N809CA, cancelled Nov 3, 2023

Service difficulty reports · 180

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 = 'N809CA' AND deregistration_id = 'N809CA-2023-11-03'
  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 SWIA202266699None · fault messageLEFT FIRE FAIL CAUTION MESSAGE CAME ON AND OFF TWICE INFLIGHT. PERFORMED QRH. (FLIGHT #5336 FILED CLOSED) T/S L/H FIRE FAIL CAUTION MSG, FOUND ENGINE NACELLE AND FIREWALL SENSING ELEMENT A END CONNECTOR DAMAGED. REMOVED AND REPLACED WIRING END CONNECTOR ASOct 31, 2022 · N809CA · Cndair CL6002B19 · Smoke DetectionSDR SWIA202265554None · failedGEAR DISAGREE WARNING MESSAGE. NOSE GEAR STUCK DOWN. RAN QRH AND ALL 3 GEARS CAME DOWN WITH THE MANUAL RELEASE HANDLE. (FLIGHT 5454 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24763990 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 247702May 3, 2022 · N809CA · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA2020033149779Nut Plate · brokenPANEL 571LL ON L/H WING HAS ONE BROKEN NUTPLATE. (C CHECK) RO 3/27/2020 REMOVED BROKEN NUTPLATE AND INSTALLED NEW P/N NAS1789-3 NUTPLATE IAW CRJ 200 SRM.Mar 10, 2020 · N809CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020033149770Fitting · brokenAVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING BROKEN. (C CHECK) RO 3/27/2020 REMOVED BROKEN AVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING. LOCATED AND DRILLED NEWAVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING REF. CRJ-200 [TR51-42] SRM. INSTALLATION PERFORMFeb 27, 2020 · N809CA · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020033049586Angle · cracked*ANGLE ATTACHED TO TOP AFT EDGE OF FRAME AT FS 682 IS CRACKED BETWEEN STGR25R AND STGR26R. (C CHECK) RO 3/27/2020 REPAIRED ANGLE ATTACHED TO TOP AFT EDGE OF FRAME AT FS 682 BETWEEN STGR25R AND STGR26R PER BOMBARDIER REO COMPLIED WITH ALL STEP OF REO.Feb 26, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049584Fitting · cracked*R/H WINDSHIELD SIDE POST AFT LWR CLIP (FITTING) IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED R/H WINDSHIELD SIDE POST FITTING REFERENCE CRJ 200 SRM AND DRAWING. COMPLIED WITH. SEE CONTINUATION FOR DETAILS.Feb 25, 2020 · N809CA · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA2020033049583Fitting · cracked*L/H WINDSHIELD SIDE POST AFT LWR CLIP (FITTING) IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED CRACKED L/H WINDSHEILD SIDE POST AFT LOWER FITTING WITH NEW FITTING. REF DRAWING AND CRJ 200 SRM. SEE CONTINUATION FOR DETAILS.Feb 25, 2020 · N809CA · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA2020033049582Frame · crackedFS 605.0 FRAME FLANGE LEFT HAND SIDE, JUST OVER AFT CARGO DOOR HAS SUSPECT CRACK AT RIVET LOCATION JUST ABOVE AND BELOW STR 9. (MARKED) (C CHECK) RO 3/27/2020 REPAIRED DAMAGE AREA AND COMPLIED WITH ALL STEPS OF BOMBARDIER REO. PRESSURE CHECK GOOD. SEE CONTFeb 24, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020033049581Rib · damagedRH INBOARD FLAP VANE LEADING EDGE INBOARD RIB REQUIRES REPLACEMENT (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AND RESTORED FINISH ON RH INBOARD FLAP VANE LEADING EDGE INBOARD RIB. REF: CRJ200 SRM. FOUND TO BE OUT OF LIMITS ON CAMP 20427303 JOB 2736661 OP Feb 20, 2020 · N809CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020033149753Channel · corrodedCORROSION FOUND ON AVIONICS BAY DOOR POSITION SENSOR MOUNTING CHANNEL AT FS.364.00, STGR 27. