# Service difficulty reports: N916SW

A list on [N916SW](https://openairdocs.org/aircraft/N916SW.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 · 286 reports

- [SDR SWIA2026101977789](https://openairdocs.org/sdr/SWIA2026101977789.md): Elec Connector · faulted · Oct 19, 2026 · N916SW · Cndair CL6002B19 · Engine Indicating System Wiring
  > WHEN CLIMBING AFTER TAKE OFF, LEFT ENGINE N1 FLUCTUATED UP TO 5 WHEN ADDING MORE THRUST IT REDUCED THRUST AND CAUSED YAWING AND ROLLING ONCE WE DECLARED THE EMERGENCY AND PULL THE THRUST, N1 STABILIZED UNTIL LANDING FLIGHT 5470. TROUBLESHOT IAW FIM 76-10-00
- [SDR SWIA2026030675430](https://openairdocs.org/sdr/SWIA2026030675430.md): Floorbeam · corroded · Mar 6, 2026 · N916SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM CORRODED AND CRACKED ON FWD FACE AT APPROX. RBL 9. COMPLIED WITH REO 601R-53-11-4061 REV--, REPAIR TO BULKHEAD WEB FS 280 LBL 20.75 & RBL 20.75 (DEVIATION TO GENERIC REO 601R-53-11-926-B) AND REO 601R-53-11-926, REV -B. COMPLIED WITH TASK C
- [SDR SWIA2026030575882](https://openairdocs.org/sdr/SWIA2026030575882.md): Floorbeam · cracked · Mar 5, 2026 · N916SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 FORWARD FLOORBEAM ANGLE, REF DWG 600-34017, SRM 53-11-19, BETWEEN RBL 9.0 AND LBL 9.0 CRACKED. REMOVED AND REPLACED THE BS 280 FORWARD FLOORBEAM ANGLE, RBL 9 AND LBL 9 IAW SRM 51-42-06, & SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.. REF 318
- [SDR SWIA2026020375885](https://openairdocs.org/sdr/SWIA2026020375885.md): Floor Support · damaged · Feb 3, 2026 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING FLOOR SUPPORT REPAIR AT RBL 9 BETWEEN BS 409.5 & 409 + 32 FOUND UNDERLYING DAMAGE ON FLOOR. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 53-00-43. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026012975101](https://openairdocs.org/sdr/SWIA2026012975101.md): Floor Support · corroded · Jan 29, 2026 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPORT AT RBL 9 BETWEEN BS 409.5 AND BS 409 + 32 FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR OF THE FLOOR SUPPORT IAW SRM 53-00-43 & REO 601R-53-31-1366 REV--. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-06 AND N
- [SDR SWIA2026012875893](https://openairdocs.org/sdr/SWIA2026012875893.md): Floor Support · corroded · Jan 28, 2026 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MULTIPLE SPOTS OF CORROSION ON RH PRESSURE FLOOR SILL FROM FS 409.00+128 TO FS 559. BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL ASSY APPROX RBL 36.00 - RBL 42.00 AND BETWEEN FS409.00 +128 AND FS559.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT RE
- [SDR SWIA2026012875881](https://openairdocs.org/sdr/SWIA2026012875881.md): Floor Support · corroded · Jan 28, 2026 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MULTIPLE SPOTS OF CORROSION ON LT PRESSURE FLOOR SUPPORT FROM BS 409+128 - 559. BLENDED CORROSION ON THE LT PRESSURE FLOOR SUPPORT ASSY APPROX LBL 36 - 42 AND BTWN BS 409 +128 & 559 IAW SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT IAW ND
- [SDR SWIA2026011375891](https://openairdocs.org/sdr/SWIA2026011375891.md): Retainer · gouged · Jan 13, 2026 · N916SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER AFT SEAL RETAINER GOUGED. REMOVED AND REPLACED THE CARGO DOOR UPPER AFT SEAL RETAINER IN REFERENCE WITH THE SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026011375890](https://openairdocs.org/sdr/SWIA2026011375890.md): Skin · gouged · Jan 13, 2026 · N916SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR OUTER SKIN HAS GOUGE LOWER FWD CORNER. BLENDED GOUGE ON CARGO DOOR OUTER SKIN, LOWER FWD CORNER WITH REFERENCE TO REO 601R-52-31-445 REV--. REFERENCE CP 31591872 FOR EDDY CURRENT INSPECTION. PERFORMED UT THICKNESS MEASUREMENT OF BLEND WITH REFER
