# Service difficulty reports: N455CA

A list on [N455CA](https://openairdocs.org/aircraft/N455CA.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 5 · 201 reports

- [SDR SWIA2020020748316](https://openairdocs.org/sdr/SWIA2020020748316.md): Control Unit · failed · Feb 7, 2020 · N455CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION WHEN EXTENDING FLAPS ON FINAL APPROACH. EXTENDED FLAPS TO 20 DEGREES. RECEIEVED FLAPS FAIL CAUTION AND NOTED THE FLAPS AT 5 DEGREES. MOVED FLAP LEVER TO ZERO DEGREE DETENT PER QRH. FLAPS DID NOT MOVE. TRI RUNWAY NOT OF SUFFICIANT LENGTH. DI
- [SDR SWIA2020012147958](https://openairdocs.org/sdr/SWIA2020012147958.md): Insert · debonded · Jan 16, 2020 · N455CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LH 9G BULKHEAD TOP INSERTS FOR PBE MOUNT BRACKET ARE DEBONDED AND STRIPPED. (C-CHECK) RO:1/17/2020REPLACED / INSTALLED 2EA. INSERTS P/N NAS1835-3 AT LH 9G BULKHEAD TOP PBE MOUNT BRACKET PER. C&D ZODIAC REPAIR PROCEDURE MANUAL.
- [SDR SWIA2020012147957](https://openairdocs.org/sdr/SWIA2020012147957.md): Beam · corroded · Jan 13, 2020 · N455CA · Cndair CL6002B19 · Aerodynamic Fairings
  > *AFT FAIRING BEAM IS CORRODED ON LOWER FLANGE, FS559.00+80 - FS568..00 STGR23R. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED WITH NEW AFT FAIRING SUPPORT BEAM AT FS559+80 TO FS568 STRG23R REF CRJ-200 SRM AND BOMBARDIER DWG.
- [SDR SWIA2020012147956](https://openairdocs.org/sdr/SWIA2020012147956.md): Support Angle · damaged · Jan 12, 2020 · N455CA · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > DURING RH PYLON DENT REPAIR ON REMOVAL DAMAGED UPPER PYLON SUPPORT ANGLE (C-CHECK) RO:1/17/2020REMOVED AND REPLACED WITH NEW SUPPORT ANGLE RH PYLON COMMON TO FUSELAGE SKIN REF CRJ-200 SRM BOMBARDIER REO AND BOMBARDIER DWG PRESSURE CHECK GOOD
- [SDR SWIA2020012147955](https://openairdocs.org/sdr/SWIA2020012147955.md): Floor Support · corroded · Jan 8, 2020 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PASSENGER CABIN FLOOR SUPPORT STRUCTURE RBL9 BETWEEN FS409.0 AND 409+112 HAS AREAS OF CORROSION AT FASTENER HOLES. (C-CHECK) RO:1/17/2020FOUND MULTIPLE LOCATION WITH 100% MATERIAL LOSS, CORROSION IS PRESENT ON MORE THAN 50% OF THE LENGTH OF PART. OUT
- [SDR SWIA2020012147954](https://openairdocs.org/sdr/SWIA2020012147954.md): Panel · cracked · Jan 7, 2020 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 326CT (STINGER PANEL) CONDUIT IS CRACKED AND STRIPPED. (C-CHECK) RO:1/17/2020ORDERED AND RECIEVED NEW CONDUIT TUBE PN# 600-56153-23 AND 2 NEW NUTS FOR PANEL 326CT. SEE JOB# 2759260 JOB# 7003.
