# Service difficulty reports: N856AS

A list on [N856AS](https://openairdocs.org/aircraft/N856AS.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 7 · 339 reports

- [SDR SWI2025F01791](https://openairdocs.org/sdr/SWI2025F01791.md): Landing Gear · warning message · Dec 3, 2025 · N856AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE. RAN QRH. 3 GREEN IND, LANDED & TAXIED TO GATE. MEL 32-30-1CAT A CAT II, SMOD APPROVAL REQUIRED FOR RTS, RUNWAY & WX CONDITIONS, MINOR BLOWING SNOW FROM CROSSWIND. PATCHES OF SNOW. RUNWAY CLEAN. ABNORMAL INDICATION SUSPECTED
- [SDR SWI2025F01718](https://openairdocs.org/sdr/SWI2025F01718.md): Landing Gear · warning message · Dec 3, 2025 · N856AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE. RAN QRH. THREE GREEN INDICATION, LANDED AND TAXIED TO GATE. MEL 32-30-1CAT A DUE ONE FLIGHT DAY 12/04/25 CAT II DOWNGRADED, ODI EVENT, SMOD APPROVAL REQUIRED FOR RTS. RUNWAY AND WX CONDITIONS WERE: MINOR BLOWING SNOW FROM CRO
- [SDR SWIA2025051911](https://openairdocs.org/sdr/SWIA2025051911.md): Warning Message · activated · May 11, 2025 · N856AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING, MEL 32-30-1CAT: AREPAIRS DUE 1 FLIGHT DAY. GEAR DISAGREE WARNING AFTER GEAR SELECTED UP. NOSE GEAR REMAINED DOWN. QRH COMPLIED WITH AND RECEIVED SUBSEQUENT DOWN AND 3 GREEN INDICATION. LANDED UNEVENTFUL. (FLIGHT 4784 - FILED CLOSED)M
- [SDR SWIA2025051201](https://openairdocs.org/sdr/SWIA2025051201.md): Warning Message · illuminated · May 11, 2025 · N856AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNINGC: MEL 32-30-1CAT: AREPAIRS DUE 1 FLIGHT DAY. GEAR DISAGREE WARNING AFTER GEAR SELECTED UP. NOSE GEAR REMAINED DOWN. QRH COMPLIED WITH AND RECEIVED SUBSEQUENT DOWN AND 3 GREEN INDICATION. LANDED UNEVENTFUL. (FLIGHT 4784) FWA--DEFERRED
- [SDR SWI202503190387](https://openairdocs.org/sdr/SWI202503190387.md): Panel · damaged · Mar 4, 2025 · N856AS · Cndair CL6002B19 · Wing Structure
  > TRANSFER FROM EAML 1549262: CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1548503, TRANSITION LEADING EDGE PANEL (620ML) ON RH SIDE REQUIRES REPLACEMENT (FLIGHT 5449 - FILED CLOSED) DRESSED DENT BACK ON PANEL 620ML AT WS139 IN REFERENCE WITH RE
- [SDR SWIA202503190004](https://openairdocs.org/sdr/SWIA202503190004.md): Structure · ground damage · Mar 4, 2025 · N856AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > TRANSFER FROM EAML 1548503: TUG WITH NO DRIVER ROLLED ACROSS RAMP AND IMPACTED RIGHT WING DURING BOARDING. LARGE DENT IN LEADING EDGE. (FILED CLOSED - FLIGHT 5449) REMOVED AND REPLACED RIGHT WING LEADING EDGE ASSEMBLY 620JL WITH REFERENCE TO AMM 57-41-0
- [SDR SWIA202503170004](https://openairdocs.org/sdr/SWIA202503170004.md): Skin · damaged · Mar 4, 2025 · N856AS · Cndair CL6002B19 · Wing Structure
  > TRANSFER FROM EAML 1549262: CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1548503, TRANSITION LEADING EDGE PANEL (620ML) ON RH SIDE REQUIRES REPLACEMENT (FLIGHT 5449 - FILED OPEN) DRESSED DENT BACK ON PANEL 620ML AT WS139 IN REFERENCE WITH REO
- [SDR SWIA202503050004](https://openairdocs.org/sdr/SWIA202503050004.md): Skin · ground damage · Mar 4, 2025 · N856AS · Cndair CL6002B19 · Wing, Plate/Skin
