# Service difficulty reports: N430SW

A list on [N430SW](https://openairdocs.org/aircraft/N430SW.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 · 219 reports

- [SDR SWIA202305300029](https://openairdocs.org/sdr/SWIA202305300029.md): Unknown · warning message · May 29, 2023 · N430SW · Cndair CL6002B19 · Landing Gear System
  > RECEIVED AN INTERMITTENT NOSE DOOR OPEN MASTER WARNING AND THEN IT REMAINED ON CONSTANTLY CLIMBING THROUGH 27,000FT. COMPLETED QRH PROCEDURE WITH NO FURTHER ISSUES. (FLT 6969 FILED CLOSED)FOUND LEFT NOSE GEAR DOOR PROX SENSOR S30 LOOSE, RE RIGGED AND SECURED P
- [SDR SWIA20230225](https://openairdocs.org/sdr/SWIA20230225.md): None · gouged · Feb 25, 2023 · N430SW · Cndair CL6002B19 · Rudder, Tab Structure
  > LOWER RUDDER PCU FWD ATTACH FITTING ASSY HAS SEVERAL DEEP GOUGES. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 WILL BE REQUIRED. (FILED CLOSED)COMPLIED WITH BLENDING OUT GOUGE MARK AND ROTO-PEEN ON LOWER RUDDER PCU FWD ATTACH FITTING ASSY (P/N 60
- [SDR SWIA202266620](https://openairdocs.org/sdr/SWIA202266620.md): None · warning message · Oct 21, 2022 · N430SW · Cndair CL6002B19 · Pneumatic System
  > JUST AFTER 1,000AGL ON CLIMBOUT WE GOT A R14TH DUCT WARNING MESSAGE. RAN THE QRH, MESSAGE INITIALLY DIDN€™T GO OUT BUT DID SO EVENTUALLY, RETURNED TO COS WITH A NORMAL LANDING AND TAXI TO THE GATE ONCE FIRE RESCUE HAD DONE AN INSPECTION. (FLIGHT #5291 FILED
- [SDR SWIA2021090760761](https://openairdocs.org/sdr/SWIA2021090760761.md): Drain · out of limits · Jul 20, 2021 · N430SW · Cndair CL6002B19 · Waste Disposal System
  > AFTER COLD WORK INSTALLATION OF FORCE MATE BUSHING AT LBL 45, BUSHING DID NOT MAINTAIN INTERFERENCE FIT. BUSHING WAS EASILY REMOVED BY HAND DURING INCORPORATION OF SERVICE BULLETIN 601R-57-054. (C-CHECK RO 8/29/2021) REPAIRED LBL45 WATER DRAIN HOLE IAW
- [SDR SWIA202160760](https://openairdocs.org/sdr/SWIA202160760.md): Intercostal · cracked · Jul 13, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > AFTER REMOVING FORMER AT FS311.75, FOUND INTERCOSTAL AT DD1A BETWEEN FS311.75 AND FS320.16 TO BE CRACKED. (C-CHECK RO 8/29/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A BETWEEN FS 311.75 AND FS 320.6 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-
- [SDR SWIA2021090760759](https://openairdocs.org/sdr/SWIA2021090760759.md): Former · corroded · Jul 13, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE REMOVING FORMER AT FS329.47 AND BETWEEN DD5 AND DD6 FOR ACCESS, FOUND THE FORMER TO BE CORRODED. (C-CHECK RO 8/29/2021) REMOVED AND REPLACED PAX DOOR FORMER AT FS 329.47 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11. COMPLETED TASK CARD 51-900
- [SDR SWIA2021090760794](https://openairdocs.org/sdr/SWIA2021090760794.md): Pcu · corroded · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Ailerons
  > R/H AILERON INBOARD PCU IS CORRODED WHERE IT CONNECTS TO FWD END OF PCU LINK. (C-CHECK RO 9/3/21) REMOVED CORRODED R/H INBOARD AILERON PCU AND INSTALLED NEW SERVICEABLE PCU IAW CRJ-200 AMM 27-14-01-000/400-801 AND COMPLIED WITH ATTACHED SKY CARD 27-900-10
- [SDR SWIA2021090760793](https://openairdocs.org/sdr/SWIA2021090760793.md): Nut · corroded · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Wing, Attach Fittings
