N909SW

Service difficulty reports · 217

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 = 'N909SW' 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 SWIA202402220019Warning Message · illuminatedAFTER CALLING V1, ROTATE, WE GOT EITHER A/SKID INBD OR A/SKID OUTBD, FOLLOWED BY L REV UNSAFE. BOTH MESSAGES WENT AWAY IN 5 TO 10 SECONDS. WE COMPLETED THE QRH FOR ALL MESSAGES. (FLIGHT 5305 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 2784326Feb 19, 2024 · N909SW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR SWIA2024022019Warning Message · illuminatedAFTER CALLING V1, ROTATE, WE GOT EITHER A/SKID INBD OR A/SKID OUTBD, FOLLOWED BY L REV UNSAFE. BOTH MESSAGES WENT AWAY IN 5 TO 10 SECONDS. WE COMPLETED THE QRH FOR ALL MESSAGES. (FLIGHT 5305 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.Feb 19, 2024 · N909SW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR SWIA2023062900008Unknown · warning messageAPU OIL TEMP CAUTION MESSAGE IN FLIGHT. RAN QRH LANDED AT NEAREST SUITABLE. (FLT 5455 FILED CLOSED)REMOVED AND REPLACED WITH SERVICEABLE THE OIL COOLER ON THE APU IN REFERENCE TO CRJ 200 AMM 49-91-07 OPS CHECKS GOOD NO LEAKS NOTED, REMOVED AND REPLACED WITH NEJun 28, 2023 · N909SW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR SWIA202266615None · failedR COWL ANTI ICE CAUTION ON CLIMB OUT WITH COWL ANTI ICE SELECTED OFF RAN QRH (FLIGHT #5015 FILED CLOSED) REFERENCE TO EAML 1012961 WITH THE FOLLOWING CORRECTIVE ACTION: 'REMOVED AND REPLACED RIGHT ENGINE PRESSURE RELIEF VALVE IN REFERENCE TO CRJ 200 AMM 30Oct 16, 2022 · N909SW · Cndair CL6002B19 · Ice/Rain Protection SystemSDR SWIA202264774None · failedGEAR DISAGREE AFTER T/O , RAN QRH AND GOT DOWN 3 GREEN. RETURNED TO FIELD DUE TO ICING CONDITIONS AND LANDED OVER WEIGHT 49,000. 300FT PER MIN ON TOUCHDOWN (FLIGHT 4771 - FILED CLOSED) VERIFIED WITH CREW THAT RH MLG WAS THE GEAR THAT FAILED TO FULLY RETRMar 6, 2022 · N909SW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202157004Angle · corrodedKICK ANGLE AT PASSENGER DOOR SILL CORRODED (C-CHECK) RO 3/24/2021 REMOVED PASSENGER DOOR KICK ANGLE. REF: CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-10, CRJ200 SRM 51-42-21. - INSTALLED NEW PASSENGER DOOR LOWER KICK ANGLE P/N 601R31527-221. REV: DWG 6Mar 8, 2021 · N909SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157002Frame · cracked*FS333.00 FRAME IS CRACKED AT THE STGR1R. (C-CHECK) RO 3/24/2021 REMOVED DAMAGED FRAME SECTOR AT FS333.00 FROM STGR-0 TO STGR-5R, REPLACED AND INSTALLED NEW FRAME SECTOR P/N#6001R32004-5. REF. CRJ-200 SRM 51-42-06,SRM 51-42-21 DWG#601R32004 REV. N, AND Mar 1, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202157022Thrust Washer · brokenRH OUTBOARD (R-1) FLAP ACTUATOR FITTING THRUST WASHER BROKEN. (C-CHECK) RO 3/24/2021 REMOVED BROKEN THRUST WASHER AND INSTALLED NEW THRUST WASHER ABOVE R-4 OTBD FLAP ACTUATOR. REF. CRJ200 SRM 51-41-02.Feb 28, 2021 · N909SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202157001Hinge · damaged*PAX DOOR FUSELAGE SIDE HINGE HAS OBLONG HOLES ON LUGS FOR PIANO HINGE PIN (C-CHECK) RO 3/24/2021 FOUND PAX DOOR HINGE HAFT FUSELAGE SIDE OUT OF LIMIT PER REO 601R-53-21-814 REV C DATED 2017-08-02 . REMOVED AND INSTALLED NEW AIRCRAFT SIDE HINGE HALF P/N 6Feb 28, 2021 · N909SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202157000Angle · crackedCLIP CRACKED AT APPROXIMATELY STGR13R ON REAR Z-MEMBER FS621 REAR BULKHEAD (C-CHECK) RO 