  > TRANSFER FROM EAML 1548503: TUG WITH NO DRIVER ROLLED ACROSS RAMP AND IMPACTED RIGHT WING DURING BOARDING. LARGE DENT IN LEADING EDGE. (FILED OPEN - FLIGHT 5449) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20250311120](https://openairdocs.org/sdr/SWIA20250311120.md): Door Sill · corroded · Jan 20, 2025 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL LOWER ANGLE (REF SRM 53-21-23 ITEM 56B) CORRODED. (FILED CLOSED) REMOVED AND REPLACED PAX DOOR SILL LOWER ANGLE WITH REFERENCE TO SRM 53-21-23, SRM 51-42-06, AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337 A
- [SDR SWIA20250120001](https://openairdocs.org/sdr/SWIA20250120001.md): Door Sill · corroded · Jan 20, 2025 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL LOWER ANGLE (REF SRM 53-21-23 ITEM 56B) CORRODED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025031117](https://openairdocs.org/sdr/SWIA2025031117.md): Track · cracked · Jan 17, 2025 · N856AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT TRACK SUPPORT ANGLE BRACKET ON THE FS 621.00 BULKHEAD IN BETWEEN WL 111.09 - 119.12 IS CRACKED. (FILED CLOSED) REMOVD AND REPLACED THE CARGO DOOR AFT TRACK SUPPORT ANGLE BRACKET ON FS621.00 IN BETWEEN WL 111.09 - 119.12 OR STGR 10L. WORK DO
- [SDR SWI2025F00070](https://openairdocs.org/sdr/SWI2025F00070.md): Support Angle · cracked · Jan 17, 2025 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR AFT TRACK SUPPORT ANGLE BRACKET ON THE FS 621.00 BULKHEAD IN BETWEEN WL 111.09 - 119.12 IS CRACKED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20250311115](https://openairdocs.org/sdr/SWIA20250311115.md): Bracket · cracked · Jan 15, 2025 · N856AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT BALANCE SPRING MOUNTING BRACKET CRACKED AROUND NUTPLATE. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT BALANCE SPRING MOUNTING BRACKET WITH REFERENCE TO SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION OF FASTENER BORES THROUGH ENTIR
- [SDR SWIA2025013000015](https://openairdocs.org/sdr/SWIA2025013000015.md): Mount Bracket · cracked · Jan 15, 2025 · N856AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT BALANCE SPRING MOUNTING BRACKET CRACKED AROUND NUTPLATE. (FILED OPEN) REMOVED AND REPLACED CARGO DOOR AFT BALANCE SPRING MOUNTING BRACKET WITH REFERENCE TO SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION OF FASTENER BORES THROUGH ENTIRE
- [SDR SWIA20250311111](https://openairdocs.org/sdr/SWIA20250311111.md): Floorbeam · corroded · Jan 11, 2025 · N856AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORT STRUCTURE ON THE FWD SIDE OF FS 349.00 BETWEEN RBL 9.00 AND RBL 27.00 (FILED CLOSED) COMPLIED WITH REO 601R-53-21-3717 DATED: 2025-01-18 REV "--" REPAIR FOR CORROSION DAMAGE TO FS349.00 CROSSBEAM BTWN RBL9.00 & RBL27.00. COMPLI
- [SDR SWI2025F00063](https://openairdocs.org/sdr/SWI2025F00063.md): Floor Support · corroded · Jan 11, 2025 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION ON FLOOR SUPPORT STRUCTURE ON THE FWD SIDE OF FS 349.00 BETWEEN RBL 9.00 AND RBL 27.00 (FILED OPEN) COMPLIED WITH REO 601R-53-21-3717 DATED: 2025-01-18 REV "--" REPAIR FOR CORROSION DAMAGE TO FS349.00 CROSSBEAM BTWN RBL9.00 & RBL27.00. COMPLIED
- [SDR SWI2025F00319](https://openairdocs.org/sdr/SWI2025F00319.md): Cargo Track · damaged · Jan 10, 2025 · N856AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND FWD UPPER CARGO TRACK BRACKET AT FS574.00 TO BE DAMAGED (FILED CLOSED) REMOVD AND REPLACED THE CARGO DOOR FWD TRACK SUPPORT ANGLE BRACKET ON FS574.00 IN BETWEEN WL 111.09 - 119.12 OR STGR 10L. WORK DONE IN REFERENCE WITH THE CRJ-200 SRM 53-61-23 A
