED NEW SERVICE DOOR GUSSET AT FS310.00 STGR 10R REF. DWG 601R38303 REV. AR & CRJ200 SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWI2024F01062](https://openairdocs.org/sdr/SWI2024F01062.md): Hinge Fitting · worn · Aug 21, 2024 · N906EV · Cndair CL6002B19 · Elevator Structure
  > DURING REMOVAL OF BEARING ON R/H ELEVATOR I/B HINGE FITTING PN 600-24043-1, FOUND BEARING BORES TO BE PITTED AND WORN. I/B HINGE FITTING REQUIRES REPLACEMENT. (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED 1 EA. HINGE FITTING ASSEMBLY P/N 600-24043-1
- [SDR SWI2024F01061](https://openairdocs.org/sdr/SWI2024F01061.md): Striker · damaged · Aug 21, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Structure
  > SERVICE DOOR LOWER SEAL STRIKER DAMAGED IN FORWARD AND AFT CORNERS AS MARKED (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND INSTALLED NEW SERVICE DOOR LOWER STRIKER SEALS ON THE AFT AND FWD SIDES REF CRJ 200 SRM 51-42-06 AND DWG 601R38340 REV. B. COMPLIED WIT
- [SDR SWIA2024102821](https://openairdocs.org/sdr/SWIA2024102821.md): Gusset · gouged · Aug 21, 2024 · N906EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR GUSSET AT FS310.0 STGR10R GOUGED AS MARKED (FILED OPEN)REMOVED DAMAGED SERVICE DOOR GUSSET & INSTALLED NEW SERVICE DOOR GUSSET AT FS310.00 STGR 10R REF. DWG 601R38303 REV. AR & CRJ200 SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA20240818](https://openairdocs.org/sdr/SWIA20240818.md): Angle · cracked · Aug 18, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED JOINT ANGLE AT FS409+32 STGR6R. REMOVED AND REPLACED CRACKED JOINT ANGLE AT FS409+32 STGR6R WITH NEW FABRICATED ANGLE PN 601R32201-12 REF CRJ 200 SRM 51-42-06 AND DWG 601R32201 REV G. COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.
- [SDR SWI2024F01263](https://openairdocs.org/sdr/SWI2024F01263.md): Window Post · cracked · Aug 15, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RH EXTERNAL WINDSHIELD SIDE POST LWR UPPER AFT BOLT HOLE CRACKED (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND REPLACED RH EXTERNAL WINDSHIELD SIDE POST REF DWG NO. 601R33007 REV -U AND CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY, 56-220
- [SDR SWIA2024111510815](https://openairdocs.org/sdr/SWIA2024111510815.md): Window Post · cracked · Aug 15, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST FS202.75 INSIDE LOWER OTBD & INBD FITTINGS CRACKED AS MARKED (C-CHECK RO 10/26/2024) (FILED CLOSED)REPLACED 2EA CENTER POST WINDSHIELD FITTINGS PN# 601R33237-1S AND 601R33237-2S. REF DWG NO. 601R33007 REV-U AND CRJ-200 SRM 51-42-21 REV-3
- [SDR SWI2024F01060](https://openairdocs.org/sdr/SWI2024F01060.md): Window Post · cracked · Aug 15, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RH EXTERNAL WINDSHIELD SIDE POST LWR UPPER AFT BOLT HOLE CRACKED (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED RH EXTERNAL WINDSHIELD SIDE POST REF DWG NO. 601R33007 REV -U AND CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY, 56-220-1
- [SDR SWIA2024102815](https://openairdocs.org/sdr/SWIA2024102815.md): Window Post · cracked · Aug 15, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST FS202.75 INSIDE LOWER OTBD & INBD FITTINGS CRACKED AS MARKED (C-CHECK RO 10/26/2024) (FILED OPEN)REPLACED 2EA CENTER POST WINDSHIELD FITTINGS PN# 601R33237-1S AND 601R33237-2S. REF DWG NO. 601R33007 REV-U AND CRJ-200 SRM 51-42-21 REV-39
- [SDR SWIA202411150813](https://openairdocs.org/sdr/SWIA202411150813.md): Skin · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Landing Gear Doors
  > NLG AFT DOOR FUSELAGE SKIN CUT OUT, THE AFT RH CORNER POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)COMPLIED WITH ALL STEPSF MHIRJ REO 601R-53-11-048 REV-D DATED 2015-06-10 AND REO 601R-53-11-3943 REV -- DATED 2024-09-02 IN THE R
