# Service difficulty reports: N876AS

A list on [N876AS](https://openairdocs.org/aircraft/N876AS.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 · 267 reports

- [SDR SWIA2026062176307](https://openairdocs.org/sdr/SWIA2026062176307.md): Warning Message · illuminated · Jun 21, 2026 · N876AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE AFTER TAKEOFF. MAINS CAME UP, NOSE WHEEL WAS AMBER AND DID NOT APPEAR TO COME UP. RAN QRH AND GEAR CAME DOWN WITH THE MANUAL DISCONNECT. DIVERTED TO GRAND RAPIDS. MEL 32-30-1CAT A DUE ODI, DIVERT, SMOD APPROVAL NEEDED FOR RTS CATII DOWNGRADED (
- [SDR SWIA2026052476034](https://openairdocs.org/sdr/SWIA2026052476034.md): Landing Gear · warning message · May 24, 2026 · N876AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON DEPARTURE AFTER MOVING LANDING GEAR LEVER UP, GOT GEAR DISAGREE WARNING MESSAGE, STEERING INOP CAUTION MESSAGE, AND WOW INPUT CAUTION MESSAGE. WOW INPUT WENT AWAY AFTER A COUPLE SECONDS. NOSE DOOR OPEN WARNING MESSAGE MOMENTARILY PRIOR TO RUNNING QRH. RAN G
- [SDR SWIA2026052376033](https://openairdocs.org/sdr/SWIA2026052376033.md): Wire Harness · kinked · May 23, 2026 · N876AS · Cndair CL6002B19 · Landing Gear System Wiring
  > NOSE WHEEL STEERING INOP CAUTION APPEARED UPON GEAR RETRACTION FOLLOWED BY GEAR DISAGREE WARNING. RAN QRH AND RETURNED TO ORD (FLIGHT 5225) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 32313779. SEE CP 32314120 AND CP 32315261 FOR TROUBLESHOOTING AND MAIN
- [SDR SWIA2026052176029](https://openairdocs.org/sdr/SWIA2026052176029.md): Bracket · illuminated · May 21, 2026 · N876AS · Cndair CL6002B19 · Main Landing Gear Attach Section
  > GEAR DISAGREE WARNING MESSAGE ON TAKEOFF. QRH RESOLVED ISSUE. (FLIGHT 5026). TROUBLESHOT GEAR DISAGREE IN REF TO FIM 32-60-07. FOUND NOSE PROX SENSORS S21, & S35 TO BE NEAR WHEN THEY SHOULD BE FAR AND FOUND S22 & S23 BE FAR WHEN THEY SHOULD BE NEAR WITH AIR
- [SDR SWIA2026021875294](https://openairdocs.org/sdr/SWIA2026021875294.md): Not Reported · warning message · Feb 18, 2026 · N876AS · Cndair CL6002B19 · Indicating/Recording System
  > EFIS COMP MON AFFECTED HEADINGS BOTH SIDES, (FLIGHT 5053) PLEASE REFERENCE AML 1824088 FOR FURTHER TROUBLESHOOTING AND SEPERATION OF TWO DISCREPENCIES.
