N925EV

Service difficulty reports · 191

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 = 'N925EV' 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 SWIA2026020275115Striker · damagedFOUND DAMAGE ON AFT UPPER PAX DOOR SEAL STRIKER NEAR DOOR ROLLER. FOUND DENT DAMAGE. (W - 0.650 D- 0.20 W - 0.15) LOCATED ON THE AFT UPPER PAX DOOR SEAL STRIKER NEAR THE DOOR ROLLER. PER REO 601R-53-22-033 REV -D DATED 2014/02/17 PERFORMED TEMP REPAIR TYPE IFeb 2, 2026 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA20260108Controller · malfunctionedWING OVHT MESSAGE ON TAKE OFF. QRH PROCEDURE WAS CONDUCTED & MESSAGE CLEARED. NO FURTHER MESSAGES DURING FLIGHT. (FLIGHT 5125) TROUBLESHOT IAW FIM 30-10-00. INTERROGATED MDC, NO FAULTS OR HISTORY FOUND. PERFORMED GVI OF WIRING GOING TO LT WAI MSOV, LOOKED ATJan 8, 2026 · N925EV · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA202505270024Landing Gear · warning messageGEAR DISAGREE WARNING ALONG WITH ASSOCIATED NOSE DOOR WARNING ON TAKEOFF. BOTH MAINS RETRACTED AND SHOWED UP BUT NOSE GEAR INDICATION SHOWED LINES. QRH RESOLVED ISSUE. RECEIVED 3 GREEN DN INDICATIONS. RTF (FLIGHT 5807 - FILED CLOSED)TROUBLESHOT GEAR DISAGRMay 24, 2025 · N925EV · Cndair CL6002B19 · Central WarningSDR SWIA2025040329Terminal Block · smokeSMOKE IN COCKPIT FROM CP SIDE WINDSHIELD HEAT. QRH RESOLVED ISSUE. (FLIGHT 5025 - FILED CLOSED)TROUBLESHOT COCKPIT SMOKE EVENT PER FIM 21-21-00 AND FOUND WHILE INSPECTING L/H WINDSHIELD WITH HEAT ON, FOUND LIGHT SMOKE COMING OUT BETWEEN L/H WINDSHIELD HEAT POWMar 29, 2025 · N925EV · Cndair CL6002B19 · Ice/Rain Protection System WiringSDR SWI2025F00404Heater · smokeSMOKE IN COCKPIT FROM CP SIDE WINDSHIELD HEAT. QRH RESOLVED ISSUE. (FLIGHT 5025 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSMar 29, 2025 · N925EV · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR SWIA202502140002Wire Harness · damagedON DEPARTURE FROM DENVER RECEIVED A NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGES. MESSAGES CLEARED WITH QRH (FLIGHT 5083 - FILED CLOSED) ARRIVED AT A/C INTERROGATED PSEU AND BASED ON THE INPUT REASONABLENESS TABLE TABLE 103 IN FIM 32-60-05 IT APPEARSFeb 12, 2025 · N925EV · Cndair CL6002B19 · Landing Gear System WiringSDR SWI202408190689Selector Valve · faultedGEAR DISAGREE ON GEAR EXTENSION ON FINAL. RAN QRH AND CYCLED THE GEAR TWICE NORMALLY WITH 30 SECOND DELAY. MESSAGE PERSISTED. QUICK CYCLED GEAR UNDER DIRECTION OF QRH AND THEN GOT THREE GEAR DOWN AND LOCKED. (FLIGHT 5391 - FILED CLOSED) THIS DISCREPANCY Aug 17, 2024 · N925EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2024060500004Warning Message · false activationD:DUE TO FLAPS FAIL CAUTION. FLAPS 0 LANDING, COMPLY WITH FULL FLAP EVAULATION PER AD 2009-06-12/09.C: FLAP FAILCAT A DUE WITHIN 10 CYCLES BY TAC 37720. SMOD APPROVAL REQIRED FOR RTS. FLAPS FAIL CAUTION. FLAPS 0 LANDING. (FLIGHT 4663) RESET AND OPERATED FLJun 4, 2024 · N925EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2024051000312Vane · chafedRH INBD FLAP VANE CHAFED AT WS104.099 (C-CHECK RO 5/9/2024) REPAIRED R/H I/B FLAP VANE L/E SKIN AT W.S. 104.099 IAW CRJ200 SRM 57-52-00 AND 57-52-00 REPAIR #1. NDT PERFORMED BY BARON NDT LLC CRS#: 5NDR545D REPORT#: S032524-1 DATED 25MAR2024. SEE REPORT FORMar 12, 2024 · N925EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA20240510229Skin · damagedLH ELEVATOR SKIN ABOVE HINGE #2 DAMAGED, EVAL (C-CHECK RO 5/9/2024) PERFORMED REPAIR AT L/H ELEVATOR SKIN ABOVE HINGE #2 IAW CRJ 200 REO 601R-55-21-591 REV -- DATE: 2024-03-15,SRM 55-20-00,SRM 51-24-36,SRM 51-12-00,SRM 51-25-06,SRM 51-25-16, PERFORMED NDTFeb 29, 2024 · N925EV · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWI2024F00399Shroud · damagedLE SHROUD LH SIDE H STAB DAMAGED (C-CHECK RO 5/9/2024) REPAIRED LH SIDE HORIZONTAL STABILIZER LEADING EDGE SHROUD BETWEEN FSS31.999 TO FSS67.790 IAW REO 601R-55-11-757 REV -- DATE: 2024-04-25, CRJ 200 AMM 20-22-01, AMM 55-10-00, CRJ 200 SRM 51-42-06, SRM Feb 27, 2024 · N925EV · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA20240510227Shroud · damagedLE SHROUD RH SIDE H STAB DAMAGED (C-CHECK RO 5/9/2024) REPAIRED RH SIDE HORIZONTAL STABILIZER OF THE LEADING EDGE SHROUD BETWEEN FSS 31.999 TO FSS 67.790 IAW MHIRJ REO 601R-55-11-757 REV -- DATE: 2024-04-25 AND IAW CRJ 200 AMM 20-22-01, AMM 55-10-00 AND Feb 27, 2024 · N925EV · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA2024051000030Skin · dentedADM N925EV-8460THERE IS A SCRATCH AND TWO DENTS ON THE UPPER FWD OF DOOR WHEN CLOSED, SCRATCH IS JUST THOUGH PAINT, MEASURING 26.75 IN FROM TOP OF DOOR, AND 4.75 IN FROM FWD EDGE. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIJan 30, 2024 · N925EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2024010200030Unknown · dentedFOUND DENT ON THE LEADING EDGE OF THE FLAP-VANE ON THE LEFT OB FLAP AT APPROX. F/STA 210.50 (FILED CLSOED) FOUND DENT AT LEFT WING O/B FLAP VANE F.S. 210.50 TO BE OUT OF LIMITS PER SRM 57-53-00 FIG 102 SHEET 3. NO DENTS PERMITTED. REF CP 27621022 FOR FURTHER Dec 30, 2023 · N925EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI20240510398Guide · erodedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA69883-601R-57-41-1124 925EV MXCODEID56613-PR - RH WING OUTBOARD LEADING EDGE (630KL) HAS EROSION. COMPLIED WITH TEMPORARY REPAIR PER REO601R-57-41-1124, REV--, DATED 2021-05-04. PERMANENT REPAIR DUE WITHIN 6000 FLT HDec 1, 2023 · N925EV · Cndair CL6002B19 · Wing StructureSDR SWI20240510397Skin · erodedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA69059-601R-57-41-1120 N925EV MXCODEID56580-PR - RH WING CENTER LEADING EDGE PANEL (630JL) HAS EROSION. COMPLIED WITH REO 601R-57-41-1120, REV. --, 2021-04-26 IN ITS ENTIRETY (STEPS 1-5). THIS REPAIR IS VALID FOR 600Dec 1, 2023 · N925EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202405101201Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA69006-601R-57-41-1119 N925EV MXCODEID56249-PR - LH WING CENTER LEADING EDGE PANEL (530JL) HAS EROSION. REMOVED EROSION DAMAGE ON L/H WING CENTER LEADING EDGE PANEL 530JL REF CRJ 200 SRM 51-12-00. COMPLIED WITH REO 60Dec 1, 2023 · N925EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202158214Support Angle · corrodedLH FWD AVIONICS BAY DOOR SEAL RETAINER SUPPORT ANGLE HAS CORROSION. (C-CHECK RO 5/16/2021) VALUATE LH FWD AVIONICS BAY DOOR SEAL RETAINER SUPPORT ANGLE CORRECTIVE ACTION: LH FWD ANGLE IS 100% EXFOLIATED, FOUND TO BE OUT OF LIMITS. REF CRJ 200 SRM 52-00Apr 21, 2021 · N925EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202158190Cup · damagedPAX DOOR UNDER FLOOR AFT HAND RAIL CUP REQUIRES REPLACEMENT. