# Service difficulty reports: N754EV

A list on [N754EV](https://openairdocs.org/aircraft/N754EV.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 · 199 reports

- [SDR SWIA20241110030](https://openairdocs.org/sdr/SWIA20241110030.md): Control Handle · faulted · Oct 30, 2024 · N754EV · Cndair CL6002C10 · Landing Gear Selector
  > RECEIVED LANDING GEAR DISAGREE WARNING MESSAGE AFTER SELECTING LANDING GEAR TO THE UP POSITION. LANDING GEAR FELT EXTENDED WITH NOSE DOOR IN THE OPEN POSITION. (FLIGHT 4900 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29078495 WITH THE FOL
- [SDR SWIA2024090900007](https://openairdocs.org/sdr/SWIA2024090900007.md): Hose · leaking · Sep 7, 2024 · N754EV · Cndair CL6002C10 · Hydraulic System, Main
  > UPON SELECTING GEAR DOWN ON APPROACH RECEIVED HYD 3 CAUTION INBD GND SPOILER CAUTION, HRDRAULIC 3 SHOWED 0% FLUID LEVEL. QRH PROCEDURE COMPLETED. (FLIGHT 4965 - FILED CLOSED) PLEASE REFERENCE AML 1426633 PLEASE REFERENCE AML 1426634 PLEASE REFERENCE
- [SDR SWIA202054876](https://openairdocs.org/sdr/SWIA202054876.md): Connector · unsecure · Dec 29, 2020 · N754EV · Cndair CL6002C10 · Fire Protection System Wiring
  > SMOKE AFT LAV WARNING MESSAGE ON APPROACH AT 7000 FT MSL. RAN QRH HALF OF QRH FOR SMOKE AFT LAV, MESSAGE PERSISTED. NO SIGN OF SMOKE OR FUMES. TROUBLESHOT AFT LAV WARNING MESSAGE, PER SERVICE LETTER, NO DEFECTS NOTED. CONTINUED TROUBLESHOOTING AFT LAV WARN
- [SDR SWIA202054760](https://openairdocs.org/sdr/SWIA202054760.md): Fairing · chafed · Dec 17, 2020 · N754EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR HINGE FAIRING 141AL IS CHAFING ON DOOR SKIN. C-CHECK RO 12/24/2020. REMOVED DAMAGED PANEL 141AL AND INSTALLED NEW SERVICEABLE PANEL, IAW CRJ-700 AMM.
- [SDR SWIA202054720](https://openairdocs.org/sdr/SWIA202054720.md): Floor Support · corroded · Dec 17, 2020 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE FROM FS 310.00 TO 333.00 AT LBL 27 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED FLOOR SUPPORT ANGLE FROM FS 310.00 TO 333.00 AT LBL 27, IAW CRJ-700 SRM.
- [SDR SWIA202054719](https://openairdocs.org/sdr/SWIA202054719.md): Intercostal · corroded · Dec 17, 2020 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FROM FS 310.00 TO 333.00 AT STRINGER 21L IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED INTERCOSTAL FROM FS 310.00 TO 333.00 AT STRINGER 21L, IAW CRJ-700 SRM. REF ATTACHED TASK CARD AND M-337 FOR RII TASKS. NO CHANGE TO WEIGHT AND BALA
- [SDR SWIA202054718](https://openairdocs.org/sdr/SWIA202054718.md): Frame · corroded · Dec 17, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SECTION AT FS 319.00 FROM STRINGER 18L-21L IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED FRAME SECTION AT 319.00 FROM STRINGER 18L-21L, IAW CRJ-700 SRM. REF ATTACHED TASK CARD AND M-337. NO CHANGE TO WEIGHT AND BALANCE. PRESSURE CHECK GOO
- [SDR SWIA202054754](https://openairdocs.org/sdr/SWIA202054754.md): Stringer Clip · corroded · Dec 5, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FOUND CORRODED CLIP AT STRGR 18L BETWEEN FS 280-FS 295. C-CHECK RO 12/24/2020. REMOVED AND REPLACED CLIP AT STRGR 18L BETWEEN FS 280-FS295, IAW CRJ700 SRM AND PAINTED AND APPLIED CIC, IAW CRJ 700 SRM.