3/24/2021 REMOVED CRACKED CLIP AT STGR 13R. REF: CRJ200 SRM 51-42-06. INSTALLED NEW CLIP P/N 601R350147-1. REF: DWG 601-35012, REV: D, REF: CRJ200 SRM 51-42-06Feb 27, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202156999Intercostal · corrodedFOUND DD3 INTERCOSTAL CORRODED AT THE FWD SIDE OF THE PAX DOOR (AS MARKED). (C-CHECK) RO 3/24/2021 REMOVED CORROSION ON PAX DOOR DD3 INTERCOSTAL AT FWD SIDE REF CRJ 200 SRM 51-21-06.FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 52-00-00. MEASURED THICKNESS RFeb 26, 2021 · N909SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157025Skin · chafedSERVICE DOOR EXTERIOR SKIN CHAFFED APPROXIMATELY 2" ABOVE FWD GUIDE PIN ON EXERIOR SERVICE DOOR HANDLE (MARKED) (C-CHECK) RO 3/24/2021 BLENDED DAMAGE AREA REF CRJ200 SRM 51-12-00.FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 52-00-31.REPAIRED REF REO 601R-5Feb 25, 2021 · N909SW · Cndair CL6002B19 · Galley DoorsSDR SWIA202156998Skin · corroded*RH WING LOWER PLANK HAS FRETTING FROM CONTACT WITH WING FAIRING 193AB AT WS 45.00R AND AFT EDGE. (C-CHECK) RO 3/24/2021 BLENDED OUT FRETTING ON RH LOWER WING PLANK WS 45 AT AFT EDGE AND FOUND IN LIMITS REF REO 601R-57-21-880 REV D 2017/03/06 ALL STEPS COFeb 25, 2021 · N909SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202156997Skin · corroded*LH WING LOWER PLANK HAS FRETTING FROM CONTACT WITH WING FAIRING 193AB AT WS 45.00L AND AFT EDGE. (C-CHECK) RO 3/24/2021 BLENDED OUT FRETTING ON LH WING LOWER PLANK AFT EDGE AT WS45 AND FOUND IN LIMITS REF REO 601R-57-21-880 REV. D, 2017/03/06 ALL STEPS CFeb 25, 2021 · N909SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202157020Seat Track · corroded*SEAT RAIL CORRODED RBL9, S358.00 - FS380.00. (C-CHECK) RO 3/24/2021 RBL9 SEAT TRACK AT FS 358.00 TO FS 380.00 IS OUT OF LIMITS HAVING CORROSION ON MORE THEN 2 ELEMENTS REF CRJ200 SRM 53-21-49. REMOVED RBL9 SEAT TRACK AT FS 358.00 TO FS 380.00 REF CRJ200 Feb 24, 2021 · N909SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202157019Seat Track · corroded*SEAT RAIL CORRODED LBL9, S358.00 - FS380.00. (C-CHECK) RO 3/24/2021 LBL9 SEAT TRACK AT FS 358.00 TO FS 380.00 IS OUT OF LIMITS HAVING CORROSION ON MORE THEN 2 ELEMENTS REF CRJ200 SRM 53-21-49. REMOVED LBL9 SEAT TRACK AT FS 358.00 TO FS 380.00 REF CRJ200 Feb 24, 2021 · N909SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202157024Skin · gouged*GOUGE ON INTERNAL FUSELAGE SKIN BETWEEN STGR 27 - 26R, FS 559.00+16 - 559.00+32 (C-CHECK) RO 3/24/2021 BLENDED OUT GOUGE ON INTERNAL FUSELAGE SKIN BETWEEN STGR 27 - 26R, FS559.00+16 - 559.00+32. REF: CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS REF CRFeb 22, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202157021Bracket · broken*AFT CARGO PRESSURE BULKHEAD FS621.0 AT RBL9 ISOLATOR BRACKET IS BROKEN. (MARKED) (C-CHECK) RO 3/24/2021 BROKEN ISOLATOR REMOVED AND REPLACED WITH FS621 BULKHEAD REINFORCEMENT ON JOB 27558105, OP 5531.Feb 22, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202156996Hinge Fitting · corroded* FOUND COROSSION ON THE BOTTOM HINGE FITTING OF THE CARGO COMPARTMENT DOOR(AREA MARKED) (C-CHECK) RO 3/24/2021 REMOVED AND INSTALLED NEW FWD AND AFT BOTTOM HINGE FITTINGS OF THE CARGO COMPARTMENT DOOR. REF: CRJ 200 SRM 51-42-21 AND DWG 601R35027 REV Y. CFeb 22, 2021 · N909SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202156995Floorbeam · damaged*280.00 LEFT FLOOR POST HAS A DRILL START AT THE TOP END FORWARD