N906EV

Service difficulty reports · 293

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2026031975560Retainer · gougedCARGO 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.Mar 19, 2026 · N906EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2026031975559Track · crackedCARGO 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.Mar 19, 2026 · N906EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2026031975558Bracket · crackedCARGO 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.Mar 19, 2026 · N906EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2026031975557Track · damagedAFT 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 Mar 19, 2026 · N906EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2026031875556Bracket · crackedTRANSFER 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 Mar 18, 2026 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2025061305Windshield · crackedIN 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 WITHJun 5, 2025 · N906EV · Cndair CL6002B19 · Flight Compartment WindowsSDR SWI2025F00713Windshield · crackedIN 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 PROGRESSJun 5, 2025 · N906EV · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA20250102Indicator · unreliableFLIGHT 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. (Jan 2, 2025 · N906EV · Cndair CL6002B19 · Airspeed/Mach IndicatorSDR SWIA20240830Splice · corrodedUNION 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 OAug 30, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024111508024Door Frame · chafedTHE 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 CONTINUATIOAug 24, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024102824Stop Fitting · chafedTHE 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 Aug 24, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20241115823Spar · gougedRH 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 LOWEAug 23, 2024 · N906EV · Cndair CL6002B19 · Wing SparSDR SWIA202411150023Spar · gougedLH 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 FURTHERAug 23, 2024 · N906EV · Cndair CL6002B19 · Wing SparSDR SWI2024F01065Hinge Fitting · gougedRH 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 #3Aug 23, 2024 · N906EV · Cndair CL6002B19 · AileronsSDR SWI2024F01064Hinge Fitting · gougedRH 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 Aug 23, 2024 · N906EV · Cndair CL6002B19 · AileronsSDR SWI2024F01063Hinge Fitting · gougedLH 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 DAug 23, 2024 · N906EV · Cndair CL6002B19 · AileronsSDR SWIA2024102823Hinge Fitting · gougedLH 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 COMPAug 23, 2024 · N906EV · Cndair CL6002B19 · AileronsSDR SWIA20241115822Hinge Fitting · wornUPON 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 600Aug 22, 2024 · N906EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2024102822Hinge Fitting · wornUPON 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 600-2Aug 22, 2024 · N906EV · Cndair CL6002B19 · Elevator StructureSDR SWI2024F01262Hinge Fitting · wornDURING 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 600-24043Aug 21, 2024 · N906EV · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR SWI2024F01261Striker · damagedSERVICE 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 WAug 21, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024111510821Gusset · gougedSERVICE 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.Aug 21, 2024 · N906EV · Cndair CL6002B19 · Service DoorsSDR SWI2024F01062Hinge Fitting · wornDURING 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 600-24043-1Aug 21, 2024 · N906EV · Cndair CL6002B19 · Elevator StructureSDR SWI2024F01061Striker · damagedSERVICE 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 WITAug 21, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024102821Gusset · gougedSERVICE 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.Aug 21, 2024 · N906EV · Cndair CL6002B19 · Service DoorsSDR SWIA20240818Angle · crackedCRACKED 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.Aug 18, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01263Window Post · crackedRH 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, 56-220Aug 15, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024111510815Window Post · crackedWINDSHIELD 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-3Aug 15, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F01060Window Post · crackedRH 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, 56-220-1Aug 15, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024102815Window Post · crackedWINDSHIELD 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 Aug 15, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202411150813Skin · crackedNLG 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 RAug 13, 2024 · N906EV · Cndair CL6002B19 · Landing Gear DoorsSDR SWI2024F01270Skin · chafedLH 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: 201Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2024F01269Attach Angle · crackedLH 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 DRAug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWI2024F01268Rib · crackedLH 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. Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWI2024F01266Frame · crackedFRAME, 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 51-42-0Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F01265Hinge · gougedPASSENGER 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 PAug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Door HingeSDR SWI2024F01264Rib · crackedRH 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 Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWI2024F01057Hinge · damagedPASSENGER 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 Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Door HingeSDR SWI2024F01056Frame · crackedFRAME, 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 Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F01055Hinge · gougedPASSENGER 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 PAXAug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage, Door HingeSDR SWI2024F01054Spar · chafedLH 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/Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F01053Rib · crackedRH 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 Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01052Rib · crackedRH 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 ANAug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01051Rib · crackedLH 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 -Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01050Rib · crackedLH 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.Aug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01049Rib · crackedLH 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. ANAug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20240813Skin · crackedNLG 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 REPAug 13, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2024F01245Intercostal · corrodedPASSENGER 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 ANDAug 12, 2024 · N906EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2024F01244Frame Splice · corrodedFRAME 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 INSTALLAug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F01243Frame · corrodedFRAME 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 WITHAug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Frame
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