N445SW

Service difficulty reports · 275

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 = 'N445SW' 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 SWIA2026040375668Flap · failedFLAP FAIL IN CRUSE AT FLAPS 0 DIVERTED BACK TO ORD FLAP 0 LANDING (FLIGHT 5076) (COMPLY WITH AD 2009-06-12 DUE TO FLAP FAIL EVENT (REFERENCE CP32008148)SEE CP 32009678 FOR REMOVAL AND REPLACEMENT OF THE RH WING BPSU.PERFORMED OPS CHECK OF THE FLAPS IAW AMMApr 3, 2026 · N445SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2026020275116Landing Gear · warning messageGEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR UP ON T/O. NOSE DOOR WAS SHOWING DN AND INDICATING GREEN. RAN QRH & ALL THREE GEARS WERE DOWN AND LOCKED. MESSAGE WAS ACCOMPANIED BY WOW OUTPUT & STEERING INOP CAUTION MESSAGE. AFTER LANDING STEERING WORKED NOFeb 2, 2026 · N445SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA202512220001Warning Message · illuminatedGEAR DISAGREE WARNING ON DEPARTURE NOSE GEAR DOWN WHILE BOTH MAINS WERE UP. RAN QRH AND EXTENDED GEAR FOR LANDING SUCCESSFULLY. (FLIGHT 5442 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31401093 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP Dec 20, 2025 · N445SW · Cndair CL6002B19 · Landing Gear SystemSDR SWI2025F01312Warning Message · activatedFLAPS FAIL CAUTION MESSAGE IN CRUISE. RAN QRH, LANDED NORMALLY. DESCENT RATE AT TOUCHDOWN 300FPM. (FLIGHT 4728 - FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLESSep 12, 2025 · N445SW · Cndair CL6002B19 · Central WarningSDR J6BA202406101114Keeper · damagedTRANSFER FROM EAML 615 : TRANSFERRED FROM CAMP 35722. UPON REMOVAL OF LT WING FLIGHT SPOILER OB PCU BOLT TO REPLACE DAMAGED ANTI ROTATION KEEPER WC5152 FOUND GOUGED SPOILER HINGE ON T/E OF WING, EVAL (C-CHECK RO 1/3/2024) REMOVED AND INSTALLED NEW SPOILERNov 14, 2023 · N445SW · Cndair CL6002B19 · Wing StructureSDR SWIA202405301114Keeper · damagedTRANSFER FROM EAML 615 : TRANSFERRED FROM CAMP 35722. UPON REMOVAL OF LT WING FLIGHT SPOILER OB PCU BOLT TO REPLACE DAMAGED ANTI ROTATION KEEPER WC5152 FOUND GOUGED SPOILER HINGE ON T/E OF WING, EVAL (C-CHECK RO 1/3/2024) REMOVED AND INSTALLED NEW SPOILERNov 14, 2023 · N445SW · Cndair CL6002B19 · SpoilersSDR J6BA2024061030919Floor Panel · crackedLH FWD EQUIPMENT COMP THE FLOOR PANEL IS CRACKED AT FR193 (C-CHECK RO 11/16/2023) PERFORMED DOUBLER REPAIR AT LH FWD EQUIPMENT COMP. FLOOR PANEL FR 193 . PERFORMED NDT INSPECTION ON CUTOUT BY BARON NDT LLC FAA CRS#5NDR545D REPORT #S101923-1 WITH NO DEFECTSep 19, 2023 · N445SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2024053000919Floor Panel · crackedLH FWD EQUIPMENT COMP THE FLOOR PANEL IS CRACKED AT FR193 (C-CHECK RO 11/16/2023) PERFORMED DOUBLER REPAIR AT LH FWD EQUIPMENT COMP. FLOOR PANEL FR 193 . PERFORMED NDT INSPECTION ON CUTOUT BY BARON NDT LLC FAA CRS#5NDR545D REPORT #S101923-1 WITH NO DEFECTSep 19, 2023 · N445SW · Cndair CL6002B19 · Fuselage Floor PanelSDR J6BA2024061000917Frame · corrodedAVIONICS BAY FR 364 FWD FACE HAS SIGNS OF CORROSION BETWEEN STGR 27 AND 25R (C-CHECK RO 11/16/2023) REMOVED CORROSION AT AVIONICS BAY FR364 FWD FACE BETWEEN STGR 27R AND 25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT # $092723-4. ORIGINAL THISep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR J6B202406100006Intercostal · corrodedAVIONICS BAY R/H O/B INTERCOSTAL BETWEEN FR 394 AND FR 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION AND PERFORMED NDT ET/UT INSPECTION NDT LLC FAA CRS#5NDR545D REPORT #S092723-2 EVALUATED BLENDED AREA AT AVIONICS BAY ON RH O/B INTERCOSTSep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR J6B202406100004Intercostal · corrodedAVIONICS BAY AT STGR 25R INTERCOASTAL BETWEEN FR 409 AND 409 + 16, SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION AT AVIONICS BAY ON STR 25R INTERCOSTAL BETWEEN FR 409 AND FR409+16,PERFORMED NDT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D RSep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR J6B202406100002Case · gougedEVAL GOUGED RT ENG FAN CASE AT 12 OCLOCK POSITION JUST FWD OF FAN CASE BOLTS (C-CHECK RO 11/16/2023) PERFORMED REPAIR OF GOUGED RT ENG. FAN CASE AT 12 OCLOCK POSITION IAW CRJ-200 REO 601R-71-61-4364. REV. -- DATE: 2023-10-12. PERFORMED NDT ET/UT INSPECTSep 17, 2023 · N445SW · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR J6B202406100001Frame · corrodedAVIONICS BAY FR 409 AFT SUPPORT BRACKETS BETWEEN STGR 26R AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION IN AVIONICS BAY FR 409 AFT SUPPORT BRACKET BTW STGR 26R AND 25R I.A.W. CRJ200 SRM 53-00-00. NDT PERFORMED BY BARON NDT LLC, FSep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, FrameSDR J6B2024061000007Frame · corrodedAVIONICS BAY FR 349 FWD FACE BETWEEN STGR 25R AND 24R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED AREA AT AVIONICS BAY ON FR 349 FWD FACE BETWEEN STGR 25R AND STGR 24R, PERFORMED NDT ET/UT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S0928Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, FrameSDR J6B2024061000005Intercostal · corrodedAVIONICS BAY L/H INBOARD INTERCOSTAL BETWEEN FR 394 AND 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT AREA ON AVIONICS BAY L/H O/B INTERCOSTAL. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #S092723-1. ORIGINAL THICKNESS 0.080" MATESep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR J6B20240610000014Frame · corrodedAVIONICS BAY FR 349 AFT FACE BETWEEN STGR 26L AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION AT AVIONICS BAY FR349 AFT FACE BETWEEN STGR26L AND STGR25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #$101223-2. ORIGINAL Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00443Intercostal · corrodedAVIONICS BAY AT STGR 25R INTERCOASTAL BETWEEN FR 409 AND 409 + 16, SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION AT AVIONICS BAY ON STR 25R INTERCOSTAL BETWEEN FR 409 AND FR409+16,PERFORMED NDT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D RSep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00442Shear Tie · corrodedAVIONICS BAY, AFT FACE FR 409, FOOT SPLICE HAS SIGNS OF CORROSION BETWEEN STGR 26L AND 26R (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION AT AFT FACE FR409 FOOT SPLICE BETWEEN STGR26R AND 26L. NDT PERFORMED BY NDT UT/ET BY BARON NDT FAA CRS #5NDR545D, REPORSep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWI2024F00441Case · gougedEVAL GOUGED RT ENG FAN CASE AT 12 OCLOCK POSITION JUST FWD OF FAN CASE BOLTS (C-CHECK RO 11/16/2023) PERFORMED REPAIR OF GOUGED RT ENG. FAN CASE AT 12 OCLOCK POSITION IAW CRJ-200 REO 601R-71-61-4364. REV. -- DATE: 2023-10-12. PERFORMED NDT ET/UT INSPECTSep 17, 2023 · N445SW · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR SWI2024F00440Support Bracket · corrodedAVIONICS BAY FR 409 AFT SUPPORT BRACKETS BETWEEN STGR 26R AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION IN AVIONICS BAY FR 409 AFT SUPPORT BRACKET BTW STGR 26R AND 25R I.A.W. CRJ200 SRM 53-00-00. NDT PERFORMED BY BARON NDT LLC, FSep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00439Frame · corrodedAVIONICS BAY FR 349 AFT FACE BETWEEN STGR 26L AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION AT AVIONICS BAY FR349 AFT FACE BETWEEN STGR26L AND STGR25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #$101223-2. ORIGINAL Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F00438Frame · corrodedAVIONICS BAY FR 349 FWD FACE BETWEEN STGR 25R AND 24R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED AREA AT AVIONICS BAY ON FR 349 FWD FACE BETWEEN STGR 25R AND STGR 24R, PERFORMED NDT ET/UT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S0928Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F00437Intercostal · corrodedAVIONICS BAY R/H O/B INTER-COASTAL BETWEEN FR 394 AND FR 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION AND PERFORMED NDT ET/UT INSPECTION BY BARON NDT LLC FAA CRS#5NDR545D REPORT #S092723-2 EVALUATED BLENDED AREA AT AVIONICS BAY ON RH O/Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00436Intercostal · corrodedAVIONICS BAY L/H INBOARD INTER-COASTAL BETWEEN FR 394 AND 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT AREA ON AVIONICS BAY L/H O/B INTERCOSTAL. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #S092723-1. ORIGINAL THICKNESS 0.080" MASep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F00435Structure · corrodedAVIONICS BAY FR 364 FWD FACE HAS SIGNS OF CORROSION BETWEEN STGR 27 AND 25R (C-CHECK RO 11/16/2023) REMOVED CORROSION AT AVIONICS BAY FR364 FWD FACE BETWEEN STGR 27R AND 25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT # $092723-4. ORIGINAL THISep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024053000917Intercostal · corrodedAVIONICS BAY L/H INBOARD INTER-COASTAL BETWEEN FR 364 AND FR 349 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION ON AVIONICS BAY L/H INBOARD INTERCOSTAL BETWEEN FR 364 AND FR349, PERFORMED NDT UT/ET INSPECTION BY BARON NDT FAA CRS#5NDR545D, RESep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR J6BA202406100916Hinge · corrodedSIGNS OF CORROSION ON LH IB FLAP HINGE FWD ATTACHMENT HOLE AT WS80.50 (C-CHECK RO 11/16/2023) REMOVED CORROSION FROM LH INBD FWD WS 80.50.NDT PERFORMED BY BARON NDT ,LLC FAA CRS # 4NDR545D, PERFORMED ET/UT REPORT #S100423-14.PERFORMED LPI REPORT #S101923-3Sep 16, 2023 · N445SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2024053000916Hinge Fitting · corrodedSIGNS OF CORROSION ON LH IB FLAP HINGE FWD ATTACHMENT HOLE AT WS80.50 (C-CHECK RO 11/16/2023) REMOVED CORROSION FROM LH INBD FWD WS 80.50.NDT PERFORMED BY BARON NDT ,LLC FAA CRS # 4NDR545D, PERFORMED ET/UT REPORT #S100423-14.PERFORMED LPI REPORT #S101923-3Sep 16, 2023 · N445SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090452266Bracket · crackedLOWER CHANNEL ON FWD SIDE OF CARGO DOOR TRACK IS CRACKED. C-CHECK RO 9/1/2020. REMOVED AND REPLACED LOWER CHANNEL BRACKET ON FWD SIDE OF THE CARGO DOOR TRACK WITH NEW PART REFERENCE CRJ200 SRM & BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.Aug 31, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452265Doubler · corrodedDOUBLER PN.601R10203-32 ATTACHED TO THE OUTBOARD OF RT BATTERY RIB AT APROXIMATELY WS53.6 IS CORRODED. C-CHECK RO 9/1/2020. BLENDED CORROSION FROM DOUBLER PN.601R10203-32 ATTACHED TO THE OUTBOARD OF RT BATTERY RIB AT APROXIMATELY WS53.6 REF CRJ 200 SRM. EVAAug 21, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020090452264Stiffener · crackedFS 621 AFT BULKHEAD LT LOWER STIFFENER OUTBOARD FOR LBL36 AT STGR 16 IS CRACKED. REMOVED AND INSTALLED NEW STIFFENER (601R36008-51) ON FS621 AFT BULKHEAD AT LBL36, STGR16, REF CRJ 200 SRM, & DWG.Aug 8, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020090452263Former · corrodedPASSENGER DOOR AFT FORMER SUPPORT ANGLE UNDER SEAL RETAINER @ FS.347 IS CORRODED. C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT FORMER SUPPORT ANGLE AT FS.347 REF CRJ 200 SRM AND DWG.Aug 6, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020090452262Bulkhead Web · chafedFS 621 BULKHEAD HAS 3 CHAFE MARKS 3"? ABOVE FLOOR AT APPROXIMATELY LBL 23, RBL 31, AND RBL 41. C-CHECK RO 9/1/2020. REMOVED DAMAGE AT PRESSURE BULKHEAD F/S 621 APPROX 3" ABOVE FLOOR AT LBL 23, AT RBL 31, AND RBL 41 IAW CRJ 200 SRM. BLENDED AREAS AT RBL41 ANAug 5, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020090452261Skin · dentedEVALUATE DENT JUST AFT OF PITOT- STATIC BELOW CO-PILOT SIDE WINDOW. REPAIRED FUSELAGE SKIN JUST AFT OF PITOT STATIC BELOW CO-PILOT SIDE WINDOW, REF REO. PRESSURE CHECK GOOD.Aug 4, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020090452260Former · corrodedPASSENGER DOOR AFT FORMER @ FS.347 IS CORRODED. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT FORMER AT FS.347, REF CRJ 200 SRM AND DWG.Aug 2, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020090452259Angle · corrodedCLIP AT FS.338 NEAR PASSENGER DOOR HINGE IS CORRODED. REMOVED CLIP AT FS.338 AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW CLIP AT FS.338 NEAR THE PASSENGER DOOR HINGE, REF MHIRJ DWG. AND CRJ 200 SRM. COMPLIED WITH TASK CARD.Aug 2, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020090452258Intercostal · corrodedINTERCOSTAL AT DD1 BETWEEN FS.323-335 IS CORRODED. REMOVED AND INSTALLED A NEW INTERCOSTAL AT DD1 BETWEEN FS323-FS335. REF DWG, CRJ 200 SRM.Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452257Intercostal · corrodedINTERCOSTAL AT DD3 BETWEEN FS.320-338 IS CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL AT DD3 BETWEEN FS.320-338 REF CRJ 200 SRM AND DWG.Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452256Intercostal · corrodedINTERCOSTAL AT DD7 BETWEEN FS.320-328 IS CORRODED. REMOVED AND INSTALLED A NEW PASSENGER DOOR INTERCOSTAL AT DD7 BETWEEN FS320-FS328. REF DWG AND SRM. DETAILS.Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452255Frame · corrodedFRAME AF FS.313 BETWEEN DD4-DD5 IS CORRODED. REMOVED AND INSTALLED NEW FRAME AT FS313 BETWEEN DD4 AND DD5. REF DWG AND CRJ 200 SRM. DETAILS.Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020090452254Intercostal · corrodedINTERCOSTAL AT DD5 BETWEEN FS.311-320 IS CORRODED. REMOVED AND INSTALLED A NEW INTERCOSTAL AT DD5 BETWEEN FS311-FS320. REF DWG AND SRM.Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452253Door Frame · corrodedTHE PASSENGER DOOR FORMER AT FS311.75 AT DD5 HAS CORROSION. REMOVED AND INSTALLED NEW PASSENGER DOOR FWD FORMER AT FS311.75 IAW SRM AND DWG.Aug 1, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020090452252Intercostal · corrodedTHE PASSENGER DOOR INTERCOSTAL BETWEEN FS329.50 AND FS338.00 AT DD6 HAS CORROSION. REMOVED AND INSTALLED A NEW INTERCOSTAL AND CLEAT AT DD6 FROM FS320-FS338. REF DWG, AND SRM.Aug 1, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020090452251Intercostal · corrodedTHE PASSENGER DOOR INTERCOSTAL BETWEEN FS320.10 AND FS329.50 AT DD4 HAS CORROSION. (MARKED). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED INTERCOSTAL AT DD4 BETWEEN FS.320.10-329.5 REF CRJ 200 SRM AND DWG.Aug 1, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020090452250Angle · corrodedRIGHT BATTERY RIB AT WS53.60 HAS CORROSION ON FORWARD CHANNEL, ANGLES AND DOUBLE. REPLACED AND INSTALLED REPLACEMENT ANGLE P/N 601R10203-25 PO: T54192 AT RT BATTERY RIB AT WS53.60. REF. CRJ 200 SRM AND DWG COMPLIED WITH SKYWEST TASK CARD.Aug 1, 2020 · N445SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA2020090452249Angle · corrodedLEFT BATTERY RIB AT WS53.60 HAS CORROSION ON THE INBOARD SIDE OF THE UPPER ANGLE AT RADIUS (MARKED). C-CHECK RO 9/1/2020. REMOVED CORROSION ON LT BATTERY RIB AT WS53.60, REF. CRJ200 SRM. REMOVED UPPER REINFORCEMENT ANGLE AND HI LITES TO FOM, REF. CRJ200 SRM.Aug 1, 2020 · N445SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA2020090452248Access Panel · gougedLT WING AUX SPAR ACCESS PANEL 540AT RECESSED AREA FOR CLOSEOUT PANEL HAS SCRAPES AND GOUGES INTO BASE METAL AS MARKED. C-CHECK RO 9/1/2020. BLENDED DAMAGE TO A SMOOTH FINISH ON LT WING AUX SPAR AT ACCESS PANEL 540AT, NDT INSPECTED NO DEFECTS NOTED, ROTO PEENJul 31, 2020 · N445SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020090452301Pin · corrodedLT EMERGENCY DOOR CUTOUT LOWER SILL CLEVIS PINS CORRODED. C-CHECK RO 9/1/2020. REMOVED AND REPLACED LT EMERGENCY DOOR CUTOUT LOWER SILL CLEVIS PIN, REF CRJ 200 AMM.Jul 30, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452300Door Sill · corrodedRT EMERGENCY DOOR CUTOUT LOWER SILL CLEVIS PINS CORRODED. C-CHECK RO 9/1/2020. REMOVED AND REPLACED RT EMERGENCY DOOR CUTOUT LOWER SILL CLEVIS PIN REF CRJ 200 AMM.Jul 30, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202052247Angle · crackedCLIP AT APPROXIMATELY STR 13R, BETWEEN FS621 AND FS625, IS CRACKED. REMOVED AND INSTALLED CLIP IAW DWG AND SRM.Jul 29, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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