- [SDR SWIA202054727](https://openairdocs.org/sdr/SWIA202054727.md): Frame · corroded · Dec 5, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Frame
  > RT FRAME SECTION AT FS 333.00 FOUND TO BE HEAVILY CORRODED. C-CHECK RO 12/24/2020. REMOVED CORRODED RT FRAME SECTION AT FS 333.00 AND INSTALLED NEW SERVICEABLE FRAME SECTION, IAW CRJ-700 SRM. COMPLIED WITH ATTACHED TASK CARD AND M-337. NO CHANGE TO WEIGHT
- [SDR SWIA202054723](https://openairdocs.org/sdr/SWIA202054723.md): Intercostal · corroded · Dec 5, 2020 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FS 319.00 AND FS 349.00 AT STRINGER 20R FOUND TO BE CORRODED. C-CHECK RO 12/24/2020. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL, IAW CRJ-700 SRM. COMPLETED ATTACHED SKY CARD AND M-337. NO CHANGE TO WEIGHT AND
- [SDR SWIA202054761](https://openairdocs.org/sdr/SWIA202054761.md): Lug · damaged · Dec 1, 2020 · N754EV · Cndair CL6002C10 · Ailerons
  > LT AILERON LUG NR 1 FOUND TO HAVE DAMAGE OUT OF LIMITS FOR REPAIR, AILERON REQUIRES REPLACEMENT. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE AILERON, REF CAMP 21674471 FOR REMOVAL AND INSTALLATION.
- [SDR SWIA202054759](https://openairdocs.org/sdr/SWIA202054759.md): Panel · chafed · Nov 29, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > RT INBOARD FLAP VANE ACCESS PANEL 684ET IS A DEEP CHAFING ON LEADING EDGE. C-CHECK RO 12/24/2020. RECEIVED SERVICABLE RT INBOARD FLAP VANE PANEL 684ET, REFERENCE MASTER PANEL BOOK CO 10173820 JOB 91017380 OP REF BINDER CAMP CP 21674491 FOR REMOVAL AND INSTAL
- [SDR SWIA202054721](https://openairdocs.org/sdr/SWIA202054721.md): Stringer · corroded · Nov 17, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 23L BETWEEN FS 1015-FS 1031 CORROSION. C-CHECK RO 12/24/2020. REMOVED AND REPLACED STR 23L BETWEEN FS 1015-FS 1031, IAW CRJ 700 SRM & SKY CARD NO WEIGHT CHANGE NO INSPECTION REQUIREMENTS FORM 337 IS ATTACHED.
- [SDR SWIA202054726](https://openairdocs.org/sdr/SWIA202054726.md): Lap Joint · corroded · Nov 16, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND AT AT STR 21L AT FS 333.00 ON CIRCUMFERENTIAL JOINT. C-CHECK RO 12/24/2020. REPAIRED CORROSION AT STR 21L AT FS 333.00 CIRCUMFERENTIAL JOINT, IAW MHIRJ REO & SKY CARD NOTE DTA REQUIREMENTS WILL BE PROVIDED WITHIN 12 MONTHS. NO WIEGHT CHANGES
- [SDR SWIA202054752](https://openairdocs.org/sdr/SWIA202054752.md): Angle · corroded · Nov 14, 2020 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE ACCESSING FOUND CIRCUMFERENTIAL JOINT ANGLE WITH CORROSION. C-CHECK RO 12/24/2020. REMOVED AND REPLACED CIRCUMFERENTIAL JOINT ANGLE, IAW CRJ 700 SRM & SKY CARD. NO WEIGHT CHANGES FORM 337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WOR
- [SDR SWIA202054751](https://openairdocs.org/sdr/SWIA202054751.md): Stringer · corroded · Nov 14, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STR 20L BETWEEN FS 319 AND FS 333. C-CHECK RO 12/24/2020. REMOVED CORRODED STRINGER 20L BETWEEN FS 319.00 AND 333.00 AND INSTALLED NEW SERVICEABLE STRINGER, IAW CRJ-700 SRM. REF ATTACHED TASK CARD AND M-337. NO CHANGE TO WEIGHT AND BALAN
- [SDR SWIA202054750](https://openairdocs.org/sdr/SWIA202054750.md): Stringer · corroded · Nov 14, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 19L FROM FS 338 TO FS 342 CORRORED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED STR 19L FROM FS 338 TO FS 342, IAW CRJ700 SRM & SKY CARD NO WEIGHT CHANGES FORM 337 IS ATTACHED.