- [SDR SWIA20250311110](https://openairdocs.org/sdr/SWIA20250311110.md): Track · damaged · Jan 10, 2025 · N856AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND TOP OF AFT CARGO DOOR TRACK AT FS621.00 TO BE DAMAGED (FILED CLOSED) REMOVED AND REPLACED AFT CARGO DOOR TRACK AT FS621.00 WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. PERFORMED EDDY CURRENT INSPECTION OF FASTENER BORES THROUGH THE ENTIRE STAC
- [SDR SWI2025F00068](https://openairdocs.org/sdr/SWI2025F00068.md): Track · damaged · Jan 10, 2025 · N856AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > FOUND FWD UPPER CARGO TRACK BRACKET AT FS574.00 TO BE DAMAGED (FILED OPEN) REMOVD AND REPLACED THE CARGO DOOR FWD TRACK SUPPORT ANGLE BRACKET ON FS574.00 IN BETWEEN WL 111.09 - 119.12 OR STGR 10L. WORK DONE IN REFERENCE WITH THE CRJ-200 SRM 53-61-23 AND
- [SDR SWI2025F00067](https://openairdocs.org/sdr/SWI2025F00067.md): Track · damaged · Jan 10, 2025 · N856AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > FOUND TOP OF AFT CARGO DOOR TRACK AT FS621.00 TO BE DAMAGED (FILED OPEN) REMOVED AND REPLACED AFT CARGO DOOR TRACK AT FS621.00 WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. PERFORMED EDDY CURRENT INSPECTION OF FASTENER BORES THROUGH THE ENTIRE STACK
- [SDR SWIA20250311105](https://openairdocs.org/sdr/SWIA20250311105.md): Access Panel · damaged · Jan 5, 2025 · N856AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LH FUEL PANEL ACCESS DOOR LANDING AT 540BB HAS 2 AREAS OF MINOR PITTING, OUTBOARD AFT EDGE APPROX. 4" TOTAL AND SEMI-CENTER FWD APPROX 1". (FILED CLOSESD) REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 540BB, OUTBOARD AFT EDGE APPROX. 4" TOTAL AND
- [SDR SWIA202501300005](https://openairdocs.org/sdr/SWIA202501300005.md): Access Panel · corroded · Jan 5, 2025 · N856AS · Cndair CL6002B19 · Standard Practices/Structures
  > LH FUEL PANEL ACCESS DOOR LANDING AT 540BB HAS 2 AREAS OF MINOR PITTING, OUTBOARD AFT EDGE APPROX. 4" TOTAL AND SEMI-CENTER FWD APPROX 1". (FILED OPEN) REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 540BB, OUTBOARD AFT EDGE APPROX. 4" TOTAL AND SE
- [SDR SWIA202305301029](https://openairdocs.org/sdr/SWIA202305301029.md): Unknown · warning message · May 29, 2023 · N856AS · Cndair CL6002B19 · Landing Gear System
  > GEAR DISAGREE (FLT 4680 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26687777 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP26687967 FOR REMOVAL AND REPLACEMENT OF LH MLG SIDE STAY ACTUATOR.REFERENCE CP26688073 FOR LANDING GEAR MECHANICAL AN
- [SDR SWIA202266738](https://openairdocs.org/sdr/SWIA202266738.md): None · pressure loss · Nov 8, 2022 · N856AS · Cndair CL6002B19 · Cabin Pressure Indicator
  > AFTER T/O CABIN WILL NOT PRESSURIZED AND LEFT PACK OFF WITH THE SWITCH PRESSED ON,STAYED BELOW 10000. QRH WAS PREFORMED DIDN€™T FIX IT. (FLIGHT 5397 - FILED CLOSED) FOUND LEFT 10TH STAGE SOV NOT TO BE OPENING WHEN SELECTED REMOVE AND REPLACED LEFT 10TH
- [SDR SWIA202266723](https://openairdocs.org/sdr/SWIA202266723.md): Warning Message · illuminated · Nov 1, 2022 · N856AS · Cndair CL6002B19 · Pneumatic Indicating System
