# Service difficulty reports: N446SW

A list on [N446SW](https://openairdocs.org/aircraft/N446SW.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 5 · 203 reports

- [SDR J6BA2024061000226](https://openairdocs.org/sdr/J6BA2024061000226.md): Fuel Line · cut · Feb 26, 2024 · N446SW · Cndair CL6002B19 · APU Engine Fuel and Control
  > AT CRUISE FL310 WE COULD SMELL A MODERATELY STRONG EXHAUST SMELL SIMILAR TO OIL OR GAS BURNING. THIS WAS STRONGEST IN THE FLIGHT DECK BUT ALSO NOTICEABLE IN THE CABIN. THE SMELL DISSIPATED DURING DESCENT AND HAD NOT BEEN PRESENT IN THE CLIMB OUT. (FLIGHT 4910
- [SDR SWIA2024053000226](https://openairdocs.org/sdr/SWIA2024053000226.md): Fuel Line · cut · Feb 26, 2024 · N446SW · Cndair CL6002B19 · APU Engine Fuel and Control
  > AT CRUISE FL310 WE COULD SMELL A MODERATELY STRONG EXHAUST SMELL SIMILAR TO OIL OR GAS BURNING. THIS WAS STRONGEST IN THE FLIGHT DECK BUT ALSO NOTICEABLE IN THE CABIN. THE SMELL DISSIPATED DURING DESCENT AND HAD NOT BEEN PRESENT IN THE CLIMB OUT. (FLIGHT 4910
- [SDR SWIA20230201](https://openairdocs.org/sdr/SWIA20230201.md): Not Entered · warning message · Feb 1, 2023 · N446SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR DISAGREE WARNING MESSAGE CAME ON AFTER TAKEOFF. RIGHT MLG INDICATED UNSAFE. RAN THE QRH. MESSAGE WENT OUT. RIGHT MLG INDICATED UP. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26157809 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 26
- [SDR SWIA202266597](https://openairdocs.org/sdr/SWIA202266597.md): None · uncontrollable · Oct 7, 2022 · N446SW · Cndair CL6002B19 · Rudder Tab Control System
  > RUDDER LOCKED UP AT FLIGHT IDLE IN THE LANDING FLARE. NO RUDDER MOVEMENT AVAILABLE. (FLIGHT 4301 - FILED CLOSED) INSPECTED RUDDER SYSTEM CONTROL PATH REFERENCE EAMLS 1009518, 1009408, 100949 NO DEFECTS NOTED. INSPECTED POTENTIOMETER IN REFERENCE TO AMM 27-
- [SDR SWIA202265545](https://openairdocs.org/sdr/SWIA202265545.md): None · odor · Apr 30, 2022 · N446SW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > STRONG SMELL OF FUEL WHEN PACKS ARE ON WITH BOTH APU AND ENGINE BLEEDS. BOTH IN AIR AND ON GROUND. (FLIGHT 4267 - FILED CLOSED) PLEASE REFERENCE AML 898096 REMOVED AND REPLACED APU FUEL LINE REFERENCING AMM 49-31-01. OPS CHECK OF FUEL SYSTEM AND AIR CONDI
- [SDR SWIA202161083](https://openairdocs.org/sdr/SWIA202161083.md): None · failed · Sep 17, 2021 · N446SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > ***CAT II NOT AUTHORIZED*** / D: DURING APPROACH, GEAR WAS SELECTED DOWN (180 KNOTS) AND RECEIVED A GEAR DISAGREE WARNING MESSAGE. THE NOSE DOOR OPENED BUT THE NOSE GEAR REMAINED UP (UP INDICATION). COMPLIED WITH QRH AND THE LANDING GEAR EXTENDED NORMALLY / C:
- [SDR SWIA202158627](https://openairdocs.org/sdr/SWIA202158627.md): Landing Gear · faulted · Jun 4, 2021 · N446SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON APPROACH GOT GEAR DISAGREE, RIGHT MAIN. FOLLOWED QRH CYCLED GEAR AND MESSAGE CLEARED. LANDING NORMAL. ON APPROACH GOT GEAR DISAGREE, RIGHT MAIN. FOLLOWED QRH CYCLED GEAR AND MESSAGE CLEARED. LANDING NORMAL. (FLIGHT 4306) DEFERRED LANDING GEAR RETRA
- [SDR SWIA202157245](https://openairdocs.org/sdr/SWIA202157245.md): Wire Harness · crushed · Apr 4, 2021 · N446SW · Cndair CL6002B19 · Landing Gear System Wiring
