# Service difficulty reports: N886AS

A list on [N886AS](https://openairdocs.org/aircraft/N886AS.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 4 · 164 reports

- [SDR 2025F00148](https://openairdocs.org/sdr/2025F00148.md): Skin · bent · Jun 28, 2025 · N886AS · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER UPPER SKIN TRAILING EDGE DAMAGE BETWEEN BL: 96.26 - BL:102.25. REPAIRED I/A/W/ MHI RJ REO 601R-55-11-793 REV. -- DATED: 2025-06-19.
- [SDR 2025FA0000429](https://openairdocs.org/sdr/2025FA0000429.md): Frame · cracked · Jun 26, 2025 · N886AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 280 FLOOR BEAM CRACKED, RH SIDE. REPAIRED I/A/W BOMBARDIER REO 601R-53-11-3994 REV. -- 2025-06-04 AND BOMBARDIER REO 601R-53-11-926 REVB 2006-05-10.
- [SDR J6BA2025070100527](https://openairdocs.org/sdr/J6BA2025070100527.md): Skin · damaged · May 27, 2025 · N886AS · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > DAMAGED UPPER SKIN ON R/H HORIZONTAL TRAILING EDGE BETWEEN BL 96.26 TO BL 102.25. REPAIRED UPPER SKIN ON R/H HORIZONTAL TRAILING EDGE BETWEEN BL96.26 TO BL102.25 IAW CRJ200 MHIRJ REO 601R-55-11-793 REV. -- 2025-06-19.ANALYSIS TO DETERMINE ADDITIONAL REQUIREME
- [SDR J6B2025F00005](https://openairdocs.org/sdr/J6B2025F00005.md): Floorbeam · cracked · Apr 17, 2025 · N886AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > F.S280.00 FLOOR BEAM IS CRACKED RH SIDE. REPAIRED AFT FLOOR BEAM ANGLE ON BULKHEAD FS280.00 BETWEEN LBL 20.75 TO RBL 20.75 IAW CRJ200 MHIRJ REO 601R-53-11-3994 REV.-- DATE 2025/06/04 AND MHIRJ REO 601R-53-11-926 REV -B 2006/05/10.
- [SDR J6BA2025070100417](https://openairdocs.org/sdr/J6BA2025070100417.md): Frame · corroded · Apr 17, 2025 · N886AS · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 409 AT S26L THERE IS SIGNS OF CORROSION. REPAIRED FRAME SECTION FS409.00 BETWEEN STRG 24L TO STGR 27 IAW CRJ-200 MHIRJ REO 601R53-21-3741 REV-- 2025-06-16
- [SDR SWIA20230329](https://openairdocs.org/sdr/SWIA20230329.md): Unknown · warning message · Mar 29, 2023 · N886AS · Cndair CL6002B19 · Engine Thrust Reverser
  > D: L REV UNLOCKED AT FL 280C; MEL 78-30-1XCAT: C DUE 04/08/23L REV UNLOCKED AT FL 280 PERFORMED QRC/QRH (FLIGHT 4230 FILED CLOSED)MAR 29, 2023 STATION: SLC--DEFERRED LEFT ENGINE THRUST REVERSER PER MEL 78-30-1, MX ACTION COMPLIED WITH DEACTIVATED LEFT THRUST
- [SDR SWIA202265113](https://openairdocs.org/sdr/SWIA202265113.md): None · none · Mar 2, 2022 · N886AS · Cndair CL6002B19 · Fuselage Main, Frame
  > INSTRUCTIONS OF REO 601R-53-51-616 REV--(P1) DATED 2022-02-25 NOT FOLLOWED DURING INSTALL OF MACHINED ANGLE RESULTING IN MACHINED ANGLE BEING MISDRILLED (C-CHECK RO 3/14/2022) COMPLIED WITH ALL STEPS OF REO BY REMOVAL AND REPLACEMENT OF MACHINED ANGLE P
- [SDR SWIA202265112](https://openairdocs.org/sdr/SWIA202265112.md): None · defective · Feb 8, 2022 · N886AS · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S 409+128 BL 0.00 RH FWD RADIUS OF VERTICAL POST DEFECT NOTED. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED NEW L/H AND R/H STIFFENERS COMMON TO FS 409+128, BL-0 VERTICAL CENTER POST PER REO # 601R-53-41-889 REV: -C DATED: 2018/01/03, AND CRJ-200 SRM 5
- [SDR SWIA202265111](https://openairdocs.org/sdr/SWIA202265111.md): None · corroded · Feb 1, 2022 · N886AS · Cndair CL6002B19 · Wing, Fuselage Attach Fittings