- [SDR SWIA2026010975884](https://openairdocs.org/sdr/SWIA2026010975884.md): Skin · corroded · Jan 9, 2026 · N916SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION AROUND 2 DRAIN HOLE IN THE BELLY OF THE CARGO BAY. LOCATED BETWEEN BS 559+96 AND 559+112 ON BOTH SIDES OF STGR 27. FOUND SURFACE CORROSION ON THE INNER DOUBLERS FOR THE 2 DRAIN HOLES IN THE BELLY OF THE CARGO BAY AT BS 559+96 AND 559+112, LT & RT
- [SDR SWIA2026010475894](https://openairdocs.org/sdr/SWIA2026010475894.md): Skin · corroded · Jan 4, 2026 · N916SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL FUSELAGE AT F.S589.00 AND STR24L.CORROSION ON INTERNAL FUSELAGE AT FS 589.00 AND STR24L IDENTIFIED AT FS589.00 FRAME FLANGE BETWEEN AND WEB BETWEEN STR24L-STR23L ALONG WITH STR24L FLANGE. REMOVED FASTENERS IAW SRM 51-42-06 AND BLENDED CO
- [SDR SWIA2025122775889](https://openairdocs.org/sdr/SWIA2025122775889.md): Pressure Blkhd · cracked · Dec 27, 2025 · N916SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > ANGLE CRACKED ON THE AFT SIDE OF THE REAR PRESSURE BULKHEAD AT FS 621.00 AND STGR 14R. REMOVED AND REPLACED CLIP/ANGLE ON THE AFT SIDE OF THE REAR PRESSURE BULKHEAD AT FS 621, STGR 14R IN REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025122775880](https://openairdocs.org/sdr/SWIA2025122775880.md): Pressure Blkhd · cracked · Dec 27, 2025 · N916SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CLIP/ANGLE CRACKED ON THE AFT SIDE OF THE REAR PRESSURE BULKHEAD AT BS 621 AND STGR 14L. REMOVED AND REPLACED THE ANGLE ON THE AFT SIDE OF THE REAR PRESSURE BULKHEAD AT BS 621, STGR 14L IAW SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025122675892](https://openairdocs.org/sdr/SWIA2025122675892.md): Rivet · sheared · Dec 26, 2025 · N916SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > TWO SHEARED RIVETS ON REAR PRESSURE BULKHEAD FWD FACE AT WL73.5 AND RBL36.20. REMOVED 2 SHEARED RIVETS ON REAR PRESSURE BULKHEAD FWD FACE AT WL73.5 AND RBL36.20 IAW SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION OF BORES THROUGH ENTIRE STACK UP WITH REFERE
- [SDR SWIA2025122275886](https://openairdocs.org/sdr/SWIA2025122275886.md): Mount · cracked · Dec 22, 2025 · N916SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FWD CARGO DOOR BALANCE SPRING BOX MOUNT IS CRACKED. REMOVED AND REPLACED FWD CARGO DOOR BALANCE SPRING BOX MOUNT IAW SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025122275883](https://openairdocs.org/sdr/SWIA2025122275883.md): Channel · cracked · Dec 22, 2025 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FWD TRACK, BOTTOM CHANNEL IS CRACKED. REF SRM 53-61-23 PAGE 4 ITEM -49. REMOVED AND REPLACED CARGO DOOR FWD TRACK BOTTOM CHANNEL IAW SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025122175887](https://openairdocs.org/sdr/SWIA2025122175887.md): Skin · corroded · Dec 21, 2025 · N916SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE BELLY HAS CORROSION ALONG STGR 27, BETWEEN FS 559.80+80 AND FS 574.00 UPON FURTHER INSPECTION - FOUND CORROSION ON FUSELAGE BELLY ALONG STR 27 TO BE BETWEEN FS559.00+80 AND FS 559.00+112 ONLY. COMPLIED WITH REO 601R-53-51-727 DATED: 2026-01-05 REV:
- [SDR SWIA2025063075888](https://openairdocs.org/sdr/SWIA2025063075888.md): Door · damaged · Jun 30, 2025 · N916SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA97957-601R-52-31-423 MXCODEID108598-PR - THIS TEMPORARY DISPOSITION IS VALID FOR 5300 FLIGHT HOURS FROM THE TIME OF INCORPORATIONOF THIS REO AT REV -, PART NUMBER: 601R35027-241 - DOOR ASSY, BAGGAGE BAY, COMPLIED WI