  > D:GEAR DISAGREE WARNING MESSAGE ON APPROACH (RIGHT MAIN GEAR), LANDING GEAR LEVER WAS SELECTED UP IN THE GO-AROUND. COMPLIED WITH QRH, ALL LANDING GEAR EXTENDED NORMALLY ON SECOND ATTEMPT. / C: MEL 32-30-1 / CAT A DUE WITHIN 1 FLIGHT DAY FROM 04/04/2021 / CAT
- [SDR SWIA202156245](https://openairdocs.org/sdr/SWIA202156245.md): Warning Message · illuminated · Feb 16, 2021 · N446SW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > ON DEPARTURE WHILE SELECTING FLAPS FROM 8 TO 0 HAD FLAPS FAIL CAUTION MSG. COMPLIED WITH QRH. FLIGHT 4240 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22314362 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH PARAGRAPH (H)(6) OF AD 200
- [SDR SWIA202053737](https://openairdocs.org/sdr/SWIA202053737.md): Panel · debonded · Oct 18, 2020 · N446SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STABILIZER PANEL 333AL HAS DISBONDED UPPER AND LOWER GROUNDING PLATES. C-CHECK RO 10/29/2020. REMOVED AND REPLACED PANEL 333AL, REF AMM, CHECK OK.
- [SDR SWIA202053757](https://openairdocs.org/sdr/SWIA202053757.md): Nut Plate · broken · Oct 16, 2020 · N446SW · Cndair CL6002B19 · Aerodynamic Fairings
  > WING TO BODY FAIRING 195AL HAS A BROKEN NUT-PLATE, MARKED. C-CHECK RO 10/29/2020. REMOVED AND INSTALLED NEW NUT-PLATE P/N NAS1474A3 AT WING TO BODY FAIRING PANEL 195AL, REF CRJ 200 SRM.
- [SDR SWIA202053736](https://openairdocs.org/sdr/SWIA202053736.md): Door Frame · corroded · Oct 9, 2020 · N446SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FRAME FS 313.56 P/N 601R318086-1 CORRODED ON MULTIPLE SURFACES. C-CHECK RO 10/29/2020. FOUND PAX DOOR FRAME AT FS OH 313.56 TO BE OUT OF LIMITS, PER CRJ 200 SRM. REMOVED AND INSTALLED A NEW PAX DOOR FRAME AT FS.313.56, REF CRJ 200 AMM AND DWG. P
- [SDR SWIA202053750](https://openairdocs.org/sdr/SWIA202053750.md): Hinge Fitting · corroded · Oct 7, 2020 · N446SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT OUTBOARD FLAP, OUTBOARD HINGE ARM ASSEMBLY, AFT ATTACH BOLT CASTLE NUT APPEARS CORRODED. C-CHECK RO 10/29/2020. REPLACED LT OUTBOARD FLAP, OUTBOARD HINGE ARM ASSEMBLY, AFT ATTACH BOLT CASTLE NUT AND COTTER PIN WITH NEW PARTS (P/N: MS17825-4 AND P/N: MS246
- [SDR SWIA202053735](https://openairdocs.org/sdr/SWIA202053735.md): Intercostal · corroded · Oct 4, 2020 · N446SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD4 INTERCOSTAL (P/N 601R31902-317) HAS CORROSION. C-CHECK RO 10/29/2020. REMOVED CORROSION AND FOUND PAX DOOR INTERCOSTAL DD4 TO BE OUT OF LIMITS, REF CRJ 200 SRM. REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD4, REF CRJ 200 SRM AND DWG. PE
- [SDR SWIA202053734](https://openairdocs.org/sdr/SWIA202053734.md): Intercostal · corroded · Oct 4, 2020 · N446SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD6 INTERCOSTAL (P/N 601R3180571) HAS CORROSION. C-CHECK RO 10/29/2020. FOUND PAX DOOR INTERCOSTAL DD6 TO BE OUT OF LIMITS, AS PER CRJ 200 SRM. REMOVED AND INSTALLED A NEW PAX DOOR INTERCOSTAL DD6, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA202053733](https://openairdocs.org/sdr/SWIA202053733.md): Former · corroded · Oct 4, 2020 · N446SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER AT FS 347.25 HAS CORROSION. C-CHECK RO 10/29/2020. REMOVED CORROSION ON THE PAX DOOR AFT FORMER AT FS 347.25, REF CRJ 200 SRM, FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW PAX DOOR AFT FORMER AT FS 347.25, REF CRJ 200 SRM AND