- [SDR SWI2024F01270](https://openairdocs.org/sdr/SWI2024F01270.md): Skin · chafed · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LH LOWER WING PLANK AND AFT WING SPAR @ APPROX. WS48.00 IS CHAFFED BY THE WING TO BODY FAIRING 193AB (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REPAIRED LH LOWER WING PLANK AND AFT WING SPAR AT APPRO. WS48.00 AS PER REO NO. 601R-57-21-880 REV. -D DATE: 201
- [SDR SWI2024F01269](https://openairdocs.org/sdr/SWI2024F01269.md): Attach Angle · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LH MLG GEAR WELL WS53.60 BATT RIB, THE ATTACH ANGLE ABOVE CANNON PLUGS J411 AND J413 IS CRACKED (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND REPLACED THE BATT RIB ATTACH ANGLE AT WS53.60 IN THE LH MLG WELL ABOVE CANNON PLUGS J411 AND J413 REF DR
- [SDR SWI2024F01268](https://openairdocs.org/sdr/SWI2024F01268.md): Rib · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LH MLG GEAR WELL WS48.30, THE BATT RIB CAP IS CRACKED (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND REPLACED BATT RIB ANGLE ON LH MLG GEAR WELL AT WS48.30 AS PER REO NO 601R-57-21-3857 REV. -- DATE: 2024-08-27. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWI2024F01266](https://openairdocs.org/sdr/SWI2024F01266.md): Frame · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME, FS333.00, IS CRACKED BETWEEN STGR1L & 3L. (MARKED IN RED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND INSTALLED NEW FRAME SECTOR AT FS333 BETWEEN STGR 1L AND STGR 3L IAW ALL STEPS OF REO 601R-53-21-3695 REV--, DATED 2024-08-22, CRJ200 SRM 51-42-0
- [SDR SWI2024F01265](https://openairdocs.org/sdr/SWI2024F01265.md): Hinge · gouged · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE HALF ON DOOR SIDE HAS GOUGED LANDINGS: #15, #18, #22, AND #27 (C-CHECK RO 10/26/2024) (FILED CLOSED)BLENDED DAMAGE FROM PIANO HINGE, EVALUATED AND FOUND OUT OF LIMITS REO 601R-52-11-1347 REV -C DATED: 2017-08-02. REPLACED WITH NEW P
- [SDR SWI2024F01264](https://openairdocs.org/sdr/SWI2024F01264.md): Rib · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RH MLG GEAR WELL WS48.30, THE BATT RIB CAP IS CRACKED (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND REPLACED BATT RIB ANGLE ON RH MLG WELL AT WS48.30 AS PER REO NO. 601R-57-51-1058 REV. -- DATE: 2024-09-11. COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWI2024F01057](https://openairdocs.org/sdr/SWI2024F01057.md): Hinge · damaged · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE HINGE LOBES ELONGATED FROM #6 THRU #27 CAUSING HINGE PIN INDENTIONS IN THE LANDINGS (C-CHECK RO 10/26/2024) (FILED OPEN)BLENDED AND EVAL'D PAX DOOR PIANO HINGE HALF ON FUSELAGE SIDE, FOUND OUT OF LIMITS PER REO
- [SDR SWI2024F01056](https://openairdocs.org/sdr/SWI2024F01056.md): Frame · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME, FS333.00, IS CRACKED BETWEEN STGR1L & 3L. (MARKED IN RED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND INSTALLED NEW FRAME SECTOR AT FS333 BETWEEN STGR 1L AND STGR 3L IAW ALL STEPS OF REO 601R-53-21-3695 REV--, DATED 2024-08-22, CRJ200 SRM 51-42-06
- [SDR SWI2024F01055](https://openairdocs.org/sdr/SWI2024F01055.md): Hinge · gouged · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE HALF ON DOOR SIDE HAS GOUGED LANDINGS: #15, #18, #22, AND #27 (C-CHECK RO 10/26/2024) (FILED OPEN)BLENDED DAMAGE FROM PIANO HINGE, EVALUATED AND FOUND OUT OF LIMITS REO 601R-52-11-1347 REV -C DATED: 2017-08-02. REPLACED WITH NEW PAX
- [SDR SWI2024F01054](https://openairdocs.org/sdr/SWI2024F01054.md): Spar · chafed · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Frame
  > LH LOWER WING PLANK AND AFT WING SPAR @ APPROX. WS48.00 IS CHAFFED BY THE WING TO BODY FAIRING 193AB (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REPAIRED LH LOWER WING PLANK AND AFT WING SPAR AT APPRO. WS48.00 AS PER REO NO. 601R-57-21-880 REV. -D DATE: 2017/