- [SDR SWIA202054749](https://openairdocs.org/sdr/SWIA202054749.md): Hinge · gouged · Nov 12, 2020 · N754EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (DOOR SIDE) LUGS NR 1, 2, 3, 4, 5, 6, 7, 8, 9, 13, 14, 15, 19, 20, 25, AND 26 ARE GOUGED. C-CHECK RO 12/24/2020. REMOVED DAMAGE BY COMPLYING WITH REPAIR TYPE 1 OF REO. COMPLETED AND ATTACHED M-337 AND SKY CARD. NO WEIGHT CHANGE. REFERENCE CO
- [SDR SWIA202054733](https://openairdocs.org/sdr/SWIA202054733.md): Window · crazed · Nov 12, 2020 · N754EV · Cndair CL6002C10 · Door Windows
  > GALLEY DOOR WINDOW IS BADLEY CRAZED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED GALLEY SERVICE DOOR WINDOW, IAW CRJ-700 AMM.
- [SDR SWIA202054722](https://openairdocs.org/sdr/SWIA202054722.md): Skin · chafed · Nov 12, 2020 · N754EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > CARGO DOOR OUTER SKIN HAS TWO CHAFES ON UPPER EDGE OF DOOR. C-CHECK RO 12/24/2020. REPAIRED CARGO OUTER DOOR CHAFES, IAW REO. COMPLETED TASK CARD AND ATTACHED FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202054753](https://openairdocs.org/sdr/SWIA202054753.md): Angle · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280 FWD J ANGLE IS CORRODED FROM BL 9.04 LT AND BL 9.04 RT SIDE. C-CHECK RO 12/24/2020. INSTALLED SERVICABLE J ANGLE AT FS 280 FROM LBL 9.04 TO RBL 9.04, IAW CRJ 700 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202054748](https://openairdocs.org/sdr/SWIA202054748.md): Stringer · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > RT STRINGER 20 R IS CORRODED AT FS 347.00. C-CHECK RO 12/24/2020. REMOVED AND REPLACED RT STRINGER 20R AT FS 347.00, IAW CRJ 700 SRM AND SKY CARD NOTE NO WEIGHT CHANGES AND FORM 337 IS ATTACHED. REF CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202054747](https://openairdocs.org/sdr/SWIA202054747.md): Seat Track · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SIDE SEAT RAIL BETWEEN FS 785.15 AND FS 797.00 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED RT CABIN SIDE SEAT RAIL BETWEEN FS 785.15-FS 847 +6", IAW CRJ700 AMM.
- [SDR SWIA202054746](https://openairdocs.org/sdr/SWIA202054746.md): Support Channel · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SIDE SEAT TRACK SUPPORT CHANNEL IS CORRODED FROM FS 785.15 TO FS 797.00. C-CHECK RO 12/24/2020. REMOVED AND REPLACED CABIN SIDE SEAT TRACK SUPPORT CHANNEL FROM FS 785.15 TO FS 797.00, IAW CRJ 700 AMM.
- [SDR SWIA202054745](https://openairdocs.org/sdr/SWIA202054745.md): Seat Track · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SIDE SEAT RAIL RT BETWEEN FS 714.00 TO FS 761.85 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED RT SIDE SEAT RAIL AT FS 714.00 TO 761.85 AND INSTALLED NEW SERVICEABLE SEAT TRACK, IAW CRJ-200 AMM.