  > CORRODED HARDWARE ON R/H FLIGHT SPOILER, INBD HINGE NUT (1) AND KEEEPER PLATE BOLTS (2), CENTER HINGES INBD AND OTBD NUTS (2), AND OTBD HINGE NUT (1 (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON R/H FLIGHT SPOILER, INBD HINGE NUT (1) AND K
- [SDR SWIA2021090760792](https://openairdocs.org/sdr/SWIA2021090760792.md): Nut · corroded · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Wing, Attach Fittings
  > CORRODED HARDWARE ON R/H SPOILERON, INBD HINGE NUT (1) AND KEEPER PLATE BOLTS (4), CENTER HINGES INBD AND OTBD NUTS ONLY (2), AND OTBD HINGE NUT (1) AND KEEPER PLATE BOLTS (4) (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON R/H SPOILERON,
- [SDR SWIA2021090760773](https://openairdocs.org/sdr/SWIA2021090760773.md): Skin · chafed · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBOARD FLAP VANE IS CHAFFED ON LEADING EDGE AT IB RUB STOP LOCATION. SKIN SECTION REQUIRES REPLACEMENT (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH IB FLAP VANE LEADING EDGE IAW CRJ 200 SRM 51-42-13
- [SDR SWIA2021090760772](https://openairdocs.org/sdr/SWIA2021090760772.md): Skin · chafed · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBOARD FLAP VANE IS CHAFFED ON LEADING EDGE AT OUTBOARD RUB STOP LOCATION. SKIN SECTION REQUIRES REPLACEMENT (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH IB FLAP VANE OB LEADING EDGE IAW CRJ 200 SRM 51-42-13.
- [SDR SWIA2021090760758](https://openairdocs.org/sdr/SWIA2021090760758.md): Skin · damaged · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H INBOARD FLAP, MID RIGHT FLAP VANE LEADING EDGE SKIN REQUIRES REPLACEMENT (C-CHECK RO 8/29/2021) REPAIRED DAMAGE TO RH INBOARD FLAP VANE MID LEADING EDGE SKIN SECTION IAW CRJ-200 SRM 57-52-00 REPAIR 1 REVISION 38B - 25 NOV 2020, CRJ 200 SRM 51-42-13
- [SDR SWIA2021090760757](https://openairdocs.org/sdr/SWIA2021090760757.md): Intercostal · corroded · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > AFTER REMOVING AFT FORMER FOR REPLACEMENT, FOUND THE INTERCOSTAL AT DD3 FROM FS338.96 TO FS347.25 TO BE CORRODED. 601R318055-1REMOVED AND REPLACED PAX DOORINTERCOSTAL DD3 AT FS 338.96 - FS 347.25 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11. COMPLETED TAS
- [SDR SWIA2021090760756](https://openairdocs.org/sdr/SWIA2021090760756.md): Intercostal · corroded · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > AFTER REMOVING THE PASSENGER DOOR AFT FORMER FOR REPLACEMENT, FOUND THE THE INTERCOSTAL AT DD4 FROM FS338.96 TO FS347.25 TO BE CORRODED. (C-CHECK RO 8/29/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 AT FS 338.96 - FS347.25 IAW CRJ 200 SRM 51-42
- [SDR SWIA2021090760755](https://openairdocs.org/sdr/SWIA2021090760755.md): Angle · corroded · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE PERFORMING ACCESS FOR PASSENGER DOOR FWD FORMER REPLACEMENT, FOUND FWD REINFORCING ANGLE TO BE CORRODED. (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR FWD REINFORCEMENT ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-14, 51-42-21, AND 51-42-22. COMPLETED
- [SDR SWIA2021090760754](https://openairdocs.org/sdr/SWIA2021090760754.md): Angle · corroded · Jul 10, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE PERFORMING ACCESS FOR REPLACEMENT OF PASSENGER DOOR AFT FORMER, FOUND AFT REINFORCING ANGLE TO BE CORRODED. (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR AFT REINFORCEMENT ANGLE IAW CRJ 200 SRM 51-42-06, 51-41-14, 51-42-21, 51-42-22, 51-40-11.
