# Service difficulty reports: N442SW

A list on [N442SW](https://openairdocs.org/aircraft/N442SW.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 · 222 reports

- [SDR SWIA20241109](https://openairdocs.org/sdr/SWIA20241109.md): Pylon · dented · Nov 9, 2024 · N442SW · Cndair CL6002B19 · Fuselage Main, Frame
  > 2 DENTS ON FUSELAGE ABOVE R/H ENGINE PYLON. NEED FURTHER INVESTIGATION. (FILED CLOSED) REPAIRED FUSELAGE SKIN ABOVE PYLON IAW REO #601R-53-61-8265 TASK CARD 51-900-1002-SKY COMPLETED M-337 ATTACHED
- [SDR SWIA202265974](https://openairdocs.org/sdr/SWIA202265974.md): None · failed · Jun 28, 2022 · N442SW · Cndair CL6002B19 · Air Conditioning System
  > L PACK HI TEMP CAUTION MESSAGE ON CLIMBOUT (FLIGHT 4270 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25070308 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED THE L/H AIR CYCLE MACHINE AS OUTLINED IN 21-51-01 OF THE CRJ 200 MAI
- [SDR SWIA2020021148392](https://openairdocs.org/sdr/SWIA2020021148392.md): Stop Fitting · corroded · Jan 28, 2020 · N442SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > THE CARGO DOOR FLOOR SILL STOP FITTINGS AND SERATED PLATES ARE CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED BOTH FWD AND AFT ON THE CARGO DOOR FLOOR SILL LOWER THE STOP FITTINGS, SERATED PLATES, SHIMS AND HARDWARE. REF CRJ 200 AMM, SRM.
- [SDR SWIA2020021148366](https://openairdocs.org/sdr/SWIA2020021148366.md): Bracket · cracked · Jan 16, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO DOOR AFT CABLE SPRING BOX MOUNTING BRACKET IS CRACKED AT FS621.00 (C-CHECK) RO 2/07/2020 REMOVED AND INSTALLED NEW SERVICEABLE CARGO DOOR AFT CABLE SPRING BOX MOUNTING BRACKET AT FS621.00. REF - CRJ 200 SRM AND BOMBARDIER DWG. ALL CHECKS GOOD.
- [SDR SWIA2020021148365](https://openairdocs.org/sdr/SWIA2020021148365.md): Floorbeam · corroded · Jan 16, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > UPON REMOVAL OF THE FLOOR STRAP AT FS559.00 RBL 27.00 FOUND AN AREA OF CORROSION AROUND THE FASTENER HOLE. (C-CHECK) RO 2/07/2020 REMOVED AND INSTALLED NEW FLOOR STRAP ANGLE AT FS 559.00 RBL 27. REF BOMBARDIER REO & CRJ 200 SRM. WEIGHT CHANGE +0.017 POUN
- [SDR SWIA2020021148364](https://openairdocs.org/sdr/SWIA2020021148364.md): Frame Angle · corroded · Jan 15, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605 LOWER FRAME REINFORCING ANGLE CORRODED IN MULTIPLE AREAS (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED FS605 REINFORCING ANGLE, REF SRM AND BOMBARDIER DWG, COMPLETED TASK CARD.