  > LH INBD FLAP VANE LOWER SKIN POSSIBLE EVIDENCE OF CORROSION UNDER THE PAINT BETWEEN THE MIDDLE AND OTBD FITTINGS (MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED CORRODED LH IB FLAP VANE LE SKIN /CAP BETWEEN MIDDLE AND OB FITTINGS, REF CRJ 200 SRM 5
- [SDR SWIA202265110](https://openairdocs.org/sdr/SWIA202265110.md): None · corroded · Jan 28, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR CLIP COMMON TO THE AFT SIDE OF FORMER 338 AND DOOR HINGE IS CORRODED (C-CHECK RO 3/14/2022) PAX DOOR CLIP COMMON TO THE AFT SIDE OF FORMER 338 AND DOOR HINGE FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 & DWG 601R3170
- [SDR SWIA202265109](https://openairdocs.org/sdr/SWIA202265109.md): None · corroded · Jan 28, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR INTERCOSTAL DD3 LOCATED BETWEEN FS311 & FS318 IS CORRODED (C-CHECK RO 3/14/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 LOCATED BETWEEN FS311 & FS318 WITH NEW ONE. P/N-601R318054-1, REF: CRJ-200 S.R.M.51-42-06. AND DRW 601R31702 REV N /
- [SDR SWIA202265108](https://openairdocs.org/sdr/SWIA202265108.md): None · corroded · Jan 27, 2022 · N886AS · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > UPON REMOVAL ON JOB 2753175 OP 103 CAMP 24214818, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION THROUGHOUT BEARING BORE. REPLACE HINGE FITTING ASSY. (C-CHECK RO 3/14/2022) REMOVED CORRODED L/H ELEVATOR L
- [SDR SWIA202265107](https://openairdocs.org/sdr/SWIA202265107.md): None · corroded · Jan 25, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR INTERCOSTAL DD5 IS CORRODED BETWEEN FS338 AND FS347 (C-CHECK RO 3/14/2022) PAX DOOR INTERCOSTAL DD5 LOCATED BETWEEN FS338 AND FS347 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 & DWG 601R31702 REV -N, COMPLIED WITH T
- [SDR SWIA202265106](https://openairdocs.org/sdr/SWIA202265106.md): None · corroded · Jan 25, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR INTERCOSTAL DD4 IS CORRODED BETWEEN FS338 AND FS347 (C-CHECK RO 3/14/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 LOCATED BETWEEN FS338 AND FS347 IAW CRJ200 SRM 51-42-06 & DWG 601R31702 REV -N. PRESSURE LEAK CHECK GOOD REF CRJ200 AMM 21
- [SDR SWIA202265105](https://openairdocs.org/sdr/SWIA202265105.md): None · corroded · Jan 25, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR INTERCOSTAL DD2 IS CORRODED BETWEEN FS338 AND FS347 (C-CHECK RO 3/14/2022) PAX DOOR INTERCOSTAL DD2 LOCATED BETWEEN FS338 AND FS347 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 & DWG 601R31702 REV -N, TASK CARD 51-9
- [SDR SWIA202265104](https://openairdocs.org/sdr/SWIA202265104.md): None · corroded · Jan 25, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR INTERCOSTAL DD1 IS CORRODED BETWEEN FS338 AND FS347 (C-CHECK RO 3/14/2022) PAX DOOR INTERCOSTAL DD1 LOCATED BETWEEN FS338 AND FS347 WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACEDIAW CRJ200 SRM 51-42-06 & DWG 601R31702 REV -N, COMPLIED WITH
- [SDR SWIA202265103](https://openairdocs.org/sdr/SWIA202265103.md): None · gouged · Jan 25, 2022 · N886AS · Cndair CL6002B19 · Fuselage Main, Frame
  > AFTER REMOVING FWD PULL IN LEVER A DEEP GOUGE WAS FOUND ON THE FWD SUPPORT ANGLE P/N-601R318731-3. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED WITH NEW FWD SUPPORT ANGLE AT F.S.311.00. REF: CRJ-200 S.R.M. 51-42-06, 51-42-21 DWG 601R31702 REV-N. COMPLIED
