# Service difficulty reports: N926EV

A list on [N926EV](https://openairdocs.org/aircraft/N926EV.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 · 195 reports

- [SDR SWIA202266418](https://openairdocs.org/sdr/SWIA202266418.md): None · failed · Sep 2, 2022 · N926EV · Cndair CL6002B19 · Pneumatic System
  > L 14TH DUCT WARNING INFLIGHT. QRH PROCEDURE DID NOT EXTINGUISH. (FLIGHT #4157 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25424973 WITH THE FOLLOWING CORRECTIVE ACTION: "VISUALLY INSPECTED LH 14TH STAGE DUCTING WHILE 14TH STAGE BLEED AIR SY
- [SDR SWIA202053949](https://openairdocs.org/sdr/SWIA202053949.md): Strap · corroded · Oct 16, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR STRAP AT FS 559.000 FROM RBL 27 TO PRESSURE FLOOR SILL IS CORRODED. C-CHECK RO 11/11/2020. REMOVED DAMAGED FLOOR STRAP AND INSTALLED A NEW PRESSURE FLOOR STRAP, IAW CRJ 200 SRM.
- [SDR SWIA202053890](https://openairdocs.org/sdr/SWIA202053890.md): Floorbeam · corroded · Oct 11, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > AT RBL 9 FS 513.00 INBOARD FLANGE OF FLOOR BEAM CORRODED. C-CHECK RO 11/11/2020. REPAIR WAS ACCOMPLISHED, IAW MHIRJ REO. NO WEIGHT AND BALANCE CHANGE REQUIRED. M-337 AND TASK CARD ATTACHED.
- [SDR SWIA202053948](https://openairdocs.org/sdr/SWIA202053948.md): Plate · corroded · Oct 3, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PLATE FOR PASSENGER DOOR FWD ANCHOR FITTING IS CORRODED. C-CHECK RO 11/11/2020. RECEIVED NEW PLATE VERIFIED TO BE P/N 600-38061-11 CRJ 200 AIPC, REF JOB 9784381 OP 139 MX TRANS NR 21619598 FOR PLATE INSTALLATION.
- [SDR SWIA202053926](https://openairdocs.org/sdr/SWIA202053926.md): Skin · loose · Sep 29, 2020 · N926EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RT OUTBOARD FLAP UPPER SKIN HAS LOOSE & SMOKING RIVETS ON THE AFT SPAR BETWEEEN F/STA 234 & 245 AND ON F/STA 245 BETWEEN AFT SPAR & TE. C-CHECK RO 11/11/2020. REPAIRED RT OUTBOARD FLAP UPPER SKIN, IAW REO. NO WEIGHT OR BALANCE CHANGE. M-337 AND TASK CARD A
- [SDR SWIA202053885](https://openairdocs.org/sdr/SWIA202053885.md): Former · corroded · Sep 25, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR FORMER 601R318078-3 TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED PAX DOOR FORMER AT FS 329.75, IAW CRJ 200 AMM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202053947](https://openairdocs.org/sdr/SWIA202053947.md): Nut · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LT FLAP HINGE BOX AT WS 220.00 NUT CORRODED ON AFT OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACED NUT P/N MS17825-7 ON LT HINGE BOX AT WS 220.00 OUTBOARD SIDE, IAW CRJ 200 AMM. REMOVED AND REPLACED NUT P/N MS17828-7 ON LT HINGE BOX AT
- [SDR SWIA202053946](https://openairdocs.org/sdr/SWIA202053946.md): Nut · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > RT FLAP HINGE BOX AT WS 220.00 NUT CORRODED ON AFT INBOARD AND OUTBOARD SIDE OF BRACKET AND FWD BRACKET. C-CHECK RO 11/11/2020. REMOVED AND REPLACED RT HINGE BOX AT WS 220.00, THE NUTS ON INBOARD AND OUTBOARD SIDE OF BRACKET AND THE FWD BRACKET, IAW CRJ 200
- [SDR SWIA202053945](https://openairdocs.org/sdr/SWIA202053945.md): Nut · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LT FLAP HINGE BOX AT WS 264.00 NUT CORRODED ON AFT INBOARD AND OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVED AND REPLACED LT HINGE BOX INBOARD & OUTBOARD NUTS (P/N MS17825-7) AT WS 264.00, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SE
- [SDR SWIA202053944](https://openairdocs.org/sdr/SWIA202053944.md): Nut · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > RT FLAP HINGE BOX AT WS 264.00 NUT CORRODED ON AFT INBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACE NUT ON RT FLAP HINGE BOX AT WS 264.00 ON AFT INBOARD SIDE OF BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPT 21.