- [SDR SWIA202160795](https://openairdocs.org/sdr/SWIA202160795.md): Pcu · corroded · Jul 9, 2021 · N430SW · Cndair CL6002B19 · Aileron Control System
  > L/H AILERON OUTBOARD PCU SEVERELY CORRODED AT PCU LINK ATTACH POINT (C-CHECK RO 9/3/21) REMOVED L/H AILERON O/B PCU IAW CRJ 200 AMM 27-14-01-000-801AND INSTALLED PCU IAW SKY CARD 27-900-1002-SKY SEE CONTINUE CARD ROR DETAILS OF WORK PERFORMED.
- [SDR SWIA2021090760791](https://openairdocs.org/sdr/SWIA2021090760791.md): Bolt · corroded · Jul 9, 2021 · N430SW · Cndair CL6002B19 · Wing, Attach Fittings
  > CORRODED HARDWARE ON L/H INBD GROUND SPOILER, CENTER HINGE LINK ASSEMBLY LOWER ATTACH BOLT AND NUT. (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON L/H INBD GROUND SPOILER, CENTER HINGE LINK ASSEMBLY LOWER ATTACH BOLT AND NUTIAW CRJ-200 AMM
- [SDR SWIA2021090760790](https://openairdocs.org/sdr/SWIA2021090760790.md): Nut · corroded · Jul 9, 2021 · N430SW · Cndair CL6002B19 · Wing, Attach Fittings
  > CORRODED HARDWARE ON L/H OTBD GROUND SPOILER OTBD HINGE NUT(1), CENTER HINGE NUT (1), AND INBD HINGE NUT (1). (C-CHECK RO 9/3/21) REMOVED AND REPLCED HARDWARE IAW CRJ 200 AMM 27-65-01-400-801, ALL CHECKS PASS. REFER TO CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202160789](https://openairdocs.org/sdr/SWIA202160789.md): Bolt · corroded · Jul 9, 2021 · N430SW · Cndair CL6002B19 · Wing, Attach Fittings
  > CORRODED HARDWARE ON L/H FLIGHT SPOILER OTBD HINGE NUT (1), OTBD CENTER HINGE NUT(1), AND INBD HINGE NUT(1) AND STOPPER BRACKET BOLTS (2). (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON L/H FLIGHT SPOILER OTBD HINGE NUT (1), OTBD CENTER HI
- [SDR SWIA2021090760788](https://openairdocs.org/sdr/SWIA2021090760788.md): Bolt · corroded · Jul 9, 2021 · N430SW · Cndair CL6002B19 · Wing, Attach Fittings
  > CORRODED HARDWARE ON L/H SPOILERON OTBD HINGE NUT, AND STOPPER BRACKET BOLTS(4), CENTER HINGES INBD AND OTBD NUTS (2), AND INBD HINGE NUT AND STOPPER BRACKET BOLTS (4). (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON L/H SPOILERON OTBD HING
- [SDR SWIA202160732](https://openairdocs.org/sdr/SWIA202160732.md): Pcu · corroded · Jul 9, 2021 · N430SW · Cndair CL6002B19 · Aileron Control System
  > L/H AILERON INBOARD PCU SEVERELY CORRODED AT PCU LINK ATTACH POINT (C-CHECK RO 9/3/21) REMOVED L/H AILERON I/B PCU IAW CRJ 200 AMM 27-14-01-000-801AND INSTALLED PCU IAW SKY CARDS 27-900-1002-SKY AND 27-900-1008- SKY SEE CONTINUE CARD ROR DETAILS OF WORK
- [SDR SWIA2021090760814](https://openairdocs.org/sdr/SWIA2021090760814.md): Web · cracked · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR STAIR FORWARD WEB IS CRACKED AND CORRODED IN MULTIPLE LOCATIONS. (C-CHECK RO 9/3/21) REPLACED PAX DOOR FWD WEB IAW CRJ 200 SRM 51-40-11.
