# Service difficulty reports: N921EV

A list on [N921EV](https://openairdocs.org/aircraft/N921EV.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 4 · 187 reports

- [SDR SWIA202266139](https://openairdocs.org/sdr/SWIA202266139.md): None · failed · Jul 15, 2022 · N921EV · Cndair CL6002B19 · Landing Gear Door Actuator
  > D: 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 - UPP
- [SDR SWIA202264090](https://openairdocs.org/sdr/SWIA202264090.md): None · malfunctioned · Jan 29, 2022 · N921EV · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR 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 IN
- [SDR SWIA202158814](https://openairdocs.org/sdr/SWIA202158814.md): Door Frame · cracked · Jun 16, 2021 · N921EV · Cndair CL6002B19 · Fuselage Main, Structure
  > TRANSFER 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
- [SDR SWIA202054407](https://openairdocs.org/sdr/SWIA202054407.md): Seat Track · corroded · Nov 9, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR 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.
- [SDR SWIA202054373](https://openairdocs.org/sdr/SWIA202054373.md): Skin · corroded · Nov 5, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INTERNAL 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.
- [SDR SWIA202054361](https://openairdocs.org/sdr/SWIA202054361.md): Intercostal · corroded · Nov 5, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CENTER 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.
- [SDR SWIA202054349](https://openairdocs.org/sdr/SWIA202054349.md): Skin · chafed · Oct 30, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > WHILE 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 PE
- [SDR SWIA202054380](https://openairdocs.org/sdr/SWIA202054380.md): Drag Angle · cracked · Oct 23, 2020 · N921EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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.
- [SDR SWIA202054372](https://openairdocs.org/sdr/SWIA202054372.md): Floor Panel · corroded · Oct 23, 2020 · N921EV · Cndair CL6002B19 · Fuselage Floor Panel
  > RT 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 DET
- [SDR SWIA202054354](https://openairdocs.org/sdr/SWIA202054354.md): Pressure Deck · corroded · Oct 23, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Structure
  > LT 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 WO
- [SDR SWIA202054371](https://openairdocs.org/sdr/SWIA202054371.md): Intercostal · damaged · Oct 22, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT 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 T
- [SDR SWIA202054370](https://openairdocs.org/sdr/SWIA202054370.md): Frame Splice · corroded · Oct 22, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Frame
  > UPPON 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.
- [SDR SWIA202054406](https://openairdocs.org/sdr/SWIA202054406.md): Anchor Fitting · corroded · Oct 20, 2020 · N921EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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.
- [SDR SWIA202054379](https://openairdocs.org/sdr/SWIA202054379.md): Bracket · cracked · Oct 20, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 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.
- [SDR SWIA202054369](https://openairdocs.org/sdr/SWIA202054369.md): Door Frame · cracked · Oct 20, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX 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.
- [SDR SWIA202054353](https://openairdocs.org/sdr/SWIA202054353.md): Bracket · cracked · Oct 20, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RT 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 AND
- [SDR SWIA202054368](https://openairdocs.org/sdr/SWIA202054368.md): Door Sill · corroded · Oct 19, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO 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
- [SDR SWIA202054348](https://openairdocs.org/sdr/SWIA202054348.md): Floorbeam · corroded · Oct 19, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 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.
- [SDR SWIA202054405](https://openairdocs.org/sdr/SWIA202054405.md): Seat Track · corroded · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO 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.
- [SDR SWIA202054404](https://openairdocs.org/sdr/SWIA202054404.md): Seat Track · corroded · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO 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.
- [SDR SWIA202054403](https://openairdocs.org/sdr/SWIA202054403.md): Seat Track · corroded · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO 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.
- [SDR SWIA202054402](https://openairdocs.org/sdr/SWIA202054402.md): Seat Track · corroded · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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.
- [SDR SWIA202054367](https://openairdocs.org/sdr/SWIA202054367.md): Fitting · cracked · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 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.
- [SDR SWIA202054357](https://openairdocs.org/sdr/SWIA202054357.md): Floor Support · corroded · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 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+1