- [SDR SWIA2020012147953](https://openairdocs.org/sdr/SWIA2020012147953.md): Lever · cracked · Jan 3, 2020 · N455CA · Cndair CL6002B19 · Wing, Attach Fittings
  > RH FLAP POSITION TRANSMITTER LEVER ARM CRACKED. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED WITH A SERVICEABLE UNIT P/N 601R93030-3. REF: CRJ200 AMM OPERATIONAL TEST GOOD. REF: CRJ200 AMM
- [SDR SWIA2020012147952](https://openairdocs.org/sdr/SWIA2020012147952.md): Anchor Fitting · corroded · Dec 30, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > UPON REMOVAL OF THE SERRATED MOUNT PLATE FOR THE PAX DOOR AFT ANCHOR FITTING FOUND CORROSION ON THE ANCHOR FITTING SERRATIONS (C-CHECK) RO:1/17/2020INSTALLED NEW PAX DOOR ANCHOR FITTING P/N 601R31976-9 REF CRJ 200 AMM ADJUSTMENT CHECK GOOD
- [SDR SWIA2020012147951](https://openairdocs.org/sdr/SWIA2020012147951.md): Door · worn · Dec 29, 2019 · N455CA · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE WORN BUTE DOOR CAM ON L/H OUTBOARD FLAP VANE AT WS296. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW BUTE DOOR CAM P/N 601R14560-5 ON L/H OUTBOARD FLAP VANE. REF: DWG AND SWA M-337.
- [SDR SWIA2020012147950](https://openairdocs.org/sdr/SWIA2020012147950.md): Lever · chafed · Dec 28, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR FWD LEVER MECHANISM IS CHAFFED. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED THE PAX DOOR FWD PULL IN LEVER REF CRJ 200 AMM. PERFORMED ADJUSTMENT OF THE PAX DOOR REF CRJ 200 AMM. ALL CHECKS GOOD.
- [SDR SWIA2020012147949](https://openairdocs.org/sdr/SWIA2020012147949.md): Stiffener · cracked · Dec 27, 2019 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H OVERWING EXTERNAL FUSELAGE HAS 2 EA VERTICAL STIFFENERS AT FS449.85 LBL45 AND FS461.00 LBL45 CRACKED AT THE RADIUS. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED THE 2 EACH VERTICAL STIFFENERS AT FS449.85 LBL45 AND FS461.00 LBL45, OVER WING ON THE L/H
- [SDR SWIA2020012147948](https://openairdocs.org/sdr/SWIA2020012147948.md): Door Sill · corroded · Dec 23, 2019 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL HAS CORROSION (MARKED) (C-CHECK) RO:1/17/2020REMOVED, REPLACED AND INSTALLED NEW PAX DOOR LOWER SILL ANGLE REF CRJ 200 SRM AND REF BOMBARDIER DWG.
- [SDR SWIA2020012147947](https://openairdocs.org/sdr/SWIA2020012147947.md): Skin · chafed · Dec 22, 2019 · N455CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RH FLAP UPPER SKIN PANELS 684AT AND 684BT ARE CHAFFED. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED 2 EA NEW PANELS 684AT AND 684BT. REF CRJ 200 SRM. / FABRICATED NEW PANELS P/N 601R14007-52 (684AT) AND 601R14007-54 (684BT) USING 2024-T3.080" PO# T522
- [SDR SWIA2020012147946](https://openairdocs.org/sdr/SWIA2020012147946.md): Floorbeam · cracked · Dec 20, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > INBOARD CLIP AT RBL9 FS 280 PART# 601R31113-58 IS CRACKED. (C-CHECK) RO:1/17/2020REMOVED, REPLACED AND INSTALLED NEW CLIP P/N 601R31113-58 AT FS 280 RBL 9 REF BOMBARDIER REO.
- [SDR SWIA2020012147942](https://openairdocs.org/sdr/SWIA2020012147942.md): Stiffener · cracked · Dec 19, 2019 · N455CA · Cndair CL6002B19 · Wing Miscellaneous Structure
  > * INSIDE WHEEL WELL R/H SIDE AFT SPAR AREA AT WS 48.30 BATT RIB STIFFNER HAS CRACK. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED A NEW BATT RIB STIFFENER ON RH SIDE AFT SPAR AREA AT WS 48.30 REF DWG AND CRJ 200 SRM.