- [SDR SWIA2021090760812](https://openairdocs.org/sdr/SWIA2021090760812.md): Web · cracked · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR STAIR AFT WEB IS CRACKED AND CORRODED IN MULTIPLE LOCATIONS. (C-CHECK RO 9/3/21) REPLACED PAX DOOR AFT WEB IAW CRJ 200 SRM 51-40-11. REFRENCE MX TRAN # 23048514 JOB 97523101 OP 238 FOR INSTALLATION OF PAX DOOR AFT WEB.
- [SDR SWIA2021090760787](https://openairdocs.org/sdr/SWIA2021090760787.md): Drag Angle · corroded · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORWARD DRAG ANGLE IS CRACKED AND CORRODED. (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR FWD DRAG ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-06.
- [SDR SWIA2021090760785](https://openairdocs.org/sdr/SWIA2021090760785.md): Angle · cracked · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INNER ANGLE AT FS.329.47 FROM DD4 TO DD5 IS CRACKED. (C-CHECK RO 9/3/21) RECIEVED LOCATED AND DRILL NEW PAX DOOR ANGLE AT F.S. 329.47 BETWEEN DD4 AND DD5 IAW CRJ-200 SRM 51-40-11. REF CAMP 23048514 FOR INSTALL.
- [SDR SWIA2021090760753](https://openairdocs.org/sdr/SWIA2021090760753.md): Intercostal · corroded · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL AT DD7A FROM FS.320.16 AND FS329.13 IS CORRODED. (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD7A FROM FS 320.16 - FS 329.13 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11. COMPLETED TASK CARD 51-900-1003-S
- [SDR SWIA2021090760752](https://openairdocs.org/sdr/SWIA2021090760752.md): Intercostal · corroded · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSSENGER DOOR INTERCOSTAL AT DD5 FROM FS.311.75 AND FS320.16 IS CORRODED. (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD5 FROM FS 311.75- FS 320.16 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11. COMPLETED TASK CARD 51-900-1003-SKY
- [SDR SWIA2021090760751](https://openairdocs.org/sdr/SWIA2021090760751.md): Intercostal · corroded · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL AT DD4 FROM FS.311.75 TO FS.320.16 IS CORRODED. (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 AT FS 311.75 TO FS 320.16 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11. COMPLETED TASK CARD 51-900-1003-SKY
- [SDR SWIA2021090760750](https://openairdocs.org/sdr/SWIA2021090760750.md): Intercostal · corroded · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL AT DD3 FROM FS.311.75 TO FS.320.16 IS CORRODED. (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 FROM FS 311.75 - FS 320.16 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-40-11. COMPLETED TASK CARD 51-900-1003-SKY
- [SDR SWIA2021090760749](https://openairdocs.org/sdr/SWIA2021090760749.md): Former · corroded · Jul 7, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FWD FORMER AT FS311.75 IS CORRODED. (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR FWD FORMER AT FS 311.75.47 IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-42-22, AND 51-40-11. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM
- [SDR SWIA2021090760784](https://openairdocs.org/sdr/SWIA2021090760784.md): Bolt · corroded · Jul 2, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORRODED HARDWARE FOUND THROUGHOUT LATCH MECHANISM ON PAX DOOR REFER TO CRJ-700 IPC 52-11-02 FIG 5A ITEMS 155. 160. 165. 170. 175. 185. 190. 205. 210. 214. 215. (C-CHECK RO 9/3/21) REPLACED CORREDED ROD END BEARINGS AND ATTACH HARDWARE ON PAX DOOR LATCH M
