# Service difficulty reports: N445SW

A list on [N445SW](https://openairdocs.org/aircraft/N445SW.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 6 · 275 reports

- [SDR SWIA2026040375668](https://openairdocs.org/sdr/SWIA2026040375668.md): Flap · failed · Apr 3, 2026 · N445SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP 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 AMM
- [SDR SWIA2026020275116](https://openairdocs.org/sdr/SWIA2026020275116.md): Landing Gear · warning message · Feb 2, 2026 · N445SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR 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 NO
- [SDR SWIA202512220001](https://openairdocs.org/sdr/SWIA202512220001.md): Warning Message · illuminated · Dec 20, 2025 · N445SW · Cndair CL6002B19 · Landing Gear System
  > GEAR 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
- [SDR SWI2025F01312](https://openairdocs.org/sdr/SWI2025F01312.md): Warning Message · activated · Sep 12, 2025 · N445SW · Cndair CL6002B19 · Central Warning
  > FLAPS 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 CYCLES
- [SDR J6BA202406101114](https://openairdocs.org/sdr/J6BA202406101114.md): Keeper · damaged · Nov 14, 2023 · N445SW · Cndair CL6002B19 · Wing Structure
  > TRANSFER 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 SPOILER
- [SDR SWIA202405301114](https://openairdocs.org/sdr/SWIA202405301114.md): Keeper · damaged · Nov 14, 2023 · N445SW · Cndair CL6002B19 · Spoilers
  > TRANSFER 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 SPOILER
- [SDR J6BA2024061030919](https://openairdocs.org/sdr/J6BA2024061030919.md): Floor Panel · cracked · Sep 19, 2023 · N445SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LH 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 DEFECT
- [SDR SWIA2024053000919](https://openairdocs.org/sdr/SWIA2024053000919.md): Floor Panel · cracked · Sep 19, 2023 · N445SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LH 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 DEFECT
- [SDR J6BA2024061000917](https://openairdocs.org/sdr/J6BA2024061000917.md): Frame · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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 THI
- [SDR J6B202406100006](https://openairdocs.org/sdr/J6B202406100006.md): Intercostal · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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 INTERCOST
- [SDR J6B202406100004](https://openairdocs.org/sdr/J6B202406100004.md): Intercostal · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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 R
- [SDR J6B202406100002](https://openairdocs.org/sdr/J6B202406100002.md): Case · gouged · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Turbine Engine Air Inlet Section
  > EVAL 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 INSPECT
- [SDR J6B202406100001](https://openairdocs.org/sdr/J6B202406100001.md): Frame · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AVIONICS 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, F
- [SDR J6B2024061000007](https://openairdocs.org/sdr/J6B2024061000007.md): Frame · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AVIONICS 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# S0928
- [SDR J6B2024061000005](https://openairdocs.org/sdr/J6B2024061000005.md): Intercostal · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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" MATE
- [SDR J6B20240610000014](https://openairdocs.org/sdr/J6B20240610000014.md): Frame · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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
- [SDR SWI2024F00443](https://openairdocs.org/sdr/SWI2024F00443.md): Intercostal · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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 R
- [SDR SWI2024F00442](https://openairdocs.org/sdr/SWI2024F00442.md): Shear Tie · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > AVIONICS 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, REPOR
- [SDR SWI2024F00441](https://openairdocs.org/sdr/SWI2024F00441.md): Case · gouged · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Turbine Engine Air Inlet Section
  > EVAL 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 INSPECT
- [SDR SWI2024F00440](https://openairdocs.org/sdr/SWI2024F00440.md): Support Bracket · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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, F
- [SDR SWI2024F00439](https://openairdocs.org/sdr/SWI2024F00439.md): Frame · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AVIONICS 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
- [SDR SWI2024F00438](https://openairdocs.org/sdr/SWI2024F00438.md): Frame · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AVIONICS 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# S0928
- [SDR SWI2024F00437](https://openairdocs.org/sdr/SWI2024F00437.md): Intercostal · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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/
- [SDR SWI2024F00436](https://openairdocs.org/sdr/SWI2024F00436.md): Intercostal · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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" MA
- [SDR SWI2024F00435](https://openairdocs.org/sdr/SWI2024F00435.md): Structure · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Main, Structure
  > AVIONICS 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 THI
- [SDR SWIA2024053000917](https://openairdocs.org/sdr/SWIA2024053000917.md): Intercostal · corroded · Sep 17, 2023 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AVIONICS 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, RE