  > GOT R 14TH DUCT WARNING MESSAGE ON TAKEOFF. CHECKED ANTI-ICE PAGE AND SAW RED LINE GOING UP THE RIGHT SIDE OF THE FUSELAGE. ANTI-ICE WAS OFF, NEVER USED. ABOUT 30 SECONDS LATER GOT BOTH L & R 10TH DUCT WARNING MESSAGES. FOLLOWED QRH, RETURNED TO FIELD WITH RIG
- [SDR SWIA202265967](https://openairdocs.org/sdr/SWIA202265967.md): None · failed · Jun 23, 2022 · N856AS · Cndair CL6002B19 · Landing Gear Door Actuator
  > D: GEAR DISAGREE ON APPROACH, (AMBER LEFT MAIN) WENT AROUND / PERFORMED QRH, GEAR ALL SHOWED GREEN/DOWN ON THIRD CYCLE. / DEN LINE MX - INTERROGATED PSEU AND FOUND CODES S19 AND S34 FOR THE LH MLG DOWN LOCK. DEFERRING LANDING GEAR RETRACTION SYSTEM REF CRJ200
- [SDR SWIA202265439](https://openairdocs.org/sdr/SWIA202265439.md): None · leaking · Apr 21, 2022 · N856AS · Cndair CL6002B19 · Aileron Tabs
  > RIGHT WING 2ND CANOE O/B OF MLG HAS FUEL LEAK AT THE FORWARD BOLTS OF THE BOX FITTING FORWARD HINGE ( REF 57-21-36) (FILED CLOSED) REMOVED AND REPLACED FOWARD AND AFT HARDWARE OF FLAP HINGE-BOX FITTING ON RIGHT WING 2ND CANOE IN REFERENCE TO AMM 57-21-36.
- [SDR SWIA202265440](https://openairdocs.org/sdr/SWIA202265440.md): None · leaking · Apr 17, 2022 · N856AS · Cndair CL6002B19 · Ailerons
  > RIGHT WING 2ND CANOE O/B OF MLG HAS FUEL LEAK. (FILED - CLOSED) REMOVED AND REPLACED THE TWO FORWARD BOLTS, TWO WASHERS, AND TWO NUTS OF R/H WING FWD HINGE-BOX FITTING BY 2ND CANOE OF MLG IN REF TO AMM 57-21-36. SEE CP 24695858 FOR LEAK CHECK.
- [SDR SWIA202162644](https://openairdocs.org/sdr/SWIA202162644.md): None · corroded · Oct 13, 2021 · N856AS · Cndair CL6002B19 · Elevator, Plate/Skin
  > LH ELEVATOR ATTATCHING HARDWARE IS CORRODED AND NEEDS REPLACED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH ELEVATOR ATTATCHING HARDWARE REFERENCE MX TRANS 22021725 FOR INSTALL
- [SDR SWIA202162643](https://openairdocs.org/sdr/SWIA202162643.md): None · corroded · Oct 8, 2021 · N856AS · Cndair CL6002B19 · Wing Structure
  > RH FLIGHT SPOILER INBOARD, IB MID, AND OB MID HINGE POINTS HAVE CORRODED HARDWARE ALONG WITH BOTH PCU LOWER ATTACH BOLT NUTS AND RETAINING PLATES. HARDWARE REQUIRES REPLACEMENT AS NEEDED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED THE RH FLIGHT SPOILER I
- [SDR SWIA202162648](https://openairdocs.org/sdr/SWIA202162648.md): None · damaged · Oct 6, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)
  > RH OTBD FLAP HINGE BOX AT WS264.00 AFT OTBD HAT BUSHING IS BROKEN THE HAT IS BROKEN OFF. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED THE RH OTBD FLAP HINGE BOX AT WS264.00 AFT OTBD HAT BUSHING IAW CRJ-200 AMM 20-26-00-910-802, 20-26-00-910-804.
- [SDR SWIA202162647](https://openairdocs.org/sdr/SWIA202162647.md): None · damaged · Oct 6, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)
  > RH OTBD FLAP HINGE BOX AT WS178.00 AFT OTBD HINGE LUG ON THE BOX HAS A BROKEN HAT BUSHING THE HAT IS BROKEN OFF. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED THE RH OTBD FLAP HINGE BOX AT WS178.00 AFT OTBD HINGE LUG ON THE BOX BUSHING IAW CRJ-200 AMM 20-26-
- [SDR SWIA202162646](https://openairdocs.org/sdr/SWIA202162646.md): None · damaged · Oct 6, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)
  > LH OTBD FLAP HINGE BOX AT WS178.00 INBD AFT BOX LUG HAT BUSHING HAS THE HAT BROKEN OFF OF IT (C-CHECK- RO 11/11/21).REMOVED AND REPLACED THE LH OTBD FLAP HINGE BOX AT WS178.00 INBD AFT LUG BUSHINGS IAW CRJ-200 AMM 20-26-00-910-802, 20-26-00-910-804.