- [SDR J6BA2025011600004](https://openairdocs.org/sdr/J6BA2025011600004.md): Hydraulic System · low pressure · Jan 14, 2025 · N916SW · Cndair CL6002B19 · Hydraulic System, Main
  > DURING FLIGHT CREW REPORTED HYD 3 LO PRESS CAUTION. COMPLIED WITH QRH AND MESSAGE CLEARED. (FLIGHT 3912 - FILED CLOSED) FOUND CBP2 - A2 BREAKER OUT. RESET THE BREAKER AND PERFORMED OPS CHECK OF HYD 3A ACMP PER AMM 29-12-03. OPS CHECK GOOD AND CIRCUIT BR
- [SDR J6BA2024061000706](https://openairdocs.org/sdr/J6BA2024061000706.md): Spar · dented · Jul 6, 2023 · N916SW · Cndair CL6002B19 · Wing Spar
  > LEFT WINGLET FWD SPAR IS DENTED AT THE UPPER EDGE (FILED CLOSED)REMOVED AND REPLACED LEFT WINGLET FWD SPARWITH A SERVICEABLE SPAR IN REFERENCE TO 51-40-00
- [SDR SWIA2023053000706](https://openairdocs.org/sdr/SWIA2023053000706.md): Spar · dented · Jul 6, 2023 · N916SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT WINGLET FWD SPAR IS DENTED AT THE UPPER EDGE (FILED CLOSED)REMOVED AND REPLACED LEFT WINGLET FWD SPARWITH A SERVICEABLE SPAR IN REFERENCE TO 51-40-00
- [SDR SWIA202266901](https://openairdocs.org/sdr/SWIA202266901.md): Intercostal · corroded · Sep 27, 2022 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF INTERCOSTAL AT STR20R FS349-364 FOUND POTABLE WATER SERVICE PAN FORMER CORRODED (C-CHECK RO 11/12/2022) REPLACED FWD POTABLE WATER SERVICE PAN FORMER SEGMENT IAW CRJ200 SRM 51-42-06, 51-42-21,DWG 601R38316 REV-Y C/W 51-900-1003-SKY LEA
- [SDR SWIA202266900](https://openairdocs.org/sdr/SWIA202266900.md): Intercostal · corroded · Sep 16, 2022 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *CORROSION NOTED ON INTERCOASTAL BETWEEN FS349.00-FS364.00 AND STRG20R (MARKED) (C-CHECK RO 11/12/2022) INSTALLED NEW INTERCOSTAL BETWEEN FS349.00-FS364.00 AND STRG20R IAW CRJ200SRM 51-42-06, CRJ200SRM 51-42-21, DWG 601R38303 REV-AR,DWGS 601R38898 REV
- [SDR SWIA202266899](https://openairdocs.org/sdr/SWIA202266899.md): Frame · corroded · Sep 16, 2022 · N916SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CORROSION NOTED ON FRAME 333 BETWEEN STRG22R-STRG24R (MARKED) (C-CHECK RO 11/12/2022) - INSTALLED NEW FS 333 LOWER RH FRAME SECTOR PN 601R32004-79 TO STR 18R-23R REF BOMBARDIER DWG 601R31021 REV H AND CRJ 200 SRM 51-42-06 & SRM 52-42-21.C/W 51-900-1003
- [SDR SWIA202266898](https://openairdocs.org/sdr/SWIA202266898.md): Floor Support · corroded · Sep 16, 2022 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM CAP AT LBL9 BETWEEN FS409.00-FS409.00+118 (MARKED) (C-CHECK RO 11/12/2022) BLENDED OUT CORROSION FROM THE FLOOR BEAM CAP AT LBL9 BETWEEN FS409.00-FS409.00+118. ORIGINAL MATERIAL THICKNESS OF FLOOR BEAM
- [SDR SWIA202266897](https://openairdocs.org/sdr/SWIA202266897.md): Floor Support · corroded · Sep 16, 2022 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *MULTIPLE SPOTS OF CORROSION NOTED ON LBL9 FLOOR BEAM CAP BETWEEN FS409.00+128-FS544.00 (MARKED) (C-CHECK RO 11/12/2022) REPAIRED CORROSION ON LBL9 FLOOR BEAM CAP BETWEEN FS409.00+128-FS544.00 REF REO 601R-53-41-3078 REV -- DATED 2022-10-06 STEPS 1-6 AN
- [SDR SWIA202266896](https://openairdocs.org/sdr/SWIA202266896.md): Intercostal · corroded · Sep 15, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE INTERCOASTAL CENTER DD1A IS CORRODED. MARKED (C-CHECK RO 11/12/2022) REMOVED PAX DOOR INTERNAL STRUCTURE INTERCOASTAL CENTER DD1A REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21. / INSTALLED NEW PAX DOOR INTERNAL STRUCTURE INTERCO
- [SDR SWIA202266895](https://openairdocs.org/sdr/SWIA202266895.md): Cleat · corroded · Sep 15, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 313.56, DATUM DD4 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 313.56, DATUM DD4 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200
