N905EV

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 = 'N905EV' 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 SWIA2026071877602Seat Track · corrodedLBL 27 SEAT RAIL SCRATCHED AND CORRODED. INSTALLED A NEW SEAT RAIL IAW AMM 53-01-11-400-802.Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071877601Seat Track · corrodedLBL 9 SEAT RAIL SCRATCHED AND CORRODED. REMOVED AND REPLACED THE SEAT RAIL IAW AMM 53-01-11-400-802.Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071877600Seat Track · corrodedSEAT RAIL SCRATCHED AND CORRODED . INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11-400-802,Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071877599Seat Track · corrodedRBL9 SEAT RAIL SCRATCHED AND CORRODED . REMOVED AND INSTALLED NEW SEAT RAIL, IAW AMM 53-01-11-400-802.Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071877598Seat Track · scratchedRBL9 SEAT RAIL SCRATCHED AND CORRODED . INSTALLED NEW RBL9 SEAT RAIL IAW AMM 53-01-11-400-802Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071877597Seat Track · scratchedRBL27 SEAT RAIL SCRATCHED AND CORRODED . INSTALLED NEW SEAT RAIL AT RBL27 IAW AMM 53-01-11-400-802.Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026071877596Seat Track · scratchedRBL27 SEAT RAIL SCRATCHED AND CORRODED BETWEEN APPROXIMATELY FS559.078 TO 559. 093 REPLACED RBL 27 SEAT TRACK IAW AMM 53-01-11-400-802.Jul 18, 2026 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA20250502001Warning Message · illuminatedDURING CLIMB THROUGH 3500 FEET RECEIVED A STAB TRIM RUNAWAY NOSE DOWN. RAN MEMORY ITEMS, QRC, QRH. RETURNED TO ORD. (FLIGHT 5852 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30068339 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 30070396 May 1, 2025 · N905EV · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA2025041500014Landing Gear · warning messageWHEN BRINGING THE GEAR DOWN RECEIVED A GEAR DISAGREE WARNING MESSAGE. NO GREEN LIGHT FOR THE GEAR. RAN QRH PROCEDURE AND GOT THE GEAR DOWN AND LOCKED. THREE GREEN LIGHT. MEL 32-30-1CAT A DUE TAC 40385 ODI SMOD APPROVAL FOR RTS CAT II DOWNGRADED (FLIGHT 5040Apr 14, 2025 · N905EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2023050100020Unknown · crackedRIGHT M/L/G WHEEL WELL. BRAKE PRESSURE TRANSDUCER BRACKET CRACKED. (C-CHECK RO 4/26/2023) REMOVED CRACKED AND INSTALLED NEW BRAKE PRESSURE TRANSDUCER MOUNT BRACKET IN RH MLG WHEEL WELL - REF REO 601R-53-42-007, REV A, DATE 31-JAN-2006. OPERATIONAL AND Apr 20, 2023 · N905EV · Cndair CL6002B19 · Landing Gear SystemSDR SWIA2023050100019Unknown · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON RH FLOOR SILL FS473.15.00 TO FS499.00 (AREA MARKED) (C-CHECK RO 4/26/2023) REMOVED CORROSION ON RH FLOOR SILL BETWEEN FS473.15.00 TO FS499.00 REF CRJ200 SRM 51-21-06FOUND TO BE WITHIN LIMITS/RESTORED FINISH REF REO 6Apr 4, 2023 · N905EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA2023050100018Unknown · dentedCREASED/DENT DAMAGE FOUND ON UPPER FUSELAGE SKIN 3.5" AFT OF 31.875% BETWEEN STR 4R-5R (C-CHECK RO 4/26/2023) COMPLIED WITH REPAIR ON UPPER FUSELAGE SKIN 3.5" AFT OF 31.875% BET. STR 4R-5R REF REO 601R-53-71-222 REV A DATED 2023-04-08, COMPLIED WITH SMar 30, 2023 · N905EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2023050100017Unknown · crackedRH FLOOR BEAM FS484.00 RBL 27 CLIP IS CRACKED (INBD CLIP) (C-CHECK RO 4/26/2023) REMOVED AND REPLACED FLOOR BEAM CLIP AT FS 484.0, RBL 27. REF. REO 601R-53-41-059 REV. -C DATED 2020-03-11. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRMar 28, 2023 · N905EV · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2023050100016Unknown · crackedLEFT SIDE. FLOOR BEAM OUTBOARD CLIP AT FS 484.0 IS CRACKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED LEFT SIDE FLOOR BEAM OUTBOARD CLIP AT FS484.0. REF. REO 601R-53-41-059 REV. -C DATED 2020-03-11.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL60Mar 28, 2023 · N905EV · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2023050100014Unknown · unknownUPON REMOVAL ON THE RIGHT STAB TIP FOUND HOLE THE FLANGE UPPER SIDE WHERE THE NUTPLATE WAS. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW SPLICE P/N 600-23037-22. REF: DWG 600-23037, REV: L, DWG 600-23026, REV: T, CRJ200 SRM 51-42-06, CRJ200 SRM 51-Mar 27, 2023 · N905EV · Cndair CL6002B19 · Fuselage, Stabilizer Attach FittingsSDR SWIA2023050100013Unknown · gougedEXISTING DOUBLER AT AFT SIDE FS.280 BULKHEAD RBL12 WL93.50 IS GOUGED AND DENTED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED DOUBLER AT AFT SIDE FS.280 BULKHEAD RBL12 WL93.50 WITH NEW REF. CRJ 200 SRM 51-42-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1Mar 23, 2023 · N905EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2023050100012Unknown · puncturedFS.280 BULKHEAD HAS A PUNCTURE AT RBL14 WL87.50. (C-CHECK RO 4/26/2023) PERFORMED DOUBLER REPAIR AT FS280 BULKHEAD AT RBL14 WL87.50 REF REO 601R-53-11-3850 REV-- DATED 2023-04-03. COMPLIED WITH TASK 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS ON WORKMar 23, 2023 · N905EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2023050100011Unknown · corroded* FUEL CELL ACCESS PANEL LANDING AT 540BB HAS CORROSION 2 PLCS, MARKED. (C-CHECK RO 4/26/2023) REMOVED CORROSION ON FUEL CELL ACCESS PANEL LANDING AT 540BB REF CRJ 200 SRM 51-21-06. FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-57-21-Mar 23, 2023 · N905EV · Cndair CL6002B19 · Fuel StorageSDR SWIA2023050100010Unknown · corrodedFUSELAGE DOOR SURROUND ANGLE IS CORRODED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED FUSELAGE PAX DOOR ANGLE REF CRJ 200 SRM 51-42-06, SRM 51-42-13, SRM 51-42-21 AND DWG 601R31527 REV AM. REMOVED AND INSTALLED FWD AND NEW AFT HANDRAIL FITTING IAW CRJ 2Mar 22, 2023 · N905EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202305010009Unknown · corrodedPASSENGER DOOR. FWD DOOR STAIRS HANDLE ARM CUT-OUT CORRODED ON THE FLOOR SUPPORT ANGLE. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW PAX FWD CUT STAIR HANDLE ARM CUT OUT IAW CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV. AM. COMPLIED WITH SKYWEST TASKMar 22, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA2023050100024Unknown · corrodedR/H SIDE SEAT RAIL FROM APPROXIMATELY FS449.85 TO FS499.00 HAS NUMEROUS SPOTS OF CORROSION AND CHAFING, MARKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED R/H SIDE SEAT RAIL FROM APPROXIMATELY FS449.85 TO FS499.00. REF. CRJ200 AMM 53-01-11-400-802Mar 20, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA2023050100008Unknown · corrodedPASSENGER DOOR. AFT DOOR STAIRS HANDLE ARM CUT-OUT CORRODED ON THE FLOOR SUPPORT ANGLE. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW AFT DOOR STAIR CUP IAW CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV. AM. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-Mar 20, 2023 · N905EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA2023050100023Unknown · corrodedR/H SIDE SEAT RAIL FROM FS409.00+16 TO FS409+112 HAS NUMEROUS SPOTS OF CORROSION AND CHAFING, MARKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED R/H SIDE SEAT RAIL FROM FS409.00+16 TO FS409+112. REF. CRJ200 AMM 53-01-11-400-802Mar 19, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA2023050100007Unknown · corrodedRIGHT HAND FLOOR SUPPORT BEAM CAP RBL9R, HAS NUMEROUS SPOTS OF CORROSIION AND WEAR, FROM FS409.0 TO FS409.0+112. (CORROSION SPOTS MARKED WITHIN RED GREASE PENCIL). (C-CHECK RO 4/26/2023) BLENDED OUT CORROSION ON RBL 9 FLOOR BEAM CAP FROM FS 409 TO 409+1Mar 18, 2023 · N905EV · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2023050100006Unknown · corrodedR/H PRESSURE FLOOR SILL. ONE (1) SPOT OF CORRORION AT FS518.0 (C-CHECK RO 4/26/2023) REMOVED CORROSION FROM RH PRESSURE FLOOR SILL AT FS518.00 REF. CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR IAW ALL STEPS OF REO 601R-53-41-3143 REMar 17, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA2023050131301Unknown · chafed*R/H WING INBOARD FLAP VANE SKIN LEADING EDGE IS CHAFED AT THE INBOARD. (C-CHECK RO 4/26/2023) REMOVED DAMAGED RH IB FLAP VANE INBOARD LEADING EDGE SKIN AND INSTALLED A NEW VANE SKIN 601R14303-54 REF CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. COMMar 13, 2023 · N905EV · Cndair CL6002B19 · Wing StructureSDR SWIA2023050100003Unknown · gouged*CARGO DOOR INTERIOR SURROUND AFT TRACK ASSY GOUGED/WORN OUTBOARD TRACK UPPER AND INBOARD TRACK UPPER SIDE (MARKED) (C-CHECK RO 4/26/2023) REMOVED DAMAGED AND INSTALLED NEW AFT CARGO DOOR AFT TRACK IAW CRJ200 SRM 51-42-06 REV. 39 ISSUED 03/10/21, SRM 5Mar 13, 2023 · N905EV · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2023050100002Unknown · dented*DENTS IN BOTTOM DOUBLER BELOW AND AFT OF GROUND AIR CONDITIONING CONNECTION PNL 172BR (MARKED) (C-CHECK RO 4/26/2023) REPAIRED DAMAGED AREA COMMON TO LOWER FUSELAGE SKIN APPROXIMATELY BETWEEN FS574 & FS621 AND STRG26L TO STRG20R IAW REO 601R-53-61-799Mar 13, 2023 · N905EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA2023050100311Unknown · chafed* L/H AILERON UPPER LEADING EDGE SKIN IS CHAFED, MARKED. (C-CHECK RO 4/26/2023) BLENDED DAMAGE ON LH AILERON UPPER LEADING EDGE REF REO 601R-57-60-013, REV -A, DATED 2013-08-05.FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW LH AILERON UPPER LMar 11, 2023 · N905EV · Cndair CL6002B19 · Wing StructureSDR SWIA2021112262663Transmitter · failedUNCOMMANDED FLAP EXTENSION IN FLIGHT WITH ASSOCIATED FLAPS DEGRADED STATUS MESSAGE. FLAPS EVENTUALLY STOWED AT 0 DEGREES OF EXTENSION. COMPLIED WITH FLAP TWIST QRH PROCEDURE. PERIODIC HYD 2B AND HYB 3B CAUTION MESSAGES. MESSAGES CLEARED WITH QRH PROCEDURE. (FNov 19, 2021 · N905EV · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA2020031049246Bracket · brokenSERVICE DOOR AFT SURROUND PANEL 232EZ LOWER BRACKET IS BROKEN WHERE MARKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED AFT LOWER BRACKET