# Service difficulty reports: N922EV

A list on [N922EV](https://openairdocs.org/aircraft/N922EV.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 · 159 reports

- [SDR SWIA202055255](https://openairdocs.org/sdr/SWIA202055255.md): Skin · dented · Dec 28, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 550059. DENT BETWEEN FS 640 AND 672.2 HAS LARGE DENT APPROXIMATELY 6.4 X 6.3 INCHES WITH HOLE IN CENTER APPROXIMATELY 2.6 X 1.8 INCHES. LT FUSELAGE STRUCTURE DAMAGE BETWEEN FS 640.00 AND FS 672.20, STR 13L AND 16L WAS REPAIRED BY BOMBARDI
- [SDR SWIA202053519](https://openairdocs.org/sdr/SWIA202053519.md): Bulkhead · damaged · Sep 29, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > EVALUATE RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOOLING DAMAGE TO RT 9G BULKHEAD AFT WALL. REPAIR DOUBLER M
- [SDR SWIA202053518](https://openairdocs.org/sdr/SWIA202053518.md): Bulkhead · damaged · Sep 29, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > EVALUATE CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE TO CENTER 9G BULKHEAD AFT WALL. REPAIR DO
- [SDR SWIA202053517](https://openairdocs.org/sdr/SWIA202053517.md): Bulkhead · damaged · Sep 29, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > EVALUATE LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL NR 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE TO LT 9G BULKHEAD AFT WALL. REPAIR DOUBLER
- [SDR SWIA202053513](https://openairdocs.org/sdr/SWIA202053513.md): Floorbeam · corroded · Sep 27, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT PLATE AT FS 559+48 BETWEEN RBL 9 AND RBL 27 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FS 559+48 BETWEEN RBL 9 AND RBL 27, IAW CRJ 200 SRM. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202053512](https://openairdocs.org/sdr/SWIA202053512.md): Control Rod · corroded · Sep 23, 2020 · N922EV · Cndair CL6002B19 · Elevator Control System
  > RT ELEVATOR SYSTEM MECHANICAL CONTROL PATH INPUT ROD BEARING AND HARDWARE LOCATED AFT END OF VERTICAL STABILIZER CANTED RIB APPEARS TO HAVE CORROSION (RUST). C-CHECK RO 10/18/2020. REMOVED AND REPLACED LT ELEVATOR CONTROL PATH INPUT ROD AND FWD AND AFT HARDW
- [SDR SWIA202053511](https://openairdocs.org/sdr/SWIA202053511.md): Control Rod · corroded · Sep 23, 2020 · N922EV · Cndair CL6002B19 · Elevator Control System
  > LT ELEVATOR SYSTEM MECHANICAL CONTROL PATH INPUT ROD BEARING AND HARDWARE LOCATED AFT END OF VERTICAL STABILIZER CANTED RIB APPEARS TO HAVE CORROSION (RUST). C-CHECK RO 10/18/2020. REMOVED AND REPLACED LT ELEVATOR CONTROL PATH INPUT ROD AND FWD AND AFT HARDW
- [SDR SWIA202053498](https://openairdocs.org/sdr/SWIA202053498.md): Window Post · cracked · Sep 18, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RT WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. C-CHECK RO 10/18/2020. REMOVED DAMAGED RT WINDSHIELD SIDE POST LOWER AFT FITTING. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE FITTING, IAW CRJ200-SRM.