SIDE. (MARKED) (C-CHECK) RO 3/24/2021 REMOVED AND INSTALLED NEW LH FLOOR POST AT FS 280 LBL 9 REF CRJ 200 SRM 51-42-06 AND DRAWING# 600-34017 REV AA, AND MHIRJ REO 601R-53-11-3674 REV --, DFeb 22, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156994Floorbeam · cracked*FLOOR MEMBER, FS280.00, FWD FLOOR ANGLE IS CRACKED OUTBOARD ENDS, LBL9 €“ RBL9. (MARKED) (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED FS280.00, FWD FLOOR ANGLE LBL9 €“ RBL9 REF. CRJ 200 SRM 51-42-06 AND DWG 600-34017 REV. AD. COMPLIED WITH TASK CARD 51Feb 22, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156993Floorbeam · cracked*FLOOR MEMBER, FS280.00, IS CRACKED OUTBOARD ENDS, LBL9 €“ RBL9. (MARKED) (C-CHECK) RO 3/24/2021 REPAIRED FS280 BULKHEAD ASSY REF. REO 601R-53-11-926 REV. -B DATED 2006-05-10 ALL STEPS COMPLIED WITH, AND REO 601R-53-11-3666 REV. -- DATED 2021-03-12 ALL Feb 22, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156992Door Sill · corroded* PAX DOOR LOWER SILL CORRODED AROUND AFT DRAIN HOLE (MARKED). (C-CHECK) RO 3/24/2021 REMOVED CORROSION ON PAX DOOR LOWER SILL NEAR AFT DRAIN HOLE REF CRJ200 SRM 51-21-06. COMPLIED WITH REO 601R-53-21-3406 REV -- DATED 2021-02-27. COMPLIED WITH 51-900-1Feb 22, 2021 · N909SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156991Floor Support · corroded* FLOOR SILL FWD OF SERVICE DOOR HAS CORROSION BETWEEN FS310.00 AND FS295.00 (MARKED). (C-CHECK) RO 3/24/2021 BLENDED OUT CORROSION ON R/H FLOOR SILL, FWD OF SERVICE DOOR BETWEEN FS295.00 AND FS310.00 REF REO 601R-53-00-530 REV-A, DATED 2014-10-07 AND DWGFeb 22, 2021 · N909SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157018Seat Track · corroded*MULTIPLE AREAS OF CORROSION ON FLOOR SEAT TRACK LBL9 BETWEEN FS 409.00+128 €“ 499.00 (C-CHECK) RO 3/24/2021 REMOVED MULTIPLE AREAS OF CORROSION ON SEAT TRACK AT LBL9 BETWEEN FS409.00+128-499.00 REF: CRJ200 SRM 51-21-06 PAGE 1 (1)FS424.00(.010) (2) FS43Feb 21, 2021 · N909SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202157017Seat Track · corroded*MULTIPLE AREAS OF CORROSION ON FLOOR SEAT TRACK LBL9 BETWEEN FS 499.00 €“ 559.00 (C-CHECK) RO 3/24/2021 REMOVED AND INSTALLED NEW CABIN FLOOR SEAT TRACK FROM FS499.00 TO FS559.00 LBL 9 REF CRJ-200 SRM 53-01-11. SEE CONTINUATION CARD FOR DETAILS.Feb 21, 2021 · N909SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202157016Spring · corroded*L/H WING O/B FLAP HINGE BOXES I/B AND O/B BUTE DOOR ACTUATOR SPRINGS HAVE CORROSION. (C-CHECK) RO 3/24/2021 REMOVED 2 EA. BAD BUTE DOOR ACTUATORS AND INSTALLED 2 EA NEW ACTUATORS ON LH WING OTBD FLAP INBD AND OTBD HINGE BOXES. REF. CRJ200 AMM 27-54-25-40Feb 21, 2021 · N909SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA202156990Pressure Deck · corroded*MULTIPLE AREAS OF CORROSION ON RH PRESSURE FLOOR SILL PANEL. AREAS MARKED. (C-CHECK) RO 3/24/2021 REPAIRED RH PRESSURE FLOOR SILL PANEL REF REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-2881 REV -- DATED 2021-03-05 AND REO 601R-53-41-2883Feb 21, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202156989Strap · corroded*CORROSION ON FLOOR SUPPORT STRAP BETWEEN RBL27 €“ RBL45 AT FS 559.00 (C-CHECK) RO 3/24/2021 FLOOR SUPPORT STRAP BETWEEN RBL27 €“ RBL45 AT FS559.00 HAS CORROSION ACROSS ENTIRE LENGTH. REPLACEMENT IS NECESSARY WHEN MORE THAN 30% OF ITS LENGTH IS DAMAGED.Feb 21, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156988Pressure Deck · dented*DENT ON LH PRESSURE FLOOR SILL