- [SDR SWIA202162645](https://openairdocs.org/sdr/SWIA202162645.md): None · damaged · Oct 5, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)
  > RH WING OTBD FLAP HINGE BOX AFT MOUNT BUSHINGS HAVE THE HAT BROKEN OFF OF 2 EA HAT BUSHINGS AND REQUIRE REPLACEMENT. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED THE RH WING OTBD FLAP HINGE BOX AT WS220 AFT MOUNT BUSHINGS IAW CRJ-200 AMM 20-26-00-910-802, 2
- [SDR SWIA202162582](https://openairdocs.org/sdr/SWIA202162582.md): None · damaged · Oct 2, 2021 · N856AS · Cndair CL6002B19 · Aileron Tabs
  > R/H WING O/B FLAP HINGE BOX AFT ATTACH FITTINGS (2 EA) HAVE TOOLING DAMAGE, I/B FITTING O/B LUG O/B AFT CORNER AND O/B FITTING I/B LUG I/B CORNER (C-CHECK- RO 11/11/21) REPAIRED DAMAGE IAW REO 601R-57-21-3524 REV -- DATED 10-4-2021. COMPLETED S
- [SDR SWIA202162581](https://openairdocs.org/sdr/SWIA202162581.md): None · cracked · Sep 20, 2021 · N856AS · Cndair CL6002B19 · Fuselage Main, Frame
  > LH F.S.605 FRAME SECTOR 601R36026-29 IN BAGGAGE BAY JUST BELOW FLOOR LEVEL HAS 2 INCH CRACK. (C-CHECK- RO 11/11/21) REPLACED LH FRAME SECTION AT F.S. 605.00 STGR 17L - 20L IAW CRJ-200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTAC
- [SDR SWIA202162580](https://openairdocs.org/sdr/SWIA202162580.md): None · bent · Sep 5, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR BEAM WEB AT LBL 9 AND FS 559+96 TO 559+112 ON INBOARD SIDE OF BEAM WAS FOUND TO BE BENT ACROSS LIGHTNING HOLES AND REQUIRES REPLACEMENT. (C-CHECK- RO 11/11/21) INSTALLED NEW WEB PN 601R31119-66 AT LBL 9 AND FS. 559 +96 TO FS. 559 +112 ON INBOARD SID
- [SDR SWIA202162642](https://openairdocs.org/sdr/SWIA202162642.md): None · corroded · Sep 3, 2021 · N856AS · Cndair CL6002B19 · Elevator, Spar/Rib
  > LH ELEVATOR VERTICAL TORQUE TUBE UPPER AND LOWER BEARINGS AND CONTROL ROD BEARINGS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPAIRED LH ELEV VERT SHAFT ATTACHING BEARINGS IAW CRJ 200 AMM 20-26-00-910-806 AND UPPER OB CONTROL ROD IAW CRJ 200 AMM 27-31-3
- [SDR SWIA202162579](https://openairdocs.org/sdr/SWIA202162579.md): None · corroded · Sep 3, 2021 · N856AS · Cndair CL6002B19 · Doors
  > FOUND SERVICE DOOR LOWER AFT PAN TO BE CORRODED OUT OF LIMITS. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SVC DOOR LOWER AFT PAN IAW CRJ 200 SRM 51-42-06, 51-42-21, AND SNIEO 601R38304 S09. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM
- [SDR SWIA202162578](https://openairdocs.org/sdr/SWIA202162578.md): None · none · Sep 2, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > AFTER REMOVAL OF FLOOR BEAM FOUND WEB AT RBL 9 AND F.S 559+16 TO 559+32 ON THE INBOARD SIDE OF FLOOR BEAM TO BE CORRODED WITH A 100% MATERIAL LOSS PART FOUND TO BE UNSERVICABLE AND REQUIRES REPLACEMENT. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED FLOOR BEA
- [SDR SWIA202162577](https://openairdocs.org/sdr/SWIA202162577.md): None · gouged · Sep 2, 2021 · N856AS · Cndair CL6002B19 · Ailerons
  > W.S. 264.00 FLAP HINGE BOX ATTACH FITTING (OUTBD AFT) FOUND TO BE GOUGED AND REQUIRES REPAIR (C-CHECK- RO 11/11/21) REPAIRED W.S 264.00 FLAP HINGE BOX ATTACH FITTING OUTBD AFT GOUGE IAW MHIRJ REO 601R-57-21-3515 REV -- DATED 2021-09-08 AND SKYCARD 51-900-1