- [SDR SWIA2020021148363](https://openairdocs.org/sdr/SWIA2020021148363.md): Angle · cracked · Jan 13, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FS 484 OUTB CLIP AT LBL36 CRACKED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED FS 484 CLIP REF SRM AND IN REFERENCE TO REO FOR FASTENER CALLOUT AND MATERIAL SPEC, COMPLETED TASK CARD, ALL CHECKS OKAY
- [SDR SWIA2020021148391](https://openairdocs.org/sdr/SWIA2020021148391.md): Seat Track · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * RBL 9.0 INSIDE FUSELAGE FLOOR SEAT TRACK HAS CORROSION AT VARIOUS LOCATIONS. AT APPROX LOCATION FS 364 TO FS 409.0 (C-CHECK) RO 2/07/2020 REMOVED BAD FUSELAGE FLOOR SEAT TRACK, REF CRJ200 AMM, RECEIVED AND WET INSTALLED NEW CABIN SEAT TRACK SECTION FROM
- [SDR SWIA2020021148390](https://openairdocs.org/sdr/SWIA2020021148390.md): Seat Track · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9.0 FLOOR SEAT TRACK FROM APPROX FS 364 TO FS409 HAS CORROSION IN VARIOUS LOCATIONS (C-CHECK) RO 2/07/2020 REMOVED BAD FLOOR SEAT TRACK, RECEIVED AND WET INSTALLED NEW CABIN SEAT TRACK SECTION FROM FS364.00 - FS409.00. REF CRJ200 AMM, TORQUE WRENCH TUC
- [SDR SWIA2020021148389](https://openairdocs.org/sdr/SWIA2020021148389.md): Cargo Track · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * CARGO DOOR FLOOR TIE DOWNS 3 EACH €“ HAS SIGNS OF CORROSION (MARKED) (C-CHECK) RO 2/07/2020 REMOVED CORROSION ON CARGO FLOOR TIE DOWNS REF CRJ200 SRM. FOUND FWD AND AFT TIE DOWN BRACKET IN LIMITS, MIDDLE BRACKET OUT OF LIMITS REF CRJ200 SRM. REMO
- [SDR SWIA2020021148388](https://openairdocs.org/sdr/SWIA2020021148388.md): Bolt · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Emergency Exits
  > *RH EMERGENCY EXIT LOWER HINGES HARDWARE CORRODED ( INSIDE) (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED 8 EACH BOLTS AND 8 EACH WASHERS ON R/H EMERGENCY EXIT DOOR AT LOWER HINGES. REF. CRJ 200 SRM. CALIBRATED TOOL USED TUC8615. CAL. DUE DATE: 31-OCT-20.
- [SDR SWIA2020021148387](https://openairdocs.org/sdr/SWIA2020021148387.md): Seat Track · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * SEAT TRACK CORRODED AT LBL 9 FROM FS 396.0 TO 409.+128 (C-CHECK) RO 2/07/2020 * SEAT TRACK REMOVED AND REPLACED AT LBL 9 FROM FS 396.0 TO 409.+128 REF CRJ.
- [SDR SWIA2020021148386](https://openairdocs.org/sdr/SWIA2020021148386.md): Seat Track · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * SEAT TRACK CORRODED AT RBL 9 FROM FS 396.0 TO 409.+128 (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED SEAT TRACK AT RBL 9 FROM FS 396.0 TO 409.+128 REF AMM.
- [SDR SWIA2020021148361](https://openairdocs.org/sdr/SWIA2020021148361.md): Support Angle · cracked · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > * CARGO DOOR FWD CAM TRACK SUPPORT " ANGLE" CRACKED FS 574.0 MARKED (C-CHECK) RO 2/07/2020 REMOVED AND INSTALLED NEW CHANNEL REF BOMBARDIER DWG AND CRJ200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020021148360](https://openairdocs.org/sdr/SWIA2020021148360.md): Floor Support · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00+112 TO FS621 L/H FLOOR SILL HAS NUMEROUS SIGNS OF LIGHT SURFACE CORROSION AROUND NUT PLATE HOLES (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED CARGO SILL REF SRM, DWG, AND REO, VERIFIED ALL STEPS COMPLIED WITH, COMPLETED TASK CARD.
- [SDR SWIA2020021148359](https://openairdocs.org/sdr/SWIA2020021148359.md): Angle · cracked · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 RBL 9.0 OUTBOARD CLIP HAS A CRACK AT UPPER RADIUS (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED NEWLY FABRICATED O/B CLIP AT FS280 RBL 9.0. REF PREVIOUSLY INCORPERATED REO.
- [SDR SWIA2020021148358](https://openairdocs.org/sdr/SWIA2020021148358.md): Strap · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *FLOOR STRAP AT FS 559 LBL 27-42 CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED THE FLOOR STRAP AT FS559.00 LBL 27.00 -42.00. REF CRJ200 SRM, BOMBARDIER DRAWING.
- [SDR SWIA2020021148357](https://openairdocs.org/sdr/SWIA2020021148357.md): Strap · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *FLOOR STRAP AT FS 559 RBL 27-42 CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND INSTALLED NEW SERVICEABLE FLOOR STRAP AT FS559.00 RBL 27-42. REF - CRJ 200 SRM AND BOMBARDIER DWG. CHECKS GOOD.