- [SDR SWIA2020012147938](https://openairdocs.org/sdr/SWIA2020012147938.md): Floor Skin · cracked · Dec 17, 2019 · N455CA · Cndair CL6002B19 · Fuselage Floor Panel
  > PERFORM F.S 460 PRESSURE FLOOR SKIN CRACK REPAIR BETWEEN LBL 9 AND RBL 9. (CRACKS FOUND ON MX TRANS#20064218 AND MX TRANS#20064231) (C-CHECK) RO:1/17/2020PERFORMED F.S 460 PRESSURE FLOOR SKIN CRACK REPAIR BETWEEN LBL 9 AND RBL 9. REF. BOMBARDIER REO. R
- [SDR SWIA2020012147937](https://openairdocs.org/sdr/SWIA2020012147937.md): Hinge Fitting · gouged · Dec 16, 2019 · N455CA · Cndair CL6002B19 · Elevator Structure
  > L/H ELEVATOR INBD HINGE FITTING REQUIRES REPLACEMENT DUE TO PITTING IN BEARING BORE. (C-CHECK) RO:1/17/2020REPLACED L/H ELAVATOR HINGE FITTING WITH NEW P/N 600-24043-1 REF BOMBARDIER DWG#.
- [SDR SWIA2020012147936](https://openairdocs.org/sdr/SWIA2020012147936.md): Frame · cracked · Dec 13, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Frame
  > *FRAME CRACKED ABOVE PAX DOOR AT FS333 BETWEEN STGR0 AND STGR1L (C-CHECK) RO:1/17/2020 / VERIFIED THE FRAME CRACK. REMOVED FRAME REF CRJ 200 SRM 51-42-06. INSTALLED NEW FRAME SECTOR AT FS333 BETWEEN STGR 0 AND STGR 1L REF DWG AND SRM.
- [SDR SWIA2020012147935](https://openairdocs.org/sdr/SWIA2020012147935.md): Plate · corroded · Dec 13, 2019 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF SERATED MOUNT PLATE FOR PAX DOOR FWD ANCOR FITTING, BRACKET ATTACHING TO FS310 UNDER SERATED MOUNT PLATE HAS CORROSION. (C-CHECK) RO:1/17/2020REMOVED, REPLACED AND INSTALLED NEW GUSSET AT FS 310 REF CRJ 200 SRM 51-42-06, REO AND BOMBARD
- [SDR SWIA2020012147934](https://openairdocs.org/sdr/SWIA2020012147934.md): Skin · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > * THE RH WING LOWER WING PLANK ACCESS HOLE FOR PANEL 650HB HAS CORROSION. (C-CHECK) RO:1/17/2020REPAIRED PITTING CORROSION R/H LOWER WING PLANK ACCESS HOLE 650HB IN ACCORDANCE WITH REO ALL CHECKS GOOD
- [SDR SWIA2020012147933](https://openairdocs.org/sdr/SWIA2020012147933.md): Skin · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > * THE RH WING LOWER WING PLANK ACCESS HOLE FOR PANEL 650GB HAS CORROSION. (C-CHECK) RO:1/17/2020REPAIRED PITTING CORROSION R/H LOWER WING PLANK ACCESS HOLE 550GB IN ACCORDANCE WITH REO.
- [SDR SWIA2020012147932](https://openairdocs.org/sdr/SWIA2020012147932.md): Skin · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > * THE RH WING LOWER WING PLANK ACCESS HOLE FOR PANEL 640FB HAS CORROSION. (C-CHECK) RO:1/17/2020REPAIRED PITTING CORROSION R/H LOWER WING PLANK ACCESS HOLE 640FB IN ACCORDANCE WITH REO. ALL CHECKS GOOD
- [SDR SWIA2020012147931](https://openairdocs.org/sdr/SWIA2020012147931.md): Skin · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > * THE RH WING LOWER WING PLANK ACCESS HOLE FOR PANEL 640EB HAS CORROSION. (C-CHECK) RO:1/17/2020REPAIRED PITTING CORROSION R/H LOWER WING PLANK ACCESS HOLE 640EB IN ACCORDANCE WITH REO. ALL CHECKS GOOD AT THIS TIME.
- [SDR SWIA2020012147930](https://openairdocs.org/sdr/SWIA2020012147930.md): Skin · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > * THE RH WING LOWER WING PLANK ACCESS HOLE FOR PANEL 640BB HAS CORROSION. (C-CHECK) RO:1/17/2020REPAIRED PITTING CORROSION R/H LOWER WING PLANK ACCESS HOLE 640BB IN ACCORDANCE WITH REO. BONDING TEST GOOD.
