# Service difficulty reports: N868AS, cancelled Oct 2, 2023

A list on [N868AS, cancelled Oct 2, 2023](https://openairdocs.org/deregistered/N868AS-2023-10-02.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 · 239 reports

- [SDR SWIA202264777](https://openairdocs.org/sdr/SWIA202264777.md): None · failed · Mar 6, 2022 · N868AS · Cndair CL6002B19 · Landing Gear Door Actuator
  > PILOT REPORTS RECEIVING GEAR DISAGREE WARNING UPON TAKEOFF. CREW PERFORMED QRH AND MANUALLY DROPPED GEAR. (FLIGHT 4724 - FILED CLOSED) INSPECTED ALL 3 LANDING GEAR AND FOUND ICE ON ALL 3 LANDING GEAR. DE ICED ALL 3 LANDING GEAR. RE-STOWED THE LANDING GEA
- [SDR SWIA202161621](https://openairdocs.org/sdr/SWIA202161621.md): Track · gouged · Oct 10, 2021 · N868AS · Cndair CL6002B19 · Doors
  > CARGO DOOR AFT TRACK HAS A GOUGE ON UPPER PORTION ABOUT 1/2 INCH LONG. DUE TO CARGO DOOR TRACK ATTACH POINT (AFT BULKHEAD). THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 WILL BE REQUIRED. (FILED CLOSED) REMOVED AND REPLACED AFT TRACK P/N 601
- [SDR SWIA2021073059790](https://openairdocs.org/sdr/SWIA2021073059790.md): Handle · out of adjust · Jul 28, 2021 · N868AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WARNING ON CLIMB OUT. ON LANDING DOOR HANDLE WAS NOT FULLY STOWED. (FLIGHT 4643 - FILED CLOSED) FOUND THE LOCK/UNLOCK INDICATOR PUSH-ROD NOT ADJUSTED CORRECTLY PUTTING A PRELOAD ON THE OUTER HANDLE. ADJUSTED THE LOCK/UNLOCK INDICATOR PUSH
- [SDR SWIA202155482](https://openairdocs.org/sdr/SWIA202155482.md): Seat Track · broken · Jan 7, 2021 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FLOOR FITTING PART NUMBER CDSP1900-17 FOR CENTER 9G BULKHEAD ASSEMBLY IS BUSTED. C-CHECK RO 1/16/2021. ORDERED AND RECEIVED NEW SEAT TRACK FLOOR FITTING PART CDSP1900-17 FOR CENTER 9G BULKHEAD ASSEMBLY. INSTALLATION OF NEW FITTING INSTALLED ON J
- [SDR SWIA202155479](https://openairdocs.org/sdr/SWIA202155479.md): Seat Track · corroded · Jan 5, 2021 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK, LBL 9 APPROXIAMTELY FS 559+4. C-CHECK RO 1/16/2021. REMOVED AND REPLACED SEAT TRACK, REF CRJ 200, AMM 53-01-11-400-802.
- [SDR SWIA202155478](https://openairdocs.org/sdr/SWIA202155478.md): Seat Track · corroded · Jan 5, 2021 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK LBL 9, APPROXIMATELY FS 559.+112. C-CHECK RO 1/16/2021. REMOVED AND REPLACED SEAT TRACK, REF CRJ 200 AMM 53-01-11-400-802.
- [SDR SWIA202155477](https://openairdocs.org/sdr/SWIA202155477.md): Seat Track · corroded · Jan 2, 2021 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND SEAT TRACK RBL 9, FS 559.+96. C-CHECK RO 1/16/2021. REMOVED DAMAGED SEAT TRACK AT RBL 9, FS 559 +96, REF CRJ 200, AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK P/N 601R38779-13 AT RBL 9, FS 559. +96, REF CRJ 200, AMM 53- 01-11-400-802, TOOL
- [SDR SWIA202155476](https://openairdocs.org/sdr/SWIA202155476.md): Seat Track · corroded · Jan 2, 2021 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK, RBL 9, FS 559.112. C-CHECK RO 1/16/2021. REMOVED DAMAGED SEAT TRACK AT RBL 9, FS 559.112, REF CRJ 200, AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK P/N 601R38779-49 AT RBL 9, FS 559.112, REF CRJ 200, AMM 53- 01-11-400-802, T
- [SDR SWIA202055475](https://openairdocs.org/sdr/SWIA202055475.md): Seat Track · corroded · Dec 29, 2020 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER SEAT TRACK P/N 601R31032-21 CORRODED AT RBL 9.0 FROM FS 409.00 TO FS 409.00+118, MARKED. C-CHECK RO 1/16/2021. REPLACED RBL 9 FLOOR SEAT TRACK FROM FS 409.00 TO FS 409.00+118 USING TOOL TUC 5657 CAL DUE 31-MAR-21, REF CRJ-200-AMM 53-01-11-400-802.