- [SDR SWIA202053497](https://openairdocs.org/sdr/SWIA202053497.md): Window Post · chafed · Sep 18, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Structure
  > STRAP ON WINDSHIELD CENTER POST, ATTACHING CENTER POST TO CENTER SUPPORT CLIPS FOUND TO BE CHAFED. CAUSED BY CRACKED LT SUPPORT CLIP, P/N 601R34012-25. C-CHECK RO 10/18/2020. REMOVED DAMAGED WINDSHIELD CENTER POST STRAP AND INSTALLED NEW SERVICEABLE STRAP,
- [SDR SWIA202053496](https://openairdocs.org/sdr/SWIA202053496.md): Angle · cracked · Sep 16, 2020 · N922EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > UPPER ANGLE COMMON TO THE LT INBOARD BATTERY RIB AT WS 48.30 IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLE, IAW CRJ 200 SRMS. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202053489](https://openairdocs.org/sdr/SWIA202053489.md): Fitting · cracked · Sep 16, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER SUPPORT CLIPS ON THE LT AND RT SIDE ARE CRACKED. C-CHECK RO 10/18/2020. REMOVED DAMAGED WINDSHIELD CENTER SUPPORT CLIPS ON THE LT AND RT SIDE AND INSTALLED NEW SERVICEABLE CLIPS, IAW CRJ200.
- [SDR SWIA202053510](https://openairdocs.org/sdr/SWIA202053510.md): Floorbeam · corroded · Sep 15, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 559.0+80 CROSS BEAM RBL 9 TO RBL 27 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FS 559.0+80 ON TOP OF CROSS BEAM RBL 9 TO RBL 27, IAW CRJ 200 SRM.
- [SDR SWIA202053495](https://openairdocs.org/sdr/SWIA202053495.md): Counterbalance · cracked · Sep 15, 2020 · N922EV · Cndair CL6002B19 · Passenger/Crew Doors
  > AFT ANCHOR FITTING FOR PASSENGER DOOR COUNTERBALANCE IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED PAX DOOR ANCHOR FITTING, IAW CRJ 200 AMM.
- [SDR SWIA202053509](https://openairdocs.org/sdr/SWIA202053509.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 27 SEAT TRACK IS CORRODED FROM FS 559.0+80 TO FS 559.0+96. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK FROM FS 559.0+80 TO FS 559.0+96 AT RBL 27, IAW CRJ 200.
- [SDR SWIA202053508](https://openairdocs.org/sdr/SWIA202053508.md): Floor Support · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 559.0+96 TO FS 559.0+112. C-CHECK RO 10/18/2020. REMOVED FABRICATED OUT OF N126-1577 EXTRUSION AND INSTALLED NEW RBL 9 FLOOR BEAM CAP BETWEEN FS 559.0+96 TO FS 559+112, IAW CRJ 200 SRM & IAW MHIRJ REO. REF ATTACHED CO
- [SDR SWIA202053507](https://openairdocs.org/sdr/SWIA202053507.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK ON RBL 9 BETWEEN FS 559.0+80 TO FS 559.0+96 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK ON RBL 9 BETWEEN FS 559.0+80 TO FS 559.0+96, IAW CRJ 200 AMM.
- [SDR SWIA202053506](https://openairdocs.org/sdr/SWIA202053506.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 574 TO FS 559.0+112. C-CHECK RO 10/18/2020. REMOVED AND REPLACED CORRODED SEAT TRACK, IAW CRJ200 AMM. USED TOOL WVACT 6025 CAL DUE 31 MAR 2021.
- [SDR SWIA202053505](https://openairdocs.org/sdr/SWIA202053505.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 FLOOR SEAT RAIL IS CORRODED BETWEEN FS 559.0+80 TO 559.0+96. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT RAIL BETWEEN LBL 27 BETWEEN FS 559.0+80 TO 559.0+96, IAW CRJ 200 AMM.
- [SDR SWIA202053504](https://openairdocs.org/sdr/SWIA202053504.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN FS 559.00+112 TO FS 574. C-CHECK RO 10/18/2020. REMOVED AND REPLACED LBL 9 CARGO SEAT TRACK, IAW AMM.