- [SDR SWIA202162618](https://openairdocs.org/sdr/SWIA202162618.md): Track · corroded · Sep 1, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 364 TO F.S. 394. (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802
- [SDR SWIA202162617](https://openairdocs.org/sdr/SWIA202162617.md): Intercostal · corroded · Aug 31, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/H FLOOR SILL IS CORRODED BETWEEN F.S. 559.0 TO F.S.559.0+16 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH FLOOR SILL FROM FS 559- FS 559+16 IAW CRJ 200 SRM 51-42-06 AND 51-42-21
- [SDR SWIA202162576](https://openairdocs.org/sdr/SWIA202162576.md): None · corroded · Aug 31, 2021 · N856AS · Cndair CL6002B19 · Fuselage Main, Frame
  > R/H F.S. 513 FRAME IS CORRODED AT STGR 17 (FLOOR LEVEL). (C-CHECK- RO 11/11/21) REPAIRED RH FS 513 FRAME CORROSION AT STGR 17 IAW MHIRJ REO 601R-41-2960 REV -- DATED 2021-09-07 AND SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE REF ATTACHED 337 FORM
- [SDR SWIA202162641](https://openairdocs.org/sdr/SWIA202162641.md): None · corroded · Aug 30, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)
  > L/H WS 53.60 BATT RIB, INBOARD ANGLE IS CORRODED COMMON TO CANNON PLUGS J411 AND J413 ATTCAHING HARDWARE. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH WS 53.60 BATT RIB ANGLES IAW CRJ 200 SRM 51-42-21 AND 51-42-06.
- [SDR SWIA202162575](https://openairdocs.org/sdr/SWIA202162575.md): None · corroded · Aug 30, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RBL 9 FLOOR BEAM BETWEEN FS 559 AND FS 559+64 CORRODED OUT OF LIMITS, FROM CAMP 23329338 JOB97404121 OP#293 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RBL9 FLOOR BEAM AT F/S 559 TO 559+64 IAW CRJ 200 SRM 51-42-06, 51-42-36 AND REO 601R-53-51-599 REV -- DA
- [SDR SWIA202162574](https://openairdocs.org/sdr/SWIA202162574.md): None · corroded · Aug 30, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LBL 9 FLOOR BEAM BETWEEN FS 559+9 AND 559+112 CORRODED OUT OF LIMITS, SEE CAMP #23328805 (C-CHECK- RO 11/11/21) REMOVE AND INSTALLED FLOOR BEAM CAP AT LBL 9 FROM FS. 559+9 TO 559+112 IAW MHIRJ REO 601R-53-51-599 REV; -- DATED: 2021-42-36, CRJ 200 SRM 51-42
- [SDR SWIA202162573](https://openairdocs.org/sdr/SWIA202162573.md): None · dented · Aug 28, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)
  > DURING NDT AND VISUAL INSPECTIONS OF THE FS 621.00 REAR PRESSURE BULKHEAD FOUND THERE TO BE SEVERAL CHAFES, DENTS, AND FAILED NDT INDICATIONS ON THE FWD FACE OF THE BULKHEAD.SEE CONTINUATION CARD FOR TYPE/LOCATION OF DAMAGE. (C-CHECK- RO 11/11/21) REMOVED
- [SDR SWIA202162649](https://openairdocs.org/sdr/SWIA202162649.md): None · bent · Aug 20, 2021 · N856AS · Cndair CL6002B19 · Doors
  > PAX DOOR AFT DRAG ANGLE BENT AND 2 RIVETS PULLED OUT WHERE ASSIST CABLE COMES OUT OF DOOR (C-CHECK- RO 11/11/21) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE IAW CRJ 200 SRM 51-42-13.
- [SDR SWIA202162616](https://openairdocs.org/sdr/SWIA202162616.md): None · corroded · Aug 20, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RBL27 FLOOR SEAT TRACK FS559+78 - FS559+96 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802

Next page: https://openairdocs.org/aircraft/N856AS/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 = 'N856AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N856AS/reports

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