- [SDR SWIA202054356](https://openairdocs.org/sdr/SWIA202054356.md): Floorbeam · corroded · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 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 AND
- [SDR SWIA202054351](https://openairdocs.org/sdr/SWIA202054351.md): Floor Support · corroded · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 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 CHANGE
- [SDR SWIA202054350](https://openairdocs.org/sdr/SWIA202054350.md): Floor Support · corroded · Oct 18, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 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.
- [SDR SWIA202054401](https://openairdocs.org/sdr/SWIA202054401.md): Seat Track · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 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.
- [SDR SWIA202054400](https://openairdocs.org/sdr/SWIA202054400.md): Seat Track · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 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.
- [SDR SWIA202054399](https://openairdocs.org/sdr/SWIA202054399.md): Seat Track · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 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.
- [SDR SWIA202054398](https://openairdocs.org/sdr/SWIA202054398.md): Floorbeam · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 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
- [SDR SWIA202054397](https://openairdocs.org/sdr/SWIA202054397.md): Strap · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX 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.
- [SDR SWIA202054396](https://openairdocs.org/sdr/SWIA202054396.md): Support Angle · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX 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.
- [SDR SWIA202054395](https://openairdocs.org/sdr/SWIA202054395.md): Doubler · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR SWIA202054394](https://openairdocs.org/sdr/SWIA202054394.md): Mount · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR SWIA202054378](https://openairdocs.org/sdr/SWIA202054378.md): Floorbeam · cracked · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 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 WOR
- [SDR SWIA202054366](https://openairdocs.org/sdr/SWIA202054366.md): Frame · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 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.
- [SDR SWIA202054360](https://openairdocs.org/sdr/SWIA202054360.md): Frame · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 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.
- [SDR SWIA202054359](https://openairdocs.org/sdr/SWIA202054359.md): Floor Support · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 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
- [SDR SWIA202054358](https://openairdocs.org/sdr/SWIA202054358.md): Floor Support · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 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
- [SDR SWIA202054355](https://openairdocs.org/sdr/SWIA202054355.md): Stringer · corroded · Oct 17, 2020 · N921EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR 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 FOR
- [SDR SWIA202054393](https://openairdocs.org/sdr/SWIA202054393.md): Nut · corroded · Oct 16, 2020 · N921EV · Cndair CL6002B19 · Spoilers
  > LEFT 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, IA
- [SDR SWIA202054392](https://openairdocs.org/sdr/SWIA202054392.md): Bolt · corroded · Oct 16, 2020 · N921EV · Cndair CL6002B19 · Spoilers
  > LEFT 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.
- [SDR SWIA202054391](https://openairdocs.org/sdr/SWIA202054391.md): Bolt · corroded · Oct 16, 2020 · N921EV · Cndair CL6002B19 · Spoilers
  > LEFT 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
- [SDR SWIA202054390](https://openairdocs.org/sdr/SWIA202054390.md): Bolt · corroded · Oct 16, 2020 · N921EV · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > HORIZONTAL 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.
- [SDR SWIA202054389](https://openairdocs.org/sdr/SWIA202054389.md): Beam · corroded · Oct 15, 2020 · N921EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RT 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.
- [SDR SWIA202054388](https://openairdocs.org/sdr/SWIA202054388.md): Bonding Wire · corroded · Oct 15, 2020 · N921EV · Cndair CL6002B19 · Wing System Wiring
  > LEFT 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.
- [SDR SWIA202054387](https://openairdocs.org/sdr/SWIA202054387.md): Bolt · corroded · Oct 15, 2020 · N921EV · Cndair CL6002B19 · Wing, Attach Fittings
  > OUTBOARD 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.
- [SDR SWIA202054386](https://openairdocs.org/sdr/SWIA202054386.md): Bolt · corroded · Oct 15, 2020 · N921EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RT 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
- [SDR SWIA202054385](https://openairdocs.org/sdr/SWIA202054385.md): Hinge Arm · corroded · Oct 15, 2020 · N921EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LT 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 178

Next page: https://openairdocs.org/aircraft/N921EV/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 = 'N921EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N921EV/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.