- [SDR SWIA2020021148356](https://openairdocs.org/sdr/SWIA2020021148356.md): Structure · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * L/H SIDE MLG WHEEL WELL STRUCTURE JUST AFT OF FLAP THERE IS CORROSION. FS 559.0 (C-CHECK) RO 2/07/2020 EVALUATED STIFFENER - FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STIFFENER (P/N 601R32026-95) WITH NEWLY FABRICATED PART. REF CRJ200 SRM AND BOMBA
- [SDR SWIA2020021148355](https://openairdocs.org/sdr/SWIA2020021148355.md): Floor Support · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *RH FLOOR SILL AT FS 559.0-559+16 HAS SEVERAL SPOTS OF CORROSION (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED *RH FLOOR SILL AT FS 559.0-559+16 REF CRJ200 SRM AND BOMBARDIER DRAWING. COMPLETED TASK CARD.
- [SDR SWIA2020021148354](https://openairdocs.org/sdr/SWIA2020021148354.md): Frame · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * F.S 589.00 FRAME - APPROX. L/H STGR 27 TO 26 AND R/H STGR 26 TO 27€“ HAS SIGNS OF CORROSION (MARKED) (C-CHECK) RO 2/07/2020 REPAIRED FS 589 DAMAGE REF REO, VERIFIED ALL STEPS COMPLIED WITH, COMPLETED TASK CARD, ALL CHECKS OKAY
- [SDR SWIA2020021148353](https://openairdocs.org/sdr/SWIA2020021148353.md): Frame · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * F.S 605.00 FRAME - APPROX. R/H STGR 26 TO L/H STGR 20 €“ HAS SIGNS OF CORROSION (MARKED) (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED FS 605 FRAME SECTOR REF. CRJ200 SRM, BOMBARDIER DWG, COMPLETED TASK CARD, ALL CHECKS OKAY.
- [SDR SWIA2020021148351](https://openairdocs.org/sdr/SWIA2020021148351.md): Floor Support · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL, FLOOR ANGLE HAS AREAS OF CORROSION FROM FS409+128-FS559 (C-CHECK) RO 2/07/2020 REPAIRED R/H PRESSURE FLOOR SILL, FLOOR ANGLE FROM FS409+128-FS559 REF REO. CHECKS GOOD.
- [SDR SWIA2020021148350](https://openairdocs.org/sdr/SWIA2020021148350.md): Floor Support · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION FROM FS409-FS559 (C-CHECK) RO 2/07/2020 REMOVED CORROSION FORM THE RH PRESSURE FLOOR SILL FROM FS409-FS559 REF BOMBARDIER REO. BLENDS WITHIN LIMITS REF BOMBARDIER REO AND BOMBARDIER REO. COMPLIED WITH S
- [SDR SWIA2020021148349](https://openairdocs.org/sdr/SWIA2020021148349.md): Floor Support · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL, FLOOR ANGLE HAS AREAS OF CORROSION FROM FS409-FS559. (C-CHECK) RO 2/07/2020 REMOVED CORROSION FORM THE LH PRESSURE FLOOR SILL FROM FS409-FS559 REF BOMBARDIER REO. BLENDS WITHIN LIMITS REF BOMBARDIER REO. CHECKS GOOD. COMPLIED WIT
- [SDR SWIA2020021148348](https://openairdocs.org/sdr/SWIA2020021148348.md): Floor Support · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION FROM FS409-FS559 (C-CHECK) RO 2/07/2020 REPAIRED L/H PRESSURE FLOOR SILL FROM FS409+128-FS559 REF REO. CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARD. COMPLIED WITH BOMBARDIER REO.
- [SDR SWIA2020021148347](https://openairdocs.org/sdr/SWIA2020021148347.md): Floor Support · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * INBD SIDE LIP CORRODED OF FLOOR BEAM AT LBL 9 FROM 409.0 TO 409.+ 128 (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED FLOOR BEAM FROM APPROX FS 409 TO APPROX FS 409+90, AND COMPLIED WITH SPLICE REPAIR FS409+90 TO APPROX 409+128 REF SRM, DWG, AND REO, COMPLET
- [SDR SWIA2020021148346](https://openairdocs.org/sdr/SWIA2020021148346.md): Floor Support · corroded · Jan 9, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * INBD SIDE LIP CORRODED OF FLOOR BEAM AT RBL 9 FROM 409.0 TO 409.+ 128 (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED FLOOR BEAM CAP RBL 9 FROM 409.0 TO 409.+ 128 REF CRJ-200 SRM, REO AND DWG. COMPLETED TASK CARD.