- [SDR SWIA202053494](https://openairdocs.org/sdr/SWIA202053494.md): Attach Angle · cracked · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBOARD AND OUTBOARD ANGLE ATTACHING TO FS 484 INTERCOSTAL BETWEEN PRESSURE FLOOR BEAM RBL 27 AND RBL 36 ARE CRACKED AT UPPER EDGE AT FASTENER HOLE. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLES, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORM
- [SDR SWIA202053493](https://openairdocs.org/sdr/SWIA202053493.md): Attach Angle · cracked · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > INBOARD AND OUTBOARD ANGLE ATTACHING TO FS 484 INTERCOSTAL BETWEEN PRESSURE FLOOR BEAM LBL 27 AND LBL 36 ARE CRACKED AT UPPER EDGE AT FASTENER HOLE. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLES, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORM
- [SDR SWIA202053488](https://openairdocs.org/sdr/SWIA202053488.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT RBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED AT MULTIPLE LOCATIONS. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK, IAW CRJ 200 AMM & REO. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202053487](https://openairdocs.org/sdr/SWIA202053487.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED MULTIPLE LOCATIONS. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK, IAW CRJ 200 AMM & REO. REFER TO CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202053486](https://openairdocs.org/sdr/SWIA202053486.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 364 TO FS 400 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 364 AND FS 400, IAW CRJ 200 AMM. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202053485](https://openairdocs.org/sdr/SWIA202053485.md): Seat Track · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT RBL 9 BETWEEN FS 364 TO FS 400 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND REPLACED SEAT TRACK, IAW CRJ 200 SRM & REO. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202053484](https://openairdocs.org/sdr/SWIA202053484.md): Floorbeam · cracked · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > INBOARD AND OUTBORD ANGLES ATTACHING THE LBL 9 FLOOR BEAM AT FS 280 CROSSBEAM ARE CRACKED IN UPPER RADIUS. C-CHECK RO 10/18/2020. REMOVED AND REPLACED CRACKED CLIPS 2 EA AT STA 280 LBL 9, IAW CRJ200 SRM.
- [SDR SWIA202053480](https://openairdocs.org/sdr/SWIA202053480.md): Floor Support · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT LBL 9 UPPER INBOARD FLANGE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED FLOORBEAM, IAW REO. WEIGHT CHANGE +1.55 LB. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. REFER TO CONTINUE CA
- [SDR SWIA202053476](https://openairdocs.org/sdr/SWIA202053476.md): Frame · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR FS 349 IS CORRODED BETWEEN STRINGERS 25L TO 26R. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FRAME SECTOR FS 349 BETWEEN STRINGERS 25L AND 26R, IAW CRJ 200 SRM. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202053474](https://openairdocs.org/sdr/SWIA202053474.md): Floor Support · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED RT SIDE PRESSURE FLOOR SILL CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559, IAW REO. MAJOR REPAIR TASK CARD & FORM M337 COMPL
- [SDR SWIA202053473](https://openairdocs.org/sdr/SWIA202053473.md): Floor Support · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT RBL 9 UPPER INBOARD FLANGE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559 AND OUTBOARD FLANGE IS CORRODED AT 1 LOCATION AT FS 559. C-CHECK RO 10/18/2020. REPAIRED FLOOR BEAM AT RBL 9 UPPER INBOARD FLANGE CORROSION AT MULTIPLE LO
- [SDR SWIA202053472](https://openairdocs.org/sdr/SWIA202053472.md): Floor Support · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE PRESSURE FLOOR SILL HAS CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED LEFT SIDE PRESSURE FLOOR SILL CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559, IAW REO. COMPLETED AND ATTACHED TAS
- [SDR SWIA202053471](https://openairdocs.org/sdr/SWIA202053471.md): Floor Support · corroded · Sep 14, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM LBL 9 UPPER INBOARD FLANGE IS CORRODED AT APPROXIMATELY FS 409+30, FS 409+60 AND FS 409+118. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND REPLACED/INSTALLED FLOORBEAM CAP, IAW REO CRJ 200 SRMS. MAJOR REPAIR TASK & FORM 337 COMPLETED AND ATTACH
- [SDR SWIA202053492](https://openairdocs.org/sdr/SWIA202053492.md): Bracket · cracked · Sep 13, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OBLIQUE ANGLE IS CRACKED IN RADIUS AT STRINGER 14R AFT SIDE OF FS 621 BULKHEAD. C-CHECK RO 10/18/2020. REMOVED AND REPLACED OBLIQUE ANGLE AT STRINGER 14R ON AFT SIDE OF FS 621 BULKHEAD, IAW BOMBARDIER REO.