- [SDR SWIA202053943](https://openairdocs.org/sdr/SWIA202053943.md): Bracket · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > RT FLAP HINGE BOX AT WS 178.00 NUT CORRODED ON AFT OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACE RT FLAP HINGE BOX AT WS 178.00 THE NUT ON THE AFT OUTBOARD SIDE OF THE BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEP
- [SDR SWIA202053942](https://openairdocs.org/sdr/SWIA202053942.md): Bracket · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR SURROUND STRUCTURE BRACKET CONNECTORS FWD AND AFT CORRODED BETWEEN FS 319.70 ND FS 333 AND BETWEEN STGR 17L AND STGR 18L. C-CHECK RO 11/11/2020. REMOVED FWD AND AFT CONNECTOR BRACKETS, IAW CRJ-200 SRM 51-42-06. LOCATED, DRILLED, AND INSTALLED NEW
- [SDR SWIA202053925](https://openairdocs.org/sdr/SWIA202053925.md): Fitting · cracked · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST LOWER FITTING IS CRACKED FROM THE LOWER VERTICAL EDGE TO THE FIRST LOWER FASTENER HOLE ON THE RT & LT SIDES. FAIL DETAILED VISUAL INSPECTION. C-CHECK RO 11/11/2020. REMOVED AND REPLACED WINDSHIELD CENTER POST RT AND LT LOWER FITTING F
- [SDR SWIA202053924](https://openairdocs.org/sdr/SWIA202053924.md): Angle · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE ANGLE CORRODED BETWEEN FS 310 AND FS 319.70 BETWEEN STGR 17L AND STGR18L. C-CHECK RO 11/11/2020. REMOVED DAMAGED PAX DOOR SURROUND STRUCTURE ANGLE AND INSTALLED A NEW ANGLE, IAW CRJ 200 SRM. COMPLETED TASK CARD FORM M-337 ATTACHE
- [SDR SWIA202053884](https://openairdocs.org/sdr/SWIA202053884.md): Intercostal · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR INTERCOSTAL DD4 TO BE CORRODED IN MULTIPLE LOCATIONS. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD4, IAW CRJ 200 SRM. COMPETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD F
- [SDR SWIA202053883](https://openairdocs.org/sdr/SWIA202053883.md): Former · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR AFT FORMER TO BE CORRODED IN MULTIPLE LOCATIONS. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR AFT FORMER, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FOR 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PE
- [SDR SWIA202053876](https://openairdocs.org/sdr/SWIA202053876.md): Floor Skin · corroded · Sep 24, 2020 · N926EV · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR SILL SKIN AT FS 518.00 AND FS 522.00 IS CORRODED. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL SKIN AT FS 518.00 AND FS 522.00 CORROSION, IAW BOMBARDIER REO. REFERANCE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202053923](https://openairdocs.org/sdr/SWIA202053923.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL IS CORRODED AT (2) LOCATIONS ON THE FLOOR SKIN, (1) LOCATION ON THE FLOOR DOUBLER AND THE FLOOR STRAP SPANNING LBL 27.00 AND FLOOR SILL IS CORRODED IN NUMEROUS LOCATIONS. DAMAGE IS BETWEEN FS 544.00 AND FS 559.00. C-CHECK RO 11/11/2020
- [SDR SWIA202053922](https://openairdocs.org/sdr/SWIA202053922.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL IS CORRODED AT (5) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 473.15 AND FS 513.00. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL AT (5) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 473.15 AND FS 513.00, IAW BOMBARDIER REO WEIGHT AND BA
- [SDR SWIA202053921](https://openairdocs.org/sdr/SWIA202053921.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL IS CORRODED AT (1) LOCATION ON THE FLOOR SKIN BETWEEN FS 449.85 AND FS 473.15. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (1) LOCATION ON THE FLOOR SKIN BETWEEN FS 449.85 AND FS 473.15, IAW BOMBARDIER REO. WEIG