- [SDR SWIA202054744](https://openairdocs.org/sdr/SWIA202054744.md): Seat Track · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SIDE SEAT RAIL LT FROM FS 379.00 TO FS 512.00 IS CORRODED. C-CHECK RO 12/24/2020. INSTALLED SERVICEABLE CABIN SIDE SEAT RAIL LT FROM FS 379.00 TO FS 512.00, IAW CRJ 700 AMM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202054743](https://openairdocs.org/sdr/SWIA202054743.md): Seat Track · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SIDE SEAT RAIL LHS BETWEEN FS 512 & FS 570 IS CORRODED. C-CHECK RO 12/24/2020. AMM INSTALLED SERVICEABLE CABIN SIDE SEAT RAIL LT BETWEEN FS 512 AND FS 570, IAW CRJ 700 AMM. REFERENCE CONTINUATION CARD FOR WORK PEERFORMED.
- [SDR SWIA202054742](https://openairdocs.org/sdr/SWIA202054742.md): Seat Track · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 CABIN FLOOR SEAT TRACK FROM FS 485.00 TO FS 581.00 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED RBL 9 CABIN FLOOR SEAT TRACK FROM FS 485.00 TO FS 581.00, IAW CRJ 700 AMM. REF ATTACHED CONTIUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202054741](https://openairdocs.org/sdr/SWIA202054741.md): Seat Track · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 CABIN FLOOR SEAT TRACK FROM FS 485.00 TO FS 581.00 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED CORRODED SEAT TRACK AT LBL 9 FS 485.00 TO FS 517.00 AND INSTALLED NEW SEAT TRACK, IAW CRJ-700 AMM.
- [SDR SWIA202054728](https://openairdocs.org/sdr/SWIA202054728.md): Intercostal · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FROM FS 310.00 TO FS 349.00 AND AFT ATTACHMENT CLIP IS CORRODED LOCATED AT STR 20R. C-CHECK RO 12/24/2020. REMOVED AND REPLACED INTERCOSTAL FROM FS 310.00 TO FS 349.00 AND AFT ATTACHMENT CLIP AT STR 20R, IAW CRJ 700 SRM AND SKY CARD. REF ATTACHE
- [SDR SWIA202054717](https://openairdocs.org/sdr/SWIA202054717.md): Intercostal · corroded · Nov 11, 2020 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STR 21L FROM FS 310.00 TO FS 349.00 IS HEAVILY CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED INTERCOSTAL FROM FS 333-349 AT STRINGER 21L, IAW CRJ-700 SRM. REF ATTACHED SKY CARD AND M-337. NO WEIGHT CHANGES.
- [SDR SWIA202054740](https://openairdocs.org/sdr/SWIA202054740.md): Link · corroded · Nov 10, 2020 · N754EV · Cndair CL6002C10 · Ailerons
  > BOTH RT WING AILERON PCU OUTPUT LINK AND HARDWARE ARE CORRODED. C-CHECK RO 12/24/2020. REPLACED THE RIGHT AILERON PCU OUTPUT LINKS AND HARDWARES, IAW CRJ-700 AMM TASK.
- [SDR SWIA202054739](https://openairdocs.org/sdr/SWIA202054739.md): Link · corroded · Nov 10, 2020 · N754EV · Cndair CL6002C10 · Ailerons
  > BOTH LT WING AILERON PCU OUTPUT LINKS AND HARDWARE ARE CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED LT AILERON PCU OUTPUT LINK AND HARDWARE, IAW CRJ700 AMM. OPERATIONS TEST GOOD.
- [SDR SWIA202054758](https://openairdocs.org/sdr/SWIA202054758.md): Skin · chafed · Nov 6, 2020 · N754EV · Cndair CL6002C10 · Ailerons
  > LT AILERON UPPER HINGE LINE SKIN IS CHAFED BETWEEN WS 282 AND WS 353 APPROXIMATELY.250IN WIDE X.020IN DEEP. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE AILERON PN: CC670-13000-1 SN: 7678, REF CAMP 21674471 FOR INSTALL.