- [SDR SWIA202265092](https://openairdocs.org/sdr/SWIA202265092.md): None · corroded · Jan 25, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR AFT FORMER IS CORRODED AT DD7, INBD SIDE (C-CHECK RO 3/14/2022) PAX DOOR AFT FORMER FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW DWG 601R31702 REV -N, CRJ200 SRM 51-42-06 & CRJ200 SRM 51-42-21, COMPLIED WITH TASK CARD 51-900-1003-SKY, LE
- [SDR SWIA202265024](https://openairdocs.org/sdr/SWIA202265024.md): None · corroded · Jan 24, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR CLIP COMMON TO INTERCOSTAL DD6 & AFT SIDE OF FORMER AT FS338 IS CORRODED (C-CHECK RO 3/14/2022) PAX DOOR CLIP COMMON TO INTERCOSTAL DD6 & AFT SIDE OF FORMER AT FS338 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 & DWG
- [SDR SWIA202265022](https://openairdocs.org/sdr/SWIA202265022.md): None · corroded · Jan 24, 2022 · N886AS · Cndair CL6002B19 · Doors
  > PAX DOOR DD7 INTERCOSTAL CLIP LOCATED BETWEEN FS338 & FS347 IS CORRODED (C-CHECK RO 3/14/2022) PAX DOOR DD7 INTERCOSTAL CLIP LOCATED BETWEEN FS338 & FS347 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 & DWG 601R31702 REV -N, CO
- [SDR SWIA202265020](https://openairdocs.org/sdr/SWIA202265020.md): None · gouged · Jan 24, 2022 · N886AS · Cndair CL6002B19 · Stabilizer Position Indicating
  > *HSTA TRIM ACTUATOR LH PIVOT FITTING ON VSTAB, SUPPORT PLATE INNER FWD EDGE GOUGED (MARKED) (C-CHECK RO 3/14/2022) REPAIRED GOUGING ON INNER FWD EDGE OF SUPPORT PLATE AT HSTA TRIM ACTUATOR LH PIVOT FITING ON V-STAB PER MHIRJ REO 601R-55-31-394 REV -- D
- [SDR SWIA202265018](https://openairdocs.org/sdr/SWIA202265018.md): None · damaged · Jan 24, 2022 · N886AS · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > R/H ELEVATOR FITTING LOCATED @ BL15.25 NEED REMOVAL AND REPLACEMENT. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED R/H ELEVATOR FITTING LOCATED @ BL15.25 REF BOMBARDIER DWG# 601R24025, REV G, AS WELL AS CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. COMPL
- [SDR SWIA202265017](https://openairdocs.org/sdr/SWIA202265017.md): None · gouged · Jan 24, 2022 · N886AS · Cndair CL6002B19 · Stabilizer Position Indicating
  > *HSTA TRIM ACTUATOR LH PIVOT FITTING ON VSTAB, OUTER DOUBLER FWD UPPER EDGE GOUGED (MARKED) (C-CHECK RO 3/14/2022) REMOVED DAMAGE FROM HSTA TRIM ACTUATOR LH PIVOT FITTING ON VSTAB OUTER DOUBLER FWD UPPER EDGE REF. SRM 51-12-00, NO DEFECTS NOTED, FINISH
- [SDR SWIA202265016](https://openairdocs.org/sdr/SWIA202265016.md): None · corroded · Jan 21, 2022 · N886AS · Cndair CL6002B19 · Doors
  > * PAX DOOR INTERCOSTAL DD3 IS CORRODED BETWEEN FS338 AND FS347 (C-CHECK RO 3/14/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 BETWEEN FS338.00 AND FS347.00 REF CRJ200 SRM 51-42-06 AND DWG 601R31702, REV N. PRESSURE LEAK CHECK GOOD REF CRJ200 AMM
- [SDR SWIA202265014](https://openairdocs.org/sdr/SWIA202265014.md): None · corroded · Jan 21, 2022 · N886AS · Cndair CL6002B19 · Fuselage Structure (General)
  > * PAX DOOR FRAME AT FS338 IS CORRODED AT DD6 (C-CHECK RO 3/14/2022) PAX DOOR LOWER FRAME AT FS338 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW DWG 601R31702 REV -N, CRJ200 SRM 51-42-06, & CRJ200 SRM 51-42-21, COMPLIED WITH TASK CARD 51-900-1003-
- [SDR SWIA202265012](https://openairdocs.org/sdr/SWIA202265012.md): None · corroded · Jan 21, 2022 · N886AS · Cndair CL6002B19 · Doors