- [SDR SWIA202053732](https://openairdocs.org/sdr/SWIA202053732.md): Attach Angle · corroded · Oct 4, 2020 · N446SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR FWD FORMER AT FS 311.75 HAS CORROSION. C-CHECK RO 10/29/2020. PAX DOOR FWD FORMER AT FS 311.75, FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRM. REMOVED AND INSTALLED A NEW PAX DOOR FWD FORMER, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD. PERFORM
- [SDR SWIA202053731](https://openairdocs.org/sdr/SWIA202053731.md): Support · cracked · Oct 1, 2020 · N446SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER NET SUPPORT, LOWER CLIP AT FS 621 CRACKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED CLIP P/N 601R35050-109, REF CRJ 200 SRM AND DWG.
- [SDR SWIA202053730](https://openairdocs.org/sdr/SWIA202053730.md): Bracket · cracked · Oct 1, 2020 · N446SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT BALANCE SPRING MOUNT STRUCTURE ON FS 621 BULKHEAD IS CRACKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET ON THE FS 621 BULKHEAD, REF CRJ 200 SRM AND DWG. PERFORMED PRESSURE CHECK, REF CRJ 200 A
- [SDR SWIA202053755](https://openairdocs.org/sdr/SWIA202053755.md): Fitting · chafed · Sep 29, 2020 · N446SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT LATCH PIN FITTING ON FS 621.00 BULKHEAD CHAFED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR AFT LOWER CROTCH FITTING, REF CRJ200 SRM. CHECKS ARE GOOD AT THIS TIME.
- [SDR SWIA202053754](https://openairdocs.org/sdr/SWIA202053754.md): Fitting · chafed · Sep 29, 2020 · N446SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD LATCH PIN FITTING ON DOOR SURROUND CHAFED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR FWD LATCH PIN FITTING, REF CRJ200 SRM. CHECKS ARE GOOD AT THIS TIME.
- [SDR SWIA202053749](https://openairdocs.org/sdr/SWIA202053749.md): Stop Fitting · corroded · Sep 29, 2020 · N446SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR BOTTOM AFT STOP FITTING ON SILL CORRODED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR LOWER AFT STOP FITTING, REF CRJ200 SRM. CHECKS ARE GOOD AT THIS TIME.
- [SDR SWIA202053748](https://openairdocs.org/sdr/SWIA202053748.md): Stop Fitting · corroded · Sep 29, 2020 · N446SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR BOTTOM FWD STOP FITTING ON SILL CORRODED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED THE CARGO DOOR LOWER FWD STOP FITTING, REF CRJ200 SRM. CHECKS ARE GOOD AT THIS TIME.
- [SDR SWIA202053747](https://openairdocs.org/sdr/SWIA202053747.md): Hinge Fitting · corroded · Sep 29, 2020 · N446SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT & RT OUTBOARD FLAP CENTER HINGEBOX AT WS 222.00, AFT ATTACHING NUTS CORRODED, MARKED. C-CHECK RO 10/29/2020. INSTALLED 4 EA NEW AFT ATTACHING NUTS ON THE LT AND RT OUTBOARD CENTER HINGEBOX AT WS 222.00, REF CRJ200 AMM. TQ WRENCH TUC7837 NEXT CAL DUE: 30-
- [SDR SWIA202053746](https://openairdocs.org/sdr/SWIA202053746.md): Ground Stud · corroded · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Fuselage Main, Bulkhead Fuselage wiring
  > FS 409.00+80 STRG 0 CORRODED GROUND STUD HARDWARE, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED STUDS, REF AMM, CHECK OK.