- [SDR SWIA202054757](https://openairdocs.org/sdr/SWIA202054757.md): Skin · chafed · Nov 6, 2020 · N754EV · Cndair CL6002C10 · Ailerons
  > LT AILERON LOWER HINGE LINE SKIN IS CHAFED BETWEEN WS 348 AND WS 353 APPROXIMATELY.750IN WIDE X.020 DEEP. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE AILERON PN: CC670-13000-1 SN: 7678, REF CAMP 21674471 FOR INSTALL.
- [SDR SWIA202054732](https://openairdocs.org/sdr/SWIA202054732.md): Skin · corroded · Nov 6, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT STR 27, FS 978-982 HAS AREA WITH A CHAFE FROM A SCREW, AN AREA OF CORROSION AROUND THAT SCREW AND AN AREA EXTENDING FROM THAT CORROSION WITH MISSING PAINT THAT HAS BEEN POORLY BLENDED AND TREATED. C-CHECK RO 12/24/2020. REPAIRED FUSELAGE SKI
- [SDR SWIA202054738](https://openairdocs.org/sdr/SWIA202054738.md): Bolt · corroded · Nov 5, 2020 · N754EV · Cndair CL6002C10 · Wing, Attach Fittings
  > RT FLAP BPSU MOUNTING HARDWARE IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED RT FLAP BPSU CORRODED HARDWARE WITH NEW SERVICEABLE HARDWARE, IAW CRJ 700 AMM. OPERATIONS AND RIG CHECKS GOOD. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202054737](https://openairdocs.org/sdr/SWIA202054737.md): Torque Tube · corroded · Nov 5, 2020 · N754EV · Cndair CL6002C10 · Trailing Edge Flap Control System
  > RT INBOARD FLAP TORQUE TUBE CARRIER BEARING AT WS 97.45 IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND INSTALLED NEW SERVICEABLE RT INBOARD FLAP TORQUE TUBE, IAW SKYWEST TASK CARDS. REFERENCE TASK CARDS FOR WORK PERFORMED.
- [SDR SWIA202054736](https://openairdocs.org/sdr/SWIA202054736.md): Bracket · corroded · Nov 5, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > BRACKET CORRODED AT STRINGER 19L AND FS 1031.00. C-CHECK RO 12/24/2020. REMOVED AND REPLACED STRINGER CLIP AT STRINGER 19L AT FS 1031, IAW CRJ 700 SRM.
- [SDR SWIA202054735](https://openairdocs.org/sdr/SWIA202054735.md): Bracket · corroded · Nov 5, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > BRACKET CORRODED AT STRINGER 19L AND FS 1015.00. C-CHECK RO 12/24/2020. REMOVED CORRODED STRINGER CLIP AT FS 1015.00 STRINGER 19L AND INSTALLED NEW SERVICEABLE CLIP, IAW CRJ-700 SRM. NOTE CLIP WAS FABRICATED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WO
- [SDR SWIA202054729](https://openairdocs.org/sdr/SWIA202054729.md): Skin · chafed · Nov 5, 2020 · N754EV · Cndair CL6002C10 · Trailing Edge Flaps
  > RT INBOARD FLAP LOWER SKIN IS CHAFED AROUND PERIMETER OF INBOARD FAIRING. C-CHECK RO 12/24/2020. REPAIRED RT INBOARD FLAP LOWER SKIN CHAFE BY DOING A SKIN SPLICE REPAIR, IAW CRJ700 SRM. COMPLETED TASK CARD AND ATTACHED FORM M-337. WEIGHT CHANGE +3.83 LBS,
- [SDR SWIA202054724](https://openairdocs.org/sdr/SWIA202054724.md): Door Sill · corroded · Nov 5, 2020 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL HAS CORROSION IN MULTIPLE PLACES. C-CHECK RO 12/24/2020. REMOVED AND REPLACED AFT CARGO DOOR SILL, IAW MHIRJ REO AND CRJ 700 SRM & SKY CARD NO WEIGHT CHANGE AND FORM M337 IS ATTACHED. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PE
- [SDR SWIA202054734](https://openairdocs.org/sdr/SWIA202054734.md): Mount · corroded · Nov 1, 2020 · N754EV · Cndair CL6002C10 · Wing, Attach Fittings
  > LT FLAP BPSU MOUNTING HARDWARE IS CORRODED. C-CHECK RO 12/24/2020. REMOVED AND REPLACED SIEZED AND CORRODED LT FLAP BPSU MOUNTING HARDWARE, IAW CRJ 700 AMM.