- [SDR SWIA2021090760783](https://openairdocs.org/sdr/SWIA2021090760783.md): Bolt · corroded · Jul 2, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORRODED HARDWARE FOUND THROUGHOUT LATCH MECHANISM ON PAX DOOR REFER TO CRJ-700 IPC 52-11-02 FIG1A ITEMS 10,15,20,25,30,115,125,130,135,155,164,165,167, (C-CHECK RO 9/3/21) REMOVED CORRODED ROD END AND ATTACH HARDWARE FOR LATCH BOX PUSH-PULL ROD ( ITEMS 1
- [SDR SWIA2021090760771](https://openairdocs.org/sdr/SWIA2021090760771.md): Latch · corroded · Jul 2, 2021 · N430SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORRODED HARDWARE FOUND THROUGHOUT LATCH MECHANISM ON PAX DOOR REFER TO CRJ-700 IPC 52-11-02 FIG 10A ITEMS 10,15,20,25,35,40,50,55,70,75,79,80,275,280,290. (C-CHECK RO 8/29/2021) REMOVED AND REPLACED CORRODED HARDWARE FOUND THROUGHOUT LATCH MECHANISM ON
- [SDR SWIA2021070760748](https://openairdocs.org/sdr/SWIA2021070760748.md): Hinge · gouged · Jun 29, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE ON A/C SIDE CHAFED/ GOUGED IN BETWEEN THE LUGS AND MISSING PAINT (C-CHECK RO 9/3/21) REMOVED AND REPLACED PAX DOOR HINGE ON AIRCRAFT SIDE IAW CRJ200 SRM 51-42-06, 51-42-21, 53-21-23 REPAIR NO. 1 AND REO 601R-53-21-656 REV. A, DATED 2
- [SDR SWIA2021090760747](https://openairdocs.org/sdr/SWIA2021090760747.md): Floor Support · corroded · Jun 29, 2021 · N430SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL FROM F.S 439 TO 559 HAS MULTIPLE AREAS OF CORROSION. (C-CHECK RO 9/3/21) REPAIRED CORROSION DAMAGE ON RH FLOOR SILL IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO
- [SDR SWIA2021090760813](https://openairdocs.org/sdr/SWIA2021090760813.md): Nut · corroded · Jun 28, 2021 · N430SW · Cndair CL6002B19 · Elevator Structure
  > R/H ELEVATOR #1 AND 24.5 HINGE BOLT NUTS ARE CORRODED. (C-CHECK RO 8/29/2021) REMOVED AND REPLACED THE RIGHT ELEVATOR #1 AND 24.5 HINGE NUTS REF ATTACHED SKY CARD 27-900-1004-SKY AND CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2021090760780](https://openairdocs.org/sdr/SWIA2021090760780.md): Bolt · corroded · Jun 28, 2021 · N430SW · Cndair CL6002B19 · Wing, Attach Fittings
  > R/H ELEVATOR POSITION TRANSMITTER LINK HARDWARE IS CORRODED. (ALL LOCATIONS) (C-CHECK RO 9/3/21) REMOVED AND REPLACED RIGHT ELEVATOR POSITION TRANSMITTER LINK HARDWARES IAW CRJ 200 AMM TASK 27-34-01-000/400-801. OP TEST OF RH POSITION TRANSMITTER GOOD.
- [SDR SWIA2021090760779](https://openairdocs.org/sdr/SWIA2021090760779.md): Nut · corroded · Jun 28, 2021 · N430SW · Cndair CL6002B19 · Wing, Attach Fittings
  > R/H ELEVATOR FLUTTER DAMPER ATTACHING HARDWARE (NUTS) AT ELEVATOR ARE CORRODED. (C-CHECK RO 9/3/21) DUPLICATE WRITE UP, REF CAMP 22978663 FOR CORRECTIVE ACTION
- [SDR SWIA2021090760770](https://openairdocs.org/sdr/SWIA2021090760770.md): Seat Track · corroded · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM FS409.00+16 TO FS409.00+112 (C-CHECK RO 8/29/2021) REMOVED AND REPLACED LH SIDE SEAT RAIL AT FS 409+16- FS409+112 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B.