  > * PAX DOOR, CLIP ATTACHING FS338 FRAME TO INTERCOSTAL BETWEEN DD6 AND DD7 IS CORRODED (C-CHECK RO 3/14/2022) PAX DOOR, CLIP ATTACHING FS338 FRAME TO INTERCOSTAL BETWEEN DD6 AND DD7 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06
- [SDR SWIA202265010](https://openairdocs.org/sdr/SWIA202265010.md): None · chafed · Jan 20, 2022 · N886AS · Cndair CL6002B19 · Fuselage Structure (General)
  > * L/H INBOARD FLAP UPPER SKIN IS CHAFED IN SEVERAL SPOTS ALONG THE LEADING EDGE, MARKED. (C-CHECK RO 3/14/2022) REMOVED CHAFING FROM LH INBD FLAP UPPER SKIN. REF CRJ200 SRM 51-12-00. NDT IS DEFECT FREE. BLENDS ARE STRUCTURALLY ACCEPTABLE PER REO 601
- [SDR SWIA202265008](https://openairdocs.org/sdr/SWIA202265008.md): None · scratched · Jan 20, 2022 · N886AS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > * FOUND DEEP SCRATCHES ON THE RH #2 I/B FLAP HINGE ARM ASSY(AREA MARKED) (C-CHECK RO 3/14/2022) BLENDED DAMAGE REF CRJ200 SRM 51-12-00 AND COMPLIED WITH ALL STEPS OF MHI RJ REO 601R-57-54-345 REV-A DATED 2022-03-09. ALL CHECKS GOOD. SEE CONTINUE CARD
- [SDR SWIA202265006](https://openairdocs.org/sdr/SWIA202265006.md): None · cracked · Jan 19, 2022 · N886AS · Cndair CL6002B19 · Fuselage Structure (General)
  > * CO-PILOT'S WINDSHIELD SIDE POST, LOWER AFT FITTING IS CRACKED, MARKED. (C-CHECK RO 3/14/2022) REMOVED AND RELACED CO-PILOT'S WINDSHIELD SIDE POST, LOWER AFT FITTING.REF CRJ 200 SRM 51-42-21-00 / DWG 601R33007 REV U. TO SEE ALL ADDITIONAL STEP SEE CON
- [SDR SWIA202265000](https://openairdocs.org/sdr/SWIA202265000.md): None · cracked · Jan 19, 2022 · N886AS · Cndair CL6002B19 · Window/Windshield System
  > * PILOT'S WINDSHIELD SIDE POST, LOWER AFT FITTING IS CRACKED, MARKED. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED PILOT'S WINDSHIELD SIDE POST, LOWER AFT FITTING. REF CRJ 200 SRM 51-42-21-00 / DWG 601R33007 REV U. TO SEE ALL ADDITIONAL STEP SEE CONTINU
- [SDR SWIA202264999](https://openairdocs.org/sdr/SWIA202264999.md): None · damaged · Jan 17, 2022 · N886AS · Cndair CL6002B19 · Fuselage Structure (General)
  > *EVALUATE DAMAGE TO RH WING LOWER SKIN SURFACE, AFT PLANK, BL 45 (WS 45) ALONG TRAILING EDGE. (C-CHECK RO 3/14/2022) EVALUATED AND REPAIRED DAMAGE TO RH WING LOWER SKIN SURFACE AFT PLANK BL 45 (WS 45) ALONG TRAILING EDGE PER CRJ200 SRM 51-12-00 REV 38
- [SDR SWIA202264998](https://openairdocs.org/sdr/SWIA202264998.md): None · cracked · Jan 17, 2022 · N886AS · Cndair CL6002B19 · Fuselage Main, Frame
  > *ANGLE IN AFT EQUIPMENT BAY HAS A CRACKED ANGLE ATTACHED TO FRAME FS 625.30. (APPROX. STGR 14L) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED CRACKED INTERCOSTAL ANGLE (P/N: 601-35012-51) ATTACHED TO FRAME FS 625.30 (APPROX. STGR 14L) IN AFT EQUIPMENT BAY
- [SDR SWIA202264997](https://openairdocs.org/sdr/SWIA202264997.md): None · none · Jan 14, 2022 · N886AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > * FLOOR BEAM INBOARD FLANGE HAS A DRILL START AT APPROXIMATELY FS357, RBL9, MARKED. (C-CHECK RO 3/14/2022) RECEIVED REO 601R-53-21-3532 REV --, DATED 2022-02-10 AND DRILLED HOLE OF 0.128 DIA. AND COUNTERSINKED HOLE ENSURING ALL DAMAGE REMOVED. WITH EDG
- [SDR SWIA202264996](https://openairdocs.org/sdr/SWIA202264996.md): None · failed · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Doors