- [SDR SWIA2020021148385](https://openairdocs.org/sdr/SWIA2020021148385.md): Bolt · corroded · Jan 8, 2020 · N442SW · Cndair CL6002B19 · Emergency Exits
  > *LH EMERGENCY EXIT AROUND OPEN HANDLE HARDWARE CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED CORRODED HARDWARE ON L/H EMERGENCY EXIT DOOR, 15 EACH NUTPLATES, 30 EACH RIVETS AND 27 EACH SCREWS. REF. CRJ 200 SRM.
- [SDR SWIA2020021148384](https://openairdocs.org/sdr/SWIA2020021148384.md): Pushrod · corroded · Jan 7, 2020 · N442SW · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE LOWER MIDDLE PUSH ROD HAS CORROSION. (MARKED) (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED PAX DOOR LOWER MIDDLE PUSH ROD P/N: 601R318908-1 REF CRJ 200 AMM. CHECKS GOOD.
- [SDR SWIA2020021148345](https://openairdocs.org/sdr/SWIA2020021148345.md): Strap · corroded · Jan 7, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * TOP OF LEFT STRAP CORRODED AT FS 364.0 FROM LEFT INTERCOSTAL 27 TO LEFT INTERCOSTAL 26 MARKED (C-CHECK) RO 2/07/2020 REMOVED CORROSION FROM LH STRAP (GUSSET PLATE) AT FS 364.0 REF. CRJ 200 SRM. 60% OF LH GUSSET PLATE TOP SURFACE IS CORRODED (MORE THAN 30
- [SDR SWIA2020021148344](https://openairdocs.org/sdr/SWIA2020021148344.md): Strap · corroded · Jan 7, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * TOP OF RIGHT STRAP CORRODED AT FS 364.0 FROM RIGHT INTERCOSTAL 27 TO RIGHT INTERCOSTAL 26 MARKED (C-CHECK) RO 2/07/2020 REMOVED CORROSION FROM RH STRAP (GUSSET PLATE) AT FS. 364.0 REF. CRJ 200 SRM. 90% OF RH GUSSET PLATE TOP SURFACE IS CORRODER (MORE THA
- [SDR SWIA2020021148343](https://openairdocs.org/sdr/SWIA2020021148343.md): Door Sill · corroded · Jan 7, 2020 · N442SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PAX DOOR UPPER SILL ANGLE CORRODED ON AFT SIDE AROUND NUTPLATES AND DOOR SWITCH (C-CHECK) RO 2/07/2020 REPLACED PAX DOOR SILL ANGLE PN 601R31527-221 PO# T-51254 AND ELECTRICAL RECEPTACLE BRACKET 601R31771-1 PO# T-51997 PER CRJ 200 AND BOMBARDIER DWG, AFTE
- [SDR SWIA2020021148383](https://openairdocs.org/sdr/SWIA2020021148383.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *LH WING OUTBD FLT SPOILER ACTUATOR UPPER ATTACH HARDWARE CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED L/H WING O/B FLIGHT SPOILER ACTUATOR UPPER ATTACH HARDWARE WITH NEW REF CRJ200 AMM.
- [SDR SWIA2020021148382](https://openairdocs.org/sdr/SWIA2020021148382.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *LH WING INBD GROUND SPOILER ACTUATOR UPPER ATTACH HARDWARE CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED L/H WING I/B GROUND SPOILER ACTUATOR UPPER ATTACH HARDWARE WITH NEW REF CRJ200 AMM.
- [SDR SWIA2020021148381](https://openairdocs.org/sdr/SWIA2020021148381.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *LH WING SPOILERON OUTBD AND INBD LOWER ACTUATOR ATTACH HARDWARE CORRODED (C-CHECK) RO 2/07/2020 LH WING SPOILERON O/B AND I/B LOWER ACTUATOR HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST OF THE FLIGHT SPOILERS/SPOILERONS CHECK
- [SDR SWIA2020021148380](https://openairdocs.org/sdr/SWIA2020021148380.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING SPOILERON INBD HINGE SAFETY HARDWARE CORRODED (C-CHECK) RO 2/07/2020 REMOVED CORRODED HARDWARE AND REPLACED WITH NEW REF. CRJ 200 AMMUSING CALIBRATED TORQUE INSTRUMENT TUC4200 DUE: 09-30-2020
- [SDR SWIA2020021148379](https://openairdocs.org/sdr/SWIA2020021148379.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING SPOILERON OUTBD LOWER ACTUATOR ATTACH HARDWARE CORRODED (C-CHECK) RO 2/07/2020 RH WING SPOILERON O/B ACTUATOR LOWER HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD
- [SDR SWIA2020021148378](https://openairdocs.org/sdr/SWIA2020021148378.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING SPOILERON INBD LOWER ACTUATOR ATTACH HARDWARE CORRODED (C-CHECK) RO 2/07/2020 RH WING SPOILERON I/B ACTUATOR LOWER HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD.