- [SDR SWIA202266894](https://openairdocs.org/sdr/SWIA202266894.md): Intercostal · corroded · Sep 15, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE INTERCOASTAL AT FWD DD3 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE INTERCOASTAL AT FWD DD3 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 AND REF DR
- [SDR SWIA202266893](https://openairdocs.org/sdr/SWIA202266893.md): Frame · corroded · Sep 15, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE FRAME AT STA. FS 313.56, BETWEEN DATUM DD4 AND DD5 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE FRAME AT STA. FS 313.56 BETWEEN DATUM DD4 AND DD5 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00,
- [SDR SWIA202266892](https://openairdocs.org/sdr/SWIA202266892.md): Cleat · corroded · Sep 14, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT COMMON TO THE AFT SIDE OF FORMER AT FS 338.963, DATUM DD5 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT COMMON TO THE AFT SIDE OF FORMER AT FS 338.963, DATUM DD5 FOUND TO BE OUT OF LIMITS
- [SDR SWIA202266891](https://openairdocs.org/sdr/SWIA202266891.md): Hinge Fitting · corroded · Sep 14, 2022 · N916SW · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL OF R/H ELEVATOR HINGE FITTING ASSY P/N 600-24043-1 ON ELEVATOR L/E @ ES16.52 FOR REPLACEMENT OF BEARING P/N MS14102-6, FOUND PITTING CORROSION IN BEARING BORE. REPLACE HINGE FITTING ASSY P/N 600-24043-1. (C-CHECK RO 11/12/2022) INSTALLED 1
- [SDR SWIA202266890](https://openairdocs.org/sdr/SWIA202266890.md): Intercostal · corroded · Sep 14, 2022 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL DD4 LOCATED BETWEEN FS338.963 AND FS347.25 IS CORRODED (C-CHECK RO 11/12/2022) INTERCOSTAL DD4 LOCATED BETWEEN FS338.963 AND FS347.25 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06. AND DWG 601
- [SDR SWIA202266889](https://openairdocs.org/sdr/SWIA202266889.md): Intercostal · corroded · Sep 14, 2022 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL DD3 LOCATED BETWEEN FS338.963 AND FS347.25 IS CORRODED (C-CHECK RO 11/12/2022) INTERCOSTAL DD3 LOCATED BETWEEN FS338.963 AND FS347.25 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06. AND DWG 601
- [SDR SWIA202266888](https://openairdocs.org/sdr/SWIA202266888.md): Window Post · cracked · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LOWER CENTER RIGHT SIDE WINDSHEILD POST FITTING HAS A POSSIBLE CRACK AT FWD RADIUS. (C-CHECK RO 11/12/2022) REMOVED, REPLACED AND INSTALLED NEW WINDSHIELD CENTER POST LOWER RIGHT SIDE FITTING P/N 601R33237-2. PER BOMBARDIER DWG # 601R33237 REV-C AND R
- [SDR SWIA202266887](https://openairdocs.org/sdr/SWIA202266887.md): Angle · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR ANGLE ON DD1A AT FS321.00 IS CORRODED. (MARKED & FLAGGED) (C-CHECK RO 11/12/2022) PASSENGER DOOR ANGLE ON DD1A AT FS321.00 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, DRG. 601R31702 RE
- [SDR SWIA202266886](https://openairdocs.org/sdr/SWIA202266886.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 320.163, DATUM DD6 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 320.163, DATUM DD6 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200
- [SDR SWIA202266885](https://openairdocs.org/sdr/SWIA202266885.md): Bracket · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 311.750, DATUM DD7 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 311.750, DATUM DD7 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CR