- [SDR SWIA202053491](https://openairdocs.org/sdr/SWIA202053491.md): Angle · cracked · Sep 13, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OBLIQUE ANGLE IS CRACKED IN RADIUS AT STRINGER 14L AFT SIDE OF FS 621 BULKHEAD. C-CHECK RO 10/18/2020. REMOVED AND REPLACED OBLIQUE ANGLE AT STRINGER 14L AFT SIDE OF FS 621 BULKHEAD, IAW BOMBARDIER REO.
- [SDR SWIA202053503](https://openairdocs.org/sdr/SWIA202053503.md): Gusset · corroded · Sep 11, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR SURROUND STRUCTURE GUSSET CORRODED AT FS 349 AT STGR 15L. C-CHECK RO 10/18/2020. REMOVE AND REPLACED PAX DOOR SURROUND STRUCTURE GUSSET AT FS 349 AT STR 15L, IAW CRJ SRM.
- [SDR SWIA202053502](https://openairdocs.org/sdr/SWIA202053502.md): Gusset · corroded · Sep 11, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR SURROUND STRUCTURE GUSSET CORRODED BETWEEN STGR 15L AND STGR 16L AT FS 310. C-CHECK RO 10/18/2020. REMOVED AND REPLACED GUSSET, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202053501](https://openairdocs.org/sdr/SWIA202053501.md): Hinge · corroded · Sep 11, 2020 · N922EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR FWD AND AFT HINGE CUPS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FWD AND AFT HINGE CUPS AT PAX DOOR LOWER SILL, IAW CRJ 200 SRM.
- [SDR SWIA202053475](https://openairdocs.org/sdr/SWIA202053475.md): Floorbeam · corroded · Sep 11, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SERVICE DOOR FLOOR BEAM ANGLE CORRODED AT STGR 18 AND AT FS 349. C-CHECK RO 10/18/2020. REPAIRED SERVICE DOOR FLOOR BEAM ANGLE AT STGR 18 AT FS 349, IAW REO. SEE ATTACHED STRUCTURAL MAJOR REPAIR TASK CARD AND CONTINUE CARD FOR DETAILS OF WORK PERFORMED. NO
- [SDR SWIA202053500](https://openairdocs.org/sdr/SWIA202053500.md): Intercostal · corroded · Sep 10, 2020 · N922EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD6 CORRODED. C-CHECK RO 10/18/2020. REPAIRED IAW REO. MAJOR REPAIR TASK CARD AND FORM M337 ATTACHED. NO MEASURABLE WEIGHT CHANGE REQUIRED. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202053483](https://openairdocs.org/sdr/SWIA202053483.md): Bracket · cracked · Sep 10, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT MLG WHEEL WELL FWD HYDRAULIC FUSE BRACKET IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED BRACKET AT RT MLG WHEEL WELL FWD HYDRAULIC FUSE, IAW CRJ200 SRM.