- [SDR SWIA202055452](https://openairdocs.org/sdr/SWIA202055452.md): Floor Support · broken · Dec 18, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM HAS BROKEN AT LBL 9, FS 559.00+48-FS 559.00+64. C-CHECK RO 1/16/2021. REMOVED AND REPLACED NEW FLOOR BEAM WEB P/N 601R31119-61 AT LBL 9 FS 559.00+48-FS 559.00 +64, REF CRJ200 SRM 51-42-06 AND DWG 601R31119 REV-H. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWIA202055451](https://openairdocs.org/sdr/SWIA202055451.md): Hinge Box · gouged · Dec 10, 2020 · N868AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > RT WING INBD FLAP, HINGE BOX AT WS 80.50, AFT OUTBOARD ATTACH LUG ON THE WING IS GOUGED, MARKED. C-CHECK RO 1/16/2021. REPAIRED RT WING INBD FLAP, HINGE BOX AT WS 80.50, AFT OUTBOARD ATTACH LUG, REF REO 601R-57-21-3401, REV-, DATE 2021-01-11. SEE CONTINUATI
- [SDR SWIA202055450](https://openairdocs.org/sdr/SWIA202055450.md): Stringer Clip · cracked · Dec 8, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CLIP ATTACHING STRINGER 3L TO FS 280 BULKHEAD IS CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CLIP AT FS 280.00 AT STRINGER 3L, IAW CRJ 200 SRM 51-42-06 DRAWING 600-34017 REV AD. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA202055449](https://openairdocs.org/sdr/SWIA202055449.md): Post · damaged · Dec 6, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 409+128 BL 0 RT VERTICAL POST FWD RADIUS DEFECT NOTED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW POST ASSEMBLY (LT & RT), AND NEW (LT & RT) SUPPORT ANGLES AT FS 409 +128 BL 0, REF CRJ 200 SRM 51-42-06 AND REO 601R-53-41-889 REV B DATED 2017-03-06, C
- [SDR SWIA202055480](https://openairdocs.org/sdr/SWIA202055480.md): Support Beam · chafed · Dec 5, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR SURROUND TRACK SUPPORT BEAM FORWARD OF FS 621 CHAFED FROM CABLE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED NEW CARGO DOOR SURROUND-TRACK SUPPORT BEAM FORWARD OF FS 621.00, CRJ 200 SRM 51-40-11, SRM 51-42-21. SEE ATTACHED CONTINUATION CARD FOR DE
- [SDR SWIA202055456](https://openairdocs.org/sdr/SWIA202055456.md): Support Beam · cracked · Dec 5, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR SURROUND TRACK SUPPORT BEAM BRACKET AT FS 574 CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED NEW BRACKET PART NUMBER 601R35050-121, IAW CRJ200 SRM 51-42-21.
- [SDR SWIA202055448](https://openairdocs.org/sdr/SWIA202055448.md): Intercostal · cracked · Dec 3, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FS 621 AND FS 625 AT STR 14L IS CRACKED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW INTERCOSTAL AT STR 14L BETWEEN FS 621 AND FS 625 WITH NO FILLERS, REF CRJ-200-SRM 51-42-21, REO 601R-53-61-422 REV NC, DATED 2001-08-23, AND REO 601R
- [SDR SWIA202055447](https://openairdocs.org/sdr/SWIA202055447.md): Skin · cracked · Dec 3, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LT TRU BAY DOOR AFT LATCH CUT-OUT ON FUSELAGE HAS A CRACK. C-CHECK RO 1/16/2021. INSTALLED NEW LT TRU LANDING SKIN PANEL P/N 600-33052-145, REF BOMBARDIER ENG DWG 600-33052 REV Y AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA202055474](https://openairdocs.org/sdr/SWIA202055474.md): Hinge Box · corroded · Nov 30, 2020 · N868AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > RT OUTBOARD FLAP HINGE BOX, FORWARD ATTACH FITTING ON WS 264.00, OUTBOARD FORWARD ATTACH BOLT IS CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED 1 EA BOLT AND 1 EA WASHER AT RT OUTBOARD FLAP HINGE BOX, FORWARD ATTACH FITTING ON WS 264.00, OUTBOARD FORWA