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED THE PAX DOOR AFT HANDRAIL CUP ASSY WITH 1EA. NEW PART REF. CRJ200 SRM 51-42-06 , CRJ200 SRM 51-42-13, & BOMBARDIER DWG 601R31527 REV W. COMPLIED WITApr 19, 2021 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202158189Bulkhead Web · crackedFS.621 PRESS BULKHEAD LWR WEB AFT STIFFENER LOCATED OUTBD OF LBL36 ABOVE FLOOR AT WL80 FOUND CRACKED . (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED REPLACEMENT FS.621 PRESS. BULKHEAD WEB AFT SIDE STIFFENER P/N 601R36008-51 AT WL.79 OUTBD OF LBL36 PER Apr 16, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202158188Angle · crackedFS 280 RBL 9, INBOARD VERTICAL ANGLE APPEARS CRACKED AT TOP END. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED VERTICAL ANGLE UNDER FLOOR LEVEL AT FS.280 RBL.9 (INBD) REF REO 601R-53-11-171 REV.-D DATED 13 FEB 07 AND CRJ 200 SRM 51-42-21 AND COMPLIED WITHApr 13, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158187Angle · crackedFS 280 LBL 9, INBOARD VERTICAL ANGLE APPEARS CRACKED AT TOP END. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED VERTICAL ANGLE UNDER FLOOR LEVEL AT FS.280 LBL.9 (INBD) REF REO 601R-53-11-171 REV.-D DATED 13 FEB 07 AND CRJ 200 SRM 51-42-21 COMPLIED WITH 51-Apr 13, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158186Frame · cracked*FS333 FRAME CRACKED BETWEEN STR1L AND STR2L (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED FRAME SECTOR 601R32004-41 REF. CRJ 200 SRM 51-42-06, CRJ-200-SRM 51-42-21. DRAWING 601R31522 REV AC AND DRAWING 601R31016 REV D. COMPILED WITH 51-900-1003-SKY ANDApr 9, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202158185Skin · chafed* THE CENTER WING LOWER PLANK IS CHAFED AT 2 LOCATIONS ALONG ITS AFT END, JUST INBOARD OF LBL 45 AND JUST INBOARD OF RBL 45, BOTH LOCATIONS ARE BELOW THE AFT SPAR. (C-CHECK RO 5/16/2021) REPAIRED THE CENTER WING LOWER PLANK CHAFE AT 2 LOCATIONS ALONG IApr 5, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202158210Hinge · gouged*RIGHT WING, AILERON HINGE FITTING #3 (CENTER OTBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #3 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14Apr 3, 2021 · N925EV · Cndair CL6002B19 · AileronsSDR SWIA202158209Hinge · gouged*RIGHT WING, AILERON HINGE FITTING #2 (CENTER INBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #2 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14Apr 3, 2021 · N925EV · Cndair CL6002B19 · AileronsSDR SWIA202158208Hinge · corroded*RIGHT WING, AILERON HINGE FITTING #1 (MOST INBD), HAS GOUGING (MARKED) (C-CHECK RO 5/16/2021) REMOVED GOUGE ON *RIGHT WING, AILERON HINGE FITTING #1 (CENTER OTBD) REF CRJ-200-SRM 51-12-00. BLENDED AREA FOR TO BE OUT OF LIMITS REF CRJ-200-SRM 57-51-14. Apr 3, 2021 · N925EV · Cndair CL6002B19 · AileronsSDR SWIA202158207Seat Track · corroded* CORROSION IN MULTIPLE SPOTS ON RBL9.00 FLOOR SEAT TRACK BETWEEN FS364.00 & FS394.00 (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW SEAT TRACK WITH RTV 157 ON FAYING SURFACE BETWEEN FS364 TO FS399 REF CRJ 200 AMM 53-01-11-400-802Apr 2, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158206Seat Track · corroded* CORROSION IN MULTIPLE SPOTS ON LBL9.00 FLOOR SEAT TRACK BETWEEN FS364.00 & FS394.00 (C-CHECK RO 5/16/2021) REMOVED DISCREPANT SEAT TRACK REF CRJ 200 SRM 51-41-02, FABRICATED AND INSTALLED NEW LBL 9 SEAT TRACK BETWEEN FS364.00 & FS394.00 , REF REO 601Apr 2, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158184Frame · corroded* CORROSION ON FRAME 409+16 FORWARD SIDE AND ATTACH FLANGE BETWEEN STR26R AND STR26L. (C-CHECK RO 