- [SDR SWIA202266884](https://openairdocs.org/sdr/SWIA202266884.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 323.363, DATUM DD1A IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 323.363, DATUM DD1A FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ2
- [SDR SWIA202266883](https://openairdocs.org/sdr/SWIA202266883.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE FRAME AT STA. FS 327.763, HINGE TO DATUM DD6 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) REMOVED AND REPLACED FRAME AT STA. FS 327.763, HINGE TO DATUM DD6 REF CRJ-200 SRM 51-42-06 AND 51-42-21 AND DWG 601R31702 REV -N. COMPL
- [SDR SWIA202266882](https://openairdocs.org/sdr/SWIA202266882.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD3 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD3 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200
- [SDR SWIA202266881](https://openairdocs.org/sdr/SWIA202266881.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD4 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD4 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ20
- [SDR SWIA202266880](https://openairdocs.org/sdr/SWIA202266880.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD5 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD5 FOUND TO NE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ20
- [SDR SWIA202266879](https://openairdocs.org/sdr/SWIA202266879.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD6 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD6 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200- SRM 51-42-06 AND DWG
- [SDR SWIA202266878](https://openairdocs.org/sdr/SWIA202266878.md): Bracket · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 347.25, DATUM DD3 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) REMOVED AND REPLACED PAX DOOR INTERNAL STRUCTURE BRACKET AT FS347.25 DD3 PER CRJ200SRM 51-42-06 AND DWG 601R31702 REV -N, COMPLIED WITH TASK CAR
- [SDR SWIA202266877](https://openairdocs.org/sdr/SWIA202266877.md): Bracket · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 347.25, DATUM DD4 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 347.25, DATUM DD4 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED REF CRJ
- [SDR SWIA202266876](https://openairdocs.org/sdr/SWIA202266876.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 347.25, DATUM DD6 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 347.25, DATUM DD6 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00 REMOVED AND REPLACED IAW CRJ200 SR
- [SDR SWIA202266875](https://openairdocs.org/sdr/SWIA202266875.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 335.763, DATUM DD1A IS CORRODED. MARKED (C-CHECK RO 11/12/2022) CORROSION ON PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 335.763, DATUM DD1A WAS FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM
- [SDR SWIA202266874](https://openairdocs.org/sdr/SWIA202266874.md): Cleat · corroded · Sep 9, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 320.163, DATUM DD4 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 320.163, DATUM DD4 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED REF: CRJ2
- [SDR SWIA202266873](https://openairdocs.org/sdr/SWIA202266873.md): Former · corroded · Sep 6, 2022 · N916SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORMER P/N 601R318078-3 AT FS329.76 BETWEEN DATUM 5 AND DATUM 6 HAS SURFACE CORROSION OVER 60% (C-CHECK RO 11/12/2022) REPLACED PASSENGER DOOR FORMER P/N 601R318078-3 AT FS329.76 BETWEEN DATUM 5 AND DATUM 6 REF CRJ200SRM 51-42-06 AND DWG

Next page: https://openairdocs.org/aircraft/N916SW/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 = 'N916SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N916SW/reports

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