- [SDR SWIA202053920](https://openairdocs.org/sdr/SWIA202053920.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SIL IS CORRODED AT (3) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 424.00 AND FS 449.85. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (3) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 424.00 AND FS 449.85, IAW BOMBARDIER REO. WEI
- [SDR SWIA202053919](https://openairdocs.org/sdr/SWIA202053919.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL IS CORRODED AT (2) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 409.00 AND FS 424.00. C-CHECK RO 11/11/2020. REMOVED LT PRESSURE FLOOR SILL CORROSION AT (2) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 409.00 AND FS 424.00, IAW BOMBARDIER REO. WE
- [SDR SWIA202053918](https://openairdocs.org/sdr/SWIA202053918.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT CABIN PRESSURE FLOOR SILL HAS (1) AREA OF CORROSION ON THE SILL SKIN, (1) AREA OF CORROSION ON THE SILL DOUBLER AND (1) AREA OF CORROSION ON THE FLOOR STRAP THAT SPANS RBL 27.00 AND THE PRESSURE FLOOR SILL. DAMAGE IS BETWEEN FS 544.00 AND FS 559.00. C-CHE
- [SDR SWIA202053917](https://openairdocs.org/sdr/SWIA202053917.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT PRESSURE FLOOR SILL HAS (3) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 529.00 AND FS 544.00. C-CHECK RO 11/11/2020. REPAIR WAS ACCOMPLISHED IAW BOMBARDIER REO. NO WEIGHT AND BALANCE CHANGE, M-337 AND TASK CARD ATTACHED.
- [SDR SWIA202053916](https://openairdocs.org/sdr/SWIA202053916.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT CABIN PRESSURE FLOOR SILL HAS (2) AREAS OF CORROSION ON THE SILL SKIN BEWTEEN FS 513.00 AND FS 529.00. C-CHECK RO 11/11/2020. REMOVED CORROSION AND TREATED AREA, IAW BOMBARDIER REO. NO WEIGHT AND BALANCE CHANGE. M-337 AND TASK CARD ATTACHED.
- [SDR SWIA202053915](https://openairdocs.org/sdr/SWIA202053915.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT CABIN PRESSURE FLOOR SILL HAS (4) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 484.00 AND FS 513.00. C-CHECK RO 11/11/2020. REPAIRED RT CABIN PRESSURE FLOOR SILL (4) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 484.00 AND FS 513.00. REMOVED CORROSION
- [SDR SWIA202053914](https://openairdocs.org/sdr/SWIA202053914.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT PRESSURE FLOOR SILL HAS (1) AREA OF CORROSION ON THE SILL SKIN AT FS 461.00. C-CHECK RO 11/11/2020. RT PRESSURE FLOOR SILL CORROSION WAS REMOVED AND TREATED, IAW BOMBARDIER REO, AS DOCUMENTED ON ATTACHED CONTINUATION CARD. NO WEIGHT AND BALANCE CHANGE, M
- [SDR SWIA202053913](https://openairdocs.org/sdr/SWIA202053913.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT PRESSURE FLOOR SILL HAS (3) AREAS OF CORROSION ON THE SILL SKIN BETWEEN FS 424.00 AND FS 439.00. C-CHECK RO 11/11/2020. REPAIR TO RT PRESSURE FLOOR SILL WAS COMPLETED, IAW BOMBARDIER REO, AS DOCUMENTED ON ATTACHED CONTINUATION CARD. M-337 AND TASK CARD A
- [SDR SWIA202053889](https://openairdocs.org/sdr/SWIA202053889.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL SKIN PANEL AT FS 473.15 LBL 36 IS CORRODED. C-CHECK RO 11/11/2020. COMPLIED WITH BOMBARDIER REO AND MHIRJ REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202053882](https://openairdocs.org/sdr/SWIA202053882.md): Door Frame · damaged · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND PAX DOOR FRAME ON FWD SIDE TO HAVE MULTIPLE OVERSIZED HOLES. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR FWD FRAME, IAW CRK 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK
- [SDR SWIA202053881](https://openairdocs.org/sdr/SWIA202053881.md): A/C Pack · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR LOWER AFT INTERCOSTAL TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVIEABLE PAX DOOR LOWER AFT INTERCOSTAL, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PE
