N455CA

Service difficulty reports · 201

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2020020748316Control Unit · failedFLAPS 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. DIFeb 7, 2020 · N455CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2020012147958Insert · debondedLH 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.Jan 16, 2020 · N455CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020012147957Beam · corroded*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.Jan 13, 2020 · N455CA · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA2020012147956Support Angle · damagedDURING 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 GOODJan 12, 2020 · N455CA · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR SWIA2020012147955Floor Support · corroded*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 Jan 8, 2020 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020012147954Panel · crackedPANEL 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 .Jan 7, 2020 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020012147953Lever · crackedRH 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 AMMJan 3, 2020 · N455CA · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2020012147952Anchor Fitting · corrodedUPON 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 GOODDec 30, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020012147951Door · wornREPLACE 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.Dec 29, 2019 · N455CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020012147950Lever · chafed* 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.Dec 28, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147949Stiffener · crackedL/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/HDec 27, 2019 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020012147948Door Sill · corrodedPAX 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.Dec 23, 2019 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020012147947Skin · chafedRH 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# T522Dec 22, 2019 · N455CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020012147946Floorbeam · crackedINBOARD 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.Dec 20, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020012147942Stiffener · cracked* 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.Dec 19, 2019 · N455CA · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2020012147938Floor Skin · crackedPERFORM 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. RDec 17, 2019 · N455CA · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2020012147937Hinge Fitting · gougedL/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#.Dec 16, 2019 · N455CA · Cndair CL6002B19 · Elevator StructureSDR SWIA2020012147936Frame · cracked*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.Dec 13, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020012147935Plate · corrodedUPON 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 BOMBARDDec 13, 2019 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020012147934Skin · corroded* 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 GOODDec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147933Skin · corroded* 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.Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147932Skin · corroded* 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 GOODDec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147931Skin · corroded* 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.Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147930Skin · corroded* 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.Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147929Check Valve · inoperativeLH 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 3EADec 12, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020012147928Skin · corroded* 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.Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147927Skin · corroded* 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.Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147926Skin · corroded* 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.Dec 12, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147925Fitting · crackedPASSENGER 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.Dec 12, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147924Door Frame · corroded* 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 FORDec 12, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020012147923Door Frame · corroded* 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 INTDec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020012147922Hinge · corroded* 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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2020012147921Hinge · corroded* 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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2020012147920Stringer Clip · cracked*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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020012147919Stringer Clip · cracked*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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020012147918Clamp · missing*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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020012147917Anchor Fitting · corroded*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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020012147916Anchor Fitting · corroded*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 GOODDec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147915Skin · chafed*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¿½Dec 11, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147914Skin · chafed*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 Dec 11, 2019 · N455CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020012147913Guide Plate · corroded* 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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147912Fitting · corrodedTHE 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 GOODDec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147911Guide Plate · corroded* 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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147910Fitting · corroded* 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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147909Guide Plate · corroded* 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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147908Fitting · corroded* 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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147907Guide Plate · corroded* 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 SRMDec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147906Fitting · corroded* 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.Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147905Gate · chafed* 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 DETAILSDec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020012147904Torque Tube · corroded* 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 Dec 11, 2019 · N455CA · Cndair CL6002B19 · Passenger/Crew Doors
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