COMMON TO SERVICE DOOR SURROUND PANEL 232EZ AND FS349 FRAME, PN 601R40170-25 PO 7632-00009/155, REFERENCE CRJ200 SRM.Mar 3, 2020 · N905EV · Cndair CL6002B19 · Service DoorsSDR SWIA2020031049185Mount Bracket · crackedRH STUB FAIRING FWD MOUNTING BRACKET CRACKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED WITH NEW RH STUB FAIRING FWD MOUNTING BRACKET REF CRJ200 SRM.Feb 21, 2020 · N905EV · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA2020031049165Floorbeam · damagedBEAM CAP AT LBL9 FS409.00+96 TO 409.00+112 FOUND TO BE OUT OF LIMITS ON CAMP # 20320140. PERFORM A SPLICE REPAIR. (C CHECK) RO 3/7/2020 PERFORMED FLOOR BEAM CAP SPLICE REPAIR FROM FS409.00+96 TO 409.00+112 LBL9 . REF CRJ-200 SRM REPAIR NO. 2 AND BOMBARDIERFeb 20, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020031049163Floorbeam · damagedBEAM CAP AT LBL9 FS409.00 TO 409.00+48 FOUND TO BE OUT OF LIMITS ON CAMP # 20320140. PERFORM A SPLICE REPAIR. (C CHECK) RO 3/7/2020 PERFORMED FLOOR BEAM CAP SPLICE REPAIR FROM FS409.00 TO 409.00+48 LBL9. REF CRJ-200 SRM, REPAIR NO. 2 AND BOMBARDIER REO. COFeb 20, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020031049230Plate · corrodedPAX DOOR AFT ANCHOR FITTING SERRATED PLATE, AIRCRAFT SIDE THAT ATTACHES TO FS349 FRAME, CORRODED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED WITH NEW PAX DOOR AFT ANCHOR FITTING SERRATED PLATE, AIRCRAFT SIDE THAT ATTACHES TO FS349 FRAME, PN 600-38061-6, REFeb 18, 2020 · N905EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020031049161Angle · crackedF.S. 280, RBL 9 O/B ANGLE CRACKED IN RADIUS AT TOP OF ANGLE. (C CHECK) RO 3/7/2020 REMOVED CRACKED ANGLE AT FS 280.0 RBL 9.0 O/B SIDE AND INSTALLED NEW ANGLE,REF BOMBARDIER REO.Feb 14, 2020 · N905EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031049159Angle · crackedF.S. 280, LBL 9 O/B ANGLE CRACKED IN RADIUS AT TOP OF ANGLE. (C CHECK) RO 3/7/2020 REMOVED CRACKED ANGLE FROM FS 280.0 LBL 9.0 AND INSTALLED NEW ANGLE,REF BOMBARDIER REO.Feb 12, 2020 · N905EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031049158Skin · gouged*RUDDER HAS GOUGE ON LH SKIN BETWEEN LOWER AND MIDDLE HINGE. ( MARKED ) (C CHECK) RO 3/7/2020 CUT AWAY DAMAGE ON RUDDER LH SKIN AND INSTALLED REPAIR TO LHS RUDDER SKIN BETWEEN R.S. 85.07 AND R.S. 90.32 IN REF REO. COMPLIED WITH SKYWEST TASK CARD. SEE CONTIFeb 12, 2020 · N905EV · Cndair CL6002B19 · Rudder, Plate/SkinSDR SWIA2020031049241Skin Panel · brokenWHILE INSPECTING PANEL 326BL FOR DISBONDED TEFLON STIPS FOR JOB 2763291 OP 82 MX TRANS. 20282016 FOUND PANEL TO BE UNSERVICABLE DUE TO BROKEN OFF SECTION OF PANEL (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PANEL 326BL OUTER SKIN P/N:600-21134-45 REF. SRM.Feb 6, 2020 · N905EV · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR SWIA2020031049176Skin · crackedCOMPLY WITH SB 601R-57-037 REV E DATED 3/5/2009 ( WINGS - LOWER WING PLANK - MODIFICATION OF THE LEFT AND RIGHT WINGS IN AREA OF THE REAR SPAR AT WS148.019 ) PART'S A AND B (C CHECK) RO 3/7/2020 SERVICE BULLETIN, WINGS --- LOWER WING PLANK --- MODIFICATIONFeb 6, 2020 · N905EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020031049184Window · crackedR/H WINDOW #4 (4CD) IS CRACKED AND CHIPPED ON THE OUTER WINDOW PANE, FWD LEADING EDGE. REQUIRES REPLACEMENT (C CHECK) RO 3/7/2020 