- [SDR SWI2024F01053](https://openairdocs.org/sdr/SWI2024F01053.md): Rib · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH MLG GEAR WELL WS48.30 BATT RIB CAP FORWARD ATTACH ANGLE IS CRACKED (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND INSTALLED NEW BATT RIB CAP ON RH MLG GEAR WELL AT WS48.30 PER DWG# 600-10204 REV -M, REF CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-42-20
- [SDR SWI2024F01052](https://openairdocs.org/sdr/SWI2024F01052.md): Rib · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH MLG GEAR WELL WS48.30, THE BATT RIB CAP IS CRACKED (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED BATT RIB ANGLE ON RH MLG WELL AT WS48.30 AS PER REO NO. 601R-57-51-1058 REV. -- DATE: 2024-09-11. COMPLIED WITH TASK CARD 51-900-1003-SKY AN
- [SDR SWI2024F01051](https://openairdocs.org/sdr/SWI2024F01051.md): Rib · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH MLG GEAR WELL WS48.30 BATT RIB CAP FORWARD ATTACH ANGLE IS CRACKED (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED LH MLG GEAR WELL WS48.30 BATT RIB CAP FORWARD ATTACH ANGLE CRJ 200 SRM 51-42-20, DWG# 601R10212 REV A, DWG# 600-10204 REV -
- [SDR SWI2024F01050](https://openairdocs.org/sdr/SWI2024F01050.md): Rib · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH MLG GEAR WELL WS53.60 BATT RIB, THE ATTACH ANGLE ABOVE CANNON PLUGS J411 AND J413 IS CRACKED (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED THE BATT RIB ATTACH ANGLE AT WS53.60 IN THE LH MLG WELL ABOVE CANNON PLUGS J411 AND J413 REF DRW.
- [SDR SWI2024F01049](https://openairdocs.org/sdr/SWI2024F01049.md): Rib · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH MLG GEAR WELL WS48.30, THE BATT RIB CAP IS CRACKED (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED BATT RIB ANGLE ON LH MLG GEAR WELL AT WS48.30 AS PER REO NO 601R-57-21-3857 REV. -- DATE: 2024-08-27. SEE CONTINUATION CARD FOR DETAILS. AN
- [SDR SWIA20240813](https://openairdocs.org/sdr/SWIA20240813.md): Skin · cracked · Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NLG AFT DOOR FUSELAGE SKIN CUT OUT, THE AFT RH CORNER POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)COMPLIED WITH ALL STEPSF MHIRJ REO 601R-53-11-048 REV-D DATED 2015-06-10 AND REO 601R-53-11-3943 REV -- DATED 2024-09-02 IN THE REP
- [SDR SWI2024F01245](https://openairdocs.org/sdr/SWI2024F01245.md): Intercostal · corroded · Aug 12, 2024 · N906EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD3 CORROSION (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND INSTALLED NEW PAX DOOR MID DD3 IAW CRJ 200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31702 REV. N. NO LEAKS NOTED AT THIS TIME SEE CONTINUATION CARD FOR DETAILS AND
- [SDR SWI2024F01244](https://openairdocs.org/sdr/SWI2024F01244.md): Frame Splice · corroded · Aug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SPLICE FS349 STGR23R HAS CORROSION AND IS BULGING (C-CHECK RO 10/26/2024) (FILED CLOSED) FRAME SPLICE FS 349.00 STGR. 23R HAS MULTIPLE SPOTS OF EXFOLATED CORROSION WITH 100% MATERIAL LOSS AND IS OUT OF LIMITS REF CRJ200 SRM 53-00-00. REMOVED AND INSTALL
- [SDR SWI2024F01243](https://openairdocs.org/sdr/SWI2024F01243.md): Frame · corroded · Aug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS333 STGR26L-STGR22R HAS AREAS OF CORROSION (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND REPLACED FRAME AT FS333 STGR26L-22R REF DRW. 601R32004 REV. N, REF DRW. 601R31022 REV. B, REF CRJ200 SRM 51-42-06 AND REF CRJ200 SRM 51-42-21. COMPLIED WITH

Next page: https://openairdocs.org/aircraft/N906EV/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 = 'N906EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N906EV/reports

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