- [SDR SWIA202053880](https://openairdocs.org/sdr/SWIA202053880.md): A/C Pack · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR INTERCOSTAL TO BE CORRODED ON AFT SIDE. C-CHECK RO 11/11/2020. INSTALLED SEVICABLE PAX DOOR INTERCOSTAL, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTIUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202053879](https://openairdocs.org/sdr/SWIA202053879.md): Intercostal · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR INTERCOSTAL DD3 TO BE CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD3, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTIUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202053878](https://openairdocs.org/sdr/SWIA202053878.md): Intercostal · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR INTERCOSTAL DD1 TO BE CORRODED ON AFT SIDE. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE PAX DOOR INTERCOSTAL DD1, IAW CRJ 200 SRM. COMPETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE, REFERENCE CONTINUATION CARD FOR WORK PE
- [SDR SWIA202053875](https://openairdocs.org/sdr/SWIA202053875.md): Floor Support · corroded · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL IS CORRODED AT (4) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 513.00 AND FS 544.00. C-CHECK RO 11/11/2020. REPAIRED LT PRESSURE FLOOR SILL CORROSION AT (4) LOCATIONS ON THE FLOOR SKIN BETWEEN FS 513.00 AND FS 544.00. REFERENCE CONTINUATIO
- [SDR SWIA202053868](https://openairdocs.org/sdr/SWIA202053868.md): Angle · cracked · Sep 23, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR LATCH BOX INBOARD ANGLE TO BE CRACKED. C-CHECK RO 11/11/2020. REMOVED AND REPLACED PAX DOOR LATCH LOCK BOX INBOARD ANGLE, IAW CRJ 200 SRM.
- [SDR SWIA202053941](https://openairdocs.org/sdr/SWIA202053941.md): Link · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Spoilers
  > LT OUTBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REPLACED LT OUTBOARD GROUND SPOILER PCU LINK HARDWARE PART NUMBERS NAS-6305U-19D AND NAS6205-12D PER CRJ200 AMM. TW SN 08158140 CAL DATE 16 MAR 20 CAL DUE 31 MAR 21.
- [SDR SWIA202053940](https://openairdocs.org/sdr/SWIA202053940.md): Bolt · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Wing, Attach Fittings
  > LT OUTBOARD GROUND SPOILER HINGE HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE LT WING OUTBOARD SPOILER INBOARD AND CENTER HINGES HARDWARE, IAW CRJ-200 AMM TASK.
- [SDR SWIA202053939](https://openairdocs.org/sdr/SWIA202053939.md): Link · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Spoilers
  > LT INBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REPLACED INBOARD GROUND SPOILER PCU LINK HARDWARE PART NUMBERS NAS-6305U-19D AND NAS6205-12D, REF CRJ200 AMM. TW SN 08158140 CAL DATE 16 MAR 20 CAL DUE 31 MAR 20.
- [SDR SWIA202053938](https://openairdocs.org/sdr/SWIA202053938.md): Hinge · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Spoilers
  > LT INBOARD GROUND SPOILER HAS CORRODED HINGE HARDWARE. C-CHECK RO 11/11/2020. INSTALLED SERVICABLE LT WING INBOARD SPOILER INBOARD AND CENTER HINGES HARDWARE, IAW CRJ-200 AMM TASK.
- [SDR SWIA202053937](https://openairdocs.org/sdr/SWIA202053937.md): Bolt · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Spoilers
  > RT OUTBOARD GROUND SPOILER PCU LINK HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. REMOVED AND REPLACED RT WING OUTBOARD GROUND SPOILER PCU LINK HARDWARE, IAW CRJ-200 AMM TASK.
- [SDR SWIA202053936](https://openairdocs.org/sdr/SWIA202053936.md): Bolt · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Wing, Attach Fittings
  > RT OUTBOARD GROUND SPOILER HAS CORRODED HINGE HARDWARE. C-CHECK RO 11/11/2020. INSTALLED SERVICEABLE RIGHT OUTBOARD GROUND SPOILER HINGE HARDWARE, IAW CRJ-200 AMM TASK. TORQUE WRENCH PN: WVACT204356, CALIBRATED DATE: 09-14-2020.