- [SDR SWIA2020012147929](https://openairdocs.org/sdr/SWIA2020012147929.md): Check Valve · inoperative · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LH SIDE PRESSURE BULKHEAD CHECK VALVE (FLIGHT COMPARTMENT DISTRIBUTION SYSTEM) FLAPERS DO NOT CLOSE. (C-CHECK) RO:1/17/2020REMOVED LH SIDE PRESSURE BULKHEAD CHECK VALVE REF CRJ 200 AMM. INSTALLED NEW 1EA LH SIDE PRESSURE BULKHEAD CHECK VALVE AND 3EA
- [SDR SWIA2020012147928](https://openairdocs.org/sdr/SWIA2020012147928.md): Skin · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > * THE LH WING LOWER WING PLANK ACCESS HOLE FOR PANEL 550HB HAS CORROSION. (C-CHECK) RO:1/17/2020REPAIRED AN AREA OF CORROSION ON THE LOWER L/H WING PLANK CUTOUT AT PANEL (550HB) LOCATION. REF: REO. SEE CONTINUATION CARD FOR FULL DETAILS.
- [SDR SWIA2020012147927](https://openairdocs.org/sdr/SWIA2020012147927.md): Skin · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > * THE LH WING LOWER WING PLANK ACCESS HOLE AT PANEL 540BB HAS CORROSION. (C-CHECK) RO:1/17/2020REPAIRED PITTING CORROSION L/H LOWER WING PLANK ACCESS HOLE 540BB IN ACCORDANCE WITH REO.
- [SDR SWIA2020012147926](https://openairdocs.org/sdr/SWIA2020012147926.md): Skin · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > * THE LH WING LOWER WING PLANK ACCESS HOLE AT PANEL 510AB HAS CORROSION. (C-CHECK) RO:1/17/2020REPAIRED PITTING CORROSION L/H LOWER WING PLANK ACCESS HOLE 510AB IN ACCORDANCE WITH REO.
- [SDR SWIA2020012147925](https://openairdocs.org/sdr/SWIA2020012147925.md): Fitting · cracked · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FWD HANDRAIL LOWER FITTING COMMON TO FLOOR SILL IS CRACK. (C-CHECK) RO:1/17/2020LOCATED AND DRILLED NEW PAX DOOR FWD HANDRAIL LOWER FITTING P/N 600-31927-7 REF CRJ 200 SRM. NEW FITTING INSTALLED ON JOB # 2759261 OP 372.
- [SDR SWIA2020012147924](https://openairdocs.org/sdr/SWIA2020012147924.md): Door Frame · corroded · Dec 12, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Structure
  > * THE PAX DOOR OUTER FORMER AT FS347.25 FROM DD6 TO DD5 HAS CORROSION. (MARKED) (C-CHECK) RO:1/17/2020BLENDED MULTIPLE ACCESSIBLE LOCATIONS ON PAX DOOR OUTER FORMER AT FS347.25. FORMER IS OUT OF LIMITS. REF: CRJ-200 SRM. REMOVED PASSENGER DOOR AFT FOR
- [SDR SWIA2020012147923](https://openairdocs.org/sdr/SWIA2020012147923.md): Door Frame · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Structure
  > * THE PAX DOOR FWD FORMER AT FS311.75 BETWEEN DD6 AND DD5 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO:1/17/2020BLENDED MULTIPLE ACCESSIBLE LOCATIONS ON PAX DOOR FWD FORMER AT FS311.75. CORROSION EXTENDS IN NON-ACCESSIBLE LOCATIONS AND UNDER INT
- [SDR SWIA2020012147922](https://openairdocs.org/sdr/SWIA2020012147922.md): Hinge · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > * THE AFT LAV SERVICE DOOR HINGE BRACKETS HAVE CORROSION. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED THE AFT LAV SERVICE DOOR HINGE BRACKETS REF CRJ200 SRM. SEE CONTINUATION CARD FOR FULL DETAILS.