- [SDR SWIA2025111400003](https://openairdocs.org/sdr/SWIA2025111400003.md): Warning Message · false activation · Nov 13, 2025 · N876AS · Cndair CL6002B19 · Cabin Pressure Control System
  > DIFF PRESS WARNING MESSAGE ON CLIME OUT (FLIGHT 4710) ARRIVED AT AIRCRAFT, AND FOUND NO HARD FAULTS. INTERROGATED LRU FAULT HISTORY, AND FOUND NO FAULTS. TROUBLESHOT PER FIM 45-45-00. REMOVED AND REPLACED CPAM, PERFORMED OPS CHECK OF CPAM IN REF TO AMM
- [SDR SWIA202506160011](https://openairdocs.org/sdr/SWIA202506160011.md): Detector · faulted · Jun 11, 2025 · N876AS · Cndair CL6002B19 · Overheat Detection
  > L SIDE FUSELAGE ANTI ICE DUCT WARNING MESSAGE IN ICING WITH WINGS/COWLS SELECTED ON. ACCOMPLISHED QRH WHICH REMOVED MESSAGE. (FLIGHT 5435 - FILED CLOSED)PLEASE REFERENCE AML 1627651 AND AML 1627747 FOR HEAT SENSING ELEMENTS A41WK AND A47WK REPLACEMENT. PERFOR
- [SDR SWIA202506120011](https://openairdocs.org/sdr/SWIA202506120011.md): Duct · warning message · Jun 11, 2025 · N876AS · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > L SIDE FUSELAGE ANTI ICE DUCT WARNING MESSAGE IN ICING WITH WINGS/COWLS SELECTED ON. ACCOMPLISHED QRH WHICH REMOVED MESSAGE. (FLIGHT 5435 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2025F00501](https://openairdocs.org/sdr/SWI2025F00501.md): Floorbeam · corroded · Feb 24, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 9.00 IS CORRODED ON THE INBOARD FLANGE FROM F.S. 409-00 TO F.S. 409.00+112 (C-CHECK RO 04/21/2025)REPLACED LBL 9 FLOOR BEAM CAP AT FS 409 - FS 409+112 IAW CRJ 200 SRM 51-42-21, 51-42-22. AND 51-42-36. COMPLETED TASK CARD 51-900-1003-SKY AND ATTCHED COMPLE
- [SDR SWI2025F00500](https://openairdocs.org/sdr/SWI2025F00500.md): Floorbeam · corroded · Feb 24, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9.00 IS CORRODED ON THE INBOARD FLANGE FROM F.S. 409.00 TO F,S. 409.00+112. (C-CHECK RO 04/21/2025) REPLACED RBL 9 FLOOR BEAM CAP AT FS 409 - FS 409+112 IAW CRJ 200 SRM 51-42-21, 51-42-22. AND 51-42-36. COMPLETED TASK CARD 51-900-1003-SKY AND ATTCHED COM
- [SDR SWIA2025042224](https://openairdocs.org/sdr/SWIA2025042224.md): Floor Support · corroded · Feb 24, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL HAS MINOR CORROSION BETWEEN F.S. 409.00+96 AND F.S. 409.00+112. (C-CHECK RO 04/21/2025)REPAIRED RH FLOOR SILL MINOR CORROSION BETWEEN FS 409.00 +96 AND FS 409.00+112 IAW MHIRJ REO 601R-53-31-1325 REV -- DATED 2025-03-12 COMPLETED TASK CARD 51-9
- [SDR SWIA2025042223](https://openairdocs.org/sdr/SWIA2025042223.md): Hinge Arm · damaged · Feb 23, 2025 · N876AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LH OUTBD FLAP HINGE ARM (WS 264) DAMAGED FROM SCREW BEING CAUGHT IN THE HINGE POINT. (C-CHECK RO 04/21/2025)REPAIRED LH OUTBD FLAP HINGE ARM (WS264) DAMGED FROM SCREW BEING CAUGHT IN THE HINGE POINT IAW GREO 601R-57-54-184 REV -- DATE 2011-03-09. COMPLETED T
- [SDR SWI2025F00510](https://openairdocs.org/sdr/SWI2025F00510.md): Floorbeam · dented · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 LBL 9.0 INBOARD FLOOBEAM CLIP IS CRACKED (C-CHECK RO 04/21/2025)INSTALLED NEW SERVICABLE FS 280 LBL 9 CLIP P/N 601R-53-11-171-2 IAW SRM 51-42-21 AND 51-42-22. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED FORM 337. NO WEIGHT CHANGE
- [SDR SWI2025F00509](https://openairdocs.org/sdr/SWI2025F00509.md): Floorbeam · cracked · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 RBL 9.0 INBOARD AND OUTBOARD FLOORBEAM CLIPS ARE CRACKED (C-CHECK RO 04/21/2025)REPLACED FS 280 RBL9 CLIP IAW CRJ 200 SRM 51-42-21 AND 51-42-22. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED 337. NO WEIGHT CHANGE