REMOVED AND REPLACED THE PASSENGER WINDOW #4 @ (4CD). REF CRJ200 AMM. PRESSURE CHECKS GOOD.Feb 4, 2020 · N905EV · Cndair CL6002B19 · Passenger Compartment WindowsSDR SWIA2020031049248Bracket · crackedCONNECTING BRACKET/BRIDGE FOR CANOE PANEL 697AB IS CRACKED. (C CHECK) RO 3/7/2020 INSTALLED NEW CONNECTING BRACKET TO CANOE PANEL # 697AB AS REQUIRED PER REF: CRJ200 SRM.Feb 3, 2020 · N905EV · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2020031049153Seat Track · corrodedSEAT TRACK AT LBL9.00 FROM FS409.00 TO FS409.00+112HAS MULTIPLE LOCATIONS OF PITTED CORROSION (C CHECK) RO 3/7/2020 BLENDED OUT CORROSION ON SEAT TRACK LBL9.0 AT FS409.00 TO FS409.00+112. REF. CRJ200 SRM. EVALUATED BLEND AS OUT-OF-LIMITS. REMOVED SEAT TRACJan 24, 2020 · N905EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020031049228Frame · corroded*FRAME 513.00 HAS HEAVY CORROSION PITTING FROM APPROXIMATELY STGR 4RH €“ STGR 7RH (MARKED) (C CHECK) RO 3/7/2020 BLENDED OUT CRROSION ON FS 513 FRAME RH AT STRINGER 4R TO 7R AND FOUND ACCEPTABLE TO ENGINEERING REF REO.Jan 23, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020031049150Stringer · corroded*BETWEEN FS333.00 AND FS349.00 / STGR. 27 REPAIR IS CORRODED. FLAGGED (C CHECK) RO 3/7/2020 NO ALLOWABLE DAMAGE ALLOWED ON REPAIR PARTS FS333.00 AND FS349.00 / STGR. 27 REPAIR REF CRJ200 SRM. REMOVED BAD REPAIR PARTS FS333.00 AND FS349.00 / STGR. 27 REF CRJan 23, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020031049148Stringer · cracked*FWD CABIN - APPROX. FS. 333.00 RIGHT HAND STGR 1 THE FRAME IS CRACKED (MARKED) (C CHECK) RO 3/7/2020 REMOVED FS 333.00 FRAME TO FOM REF CRJ200 SRM. INSTALLED NEW FS 333.0 FRAME REF CRJ200 SRM AND DRW. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAJan 23, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020031049245Guide · broken*ALL 4 OF THE AVIONICS BAY DOOR GUIDES ON THE SURROUND (2EA FWD AND 2EA AFT) ARE BROKEN (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED ALL FOUR (2EA. FWD AND 2EA. AFT) NEW AVIONICS BAY DOOR GUIDES REF BOMBARDIER CRJ-200 CMM. SEE CONTINUATION CARD FOJan 22, 2020 · N905EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020031049225Damper · corroded*RH ELEV CENTER HINGE INBD FLUTTER DAMPER CORRODED HARDWARE AT ELEV ATTACH POINT (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED RH ELEVATOR INBD AND OTBD FLUTTER DAMPER CORRODED HARDWARE REF. CRJ-200 AMM. PERFORMED OPERATIONAL TEST OF THE ELEVATOR COJan 22, 2020 · N905EV · Cndair CL6002B19 · Elevator Control SystemSDR SWIA2020031049146Cleat · cracked*FWD CABIN - FS. 280 BULKHEAD LEFT HAND STGR 3 - STRINGER TO FRAME CLEAT HAS SIGNS OF A CRACK (MARKED). (C CHECK) RO 3/7/2020 REMOVED AND REPLACED CRACKED CLEAT AT FS. 280 BULKHEAD LEFT HAND STGR 3 WITH NEW REF. CRJ 200 SRM AND BOMBARDIER DWG.Jan 22, 2020 · N905EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020031049144Attach Fitting · crackedWINDSHIELD CENTER POST LOWER LH & RH ATTACH FITTINGS CRACKED IN RADIUS. MARKED IN RED. (C CHECK) RO 3/7/2020 REMOVED CRACKED ATTACH FITTINGS AND INSTALLED NEW ATTACH FITTINGS 2EA. IN THE WINDSHIELD CENTER POST REF BOMBARDIER DWG AND CRJ 200 SRM. SEE CONTINJan 22, 2020 · N905EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
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