- [SDR SWIA2021090760769](https://openairdocs.org/sdr/SWIA2021090760769.md): Seat Track · corroded · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM FS409.00+112 TO FS449.00 (C-CHECK RO 8/29/2021) REMOVED AND REPLACED LH SIDE SEAT RAIL AT FS 409+112 - FS 449 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B.
- [SDR SWIA2021090760768](https://openairdocs.org/sdr/SWIA2021090760768.md): Seat Track · corroded · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM FS544.00 TO FS559.00+80 (C-CHECK RO 8/29/2021) REMOVED AND REPLACED LH SIDE SEAT RAIL AT FS 544- FS 559+80 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B.
- [SDR SWIA2021090760767](https://openairdocs.org/sdr/SWIA2021090760767.md): Seat Track · corroded · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM FS449.00 TO FS544.00 (C-CHECK RO 8/29/2021) REMOVED AND REPLACED LH SIDE SEAT RAIL AT FS449 - FS 544 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B.
- [SDR SWIA2021090760766](https://openairdocs.org/sdr/SWIA2021090760766.md): Seat Track · corroded · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM FS544.00 TO FS559.00+80 (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS 544 - FS 559+80 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B. AND CRJ 200AMM 53-01-11-400-802
- [SDR SWIA2021090760765](https://openairdocs.org/sdr/SWIA2021090760765.md): Seat Track · corroded · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM FS449.00 TO FS544.00 (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS 449 - FS 544 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B. AND CRJ 200 AMM 53-01-11-400-802
- [SDR SWIA2021090760764](https://openairdocs.org/sdr/SWIA2021090760764.md): Seat Track · corroded · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM FS409.00+112 TO FS449.00 (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS 409+112 - FS 449 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B. AND CRJ 200 AMM 53-01-11-400-80
- [SDR SWIA2021090760763](https://openairdocs.org/sdr/SWIA2021090760763.md): Seat Track · corroded · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION FROM FS409+16 TO FS409+112 (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS 409+16 - FS 409+112 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B. AND CRJ 200 AMM 53-01-11-400-80
- [SDR SWIA2021090760746](https://openairdocs.org/sdr/SWIA2021090760746.md): Bracket · cracked · Jun 27, 2021 · N430SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RH MLH #2 HYD RETURN LINE BRACKET CRACKED JUST FWD OF FS559.00 (C-CHECK RO 9/3/21) REMOVED AND REPLACED RH MLG #2 HYD RETURN LINE BRACKET IAW CRJ 200 SRM 51-42-06.. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTE
- [SDR SWIA2021090760762](https://openairdocs.org/sdr/SWIA2021090760762.md): Angle · sheared · Jun 25, 2021 · N430SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CONNECTING INTERCOSTAL BETWEEN FS.449.85 & FS.461.00 TO PRESSURE FLOOR SUPORT BEAM AT LBL9.00 HAS ONE SHEARED RIVET HEAD. (C-CHECK RO 8/29/2021) REMOVED AND REPLACED 1EA SOLID RIVET IN THE INTERCOSTAL ATTACH ANGLE BETWEEN FS 449.85 AND FS 461 AT L
- [SDR SWIA2021090760745](https://openairdocs.org/sdr/SWIA2021090760745.md): Floor Support · corroded · Jun 25, 2021 · N430SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL FROM FS. 439.00 TO 559.00 HAS SEVERAL AREAS OF CORROSION MARKED WITH TAPE THAT REQUIRE EVALUATION. (C-CHECK RO 9/3/21) REMOVED CORROSION FROM LH PRESSURE FLOOR SILL FROM FS 439- FS 559 IAW REO 601R-53-41-666 REV C DATED 2012-11-06

Next page: https://openairdocs.org/aircraft/N430SW/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 = 'N430SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N430SW/reports

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