- [SDR SWIA202053743](https://openairdocs.org/sdr/SWIA202053743.md): Doubler · corroded · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LT WS 53.60 BATT RIB CANNON PLUG DOUBLER CORRODED, MARKED. C-CHECK RO 10/29/2020. REMOVED CORRODED CANNON PLUG DOUBLER AND INSTALLED NEW LT WS 53.60 BATT RIB CANNON PLUG DOUBLER P/N 601R10203-33, REF CRJ 200 SRM AND DWG. SEE CONTINUATION FOR DETAILS.
- [SDR SWIA202053742](https://openairdocs.org/sdr/SWIA202053742.md): Doubler · corroded · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RT WS 53.60 BATT RIB CANNON PLUG DOUBLER CORRODED, MARKED. C-CHECK RO 10/29/2020. INSTALLED NEW REPLACEMENT DOUBLER ON RT WS 53.60 BATT RIB, REF CRJ200 SRM.
- [SDR SWIA202053729](https://openairdocs.org/sdr/SWIA202053729.md): Channel · cracked · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RT WS 53.60 BATTERY RIB AFT CHANNEL CRACKED AT TOP, MARKED. C-CHECK RO 10/29/2020. REMOVED AND INSTALLED NEW BATTERY RIB ASSEMBLY P/N 601R10203-8, REF DWG CRJ200 SRM.
- [SDR SWIA202053728](https://openairdocs.org/sdr/SWIA202053728.md): Rib · cracked · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RT WS 48.30 BATTERY RIB CAP CRACKED AT FWD/AFT ENDS, MARKED. C-CHECK RO 10/29/2020. INSTALLED NEW CAP ANGLE, PER CRJ 200 SRM AND INSTALLATION DWG.
- [SDR SWIA202053727](https://openairdocs.org/sdr/SWIA202053727.md): Rib · cracked · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LT WS 48.30 BATTERY RIB CAP CRACKED AT FWD/AFT ENDS, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED DAMAGED BATTERY RIB CAP ANGLE AT LT WS48.30, REF DWG AND CRJ200 SRM.
- [SDR SWIA202053726](https://openairdocs.org/sdr/SWIA202053726.md): Attach Fitting · cracked · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD UPPER ROLLER ATTACH FITTING ON DOOR CRACKED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED CARGO DOOR FITTING, REF SRM AND DWG. COMPLETED TASK CARD.
- [SDR SWIA202053725](https://openairdocs.org/sdr/SWIA202053725.md): Rib · cracked · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBOARD FLAP VANE ASSEMBLY INBOARD END RIB P/N 601R14304-14 AT FLAP STA 50.498 CRACKED. C-CHECK RO 10/29/2020. INSTALLED NEW END RIB PN 601R14304-14 ON RT INBOARD VANE ASSEMBLY, REF BOMBARDIER DWG AND CRJ200 SRM.
- [SDR SWIA202053724](https://openairdocs.org/sdr/SWIA202053724.md): Frame · cracked · Sep 28, 2020 · N446SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333.00 BETWEEN STRG 0 TO 1 LT FRAMED CRACKED, MARKED. C-CHECK RO 10/29/2020. REMOVED AND INSTALLED NEW FRAME AT FS 333.00 AT STGR 0-STGR 1L, REF CRJ200 SRM AND BOMBARDIER DRAWING. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA202053760](https://openairdocs.org/sdr/SWIA202053760.md): Stop Fitting · gouged · Sep 27, 2020 · N446SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVI COMPARTMENT RT FWD DOOR STOP FITTING ON SURROUND GOUGED ON UPPER EDGE, MARKED. C-CHECK RO 10/29/2020. EVAAULATED AND DETERMINED DAMAGE TO BE OUT OF LIMITS. INSTALLED NEW AVIONICS DOOR COMPARTMENT RIGHT DOOR SURROUND FITTING, IAW CRJ200 SRM. OPERATIONAL
- [SDR SWIA202053759](https://openairdocs.org/sdr/SWIA202053759.md): Stop Fitting · gouged · Sep 27, 2020 · N446SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVI COMPARTMENT LT FWD DOOR STOP FITTING ON SURROUND GOUGED ON UPPER EDGE, MARKED. C-CHECK RO 10/29/2020. EVAULATED AND DETERMINED DAMAGE TO BE OUT OF LIMITS. INSTALLED NEW AVIONICS COMPARTMENT LT DOOR SURROUND STOP FITTING, REF CRJ200 SRM. OPERATIONAL, RI
- [SDR SWIA202053745](https://openairdocs.org/sdr/SWIA202053745.md): Floor Support · corroded · Sep 27, 2020 · N446SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409.00+128-FS 559.00 LBL 9 FLOOR BEAM CAP HAS SEVERAL AREAS OF CORROSION ON TOP, MARKED. C-CHECK RO 10/29/2020. COMPLIED WITH PERMANENT REPAIR FS 409.00+128-FS 559.00 LBL 9 FLOOR BEAM CAP DAMAGE, REF REO. ALL APPLICABLE STEPS COMPLIED WITH.