- [SDR SWIA202053935](https://openairdocs.org/sdr/SWIA202053935.md): Bolt · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Wing, Attach Fittings
  > RT INBOARD GROUND SPOILER PCU LINK HAS CORRODED HARDWARE. C-CHECK RO 11/11/2020. REMOVED AND REPLACED CORRODED HARDWARE ON INBOARD GROUND SPOILER PCU LINK WITH SERVICABLE P/N; NAS6305U19D, IAW CRJ-200 AMM TASK. CALIBRATED TOOL REQUIRED, TORQUE WRENCH WVACT
- [SDR SWIA202053934](https://openairdocs.org/sdr/SWIA202053934.md): Hinge · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Spoilers
  > RT INBOARD GROUND SPOILER HINGE HARDWARE IS CORRODED. C-CHECK RO 11/11/2020. REMOVED CORRODED HARDWARE AT RT INBOARD GROUND SPOILER HINGES AND REPLACED WITH SERVICABLE PARTS, IAW CRJ-200 AMM TASK. CALIBRATED TOOL REQUIRED, TORQUE WRENCH WVACT 0083 CAL 9/14/
- [SDR SWIA202053912](https://openairdocs.org/sdr/SWIA202053912.md): Hinge · gouged · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE SIDE OF PASSENGER DOOR HINGE, MOST AFT LANDING HAS A DEEP GOUGE AT A PREVIOUS REPAIR. C-CHECK RO 11/11/2020. REPAIRED FUSELAGE SIDE OF PASSENGER DOOR HINGE, IAW CRJ-200 AMM SRM, BOMBARDIER REO, AND MHIRJ REO. REFERENCE CONTINUATION CARD FOR WORK PE
- [SDR SWIA202053895](https://openairdocs.org/sdr/SWIA202053895.md): Floor Support · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT CABIN FLOOR BEAM ON RBL 9.00 HAS A HOLE CORRODED THROUGH IT AND NUMEROUS OTHER LOCATIONS WITH HEAVY CORROSION BETWEEN FS 409.00 TO FS 409.00+128. C-CHECK RO 11/11/2020. REPAIRED RT CABIN FLOOR BEAM AT RBL 9.00, HOLE CORRODED THROUGH IT AND NUMEROUS OTHER
- [SDR SWIA202053874](https://openairdocs.org/sdr/SWIA202053874.md): Cup · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HAND RAIL STOW CUPS ARE CORRODED. C-CHECK RO 11/11/2020. LOCATED, DRILLED, AND INSTALLED NEW FWD AND AFT STOW CUP ASSEMBLY'S, IAW CRJ-200 SRM.
- [SDR SWIA202053870](https://openairdocs.org/sdr/SWIA202053870.md): Frame · corroded · Sep 22, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 409.00 IS CORRODED ON THE FORWARD SIDE ON THE FRAME DOUBLER BETWEEN STR 26 AND STR 27 AND ON THE AFT SIDE ON THE FRAME DOUBLER. C-CHECK RO 11/11/2020. REMOVED UNSERVICEABLE FS 409.00 FRAME DOUBLER BETWEEN STR 26 AND STR 27 AND AFT SIDE ANGLE ON THE FRAME
- [SDR SWIA202053933](https://openairdocs.org/sdr/SWIA202053933.md): Floorbeam · corroded · Sep 21, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR CROSSBEAM CAP BETWEEN LBL 9.00 AND LBL 27.00 AT FS 589.00 IS CORRODED. C-CHECK RO 11/11/2020. REPLACED UNSERVICEABLE FLOOR CROSSBEAM CAP AT FS 589 BETWEEN LBL 9 AND LBL 27, IAW CRJ200 SRM.
- [SDR SWIA202053932](https://openairdocs.org/sdr/SWIA202053932.md): Floorbeam · corroded · Sep 21, 2020 · N926EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR CROSSBEAM CAP IS CORRODED BETWEEN RBL 9.00 AND LBL 9.00 AT FS 559.00+80. C-CHECK RO 11/11/2020. REMOVED CORRODED CROSS BEAM CAP, INSTALLED NEW SERVICEABLE FLOOR CROSSBEAM CAP BETWEEN RBL 9.00 AND LBL 9.00 AT FS 559.00+80, IAW CRJ 200 SRM REFERENCE CONT

Next page: https://openairdocs.org/aircraft/N926EV/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 = 'N926EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N926EV/reports

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