- [SDR SWI2025F00508](https://openairdocs.org/sdr/SWI2025F00508.md): Floor Support · corroded · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H CABIN FLOOR SILL CORRODED (3) LOCATIONS BETWEEN FS 349.00 AND 364.00 (C-CHECK RO 04/21/2025)REPAIRED LH CABIN FLOOR SILL CORROSION IN 3 LOCATIONS BETWEEN FS 349.00 AND FS 364.00 IAW GREO 601R-53-00-530 REV A DATED 2014-10-07 COMPLETED TASK CARD 51-900-100
- [SDR SWI2025F00507](https://openairdocs.org/sdr/SWI2025F00507.md): Floor Support · corroded · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H CABIN FLOOR SILL CORRODED FS 319.00 (C-CHECK RO 04/21/2025)REPAIRED RH CABIN FLOOR SILL CORROSION FS 319.00 IAW GENERIC REO 601R-53-00-530 REV A DATED 2014-10-07 AND SKY CARD 51-900-1003-SKY COMPLETED FORM 337 NO WEIGHT CHANGE REF CONTINUATION CARD FOR DE
- [SDR SWIA2025042202](https://openairdocs.org/sdr/SWIA2025042202.md): Skin · chafed · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Trailing Edge Flaps
  > CHAFE ON FLAP UPPER SKIN INNER SURFACE FROM CONTACT WITH BONDING JUMPER UNDER PANEL 684CB (C-CHECK RO 04/21/2025)REPAIRED CHAFE ON FLAP INNER SKIN SURFACE FROM CONTACT WITH BONDING JUMPER UNDER PANEL 684CB IAW GREO 601R-57-52-1914 REV A DATED 2013-02-16 NO WE
- [SDR SWI2025F00506](https://openairdocs.org/sdr/SWI2025F00506.md): Skin · chafed · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Trailing Edge Flaps
  > CHAFE ON FLAP UPPER SKIN INNER SURFACE FROM CONTACT WITH BONDING JUMPER UNDER PANEL 684AB (C-CHECK RO 04/21/2025)REPAIRED CHAFE ON FLAP UPPER SKIN INNER SURFACE FROM CONTACT WITH BONDING JUMPER UNDER PANEL 684AB IAW GREO 601R-57-52-1914 REV A DATED 2013-02-16
- [SDR SWI2025F00505](https://openairdocs.org/sdr/SWI2025F00505.md): Door Sill · corroded · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL CORRODED AROUND SEVERAL NUTPLATE HOLES BETWEEN FS574.00 AND FS621.00. (C-CHECK RO 04/21/2025)REPAIRED LH FLOOR SILL CORROSION AROUND SEVERAL NUTPLATES HOLES BETWEEN FS574.00 AND FS621.00 IAW GREO 601R-53-00-526 REV -- DATED 22 MAY 2013 COMPLETED
- [SDR SWI2025F00504](https://openairdocs.org/sdr/SWI2025F00504.md): Floorbeam · corroded · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP CORRODED AROUND NUTPLATE AT RBL27 BETWEEN FS605.00 AND FS621.00. (C-CHECK RO 04/21/2025)REPAIRED FLOORBEAM CAP CORRODED AROUND NUTPLATE AT RBL 27 BETWEEN FS 605.00 AND FS621.00 IAW CRJ 200 SRM 51-21-06 AND REO 601R-53-00-005 REV B DATED 2011/01/
- [SDR SWI2025F00503](https://openairdocs.org/sdr/SWI2025F00503.md): Floorbeam · corroded · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RH FLOORSILL CORRODED JUST FWD OF FS621.00. (C-CHECK RO 04/21/2025)REPAIRED RH FLOOR SILL CORROSION JUST FWD OF FS 621.00 IAW GREO 601R-53-00-526 REV -- DATED 22 MAY-2013. COMPLETED TASK CARD 51-900-1003-SKY AND COMPLETED FORM 337. NO WEIGHT CHANGE
- [SDR SWI2025F00502](https://openairdocs.org/sdr/SWI2025F00502.md): Floorbeam · corroded · Feb 22, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP CORRODED AT RBL9 BETWEEN FS559+16 TO FS559+64. (C-CHECK RO 04/21/2025)REPAIRED FLOORBEAM CAP CORRODED AT RBL 9 BETWEEN FS 559+16 TO FS559+64 IAW CRJ 200 SRM 51-21-06 REO 601R-53-00-005 REV B DATED 2011/01/00 REF ATTACHED CONTINUATION CARD FOR DE
- [SDR SWI2025F00499](https://openairdocs.org/sdr/SWI2025F00499.md): Striker · damaged · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR CUTOUT, SEAL STRIKER AT FS349.00 BESIDE UPPER STOP FITTING APPEARS TO HAVE A DAMAGED PREVIOUS REPAIR. (C-CHECK RO 04/21/2025)INSTALLED NEW PAX DOOR CUTOUT SEAL STRICKER AT FS 349 IAW SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMP
- [SDR SWI2025F00498](https://openairdocs.org/sdr/SWI2025F00498.md): Striker · chafed · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR CUTOUT, SEAL STRIKER CHAFED AT FS310.00 BESIDE CENTER STOP FITTING. (C-CHECK RO 04/21/2025)REPAIRED IAW REO 601R-53-21-816 REV -- DATED 30-OCT-07. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWI2025F00497](https://openairdocs.org/sdr/SWI2025F00497.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL RBL 36.0 CORROSION AROUND ROW OF SOLID FASTENERS FROM FS 531.00 TO FS 559.00 (C-CHECK RO 04/21/2025)REPAIRED RH PRESSURE FLOOR SILL IAW REO 601R-53-41-3293 REV -- DATED 2025-03-06.COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPL
- [SDR SWI2025F00496](https://openairdocs.org/sdr/SWI2025F00496.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL CORRODED FS 524.00 TO FS 529.00 (C-CHECK RO 04/21/2025)REPAIRED RH PRESSURE FLOOR SILL IAW REO 601R-53-41-3293 REV -- DATED 2025-03-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWI2025F00495](https://openairdocs.org/sdr/SWI2025F00495.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL ANGLE CORRODED FS 509.00 TO FS 517.00 (C-CHECK RO 04/21/2025)REPAIRED RH PRESSURE FLOOR SILL ANGLE IAW REO 601R-53-41-3293 REV -- DATED 2025-03-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE N
- [SDR SWI2025F00524](https://openairdocs.org/sdr/SWI2025F00524.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL CORRODED BETWEEN FS 510.00 AND FS 516.00 (C-CHECK RO 04/21/2025)REMOVED CORROSION FROM FS 510- 516 RH PRESSURE FLOOR SILL AND REPAIRED IAW REO 601R-53-41-3293 REV -- DATED 202-03-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COM
- [SDR SWI2025F00523](https://openairdocs.org/sdr/SWI2025F00523.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL CORRODED AT FS 484.00 (C-CHECK RO 04/21/2025)REPAIRED RH PRESSURE FLOOR SILL CORROSION AT FS 484 IAW REO 601R-53-41-3293 REV -- DATED 2025-03-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NO
- [SDR SWI2025F00522](https://openairdocs.org/sdr/SWI2025F00522.md): Fitting · cracked · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 460.00 FITTING OUTBOARD SIDE OF RBL 27.0 IS CRACKED (C-CHECK RO 04/21/2025)REPLACED FS 460 FITTING OB OF RBL 27 IAW CRJ 200 SRM 51-25-01. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWIA20250422012](https://openairdocs.org/sdr/SWIA20250422012.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL ANGLE CORRODED AT FS 449.00 (C-CHECK RO 04/21/2025)REPAIRED RH PRESSURE FLOOR SILL IAW REO 601R-53-41-3293 REV -- DATED 2025-03-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWIA2025042211](https://openairdocs.org/sdr/SWIA2025042211.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH/ PRESSURE FLOOR SILL CORRODED AT FS 449.00 (C-CHECK RO 04/21/2025)REMOVED CORRISION FROM FS 449 AND REPAIRED IAW REO 601R-53-41-3293 REV -- DATED 2025-03-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWI2025F00515](https://openairdocs.org/sdr/SWI2025F00515.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL CORRODED AROUND NUTPLATE HOLES FS 541.00 AND 549.00 (C-CHECK RO 04/21/2025)REMOVED CORROSION FROM RH PRESSURE FLOOR SILL AND FOUND WITHIN LIMITS OF REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTA
- [SDR SWI2025F00514](https://openairdocs.org/sdr/SWI2025F00514.md): Strap · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 559.00 STRAP UPPER SURFACE CORRODED RBL 36.0- RBL 45.0 (C-CHECK RO 04/21/2025)REPLACED RBL 36 -45 FS 559 STRAP IAW CRJ 200 SRM 51-42-06 AND 51-42-22. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.