PANEL BETWEEN FS 449.085 €“ 439.00, LBL27 -LBL45 (C-CHECK) RO 3/24/2021 DENT DIMENSIONS ARE AS FOLLOWS: WMAX=WMIN=1.0", D=0.022", T=0.080", TMAX=0.063", D/T=0.275 AND WMIN/D= 45.45 WHERE TMAX. PERMITTED FOR DENT IS 0.063" Feb 21, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202156987Pressure Deck · corroded*MULTIPLE AREAS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL. AREAS MARKED. (C-CHECK) RO 3/24/2021 REPAIRED MULTIPLE AREAS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL BY COMPLYING WITH REO 601R-53-41-666 REV -C DATED 2012-11-06, AND REO 601R-53-41-2881 RFeb 21, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202156986Floor Support · gouged*GOUGE ON FLOOR BEAM LBL9 OTBD FLANGE BETWEEN FS 559.00+112 €“ 574.00 (C-CHECK) RO 3/24/2021 BLENDED GOUGE ON FLOOR BEAM LBL9 OTBD FLANGE BETWEEN FS 559.00+112 €“ 574.00. WITHIN LIMITS REF REO 601R-53-51-563 REV-- DATED 2021-02-28. COMPLIED WITH 51-900-Feb 21, 2021 · N909SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156985Hinge · chafed*R/H AILERON UPPER L/E AT CENTER HINGE CHAFED. (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED RH LEADING EDGE UPPER SKIN PER REFERENCE DRAWING# 601R13031 REV K AND REO 601R-57-61-773 REV --, DATED 2021-03-02 (STEPS 1, 2, AND 3) COMPLIED WITH 51-900-1003-SKYFeb 21, 2021 · N909SW · Cndair CL6002B19 · AileronsSDR SWIA202156984Intercostal · cracked* REAR PRESSURE BULKHEAD AFT SIDE HAS CRACKED INTERCOSTAL ON RH SIDE (MARKED WITH ORANGE STREAMER) (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED REAR PRESSURE BULKHEAD AFT SIDE CRACKED INTERCOSTAL WITH NEW P/N: 601-35012-52 ON RH SIDE. REF: , CRJ-200 SRM 51Feb 20, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202156983Skin · chafed*SKIN AROUND APU EXHAUST HAS 2EA SMALL CHAFES AT THE AFT EDGE OF THE SKIN CUTOUT. (C-CHECK) RO 3/24/2021 BLENDED OUT CHAFES ON SKIN AROUND APU EXAUST CUTOUT REF CRJ 200 SRM 51-21-06, FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-31. MEASURED THICKNESSFeb 19, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202156982Vane · wornRH INBD FLAP VANE INBD LEADING EDGE SKIN WORN FROM BUMPER STOP (C-CHECK) RO 3/24/2021 COMPLIED WITH REO 601R-57-52-004 REV-D DATE 2012-12-19 REPAIRS TO LEADING EDGE SKIN - INBOARD FLAP VANE. FOUND TO BE OUT OF LIMITS, REPLACED SKIN WITH NEW P/N 601R14303Feb 19, 2021 · N909SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202157023Access Panel · gougedGOUGE FOUND ON INBOARD FLAP ACCSS PANEL 584AB (C-CHECK) RO 3/24/2021 DAMAGE ON FLAP PANEL 584AB FOUND OUT OF LIMITS REF CRJ 200 SRM 57-52-00, RECEIVED NEW PANEL , LOCATED AND DRILLED REF CRJ 51-40-11 , INSTALLED ON MX 22298612 JOB 27558100 OP 7005.Feb 18, 2021 · N909SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202157015Bolt · corroded* RH OUTBD GROUND SPOILER ALL ATTACH AND PCU LINK HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW RH OUTBD GROUND SPOILER ATTACH AND PCU LINK HARDWARE REF CRJ-200 AMM 27-63-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DFeb 18, 2021 · N909SW · Cndair CL6002B19 · SpoilersSDR SWIA202157014Bolt · corroded* RH INBD GROUND SPOILER ATTACH, PCU LINK AND BONDING WIRE HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW RH INBD GROUND SPOILER ATTACH, PCU LINK AND BONDING WIRE HARDWARE REF CRJ-200 AMM 27-63-01-400-801, OPERATIONAL TEST OF THE GROUND SPOILFeb 18, 2021 · N909SW · Cndair CL6002B19 · SpoilersSDR SWIA202157013Bolt · corroded* RH FLIGHT SPOILER