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM AVIONICS BAY DOOR POSITION SENSOR CHANNELS AT FS364.00 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NFeb 19, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049580Floor Skin · cracked*PRESSURE FLOOR SKIN IS CRACKED AT 2EA LOCATIONS AT APPROX FS 461 BETWEEN BL0 AND LBL 9 AND BL0 TO RBL9. SUSPECT AREAS ARE MARKED WITH RED GREASE PENCIL. (C CHECK) RO 3/27/2020 REPAIRED PRESSURE FLOOR SKIN @ 2EA LOCATIONS AT APPROX FS.461.00 BETWEEN BL0 ANFeb 19, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049579Frame Splice · corrodedCORROSION FOUND ON UPPER SPLICE ANGLE FOR LOWER FRAME SECTOR AT FS.364.00 AND STGR 27. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION ON UPPER SPLICE ANGLE FOR LOWER FRAME SECTOR AT FS364.00 STGR 27 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NEFeb 19, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020033049578Fitting · cracked*AFT LINTEL CLIP IS POSSIBLY CRACKED. FLAGGED (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AFT LINTEL CLIP REF. CRJ-200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.Feb 17, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033149764Not Reported · corroded*FS559.00+80 €“ 559.00+112 STGR 26L €“ 26R CORROSION AROUND SEVERAL FASTENERS (MARKED) (C CHECK) RO 3/27/2020 REPAIRED CORROSION DAMAGE AT FS559+80 TO FS574 STGR25L TO STGR26R COMPLIED WITH ALL APPLICABLE STEPS OF BOMBARDIER REO. LEAK CHECK GOOD. SEE COFeb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033149752Floor Support · corrodedAFT CARGO APPROX.€¦ FS.559.00+118 TO FS. 621.00 LEFT HAND LBL 27.00 FLOOR BEAM HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 COMPLIED WITH REO FOR THE REMOVAL OF CORROSION FROM FLOOR BEAM FS. 559.00+118 TO FS. 621.00 LBL 27.Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033149751Hinge · corroded*RUDDER CENTER HINGE AREA, UPPER AND LOWER GROUND STUD AND HARDWARE ON RUDDER, CORRODED (MARKED, OUT OF SCOPE) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW RUDDER CENTER HINGE, UPPER AND LOWER GROUND STUD AND HARDWARE REF CRJ 200 AMM.Feb 13, 2020 · N809CA · Cndair CL6002B19 · Rudder StructureSDR SWIA2020033149750Seat Track · corrodedTHE SEAT TRACK AT RBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 BLENDED SEAT TRACK AT RBL9 FS409+128 TO FS559.00 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK. REF: BOMBARFeb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020033149749Seat Track · corrodedTHE SEAT TRACK AT LBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORRODED SET TRACK LBL BETWEEN FS. 409.00+128 AND FS. 559.00 AND INSTALLED NEWLY FABRICATED SEAT TRACK IAW CRJ 200 AMM ANDFeb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020033149748Stand Off · corroded* THE LH FLOOR SILL HAS 3EA ELECTRICAL STANDOFFS THAT ARE CORRODED BETWEEN FS409.00+64 TO FS409.00+80. (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED 3 EACH STAND OFFS PER REFERENCE CRJ 200 SRM.Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049576Bracket · cracked*FS621.00 - 625.30 STGR APPROX. 14R ANGLE CRACKED (MARKED) (C CHECK) RO 3/27/2020 REMOVED CRACKED ANGLE BRACKET FROM FS. 625.30 STRINGER 14R AND INSTALLED NEW ANGLE BRACKET IAW CRJ 200 SRM. COMPLIED WITH TASK CARD.Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049575Bracket · cracked*FS621.00 - 625.30 STGR APPROX. 14L ANGLE CRACKED (MARKED) (C CHECK) RO 3/27/2020 REMOVED CRACKED ANGLE BRACKET FROM FS. 625.3.0 STRINGER 14L AND INSTALLED NEW ANGLE BRACKET IAW CRJ 200 SRM. COMPLIED WITH TASK CARD.Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049574Frame · corrodedFRAME AT L/H FS 513 WL73 (FLOOR LEVEL) HAS SMALL AREA OF CORROSION. (C CHECK) RO 3/27/2020 REMOVED CORROSION ON FRAME @ FS.513 WL.73. FOUND TO BE OUT OF LIMITS. COMPLIED WITH ALL APPLICABLE STEPS OF REO. SEE CONTINUATION FOR FURTHER DETAILS.Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020033049570Door Sill · cracked*FRAME FROM PAX DOOR UPPER SILL TO STGR 0 AT FS 333 IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW FRAME @ FS.333.00 FROM PAX DOOR UPPER SILL TO STRG 0 REF CRJ 200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE COFeb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049568Intercostal · corroded*CORROSION FOUND ON INTERCOSTAL AFT OF AVIONICS BAY DOOR ON R/H SIDE OF STGR27. (C CHECK) RO 3/27/2020 REMOVED AND REINSTALLED A NEW INTERCOSTAL AT STRG 27 RH FROM FS.394.00 TO FS.409.00 REF CRJ 200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. COMPLIED WITFeb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049566Intercostal · corroded*CORROSION FOUND ON INTERCOSTAL AFT OF AVIONICS BAY DOOR ON L/H SIDE OF STGR27. (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW INTERCOSTAL AFT OF AVIONICS BAY DOOR ON THE LH SIDE OF STRG 27 REF BOMBARDIER DWG AND CRJ 200 SRM. COMPLIED WITH TASK CARD. PFeb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049563Stringer Clip · crackedFWD CABIN - APPROX.€¦ FS280.00 STGR 3 €“ STRINGER CLIP HAS SIGNS OF A CRACK AND WORKING RIVETS (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW FWD CABIN STRINGER CLIP ON RH STRG 3 @ FS.280.00 REF CRJ 200 SRM AND BOMBARDIER DWG.LEAK CHECK GOODFeb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020033049560Panel · corrodedTHE RH FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (MARKED) (C CHECK) RO 3/27/2020 BLENDED MULTIPLE AREAS OF CORROSION FROM R/H FLOOR SILL PANEL FROM FS. 409.00+128 TO FS. 559.00 IAW REO CRJ-200 SRM.Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049559Not Reported · corroded*FS559.00 STGR 26L €“ 26R HAS CORROSION ON FASTENERS AND AROUND THE FASTENERS(MARKED) (C CHECK) RO 3/27/2020 REPAIRED FS559.00 STR26L -26R REFERENCING REO. ALL STEPS COMPLIED WITH.Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049556Floorbeam · corrodedTHE FLOORBEAM AT LBL9.00 FROM FS409.00 TO FS409.00+128 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM FLOOR BEAM AT LBL 9.00 FROM FS. 409.00 TO FS. 409.00+128 IAW REO ( SEE CONTINUATION CARD FOR DETAILS ).Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020033149776Hinge Fitting · gouged*LH SPOILERON THIRD HINGE FITTING GOUGED ON THE OUTBD UPPER AFT EDGE (MARKED) (C CHECK) RO 3/27/2020 REMOVED GOUGE ON THE LH SPOILERON THIRD HINGE FITTING OUTBD UPPER AFT EDGE. FOUND TO BE OUT OF LIMITS. RECEIVED REO. FOUND TO BE IN LIMITS . COMPLIED WITHFeb 12, 2020 · N809CA · Cndair CL6002B19 · AileronsSDR SWIA2020033149747Seat Track · chafed*NUMEROUS AREAS OF CHAFEING, FRETTING, AND CORROSION ON SEAT RAIL FROM FS409 TO FS409+128 AT RBL9 (C CHECK) RO 3/27/2020 REPLACED SEAT RAIL FROM FS409 TO FS409+128 AT RBL9 WITH A NEW FABRICATED PART REF REO, SEE CONTINUATION CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020033149746Seat Track · chafed*NUMEROUS AREAS OF CHAFEING, FRETTING, AND CORROSION ON SEAT RAIL FROM FS364 TO FS409 AT RBL9. (C CHECK) RO 3/27/2020 BLENDED SEAT TRACK AT RBL 9.00 FROM FS 364.00 TO FS 409.00 . REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK. REF: Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020033149745Fastener · corroded*RH SPOILERON BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE AT BOTTOM ATTACH POINT AT RH SPOILERON OUTBOARD PCU REF CRJ200 AMM. OPS TEST GOOD, SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149744Fastener · corroded*RH FLIGHT SPOILER BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON BOTTOM ATTACHING OINTS ON RH FLIGHT SPOILER PCU REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149743Nut · corroded*RH SPOILERON HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED THE HARDWARE WITH NEW ON THE RH SPOILERON HINGE ATTACH POINTS. REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149742Nut · corroded*RH FLIGHT SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON RH FLIGHT SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149741Nut · corroded*RH OUTBD GROUND SPOILER INBD/OUTBD HINGE ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED THE ATTACHING HARDWARE ON THE RIGHT OUTBOARD GROUND SPOILER HINGES, REF CRJ 200 AMM. OPERATIONAL TEST OF GROUND SPOILERS CHECKED GFeb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149740Nut · corroded*RH INBD GROUND SPOILER OUTBD HINGE ATTACH HARDWARE NUT CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED HARDWARE OF THE RH INBOARD GROUND SPOILER OUTBOARD HINGE WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST OF THE GROUND SPOILERS CHECKED GOOD. Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149739Fastener · corroded*LH SPOILERON BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON LH INBOARD SPOILER PCU BOTTOM ATTACH POINT REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149738Fastener · corroded*LH FLIGHT SPOILER BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE AT BOTTOM ATTACHING POINTS OF THE LH FLIGHT SPOILER PCU'S REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149737Nut · corroded*LH SPOILERON HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH SPOILERON END HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149736Nut · corroded*LH FLIGHT SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 LEFT FLIGHT SPOILER CENTER HINGES HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149735Nut · corroded*LH OUTBD GROUND SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH OUTBOARD GROUND SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033149734Nut · corroded*LH INBD GROUND SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH INBOARD GROUND SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.Feb 12, 2020 · N809CA · Cndair CL6002B19 · SpoilersSDR SWIA2020033049554Frame · corrodedAFT CARGO APPROX.€¦ FS.574.00 LEFT HAND STGR 25 TO STGR 18 - FRAME HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CARGO APPROX FS574.00 LEFT HAND STGR25 TO STGR18 FRAME REF CRJ 200 SRM AND BOMBARDIER DWG LEAK TEST GOOD. SEE CFeb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020033049553Door Sill · corroded*R/H FLOOR SILL HAS 4EA AREAS OF CORROSION BETWEEN FS310 AND FS319.70. AREAS MARKED WITH RED GREASE PENCIL. (C CHECK) RO 3/27/2020 REMOVED AND REPLACE RH FLOOR SILL BETWEEN FS310 AND FS319.70 REF DWG 601R31148 REV Y. SEE CONTINUATION CARD FOR DETAILSFeb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049551Door Sill · corrodedAFT CABIN APPROX. FS 559.00 TO 559.00 +96 RIGHT HAND FLOOR SILL BL 42.90 HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CABIN APPROX FS559.00 TO FS559.00+16 RIGHT HAND FLOOR SILL INTERCOSTAL BL42.90 REF BOMBARDIER DWG, CRJ 20Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049550Strap · corrodedAFT CABIN APPROX. FS 559.00 RIGHT HAND RBL 42.90 TO RBL27.00- INTERCOSTAL STRAP HAS SIGNS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CABIN APPROX FS559.00 RIGHT HAND RBL 42.90 INTERCOSTAL STRAP WITH NEW REF BOMBARDIER DWG, CRJ 200 SRM. SEE CFeb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020033049548Plate · corrodedTHE PLATE UNDER THE TRANSMITTER ANTENNA NO.2 HAS CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM PLATE UNDER TRANSMITTER ANTENNA #2 REF CRJ 200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW PLATE UNDER THE TRANSMITTER ANTENFeb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020033149772Trim Panel · crackedCREW ESCAPE HATCH TRIM ASSY CRACKED IN SEVERAL AREAS (C CHECK) RO 3/27/2020 REPAIRED THE CREW ESCAPE HATCH TRIM ASSEMBLY USING PO# 24268 PER BOMBARDIER REO.Feb 11, 2020 · N809CA · Cndair CL6002B19 · Emergency Exits
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