- [SDR SWIA202054731](https://openairdocs.org/sdr/SWIA202054731.md): Skin · chafed · Nov 1, 2020 · N754EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LT INBOARD FLAP LOWER SKIN IS CHAFED AROUND PERIMETER OF INBOARD HINGE FAIRING. C-CHECK RO 12/24/2020. REPAIRED LT INBOARD FLAP LOWER SKIN CHAFE BY DOING A SKIN SPLICE REPAIR, IAW CRJ700 SRM. COMPLETED TASK CARD AND ATTACHED FORM M-337. WEIGHT CHANGE +3.83
- [SDR SWIA202054756](https://openairdocs.org/sdr/SWIA202054756.md): Panel · chafed · Oct 31, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > PANEL 584 BB IS CHAFED AROUND FAIRING CONTACT. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE PANEL 584BB, REF ATTACHED CONTINUATION FOR WORK PERFORMED. REF CAMP 21674490 FOR INSTALL OF PANEL.
- [SDR SWIA202054755](https://openairdocs.org/sdr/SWIA202054755.md): Panel · chafed · Oct 31, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Structure
  > PANEL 684 BB IS CHAFFED AROUND HINGE FAIRING CONTACT. C-CHECK RO 12/24/2020. RECIEVED NEW SERVICEABLE PANEL 684BB, SEE CONTINUATION FOR WORK PERFORMED. REF CAMP 21674491 FOR INSTALL OF PANEL.
- [SDR SWIA202054725](https://openairdocs.org/sdr/SWIA202054725.md): Vane · chafed · Oct 30, 2020 · N754EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LT OUTBOARD FLAP VANE LEADING EDGE HAS VERTICLE CHAFE ON LOWER LEADING EDGE SURFACE AT WS 266. C-CHECK RO 12/24/2020. REMOVED DAMAGED LT OUTBOARD FLAP SKIN PANEL AND INSTALLED NEW PANEL, IAW CRJ-700 SRM. COMPLETED ATTACHED TASK CARD AND M-337. NO CHANGE TO
- [SDR SWIA202054730](https://openairdocs.org/sdr/SWIA202054730.md): Skin · damaged · Sep 23, 2020 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA53479-670-53-00-045 754EV FS256 ON STR23R-PR1. COMPLIED WITH TEMPORARY REPAIR, PER REO BLENDED DAMAGED SKIN AS REQUIRED AT FS 256 ON STR 23R. REPAIR IS VALID UNTIL NEXT HEAVY MAINTENANCE CHECK OR FOR 8000 FLIGHT HOUR
- [SDR SWIA2019121346869](https://openairdocs.org/sdr/SWIA2019121346869.md): Strut · collapsed · Dec 13, 2019 · N754EV · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/Axle
  > RECEIVED GEAR DISAGREE AFTER SELECTING GEAR HANDLE UP. AFTER SELECTING GEAR DOWN, WAITED A LONGER THAN NORMAL FOR 3 GREEN DOWN AND LOCKED INDICATIONS. DECLARED AN EMERGENCY AND LANDED. FLIGHT 3126 CLOSED "UPON INSPECTION OF AIRCRAFT FOUND NLG SHOCK STRUT
- [SDR SWIA2019121346868](https://openairdocs.org/sdr/SWIA2019121346868.md): Warning Message · false activation · Dec 13, 2019 · N754EV · Cndair CL6002C10 · Landing Gear Steering System
  > AFTER TAKE OFF RECEIVED STEERING IN-OP CAUTION MESSAGE, RAN QRH, RETURNED TO FIELD AND LANDED. LANDED WITHOUT NWS. FLIGHT 3126 CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 20065245 WITH THE FOLLOWING CORRECTIVE ACTION: "FOUND B1 CODE 007460 NGDL DIS

Next page: https://openairdocs.org/aircraft/N754EV/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 = 'N754EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N754EV/reports

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