ALL ATTACH AND SAFETY TAB HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW RH FLIGHT SPOILER ATTACH AND SAFETY TAB HARDWARE REF CRJ-200 AMM 27-64-05-400-801, OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON CHECKED GOOD, SEEFeb 18, 2021 · N909SW · Cndair CL6002B19 · SpoilersSDR SWIA202157012Bolt · corroded* RH SPOILERON ALL ATTACH AND SAFETY TAB HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW RH SPOILERON ATTACH AND SAFETY TAB HARDWARE REF CRJ-200 27-64-01-400-801, OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON CHECKED GOOD, SEE CONTINUATION Feb 18, 2021 · N909SW · Cndair CL6002B19 · SpoilersSDR SWIA202157011Bolt · corroded* LH INBD GROUND SPOILER OUTBD ATTACH HINGE AND PCU LINK HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW LH INBD GROUND SPOILER OUTBD ATTACH HINGE AND PCU LINK HARDWARE REF CRJ-200 AMM 27-65-01-400-801, OPERATIONAL TEST OF THE GROUND SPOILERS Feb 18, 2021 · N909SW · Cndair CL6002B19 · SpoilersSDR SWIA202157010Bolt · corroded* LH OUTBD GROUND SPOILER ALL ATTACH AND PCU LINK HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 INSTALLED NEW LH OTBD GROUND SPOILER ATTACH AND PCU LINK HARDWARE REF CRJ-200 AMM 27-65-01-400-801, OPERATIONAL TEST OF THE GROUND SPOILERS CHECKED GOOD, SEE CFeb 18, 2021 · N909SW · Cndair CL6002B19 · SpoilersSDR SWIA202157009Bolt · corroded* LH FLIGHT SPOILER ALL ATTACH, SAFETY TAB AND BONDING WIRE HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 REPLACED LH FLIGHT SPOILER INBOARD AND OUTBOARD SAFETY TABS AND 4 BOLTS THAT HOLD THE TABS TO A/C, REPLACED BROKEN OUTBOARD BONDING WIRE AND THE 2 SCFeb 18, 2021 · N909SW · Cndair CL6002B19 · SpoilersSDR SWIA202157008Bolt · corroded* LH SPOILERON ALL ATTACH AND SAFETY TAB HARDWARE HAS CORROSION (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED ALL ATTACH AND SAFETY TAB HARDWARE THAT HAVE CORROSION WITH NEW HARDWARE IAW CRJ200 AMM 27-64-01-400-801STEP 2.B AND STEP 2.C. AND CRJ200 AMM 27-62Feb 18, 2021 · N909SW · Cndair CL6002B19 · SpoilersSDR SWIA202157007Frame · cracked* ACFT SIDE, FS394.00 AVIONICS AFT FRAME / RH DOOR GUIDE IS CRACKED. FLAGGED (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED THE R/H DOOR QUIDE ON THE AVIONICS AFT FRAME IAW CRJ 200 SRM 51-41-02Feb 16, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202157006Frame · cracked* ACFT SIDE, FS394.00 AVIONICS AFT FRAME / LH DOOR GUIDE IS CRACKED. FLAGGED (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED L/H DOOR GUIDE ON THE AVIONICS AFT FRAME IAW CRJ 200 SRM 51-41-02Feb 16, 2021 · N909SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202157005Frame · cracked* ACFT SIDE, FS364.00 AVIONICS FWD FRAME / LH DOOR GUIDE IS CRACKED. FLAGGED (C-CHECK) RO 3/24/2021 REMOVED AND REPLACED L/H DOOR GUIDE ON THE AVIONICS FWB FRAME IAW CRJ 200 SRM 51-41-02Feb 16, 2021 · N909SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201904035713Power Supply · failedFLAP FAIL ON DEPARTURE, COMPLIED WITH QRH. RETURNED TO FIELD. LANDED WITHOUT INCIDENT. (FLT#5300) CLOSED REMOVED AND REPLACED LEFT BPSU IAW AMM. OPS AND RIG CHECKS GOOD.Apr 3, 2019 · N909SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2018081044978Wire Harness · failedGEAR DISAGREE WARNING MESSAGE DURING CLIMB. REMOVED AND REPLACED THE NLG DOWNLOCK WIRE HARNESS NR 2 PS2GA IAW AMM. OPS CHECKED GOOD.Aug 9, 2018 · N909SW · Cndair CL6002B19 · Landing Gear System Wiring
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