- [SDR SWIA2020012147921](https://openairdocs.org/sdr/SWIA2020012147921.md): Hinge · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > * THE AFT LAV SERVICING DOOR HINGES AND HARDWARE HAVE CORROSION. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED THE AFT LAV SERVICING DOOR HINGES AND HARDWARE REF CRJ200 SRM. SEE CONTINUATION CARD FOR FULL DETAILS.
- [SDR SWIA2020012147920](https://openairdocs.org/sdr/SWIA2020012147920.md): Stringer Clip · cracked · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > *AFT EQUIPMENT BAY FS624 STGR 14 R/H CLIP IS CRACKED. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW CLIP P/N 601-350-52 AT R/H STGR 14. REF: CRJ200 SRM AND DWG COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA2020012147919](https://openairdocs.org/sdr/SWIA2020012147919.md): Stringer Clip · cracked · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > *AFT EQUIPMENT BAY FS624 STGR 14 L/H CLIP IS CRACKED. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW CLIP P/N 601-350-51 AT L/H STGR 14. REF: CRJ200 SRM AND DWG COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA2020012147918](https://openairdocs.org/sdr/SWIA2020012147918.md): Clamp · missing · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *AFT EQUIPMENT BAY ABOVE ENGINE BEAM AT BL0 VERTICAL STIFFENER, PRESSURE LINE CLAMP MISSING CUSHION. (MARKED) (C-CHECK) RO:1/17/2020REMOVED OLD AND INSTALLED NEW ADEL CLAMP AT AFT SIDE OF FS621 BL0 VERTICAL STIFFENER REF SRM.
- [SDR SWIA2020012147917](https://openairdocs.org/sdr/SWIA2020012147917.md): Anchor Fitting · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Structure
  > *SERATED MOUNT PLATE FOR PAX DOOR AFT ANCOR FITTING IS CORRODED. (C-CHECK) RO:1/17/2020REMOVED THE SERRATED MOUNT PLATE FOR THE PAX DOOR AFT ANCHOR FITTING REF. CRJ200 AMM. INSTALLED NEW PAX DOOR AFT SERRATED PLATE WITH NEW HARDWARE REF CRJ 200 AMM.
- [SDR SWIA2020012147916](https://openairdocs.org/sdr/SWIA2020012147916.md): Anchor Fitting · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > *SERATED MOUNT PLATE FOR PAX DOOR FWD ANCOR FITTING IS CORRODED. (C-CHECK) RO:1/17/2020INSTALLED NEW PAX DOOR ANCHOR FITTING P/N 601R31976-11 AND NEW SERRATED MOUNT PLATE REF CRJ 200 AMM ADJUSTMENT CHECK GOOD
- [SDR SWIA2020012147915](https://openairdocs.org/sdr/SWIA2020012147915.md): Skin · chafed · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > *R/H WING LOWER AFT SKIN PLANK MATING SURFACE FOR MLG FAIRING AT RBL45 CHAFED (MARKED). (C-CHECK) RO:1/17/2020THE CHAFE ON THE LOWER WING PLANK AT RBL45 WAS BLENDED. NDT MEASURED THE REMAINING MATERIAL THICKNESS AT 0.255Ï¿½. MATERIAL LOSS WAS 0.045Ï¿½
- [SDR SWIA2020012147914](https://openairdocs.org/sdr/SWIA2020012147914.md): Skin · chafed · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/Skin
  > *L/H WING LOWER AFT SKIN PLANK MATING SURFACE FOR MLG FAIRING AT LBL45 CHAFED (MARKED). (C-CHECK) RO:1/17/2020REPAIRED CHAFED AREA ON L/H WING LOWER AFT SKIN PLANK MATING SURFACE AT ZONE C BLEND AREA FOR MLG FAIRING #193AB AT LBL45 PER BOMBARDIER REO
- [SDR SWIA2020012147913](https://openairdocs.org/sdr/SWIA2020012147913.md): Guide Plate · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR AFT LOWER TENSION FITTING GUIDE PLATE HARDWARE IS CORRODED. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED ALL CORRODED HARDWARE ON THE PAX DOOR AFT LOWER TENSION FITTING GUIDE PLATE. REF CRJ 200 SRM.