- [SDR J6BA202406100916](https://openairdocs.org/sdr/J6BA202406100916.md): Hinge · corroded · Sep 16, 2023 · N445SW · Cndair CL6002B19 · Trailing Edge Flaps
  > SIGNS 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 #S101923-3
- [SDR SWIA2024053000916](https://openairdocs.org/sdr/SWIA2024053000916.md): Hinge Fitting · corroded · Sep 16, 2023 · N445SW · Cndair CL6002B19 · Trailing Edge Flaps
  > SIGNS 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 #S101923-3
- [SDR SWIA2020090452266](https://openairdocs.org/sdr/SWIA2020090452266.md): Bracket · cracked · Aug 31, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER 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.
- [SDR SWIA2020090452265](https://openairdocs.org/sdr/SWIA2020090452265.md): Doubler · corroded · Aug 21, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DOUBLER 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. EVA
- [SDR SWIA2020090452264](https://openairdocs.org/sdr/SWIA2020090452264.md): Stiffener · cracked · Aug 8, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 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.
- [SDR SWIA2020090452263](https://openairdocs.org/sdr/SWIA2020090452263.md): Former · corroded · Aug 6, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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.
- [SDR SWIA2020090452262](https://openairdocs.org/sdr/SWIA2020090452262.md): Bulkhead Web · chafed · Aug 5, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 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 AN
- [SDR SWIA2020090452261](https://openairdocs.org/sdr/SWIA2020090452261.md): Skin · dented · Aug 4, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EVALUATE 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.
- [SDR SWIA2020090452260](https://openairdocs.org/sdr/SWIA2020090452260.md): Former · corroded · Aug 2, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT FORMER @ FS.347 IS CORRODED. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT FORMER AT FS.347, REF CRJ 200 SRM AND DWG.
- [SDR SWIA2020090452259](https://openairdocs.org/sdr/SWIA2020090452259.md): Angle · corroded · Aug 2, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CLIP 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.
- [SDR SWIA2020090452258](https://openairdocs.org/sdr/SWIA2020090452258.md): Intercostal · corroded · Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT DD1 BETWEEN FS.323-335 IS CORRODED. REMOVED AND INSTALLED A NEW INTERCOSTAL AT DD1 BETWEEN FS323-FS335. REF DWG, CRJ 200 SRM.
- [SDR SWIA2020090452257](https://openairdocs.org/sdr/SWIA2020090452257.md): Intercostal · corroded · Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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.
- [SDR SWIA2020090452256](https://openairdocs.org/sdr/SWIA2020090452256.md): Intercostal · corroded · Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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.
- [SDR SWIA2020090452255](https://openairdocs.org/sdr/SWIA2020090452255.md): Frame · corroded · Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 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.
- [SDR SWIA2020090452254](https://openairdocs.org/sdr/SWIA2020090452254.md): Intercostal · corroded · Aug 2, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT DD5 BETWEEN FS.311-320 IS CORRODED. REMOVED AND INSTALLED A NEW INTERCOSTAL AT DD5 BETWEEN FS311-FS320. REF DWG AND SRM.
- [SDR SWIA2020090452253](https://openairdocs.org/sdr/SWIA2020090452253.md): Door Frame · corroded · Aug 1, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Structure
  > THE 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.
- [SDR SWIA2020090452252](https://openairdocs.org/sdr/SWIA2020090452252.md): Intercostal · corroded · Aug 1, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew Doors
  > THE 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.
- [SDR SWIA2020090452251](https://openairdocs.org/sdr/SWIA2020090452251.md): Intercostal · corroded · Aug 1, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew Doors
  > THE 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.
- [SDR SWIA2020090452250](https://openairdocs.org/sdr/SWIA2020090452250.md): Angle · corroded · Aug 1, 2020 · N445SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > RIGHT 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.
- [SDR SWIA2020090452249](https://openairdocs.org/sdr/SWIA2020090452249.md): Angle · corroded · Aug 1, 2020 · N445SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT 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.
- [SDR SWIA2020090452248](https://openairdocs.org/sdr/SWIA2020090452248.md): Access Panel · gouged · Jul 31, 2020 · N445SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LT 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 PEEN
- [SDR SWIA2020090452301](https://openairdocs.org/sdr/SWIA2020090452301.md): Pin · corroded · Jul 30, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT 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.
- [SDR SWIA2020090452300](https://openairdocs.org/sdr/SWIA2020090452300.md): Door Sill · corroded · Jul 30, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT 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.
- [SDR SWIA202052247](https://openairdocs.org/sdr/SWIA202052247.md): Angle · cracked · Jul 29, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT APPROXIMATELY STR 13R, BETWEEN FS621 AND FS625, IS CRACKED. REMOVED AND INSTALLED CLIP IAW DWG AND SRM.

Next page: https://openairdocs.org/aircraft/N445SW/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 = 'N445SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N445SW/reports

---
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.