- [SDR SWIA202053744](https://openairdocs.org/sdr/SWIA202053744.md): Seat Track · corroded · Sep 27, 2020 · N446SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS 409.00+128-FS 559.00 LBL 9 FLOOR SEAT TRACK HAS SEVERAL AREAS OF CORROSION/GOUGES, MARKED. C-CHECK RO 10/29/2020. REPLACED CORRODED LBL 9 SEAT TRACK BETWEEN FS 409.00+128-FS 559.00, REF CRJ200 AMM.
- [SDR SWIA202053723](https://openairdocs.org/sdr/SWIA202053723.md): Floor Support · corroded · Sep 27, 2020 · N446SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409.00+128 TO FS 559.00 RBL 9 FLOOR BEAM CAP HAS SEVERAL AREAS OF CORROSION ON TOP, MARKED. C-CHECK RO 10/29/2020. BLENDED RBL 9 CORRODED AREAS TO A SMOOTH CONTOUR BETWEEN FS 409.00+128 AND FS 529.00, REF CRJ200 SRM. REMAINING MATERIAL IS WITHIN LIMITS.
- [SDR SWIA202053753](https://openairdocs.org/sdr/SWIA202053753.md): Hinge · chafed · Sep 26, 2020 · N446SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > SERVICE DOOR HINGE IS CHAFED AND GOUGED IN SEVERAL LOCATIONS, MARKED. C-CHECK RO 10/29/2020. BLENDED, NO DEFECTS NOTED, EVALUATED REPAIR, FOUND OUT OF LIMITS. RECEIVED ENGINEERING REQUESTED SUPPORT REO COMPLIED WITH ALL STEPS OF REO PART IN LIMITS, ROTO PEE
- [SDR SWIA202053738](https://openairdocs.org/sdr/SWIA202053738.md): Attach Angle · cracked · Sep 26, 2020 · N446SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT EQUIPMENT BAY, FS 621.00-FS 625.30, ATTACHING "CLIP" AT STGR 14L LEVEL CRACKED, FLAGGED. C-CHECK RO 10/29/2020. REMOVED AND REPLACED WITH NEW ATTACH CLIP AT STR 14L FS 621.0-FS 625.30, REF CRJ 200 SRM.
- [SDR SWIA202053722](https://openairdocs.org/sdr/SWIA202053722.md): Intercostal · corroded · Sep 25, 2020 · N446SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LT SIDE AFT SPAR INTERCOSTAL HAS EVIDENCE OF CORROSION (AT BOTTOM) AT WS 53.60. C-CHECK RO 10/29/2020. FOUND LT SIDE AFT SPAR INTERCOSTAL CRACKED. REMOVED AND REPLACED LT SIDE AFT SPAR INTERCOSTAL (BATT RIB), REF CRJ 200 SRM, DWG. COMPLIED WITH TASK CARDS.
- [SDR SWIA202053721](https://openairdocs.org/sdr/SWIA202053721.md): Intercostal · corroded · Sep 25, 2020 · N446SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RT SIDE AFT SPAR INTERCOSTAL AT WS 53.60 HAS EVIDENCE OF CORROSION. C-CHECK RO 10/29/2020. REMOVED AND REPLACED RT AFT SPAR INTERCOSTAL AND SEAL AT WS 53.60. INSTALLATION COMPLETED, PER SRM AND DWG INSTALLATION. COMPLETED TASK CARD.