- [SDR SWIA2020012147912](https://openairdocs.org/sdr/SWIA2020012147912.md): Fitting · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > THE PAX DOOR AFT LOWER TENSION FITTING HARDWARE IS CORRODED. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW KEY LOCK AND NUT ON AFT LOWER PAX DOOR TENSION TIE REF. CRJ-200 AMM.ADJUSTMENT CHECK GOOD. OP CHECK GOOD
- [SDR SWIA2020012147911](https://openairdocs.org/sdr/SWIA2020012147911.md): Guide Plate · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR AFT UPPER TENSION FITTING GUIDE PLATE HARDWARE CORRODED. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED ALL CORRODED HARDWARE ON THE PAX DOOR AFT UPPER TENSION FITTING GUIDE PLATE. REF CRJ 200 SRM.
- [SDR SWIA2020012147910](https://openairdocs.org/sdr/SWIA2020012147910.md): Fitting · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR AFT UPPER TENSION FITTING HAS CORRODED HARDWARE. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW KEY LOCK AND NUT ON AFT UPPER PAX DOOR TENSION TIE REF. CRJ-200 AMM.ADJUSTMENT CHECK GOOD. OP CHECK GOOD.
- [SDR SWIA2020012147909](https://openairdocs.org/sdr/SWIA2020012147909.md): Guide Plate · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR LOWER FWD TENSION FITTING GUIDE PLATE HARDWARE IS CORRODED. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED ALL CORRODED HARDWARE ON THE PAX DOOR LOWER FWD TENSION FITTING GUIDE PLATE. REF CRJ 200 SRM.
- [SDR SWIA2020012147908](https://openairdocs.org/sdr/SWIA2020012147908.md): Fitting · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR LOWER FWD TENSION FITTING HARDWARE CORRODED. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW KEY LOCK AND NUT ON FWD LOWER PAX DOOR TENSION TIE REF. CRJ-200 AMM.ADJUSTMENT CHECK GOOD. OP CHECK GOOD.
- [SDR SWIA2020012147907](https://openairdocs.org/sdr/SWIA2020012147907.md): Guide Plate · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR UPPER FWD TENSION FITTING GUIDE PLATE 1EA CORRODED HARDWARE. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED ALL CORRODED HARDWARE ONTHE PAX DOOR UPPER FWD TENSION FITTING GUIDE PLATE. REF CRJ 200 SRM
- [SDR SWIA2020012147906](https://openairdocs.org/sdr/SWIA2020012147906.md): Fitting · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR FWD UPPER TENSION FITTING HARDWARE IS CORRODED. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW KEY LOCK AND NUT ON FWD UPPER PAX DOOR TENSION TIE REF. CRJ-200 AMM. ADJUSTMENT CHECK GOOD. OP CHECK GOOD.
- [SDR SWIA2020012147905](https://openairdocs.org/sdr/SWIA2020012147905.md): Gate · chafed · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR PRESSURE VENT FLAP IS CHAFFED. (MARKED) (C-CHECK) RO:1/17/2020REPLACED PAX DOOR PRESSURE VENT FLAP. REF CRJ200 AMM. PERFORMED OPERATIONAL TEST OF THE PAX DOOR. REF CRJ200 AMM. NO DEFECTS NOTED AT THIS TIME. SEE CONTINUE CARD FOR DETAILS
- [SDR SWIA2020012147904](https://openairdocs.org/sdr/SWIA2020012147904.md): Torque Tube · corroded · Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PAX DOOR LOWER AFT TORQUE TUBE BEARING ASSEMBLY IS CORRODED AF FS338.963 BETWEEN DD5 AND DD4. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED PAX DOOR LOWER AFT TORQUE TUBE BEARING ASSEMBLY AT FS338.963 BETWEEN DD5 AND DD4 WITH NEW HARDWARE. REF CRJ

Next page: https://openairdocs.org/aircraft/N455CA/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 = 'N455CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N455CA/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.