- [SDR SWI2025F00513](https://openairdocs.org/sdr/SWI2025F00513.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL ANGLE CORRODED AT FS 559.00. (C-CHECK RO 04/21/2025)REMOVED CORROSION FROM LH FLOOR SILL ANGLE IAW REO 601R-53-41-666 REV DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTCHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED
- [SDR SWI2025F00512](https://openairdocs.org/sdr/SWI2025F00512.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL CORRODED BETWEEN FS 529-FS 544 (C-CHECK RO 04/21/2025)REPAIRED LH PRSSURE FLOOR SILL CORROSION BETWEEN GS 529-FS544 IAW BOMBARDIER REO 601R-53-41-666 REV-C DATED 2012-11-06 NO WEIGHT CHANGE REF ATTACHED CONTINUATION CARD FOR DETAILS OF
- [SDR SWI2025F00511](https://openairdocs.org/sdr/SWI2025F00511.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL ANGLE CORRODED FS529-FS544 (C-CHECK RO 04/21/2025)REMOVED CORROSION FROM LH PRESSURE FLOOR SILL ANGLE AND FOUND TO BE WITHIN LIMITS IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLET
- [SDR SWI2025F00517](https://openairdocs.org/sdr/SWI2025F00517.md): Attach Angle · cracked · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > INTERCOSTAL AT FS484 ATTACH ANGLES CRACKED AT LBL27 AND LBL36 (PREVIOUSLY REPAIRED) (C-CHECK RO 04/21/2025)REMOVED AND REPLACED 2 EA. CLIPS @ FS 484 INTERCOSTAL IAW CRJ200 SRM 51-42-06, SRM 51-42-21 AND REO 601R-53-41-059 REV-C DATED 2020-03-11.COMPLETED TASK
- [SDR SWI2025F00516](https://openairdocs.org/sdr/SWI2025F00516.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL ANGLE REPAIR DOUBLER CORRODED AROUND (2) NUTPLATE HOLES FS499-FS513 (C-CHECK RO 04/21/2025)REMOVED CORROSION FROM LH PRESSURE FLOOR SILL ANGLE DOUBLER AND FOUND WITHIN LIMITS OF REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK
- [SDR SWI2025F00521](https://openairdocs.org/sdr/SWI2025F00521.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL CORRODED AROUND (2) NUTPLATE HOLES FS 484-FS499 (C-CHECK RO 04/21/2025)REMOVED CORROSION FROM THE LH PRESSURE FLOOR SILL CORROSION AT FS 484 - FS 499 IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AN
- [SDR SWI2025F00520](https://openairdocs.org/sdr/SWI2025F00520.md): Angle · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H SILL ANGLE CORRODED FS473-FS477 (C-CHECK RO 04/21/2025)REPAIRED LH FLOOR SILL ANGLE IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED
- [SDR SWI2025F00519](https://openairdocs.org/sdr/SWI2025F00519.md): Angle · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > (2) FASTENER HEADS CORRODED L/H SILL ANGLE FS450-FS451 (C-CHECK RO 04/21/2025)REPAIRED LH SILL ANGLE IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE
- [SDR SWI2025F00518](https://openairdocs.org/sdr/SWI2025F00518.md): Floor Support · corroded · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL CORRODED AROUND (2) NUTPLATE HOLES BETWEEN FS 439 AND FS449 (C-CHECK RO 04/21/2025)REPAIRED CORROSION ON LH PRESSSURE FLOOR SILL AROUND 2 EA NUTPLATES IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 NO WEIGHT CHANGE REF CONTIN
