N921EV

Service difficulty reports · 187

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 = 'N921EV' 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 SWIA202266139None · failedD: NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGES APPEARED AFTER TAKEOFF WHEN SELECTING LANDING GEAR UP. WAS ABLE TO GET ALL THREE DOWN AND LOCKED AFTER COMPLETION OF QRH. / C: MEL 32-30-1 / CAT: A DUE: 1 FLT DAY / ***CAT II NOT AUTHORIZED*** / ***ODI - UPPJul 15, 2022 · N921EV · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202264090None · malfunctionedGEAR DISAGREE WARNING WITH GEAR HANDLE UP AFTER TAKEOFF, NOSE WHEEL DID NOT RETRACT. NOSE DOOR OPEN WARNING. (FLIGHT 4278 - FILED CLOSED) INSPECTED NLG WITH NO DAMAGE NOTED. BRACKETS HOLDING SENSORS ARE NOT BENT AND ALL SENSORS ARE SECURE. FOUND FAULT INJan 29, 2022 · N921EV · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202158814Door Frame · crackedTRANSFER FROM EAML 660702 : TRANSFERRED FROM CAMP 22966043. PASSENGER DOOR AFT FRAME HAS A CRACK RUNNING APPROX. 3" ALONG ANGLE JUST BELOW WHERE DOOR PULLEY IS ATTACHED. (R-O 6/19/21 - IN SERVICE - FILED CLOSED)REPAIRED MCD AFT FORMER UNDER PULLEY MOUNTING Jun 16, 2021 · N921EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202054407Seat Track · corrodedFLOOR SEAT TRACK LBL 9 FS 409+18 TO FS 559+4 CORRODED BEYOND LIMITS, REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. INSTALLED A NEW SEAT TRACK, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Nov 9, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202054373Skin · corrodedINTERNAL SIDE OF EXTERNAL SKIN CORRODED AT DOOR DATUM 2 AND FS 329.5. C-CHECK RO 11/24/2020. REPAIRED PAX DOOR OUTER SKIN AT DATUM 2 AND FS 329.5, IAW MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. WEIGHT ADDED 0.18 LBS.Nov 5, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202054361Intercostal · corrodedCENTER INTERCOSTAL CORRODED AT DOOR DATUM 2 OF PAX DOOR. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CENTER INTERCOSTAL AT DATUM 2 OF PAX DOOR, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.Nov 5, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054349Skin · chafedWHILE PERFORMING REINSPECT FOR RA REPAIRED CENTER WING LOWER PLANK CHAFFED AT LT AFT OUTBOARD CORNER UNDER PANEL 193AB, PER REO, REQUIRES SPECIAL DETAILED INSPECTIONS, NDT INSPECT REWORKED AREA. ADDITIONAL DAMAGE WAS FOUND AND EDDY CURRENT WAS UNABLE TO BE PEOct 30, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202054380Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. C-CHECK RO 11/24/2020. REPLACED PAX DOOR AFT DRAG ANGLE, IAW CRJ 200 SRM. REFERENCE REO FOR MATERIAL CALL OUT AND FASTENER SIZE. REFERENCE MX TRAN 21722399 JOB 9781981 OPERATIONS 484 FOR INSTALL OF DRAG ANGLE.Oct 23, 2020 · N921EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202054372Floor Panel · corrodedRT PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION AROUND SCREW HOLES AT FRAME STATIONS 424, 428, 435, 441, 447, 453, 459, 467, 486, 493, 501, 507, 521, 531, 537, 542, 548 AND 555. C-CHECK RO 11/24/2020. COMPLETED REO. SEE CONTINUATION CARD FOR DETOct 23, 2020 · N921EV · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA202054354Pressure Deck · corrodedLT PRESSURE FLOOR SILL PANEL HAS 17 AREAS OF CORROSION AROUND SCREW HOLES AT FRAME STATIONS 424, 429, 435, 441, 447, 453, 459, 467, 478, 486, 493, 503, 518, 522, 531, 539 AND 555. C-CHECK RO 11/24/2020. COMPLETED REO. SEE CONTINUATION CARD FOR DETAILS OF WOOct 23, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202054371Intercostal · damagedLT EMERGENCY EXIT SURROUND STRUCTURE INTERCOSTAL FWD OF OPENING AT FS 444, BETWEEN STRINGERS 9L AND 10L, HAS TOOLING DAMAGE. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT EMERGENCY EXIT INTERCOSTALS AT FS 444 AT STR 9L AND 10L, IAW CRJ 200 SRM. COMPLETED TOct 22, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054370Frame Splice · corrodedUPPON REMOVAL OF FS 333.00 FRAME LOWER SEGMENT, FOUND FS 333.00 CIRCUMFRENTIAL SPLICE TO BE CORRODED AT STR 27. C-CHECK RO 11/24/2020. REPAIRED FS 333 FRAME, IAW MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.Oct 22, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202054406Anchor Fitting · corrodedPAX DOOR FORWARD ANCHOR FITTING SERRATED PLATE IS CORRODED. C-CHECK RO 11/24/2020. REPLACED PAX DOOR FORWARD ANCHOR FITTING SERRATED PLATE, PER CRJ 200 AMM TORQUE WRENCH 204360 DUE 30-SEP-21.Oct 20, 2020 · N921EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202054379Bracket · crackedFS 621.00 TO FS 625.30 ANGLES AT STGR 14L AND 14R ARE CRACKED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED 2 EA ANGLES AT FS 621-625.30 STR 14L AND 14R, IAW CRJ200 SRM.Oct 20, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA202054369Door Frame · crackedPAX DOOR UPPER SILL, STRINGER 3L IS CRACKED AT FS 379.00. C-CHECK RO 11/24/2020. REPAIRED STR 3L AT FS 379, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM M-337. NO WEIGHT CHANGE.Oct 20, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054353Bracket · crackedRT WINDSHIELD SIDEPOST LOWER AFT BRACKET IS CRACKED. C-CHECK RO 11/24/2020. REMOVED DAMAGED RT WINDSHIELD SIDEPOST LOWER AFT BRACKET. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE BRACKET, IAW CRJ200. COMPLETED TASK CARD, FORM M-337 ATTACHED. WEIGHT ANDOct 20, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202054368Door Sill · corrodedCARGO DOOR SILL HAS MULTIPLE AREAS OF CORROSION ALONG LENGTH OF SILL. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CARGO SILL, IAW REO FORM M-337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK Oct 19, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054348Floorbeam · corrodedLBL 27.00 FLOORBEAM IS CORRODED AT (1) LOCATION BETWEEN FS 559.00+96 AND FS 559.00+112. C-CHECK RO 11/24/2020. PERFORMED A MAJOR REPAIR TO FLOOR BEAM AT LBL 27 BETWEEN FS 559.00+96 AND FS 559.00+112, IAW CRJ200 SRM. COMPLETED SKYWEST MAJOR REPAIR TASK CARD.Oct 19, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202054405Seat Track · corrodedCARGO SEAT TRACK ON LBL 9.00 JUST FORWARD OF FS 621.00 IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK, IAW CRJ200 AMM.Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202054404Seat Track · corrodedCARGO SEAT TRACK BETWEEN FS 559.00+112 AND APPROXIMATELY FS 570.00, RBL 9.00 AND LBL 9.00 ARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED TRACK, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202054403Seat Track · corrodedCARGO SEAT TRACKS BETWEEN FS 559.00+80 AND FS 559.00+96 AT RBL 27.00, RBL 9.00, LBL 9.00 AND LBL 27.00 ARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CARGO SEAT TRACKS BETWEEN FS 559.00+80 AND 559.00+96 AT RBL 27.00, RBL 9.00, LBL 9.00 AND LBL 27.Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202054402Seat Track · corrodedSEAT TRACK ON RBL 9.00 IS CORRODED BETWEEN FS 409.00+128 TO FS 559.00. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK ON RBL 9.00 BETWEEN FS 409.00+128 TO FS 559.00, IAW CRJ200 AMM. REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202054367Fitting · crackedFS 461.00 FLOORBEAM FITTING IS CRACKED ON THE OUTBOARD SIDE OF BEAM, RBL 9.00. C-CHECK RO 11/24/2020. REMOVED AND REINSTALLED FLOOR BEAM FITTING AT RBL 9 FS 461, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGES NOTED.Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054357Floor Support · corrodedLBL 9.00 FLOORBEAM CAP IS CORRODED AROUND MOST NUTPLATES ON THE INBOARD SIDE OF BEAM BETWEEN FS 409.00+128 TO FS 559.00. C-CHECK RO 11/24/2020. REPAIRED LBL 9.00 FLOORBEAM CAP IS CORROSION AROUND MOST NUTPLATES ON THE INBOARD SIDE OF BEAM BETWEEN FS 409.00+1Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054356Floorbeam · corrodedRBL 27.00 FLOORBEAM CAP IS HEAVILY CORRODED AT FS 559.00+80, INBOARD AND OUTBOARD SIDE OF BEAM. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RBL 27.00 FLOORBEAM CAP AT FS 559+64 TO FS 559+112, IAW CRJ200 SRM. FORM 337 AND MAJOR REPAIR TASK CARD COMPLETED ANDOct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202054351Floor Support · corrodedRBL 9.00 FLOORBEAM CAP IS CORRODED AROUND MOST NUTPLATES ON THE INBOARD SIDE OF BEAM BETWEEN FS 409.00+128 TO FS 559.00. C-CHECK RO 11/24/2020. REPAIRED RBL 9 FLOORBEAM CAP, IAW REO. FORM 337 AND MAJOR REPAIR TASK CARD COMPLETED AND ATTACHED. WEIGHT CHANGEOct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054350Floor Support · corrodedRBL 9.00 FLOORBEAM CAP IS CORRODED AT MULTIPLE LOCATIONS ON THE INBOARD SIDE BETWEEN FS 559.00 AND FS 559.00+48. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FLOORBEAM CAP FROM FS 559+10-FS 559+112, IAW MHIRJ REO. FLOORBEAM CAP FABRICATED, IAW CRJ 200 SRM. Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054401Seat Track · corrodedLBL 9 FLOOR SEAT TRACK FS 400-FS 409+128 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK SEGMENT, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202054400Seat Track · corrodedRBL 9 FLOOR SEAT TRACK FS 364-FS 400 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202054399Seat Track · corrodedLBL 9 FLOOR SEAT TRACK FS 364-FS400 SEGMENT IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED SEAT TRACK, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202054398Floorbeam · corrodedFS 280 CROSSBEAM AND FWD "J" ANGLE ARE CORRODED BETWEEN LBL 11 AND RBL 27. C-CHECK RO 11/24/2020. REMOVED AND INSTALLED J-ANGLE AT FS 280, IAW CRJ-200 SRM. INSTALLED FS 280 CROSSBEAM CENTER SECTION OF PREVIOUS REPAIR, IAW CRJ-200 SRM AND REF BOMBARDIER REO Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202054397Strap · corrodedPAX DOOR LOWER SILL FRAME STRAP IS CORRODED AT FS 349. C-CHECK RO 11/24/2020. REPAIRED PAX DOOR LOWER SILL FRAME STRAP, IAW CRJ200 SRM. REFER TO CONTINUATION CARD FOR REPAIR DETAILS.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054396Support Angle · corrodedPAX DOOR SILL FLOOR SUPPORT ANGLES AND CUPS ARE CORRODED BETWEEN FS 310 AND FS 349. C-CHECK RO 11/24/2020. REMOVED AND REPLACED PAX DOOR SILL FLOOR SUPPORT ANGLE AT FS 310-FS 349, IAW CRJ200 SRM.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054395Doubler · corrodedFLOOR SUPPORT BOLT HOLE DOUBLER AT FS 286 RBL 37 IS CORRODED. C-CHECK RO 11/24/2020. INSTALLED SERVICABLE BOLT HOLE DOUBLER, IAW CRJ 200 SRM.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054394Mount · corrodedFLOOR SUPPORT BOLT HOLE DOUBLER AT FS 297 RBL 6 IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FLOOR SUPPORT BOLT HOLE DOUBLER AT FS 297 RBL 6, IAW CRJ-200 SRMS.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054378Floorbeam · crackedRBL 9 FLOORBEAM INBOARD AND OUTBOARD CLIP ANGLE AT FS 280 IS CRACKED. C-CHECK RO 11/24/2020. REMOVED AND FABRICATED NEW AND REPLACED RBL 9 INBOARD AND OUTBOARD CLIP ANGLE AT FS 280, IAW CRJ 200 SRM AND IN REF TO REO. SEE CONTINUATION CARD FOR DETAILS OF WOROct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202054366Frame · corrodedFS 319 FRAME IS CORRODED BETWEEN STGR 26L AND STGR 25R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LOWER FRAME SEGMENT AT FS 319, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202054360Frame · corrodedFS 333 FRAME IS CORRODED BETWEEN STGR 25L AND STGR 25R. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LOWER FRAME SEGMENT FS 333 LOWER FRAME SEGMENT, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE.Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202054359Floor Support · corrodedRBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 409+52 AND FS 409+128. C-CHECK RO 11/24/2020. PERFORMED MAJOR REPAIR ON RBL 9 FLOORBEAM CAP BETWEEN FS 409+48.00 AND FS 409+118.00, IAW CRJ200 SRM AND MHIRJ REO. COMPLETED TASK CARD FOR STRUCTURAL MAJOR REPAIR. FORM Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054358Floor Support · corrodedLBL 9 FLOORBEAM IS CORRODED BETWEEN FS 409+5 AND FS 409+128. C-CHECK RO 11/24/2020. PERFORMED MAJOR REPAIR TO LBL 9 FLOOR BEAM CAP FROM FS 409+5.00 TO FS 409+118.00, IAW CRJ200 SRM AND MHIRJ REO. COMPLETED TASK CARD FOR STRUCTURAL MAJOR REPAIR. FORM M-337 Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202054355Stringer · corrodedSTGR 27 IS CORRODED BETWEEN FS 319 AND FS 349. C-CHECK RO 11/24/2020. REPAIRED STGR 27 BETWEEN FS 319 AND FS 349 BY STRINGER SPLICE REPAIR, IAW CRJ SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOROct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202054393Nut · corrodedLEFT FLIGHT SPOILER HINGE BOLTS HAVE CORRODED NUTS (3 EA) AT THE CENTER AND OUTBOARD HINGES. C-CHECK RO 11/24/2020. REMOVED AND REPLACED WITH SERVICEABLE NUTS (P/N MS17825-6, 1 EA AND MS17825-5, 2 EA ON LEFT HAND FLIGHT SPOILER CENTER AND OUTBOARD HINGES, IAOct 16, 2020 · N921EV · Cndair CL6002B19 · SpoilersSDR SWIA202054392Bolt · corrodedLEFT SPOILERON HINGE BOLTS HAVE CORRODED NUTS (3 EA) AT THE OUTBOARD, CENTER AND INBOARD LOCATIONS. C-CHECK RO 11/24/2020. REMOVED AND REPLACED HARDWARE, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 16, 2020 · N921EV · Cndair CL6002B19 · SpoilersSDR SWIA202054391Bolt · corrodedLEFT SPOILERON OUTBOARD HINGE BOLT STOPPER BRACKET HAS 1 EA CORRODED BOLT AND INBOARD HINGE STOPPER BRACKETS HAVE 4 EA CORRODED BOLTS. C-CHECK RO 11/24/2020. REMOVED AND REPLACED LT SPOILERON OUTBOARD HINGE BOLT STOPPER BRACKET BOLT (1 EA) AND INBOARD HINGE Oct 16, 2020 · N921EV · Cndair CL6002B19 · SpoilersSDR SWIA202054390Bolt · corrodedHORIZONTAL STAB FWD STEADY FITTING 5 EA LOWER MOUNT BOLTS ARE CORRODED. C-CHECK RO 11/24/2020. REPLACED 5 CORRODED BOLTS ON THE HORIZONTAL STAB FWD FITTING LOWER MOUNT, IAW CRJ 200 AMM. CALIBRATED TORQUE WRENCH USED NR WVACT203581 DUE 31-DEC-20.Oct 16, 2020 · N921EV · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202054389Beam · corrodedRT INBOARD FLAP, INBOARD VANE SLIDING BEAM, INBOARD SPRING AND HARDWARE ARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED CORRODED HARDWARE, IAW CRJ200 AMM.Oct 15, 2020 · N921EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202054388Bonding Wire · corrodedLEFT OUTBOARD FLIGHT SPOILER OUTBOARD PCU BONDING WIRE HARDWARE IS CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED BONDING WIRE, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 15, 2020 · N921EV · Cndair CL6002B19 · Wing System WiringSDR SWIA202054387Bolt · corrodedOUTBOARD GROUD SPOILER PCU MOUMTING BOLT NUTS 2 EA ARE CORRODED. C-CHECK RO 11/24/2020. REMOVED AND REPLACED NUT, IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 15, 2020 · N921EV · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA202054386Bolt · corrodedRT OUTBOARD FLAP INBOARD HINGE ARM LOCATED AT WS 178.00 AND OUTBOARD HINGE ARM LOCATED AT WS 264.00 ATTACHING HARDWARE FOUND TO BE CORRODED AND REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED RT OUTBOARD FLAP HINGE ARM HARDWARE, IAW CRJ200 Oct 15, 2020 · N921EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202054385Hinge Arm · corrodedLT OUTBOARD FLAP INBOARD HINGE ARM LOCATED AT WS 178.00 AND OUTBOARD HINGE ARM LOCATED AT WS 26400 ATTACHING HARDWARE FOUND TO BE CORRODED AND REQUIRES REPLACEMENT. C-CHECK RO 11/24/2020. REMOVED AND REPLACED HARDWARE AT LT OUTBOARD FLAP HINGE ARMS AT WS 178Oct 15, 2020 · N921EV · Cndair CL6002B19 · Trailing Edge Flaps
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