  > CREW ESCAPE HATCH FAILED FUNCTIONAL CHECK. EXTERIOR HANDLE FAILED TO EJECT WHEN TRIGGER PLATE WAS PUSHED. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED LATCH HANDLE ASSEMBLY P/N: 601R33050-1 ON TO CREW ESCAPE HATCH. REF CRJ200 SRM 51-42-06 REV 38 JUL 10/
- [SDR SWIA202264995](https://openairdocs.org/sdr/SWIA202264995.md): None · corroded · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > * L/H FLOOR SUPPORT STRAP AT FS559, LBL27-LBL36 IS CORRODED, MARKED. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED L/H FS559 LBL27-LBL36 FLOOR SUPPORT STRAP PN: 601R31025-29. REF CRJ200 SRM 51-42-06 REV 38 JUL 10/19 AND DWG 601R31025 REV N. PRESSURE LEA
- [SDR SWIA202264994](https://openairdocs.org/sdr/SWIA202264994.md): None · corroded · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > * R/H PRESSURE FLOOR SILL ANGLE IS CORRODED IN MULTIPLE SPOTS, MARKED. (C-CHECK RO 3/14/2022) REMOVED 72EA HILITES AND 17EA RIVETS TO FOM PER CRJ 200 SRM 51-42-06-00 TO FACILITATE REMOVAL OF CORROSION ON MULTIPLE SPOTS @ RH PRESSURE FLOOR SILL ANGLE P
- [SDR SWIA202264993](https://openairdocs.org/sdr/SWIA202264993.md): None · corroded · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > * R/H PRESSURE FLOOR SILL PANEL IS CORRODED IN MULTIPLE SPOTS, MARKED. (C-CHECK RO 3/14/2022) REPAIRED R/H PRESSURE FLOOR SILL PANEL BY BLENDING 12 DISCREPANT AREAS REF GREO 601R-53-41-666 REV -C, DATED 2012-11-06 AND REO 601R-53-41-3015, REV --, DATED
- [SDR SWIA202264992](https://openairdocs.org/sdr/SWIA202264992.md): None · corroded · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > * L/H PRESSURE FLOOR SILL ANGLE IS CORRODED IN MULTIPLE SPOTS, MARKED. (C-CHECK RO 3/14/2022) REPAIRED CORROSION ON LH FLOOR SILL ANGLE AT 10 EA LOCATIONS PER REO 601R-53-41-3014, REV --, DATED 2022-02-01. PRESSURE LEAK CHECK GOOD REF CRJ200 AMM 21-32
- [SDR SWIA202264991](https://openairdocs.org/sdr/SWIA202264991.md): None · corroded · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > * L/H PRESSURE FLOOR SILL PANEL IS CORRODED IN MULTIPLE SPOTS, MARKED. (C-CHECK RO 3/14/2022) REPAIRED L/H PRESSURE FLOOR SILL PANEL DISCREPANT AREAS REF REO 601R-53-41-3014, REV --, DATED 2022-02-01. AND REO 601R-53-41-666 REV C DATED 2012-11-06 P
- [SDR SWIA202264990](https://openairdocs.org/sdr/SWIA202264990.md): None · damaged · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Ailerons
  > REPLACE R/H WING FLAP VANE OUTBOARD VANE CAP ( MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED R/H WING FLAP VANE OUTBOARD VANE CAP. REF CRJ200 SRM 51-42-13 REV 38 JUL 10/2019 AND DWG # 601R14302 REV E. SEE CONTINUE CARD FOR DETAILS. COMPLIED WIT
- [SDR SWIA202264989](https://openairdocs.org/sdr/SWIA202264989.md): None · damaged · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Ailerons
  > REPLACE R/H WING FLAP VANE CENTER VANE CAP ( MARKED (C-CHECK RO 3/14/2022) REPLACED RH WING FLAP VANE CENTER CANE CAP REF. CRJ200 SRM 51-42-13-00 AND DWG 601R14302 REV.E / COMPLIED WITH TASK CARD 51-900-1003-SKY AND SKYWEST FORM M-337
- [SDR SWIA202264988](https://openairdocs.org/sdr/SWIA202264988.md): None · damaged · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Ailerons
  > REPLACE R/H WING FLAP VANE INBOARD VANE CAP ( MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED THE R/H INBD VANE CAP ON THE R/H INBD FLAP VANE REF CRJ-200 SRM 51-42-13 REV 38 JUL 10/2019 AND DWG# 601R14302,REV E. COMPLIED WITH 51-900-1003-SKY. SEE