- [SDR SWIA2020021148377](https://openairdocs.org/sdr/SWIA2020021148377.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING SPOILERON UPPER INBD ACTUATOR HARDWARE CORRODED (C-CHECK) RO 2/07/2020 RH WING SPOILERON I/B ACTUATOR UPPER HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD.
- [SDR SWIA2020021148376](https://openairdocs.org/sdr/SWIA2020021148376.md): Nut · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Ailerons
  > *RH AILERON OUTBD HINGE HARDWARE CORRODED (NUT) (C-CHECK) RO 2/07/2020 ORDERED AND RECEIVED 1 NEW NUT. SEE JOB# 2760985 OP# 5175 MXTRANS# 20096923 FOR INSTALLATION.
- [SDR SWIA2020021148375](https://openairdocs.org/sdr/SWIA2020021148375.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING INBD GROUND SPOILER ON LOWER ATTACH TO ACTUATOR HARDWARE CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED HARDWARE WITH NEW ON RH WING INBOARD GROUND SPOILER CENTER ACTUATOR FORK TO SPOILER. REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD.
- [SDR SWIA2020021148374](https://openairdocs.org/sdr/SWIA2020021148374.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING INBD GROUND SPOILER OUTBD HINGE HARDWARE CORRODED (C-CHECK) RO 2/07/2020 RH WING IB GROUND SPOILER O/B HINGE HARDWARE REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD.
- [SDR SWIA2020021148373](https://openairdocs.org/sdr/SWIA2020021148373.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING INBD GROUND SPOILER CENTER HINGE HARDWARE CORRODED (C-CHECK) RO 2/07/2020 RH WING IB GROUND SPOILER CENTER HINGE HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TESTCHECKED GOOD.
- [SDR SWIA2020021148372](https://openairdocs.org/sdr/SWIA2020021148372.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING INBD GROUND SPOILER INBD HINGE HARDWARE CORRODED (C-CHECK) RO 2/07/2020 RH WING I/B GROUND SPOILER I/B HINGE HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD
- [SDR SWIA2020021148371](https://openairdocs.org/sdr/SWIA2020021148371.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING OB GROUND SPOILER CENTER HINGE HARDWARE CORRODED (C-CHECK) RO 2/07/2020 RH WING OB GROUND SPOILER CENTER HINGE HARDWARE REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD.
- [SDR SWIA2020021148370](https://openairdocs.org/sdr/SWIA2020021148370.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING OB GROUND SPOILER OB HINGE HARDWARE CORRODED (C-CHECK) RO 2/07/2020 RH WING OB GROUND SPOILER O/B HINGE HARDWARE REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD.
- [SDR SWIA2020021148369](https://openairdocs.org/sdr/SWIA2020021148369.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING FLT SPOILER OB HINGE HARDWARE CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED CORRODED HARDWARE WITH NEW ON RH WING FLT SPOILER OB HINGE. REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD.
- [SDR SWIA2020021148368](https://openairdocs.org/sdr/SWIA2020021148368.md): Bolt · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Spoilers
  > *RH WING FLT SPOILER UPPER OB ACTUATOR HARDWARE CORRODED (C-CHECK) RO 2/07/2020 INSTALLED NEW HARDWARE REF CRJ200 AMM. OPS CHECK GOOD.
- [SDR SWIA2020021148367](https://openairdocs.org/sdr/SWIA2020021148367.md): Nut · corroded · Jan 6, 2020 · N442SW · Cndair CL6002B19 · Ailerons
  > *RH AILERON CENTER HINGE HARDWARE ( NUTS) CORRODED (C-CHECK) RO 2/07/2020 ORDERED AND RECEIVED 1 NEW PLATE, 3 NEW NUTS, 1 BOLT AND 2 WASHERS. SEE JOB# 2760985 OP# 5175 MXTRANS# 20096923 FOR INSTALLATION.

Next page: https://openairdocs.org/aircraft/N442SW/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 = 'N442SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N442SW/reports

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