- [SDR SWIA20250422221](https://openairdocs.org/sdr/SWIA20250422221.md): Lintel · cracked · Feb 21, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD AFT SIDE-AT CARGO DOOR LINTEL REPAIR, SUSPECT UPPER ANGLE AFT RADIUS TO BE CRACKED. (C-CHECK RO 04/21/2025)INSTALLED FS 621 - 625 LINTEL ASSY IAW CRJ 200 SRM 51-42-06, 51-42-41, AND 51-42-22. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED C
- [SDR SWIA20250422219](https://openairdocs.org/sdr/SWIA20250422219.md): Skin · dented · Feb 19, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN HAS 1EA. DENT/ LOCATED BETWEEN FS 755.00-789.75, BETWEEN STRGS 12L AND 13L. (C-CHECK RO 04/21/2025)REMOVED DAMAGE AND REPAIRED IAW REO 601R-53-71-234 REV -- DATED 3/21/25, COMPLETED TASK CARD 51-900-1003-SKY AND ATTCHED COMPLETED FORM 3
- [SDR SWIA20250422214](https://openairdocs.org/sdr/SWIA20250422214.md): Skid Shoe · bent · Feb 14, 2025 · N876AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > GROUND AIR SERVICE DOOR 311AL, FORWARD AND AFT LANDING ON AIRFRAME SIDE ARE BENT (C-CHECK RO 04/21/2025)REPAIRED GROUND AIR SERVICE DOOR FORWARD AND AFT LANDINGS IAW REO 601R-53-61-6078 REV. --, DATED 2018-04-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTAC
- [SDR SWIA20250422212](https://openairdocs.org/sdr/SWIA20250422212.md): Skin · dented · Feb 12, 2025 · N876AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR OUTER SKIN, FORWARD LOWER EDGE IS DENTED. (C-CHECK RO 04/21/2025)REPAIRED CARGO DOOR FWD LOWER EDGE OUTER SKIN DENT IAW MHIRJ REO 601R-52-31-431--CATDRAWING REV-- DATED 2025-03-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337
- [SDR SWIA20231002](https://openairdocs.org/sdr/SWIA20231002.md): Unknown · cracked · Oct 2, 2023 · N876AS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > DUE TO LH WSHLD HEAT CAUTION AND LH WINDSHIELD BEING CRACKED, LH WINDSHIELD REQUIRES REPLACEMENT. (FILED CLOSED)REMOVED LH WINDSHIELD IAW AMM 56-11-01. (REF. CP 27240497 FOR INSTALLATION OF LH WINDSHIELD AND PARTS INFO).
- [SDR SWIA202158811](https://openairdocs.org/sdr/SWIA202158811.md): Selector Valve · faulted · Jun 21, 2021 · N876AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > WAS ON APPROACH INTO KMCW WHEN FO FLYING CALLED FOR GEAR DOWN. GOT A GEAR DISAGREE WARNING MESSAGE AND NOSE GEAR DID NOT COME DOWN.PERFORMED QRH PROCEDURE FOR GEAR DISAGREE WARNING AND NOSE GEAR STILL DIDN€™T COME DOWN.DECIDE WITH CRM AND TEM TO DIVERT TO KDS
- [SDR SWIA202156216](https://openairdocs.org/sdr/SWIA202156216.md): Support · cracked · Feb 1, 2021 · N876AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SUPPORT LEG IS CRACKED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED PAX DOOR SUPPORT LEG. REF: CRJ200 AMM 52-11-13-000-806 AND CRJ200 AMM 52-11-13-400-804, NO ADJUSTMENT REQUIRED.

Next page: https://openairdocs.org/aircraft/N876AS/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 = 'N876AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N876AS/reports

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