- [SDR SWIA202264987](https://openairdocs.org/sdr/SWIA202264987.md): None · damaged · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Aileron Tabs
  > REPLACE L/H WING FLAP VANE OUTBOARD VANE CAP ( MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED LH IB FLAP VANE, OB VANE CAP WITH NEW, REF CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV E. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19)
- [SDR SWIA202264986](https://openairdocs.org/sdr/SWIA202264986.md): None · damaged · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Ailerons
  > REPLACE L/H WING FLAP VANE CENTER VANE CAP ( MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED LH IB FLAP VANE, CENTER VANE CAP WITH NEW, REF CRJ 200 SRM 51-42-13 AND DWG 601R-14302 REV D. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B1
- [SDR SWIA202264985](https://openairdocs.org/sdr/SWIA202264985.md): None · damaged · Jan 13, 2022 · N886AS · Cndair CL6002B19 · Ailerons
  > REPLACE L/H WING FLAP VANE INBOARD VANE CAP ( MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED L/H WING FLAP VANE INBOARD VANE CAP REF CRJ200 SRM51-42-13 AND DWG NO. 601R14302 REV -E / COMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202264984](https://openairdocs.org/sdr/SWIA202264984.md): None · corroded · Jan 7, 2022 · N886AS · Cndair CL6002B19 · Wing Structure
  > * L/H WING AILERON PCU BAY, INBOARD AND OUTBOARD PANNELL ATTACH FLANGES HAVE CORROSION AROUND 15 EA. FASTENER HOLES. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM LH WING PCU BAY INBD AND OTBD PANEL ATTACH FLANGES REF CRJ200 SRM 51-21-06. NDT IS DEFEC
- [SDR SWIA202265114](https://openairdocs.org/sdr/SWIA202265114.md): None · cracked · Jan 5, 2022 · N886AS · Cndair CL6002B19 · Doors
  > * PAX DOOR AFT STAIR RISER DRAG ANGLE IS CRACKED AT THE DOOR ASSISTPULLEY BRACKETREMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE. REF: CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-13
- [SDR SWIA202264983](https://openairdocs.org/sdr/SWIA202264983.md): None · cracked · Jan 5, 2022 · N886AS · Cndair CL6002B19 · Wing Structure
  > CRACK NOTED AND MARKED DURING SPECIAL DETAILED INSPECTION OF THE LEFT WING AFT LOWER WING PLANK AT WS148.019 (C-CHECK RO 3/14/2022) REPAIRED CRACK PER GREO 601R-57-21-130 REV-L DATED 2017/03/06 REPAIR OPTION II. COMPLIED WITH TASK CARD 28-900-1000-SKY
- [SDR SWIA202158810](https://openairdocs.org/sdr/SWIA202158810.md): Warning Message · illuminated · Jun 17, 2021 · N886AS · Cndair CL6002B19 · Landing Gear Door Retract Section
  > ***CAT II DOWNGRADED*** / D:GEAR DISAGREE AS WELL AS NOSE DOOR OPEN WARNING MESSAGE ON TAKE OFF, COMPLIED WITH QRH AND MESSAGE WENT AWAY. GEAR OPERATED NORMALLY ON LANDING. / C:MEL 32-30-1 / CAT "A" DUE 1 FLT DAY / MX ACTION COMPLIED WITH / GEAR DISAGREE AS WE
- [SDR SWIA201904250785](https://openairdocs.org/sdr/SWIA201904250785.md): Support Beam · chafed · Mar 22, 2019 · N886AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR SUPPORT BEAM HAS CHAFE MARK ON FWD AND AFT LOWER CHANNEL. (C-CHECK) RO: 04/21/2019 REMOVED AND INSTALLED NEW CARGO BEAM SUPPORT ANGLE IAW SRM AND REO. PRESSURE CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N886AS/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 = 'N886AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N886AS/reports

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