- [SDR SWIA202053482](https://openairdocs.org/sdr/SWIA202053482.md): Bracket · cracked · Sep 10, 2020 · N922EV · Cndair CL6002B19 · Wing, Attach Fittings
  > LT MLG WHEEL WELL FWD HYDRAULIC FUSE BRACKET IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED HYD FUSE BRACKET, IAW CRJ200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202053490](https://openairdocs.org/sdr/SWIA202053490.md): Support · cracked · Sep 9, 2020 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT WINDSHIELD SIDE POST SUPPORT P/N 601R34032-21 IS CRACKED AT THE RADIUS ABOVE STRINGER. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SUPPORT, IAW CRJ 200 SRM. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, WAS A PART FOR PART
- [SDR SWIA202053470](https://openairdocs.org/sdr/SWIA202053470.md): Support · cracked · Sep 9, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT WINDSHIELD SIDE POST SUPPORT P/N 601R34032-22 IS CRACKED IN THE RADIUS ABOVE THE STRINGER. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SUPPORT, IAW CRJ 200 SRM. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, WAS A PART FOR
- [SDR SWIA202053499](https://openairdocs.org/sdr/SWIA202053499.md): Skin · corroded · Sep 8, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND MINOR EXTERNAL SKIN CORROSION ON BELLY SKIN PANEL FS 559.00+92 TO FS 559.00+112 BETWEEN STGR 26L AND 26R. C-CHECK RO 10/18/2020. REPAIRED IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASURABLE WEIGHT CHANGE. REFER TO CONTINUE
- [SDR SWIA202053481](https://openairdocs.org/sdr/SWIA202053481.md): Angle · cracked · Sep 8, 2020 · N922EV · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RT WHEEL WELL AT WS 50.54 THERE IS A CRACKED ANGLE. C-CHECK RO 10/18/2020. REMOVED DAMAGED ANGLE IN RT WHEEL WELL AT WS 50.54. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ200-SRM.
- [SDR SWIA202053479](https://openairdocs.org/sdr/SWIA202053479.md): Access Panel · corroded · Sep 6, 2020 · N922EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER SKIN FUEL PANEL ACCESS PANEL CUT OUT 640BB IS CORRODED AROUND CIRFUMFERENCE. C-CHECK RO 10/18/2020. REPAIRED RT WING LOWER SKIN FUEL PANEL ACCESS PANEL CUT OUT 640BB IS CORRODED AROUND CIRFUMFERENCE. BOMBARDIER REO IT WAS IN THE CRITICAL AREA.
- [SDR SWIA202053477](https://openairdocs.org/sdr/SWIA202053477.md): Access Panel · corroded · Sep 6, 2020 · N922EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING LOWER WING PLANK ACCESS PANEL CUTOUT AT 510AB IS CORRODED AROUND THE CIRCUMFERENCE. C-CHECK RO 10/18/2020. REPAIRED LT WING PLANK ACCESS PANEL CUTOUT AT 510AB CORROSION, IAW MHIRJ REO AND BOMARDIER REO. SPECIAL INSPECTION PER NDTM IS DUE AT 62883 FL
- [SDR SWIA202053469](https://openairdocs.org/sdr/SWIA202053469.md): Skin · chafed · Sep 6, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LOWER WING PLANK HAS MINOR CHAFING DAMAGE FROM FUSELAGE FAIRING AT AT BOTH LBL 45 AND RBL 45 AT APPROXIMATELY FS 513. C-CHECK RO 10/18/2020. REPAIRED IAW REO. NO MEASUREABLE WEIGHT CHANGES. MAJOR REPAIR TASK CARD & FORM M337 COMPLETED AND ATTACHED. REFER
- [SDR SWIA202053516](https://openairdocs.org/sdr/SWIA202053516.md): Bulkhead · chafed · Sep 5, 2020 · N922EV · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > RT ENGINE NOSE INLET AFT BULKHEAD INSPECTION HOLES AT 7, 10, AND 12 O`CLOCK POSITIONS ARE CHAFED AND HAVE BENT/MISSING INSPECTION DOORS. C-CHECK RO 10/18/2020. REPAIRED RT ENGINE NOSE INLET AFT BULKHEAD INSPECTION HOLES AT 7, 10, AND 12 O`CLOCK POSITIONS ARE
- [SDR SWIA202053478](https://openairdocs.org/sdr/SWIA202053478.md): Skin · dented · Sep 3, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ADM NR N922EV-6861. THE DENT IS ON THE LT SIDE OF THE FUSELAGE AT FS 262.00 AND APPROXIMATELY 35 INCHES DOWN FROM WL 73.50. THE DAMAGE IS A DENT WITH A LENGTH OF 0.975 INCHES AND A WIDTH OF 0.446 INCHES. THE DEPTH OF THE DENT IS 0.012 INCHES. PLOT, MAP, AN

Next page: https://openairdocs.org/aircraft/N922EV/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 = 'N922EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N922EV/reports

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