5/16/2021) REPAIRED FRAME 409+16 FORWARD SIDE AND ATTACH FLANGE BETWEEN STR25R AND STR25L REF CRJ-200-SRM 53-00-15. PREESURE CHECK GOOD AND COMPLIED WITH Apr 2, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202158205Web · corroded* PASSENGER DOOR AFT WEB NEAR PULLEY BRACKET FOR SUPPORT WHEEL CABLE HAS CORROSION (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND REPLACED WITH NEW PAX DOOR AFT WEB REF CRJ 200 SRM 51-42-06 SEE CONTINUE CARD FO DETAILSApr 1, 2021 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202158204Angle · corroded* PASSENGER DOOR ANGLE ATTACHED TO INNER SKIN FOR PANEL 832AT HAS CORROSION (MARKED). (C-CHECK RO 5/16/2021) REMOVED AND REPLACED PAX DOOR ANGLE ATTACHED TO INNER SKIN FOR PANEL 832AT REF. CRJ200 SRM 51-42-13.Apr 1, 2021 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202158183Floorbeam · corroded* CORROSION ON FS280.00 BEAM BETWEEN RBL9.00 & LBL9.00 (MARKED WITH ORANGE STREAMER) (C-CHECK RO 5/16/2021) REMOVED CORROSION ON FS280 BEAM BETWEEN RBL9 & LBL9, REF CRJ 200 SRM 51-21-06, FWD ANGLE IS OUT OF LIMITS PER REF CRJ 200 SRM 53-00-00, AFT ANGLEApr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202158182Floorbeam · corroded* CORROSION ON FLOOR SUPPORT ANGLE AT FS621 OUTBOARD OF LBL27. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT FS621 OUTBOARD OF LBL27 REF REO 601R-53-61-117 REV -E DATED 2018-01-15, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESApr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202158181Tie Down · corroded* CORROSION ON PLATES FOR CARGO NET TIE DOWNS BETWEEN FS574 AND FS621. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FWD, MID, AND AFT TIE DOWN PLATES FLOOR SUPPORTS. IAW CRJ200 SRM 51-42-06, 51-45-00, AND BOMBARDIER INC. CANADAIR ENGINEER DWG NO. 601R3Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158180Frame · cracked* FS605 FRAME LOWER FLANGE CRACKED AT STR24L. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW LOWER FRAME SECTOR, 4(EA) SPLICES AND 2(EA) SUPPORT CLIPS OF FS605 REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG601R36026 REV.AF. COMPLIED WITH 51-9Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202158179Cargo Track · cracked* BRACKET ON BOTTOM OF CARGO TRACK SUPPORT AT FS621 CRACKED. (C-CHECK RO 5/16/2021) REMOVED AND REPLACED 1EA. NEW SUPPORT BRACKET FOR CARGO DOOR TRACK, LOCATED AT BOTTOM OF DOOR SUPPORT TRACK AT FS621 REF. BOMBARDIER DWG#601R35050 REV Y. & SRM 51-42-Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158178Floor Support · corroded* LH PRESSURE FLOOR SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REPAIRED LH PRESSURE FLOOR SILL REF REO 601R-53-41-2901 REV-- DATED 2021-04-16 AND REO 601R-53-41-666 REV C DATED 2012-11-06. PRESSURE CHECK GOOD AND COMPLIED WITH 51Apr 1, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158203Hinge · corrodedRH SPOILERON INBD AND OTBD HINGE POINT COVER PLATE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED INBD AND OTBD HINGE POINT COVER PLATE HARDWARE REF CRJ 200 AMM 27-64-01-400-801Mar 31, 2021 · N925EV · Cndair CL6002B19 · SpoilersSDR SWIA202158202Hinge · corrodedRH FLIGHT SPOILER INBD AND MIDDLE HINGE POINT HARDWARE AND INBD COVER PLATE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED FLIGHT SPOILER INBD AND MIDDLE HINGE POINT HARDWARE & INBD COVER PLATE HARDWARE REF CRJ200 AMM 27-64-05-400-801Mar 31, 2021 · N925EV · Cndair CL6002B19 · SpoilersSDR SWIA202158201Attach Fitting · corrodedRH OTBD GROUND SPOILER INBD, MIDDLE, OTBD AND PCU CONNECT HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACE CORRODED HARDWARE WITH NEW HARDWARE ON RH OTBD GROUND SPOILER AT INBD, MIDDLE, OTBD, AND PCU ATTATCHING POINTS. REF CRJ 200 AMM 27-65-Mar 31, 2021 · N925EV · Cndair CL6002B19 · SpoilersSDR SWIA202158200Hinge · corrodedRH INBD GROUND SPOILER OTBD HINGE HARDWARE CORRODED (C-CHECK RO 5/16/2021) REMOVED AND REPLACED HARDWARE ON RH INBD GROUND SPOILER OTBD HINGE REF CRJ 200 AMM 27-65-01-000-801Mar 31, 2021 · N925EV · Cndair CL6002B19 · SpoilersSDR SWIA202158177Seat Track · corrodedCORROSION ON THE SEAT RAIL SUPPORT BEAM FS424 TO FS513 RBL9.0 / 783161$M255 (C-CHECK RO 5/16/2021) REPAIRED SEAT RAIL PER MHIRJ REO 601R-53-41-2907, REV -- , DATED 2021-05-07 AND COMPLIED WITH ALL STEPS OF THE REO. SEE CONTIUATION CARD FOR FURTHER DETAIMar 31, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158176Seat Track · corrodedCORROSION ON THE SEAT RAIL SUPPORT BEAM FS409+118 TO FS559-10 LBL9.0 (C-CHECK RO 5/16/2021) / REMOVED CORROSION ON THE SEAT RAIL SUPPORT BEAM FROM FS409+118 TO FS559+10 LBL9, & FOUND TO BE OUT OF LIMITS PER REF REO 601R-53-00-005, REV -B, DATE 2011-01-Mar 31, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158175Skin · damagedWHILE COMPLYING WITH SB 601R-57-046 REV C ( PART A) LHS 1EA O/S FASTENER FOUND INSTALLED IN HOLE #14. FASTENER TYPE IS (HST411-10, HOLE DIA. IS .340". (C-CHECK RO 5/16/2021) REPAIRED L/H SIDE 1 EA OVERSIZE FASTENER HOLE IN WING PLANK ASSY ( STEEL STRAMar 31, 2021 · N925EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202158174Floor Support · corroded* RH PRESSURE FLOOR SILL ANGLE CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REMOVED CORROSION FROM R/H PRESSURE FLOOR SILL ANGLE AT MULTIPLE LOCATIONS REF REO 601R-53-41-666, REV -C, 2012-11-06 AND REO 601R-53-41-2902 REV-- DATED: 2021-04Mar 31, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158173Floor Support · corroded* RH PRESSURE FLOOR SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 5/16/2021) REPAIRED RH PRESSURE FLOOR SILL REF REO 601R-53-41-2902 REV-- DATED: 2021-04-16 AND REO 601R-53-41-666 REV. €“C DATE 2012-11-06. . PRESSURE CHECK GOOD AND COMPLIED WIMar 31, 2021 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158199Seat Track · corroded* THE CABIN FLOOR SEAT RAIL/TRACK ON RBL 9.0 BETWEEN FS 409+128 AND FS 559 HAS MULTIPLE SPOTS OF CORROSION, SCRATCHES AND NICKS. (C-CHECK RO 5/16/2021) REMOVED THE CORROSION AND OTHER DAMAGE FROM THE SEAT TRACK, FS409+126 TO FS559+4 RBL9.0 PART # 601R3Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158198Seat Track · corroded* THE CABIN FLOOR SEAT RAIL/TRACK ON LBL 9.0 BETWEEN FS 409+128 AND FS 559 HAS MULTIPLE SPOTS OF CORROSION, SCRATCHES AND NICKS. (C-CHECK RO 5/16/2021) REMOVED THE CORROSION AND OTHER DAMAGE FROM THE SEAT TRACK, FS409+126 TO FS559+4 LBL9.0 PART # 601R31Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158197Floorbeam · corroded* THE LBL 9.0 FLOOR BEAM ATTACHMENT TO THE FS 621 BULKHEAD'S SEAT TRACK HAS CORROSION AROUND ITS SCREW HOLES. (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED NEW CARGO TIE-DOWN TRACK AT LBL9 APPROX. FS621 REF CRJ200 AMM 53-00-49-000-801 & 53-00-49-400-80Mar 30, 2021 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
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