- [SDR SWIA202053741](https://openairdocs.org/sdr/SWIA202053741.md): Seat Track · corroded · Sep 24, 2020 · N446SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 9 HAS SEVERAL SPOTS OF CORROSION FROM FS 409+64-FS 409+128. C-CHECK RO 10/29/2020. COMPLIED WITH REPLACEMENT OF SEAT TRACK RAIL, AT FS 409-00+64- FS 409+128 LBL 9, REF CRJ-200 AMM. TORQUE TUC4978 CAL DUE DATED 30-JUN-21.
- [SDR SWIA202053740](https://openairdocs.org/sdr/SWIA202053740.md): Seat Track · corroded · Sep 24, 2020 · N446SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL IS CORRODED AT APPROXIMATELY FS 510. C-CHECK RO 10/29/2020. REMOVED AND REPLACED LT SIDE SEAT RAIL FROM FS 501 TO FS 547, REF CRJ200 AMM.
- [SDR SWIA202053739](https://openairdocs.org/sdr/SWIA202053739.md): Seat Track · corroded · Sep 24, 2020 · N446SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL HAS CORROSION FROM APPROXIMATELY FS 461-FS 484. C-CHECK RO 10/29/2020. REMOVED AND REPLACED LT SIDE SEAT TRACK FROM APPROXIMATELY FS 449.85 TO FS 499.00, REF CRJ200 AMM.
- [SDR SWIA202053720](https://openairdocs.org/sdr/SWIA202053720.md): Frame · corroded · Sep 24, 2020 · N446SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FS 310 FRAME BETWEEN STR 26L AND 27. C-CHECK RO 10/29/2020. INSTALLED NEW FRAME SECTION AT FS 310, PER CRJ200 SRM AND INSTALLATION DRAWING. INSTALLED NEW ANGLE SPLICE BRACKET, REF CRJ200 SRM AND INSTALLATION DRAWING. LEAK CHECKS ARE GOOD AT TH
- [SDR SWIA202053719](https://openairdocs.org/sdr/SWIA202053719.md): Floor Support · corroded · Sep 24, 2020 · N446SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LT PRESSURE FLOOR SILL PANEL IN SEVERAL SPOTS BETWEEN FS 409+128 AND 559. C-CHECK RO 10/29/2020. REMOVED CORROSION FROM LT PRESSURE FLOOR SILL PANEL BETWEEN FS 409+128 AND FS 559.00. COMPLIED WITH ALL STEPS OF REO, LEAK CHECK GOOD, NO LEAKS FOU
- [SDR SWIA202053718](https://openairdocs.org/sdr/SWIA202053718.md): Floor Support · corroded · Sep 24, 2020 · N446SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LT PRESSURE FLOOR ANGLE IN SEVERAL SPOTS BETWEEN FS 409+128 AND 559. C-CHECK RO 10/29/2020. REMOVED CORROSION ON THE LT PRESSURE FLOOR ANGLE, REF REO. FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO. PRESSURE CHECK GOOD. SEE CONTIN
- [SDR SWIA202053717](https://openairdocs.org/sdr/SWIA202053717.md): Strap · corroded · Sep 24, 2020 · N446SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SUPPORT STRAP AT FS 559 OUTBOARD OF LBL 27 IS CORRODED. C-CHECK RO 10/29/2020. FOUND LT FLOOR SUPPORT STRAP AT FS 559 OUTBOARD OF LBL 27 TO BE OUT OF LIMITS, REF CRJ 200 SRM. REMOVED AND REPLACED FLOOR STRAP, REF CRJ200 SRM AND DWG. COMPLIED WITH
- [SDR SWIA202053716](https://openairdocs.org/sdr/SWIA202053716.md): Floor Support · corroded · Sep 24, 2020 · N446SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RT PRESSURE FLOOR SILL PANEL IN SEVERAL SPOTS BETWEEN FS 409+128 AND 559. C-CHECK RO 10/29/2020. REMOVED CORROSION FROM PRESSURE FLOOR SILL AT SEVERAL SPOTS PANEL BETWEEN FS 409+128 AND FS 559, REF REO. ALL SPOTS FOUND TO BE WITHIN LIMITS, AS P

Next page: https://openairdocs.org/aircraft/N446SW/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 = 'N446SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N446SW/reports

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