- [SDR SWIA202055473](https://openairdocs.org/sdr/SWIA202055473.md): Hinge Box · corroded · Nov 30, 2020 · N868AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > RT OUTBOARD FLAP HINGE BOX, FORWARD ATTACH FITTING ON WS 220.00, INBOARD AND OUTBOARD FORWARD ATTACH BOLTS ARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED WITH NEW 2 EA BOLTS AND 2 EA WASHERS AT RT OUTBOARD FLAP HINGE BOX, FORWARD ATTACH FITTING ON
- [SDR SWIA202055446](https://openairdocs.org/sdr/SWIA202055446.md): Vane · damaged · Nov 30, 2020 · N868AS · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE RT WING INBOARD FLAP VANE OUTBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REPLACED RT WING INBOARD FLAP VANE ONBOARD LEADING EDGE WITH A SERVICEABLE UNIT, REF CRJ-200 SRM 51-42-13, CRJ-200-SRM 51-40-11, AND DWG 601R14303 REV J. COMPLIED WITH TASK CARD
- [SDR SWIA202055445](https://openairdocs.org/sdr/SWIA202055445.md): Vane · damaged · Nov 30, 2020 · N868AS · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE RT WING INBOARD FLAP VANE CENTER OUTBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RIGHTHAND WING INBOARD FLAP VANE CENTER SKIN OUTBOARD LEADING EDGE, IAW CRJ200 SRM 51-42-13 AND DRAWING 601R14303 REV J. SEE CONTINUATION FOR FUTHER D
- [SDR SWIA202055444](https://openairdocs.org/sdr/SWIA202055444.md): Vane · damaged · Nov 30, 2020 · N868AS · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE RT WING INBOARD FLAP VANE INBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REPLACED RT WING INBOARD FLAP VANE INBOARD LEADING EDGE WITH A SERVICEABLE UNIT, REF CRJ-200 SRM 51-42-13, CRJ-200 SRM 51-40-11, AND DWG 601R14303 REV J. COMPLIED WITH TASK CARD 5
- [SDR SWIA202055443](https://openairdocs.org/sdr/SWIA202055443.md): Hinge Fitting · damaged · Nov 30, 2020 · N868AS · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL OF RT ELEVATOR HINGE FITTING BEARING BORE WAS FOUND TO BE PITTED AND REQUIRES REPLACEMENT. HINGE FITTING PN IS 600-24043-1. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT ELEVATOR HINGE FITTING P/N 600-24043-1, REF BOMBARDIER DWG. 601R24025, REV
- [SDR SWIA202055472](https://openairdocs.org/sdr/SWIA202055472.md): Seat Track · corroded · Nov 29, 2020 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT RAIL STRUCTURE FROM FS 349.0 TO FS 559+80 HAS SEVERAL AREAS OF CORROSION. C-CHECK RO 1/16/2021. BLENDED CORROSION AT RT SEAT RAIL STRUCTURE FROM FS 349.0 TO FS 559.0+80, IAW CRJ200 SRM 51-25-16. CORROSION AREA BETWEEN FS 548 TO FS 559+40 OUT OF LIMI
- [SDR SWIA202055442](https://openairdocs.org/sdr/SWIA202055442.md): Floor Support · corroded · Nov 29, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON RT PRESSURE FLOOR SILL PANEL. C-CHECK RO 1/16/2021. REPAIRED RT PRESSURE FLOOR SILL PANEL, REF REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-2825 REV - DATED 2021-01-05. PRESSURE CHECK GOOD. COMPLIED WITH 51-9
- [SDR SWIA202055441](https://openairdocs.org/sdr/SWIA202055441.md): Floor Support · corroded · Nov 29, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON LT PRESSURE FLOOR SILL PANEL. C-CHECK RO 1/16/2021. REPAIRED LT PRESSURE FLOOR SILL PANEL, REF REO 601R-53-41-666 REV C DATED 2012-11-06, REO 601R-53-41-2825 REV- DATED 2021-01-05 AND CRJ-200-SRM 51-21-06. COMPLIED WITH 51-90
- [SDR SWIA202055455](https://openairdocs.org/sdr/SWIA202055455.md): Frame · cracked · Nov 28, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CLIP CRACKED ON TOP FLANGE OF FRAME AT FS 589 BETWEEN STGR 26R AND STGR 25R. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CLIP ON TOP FLANGE OF FRAME AT FS 589 BETWEEN STGR 26R AND STGR 25R, REF CRJ 200 SRM 51-42-06.
- [SDR SWIA202055440](https://openairdocs.org/sdr/SWIA202055440.md): Skin · corroded · Nov 28, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL SKIN AT BETWEEN FS 559+80 AND FS 559+112 AND BETWEEN STR 26L AND STR 26R, AREA MARKED. C-CHECK RO 1/16/2021. REMOVED CORROSION ON EXTERNAL SKIN AT BETWEEN FS 559+80 AND FS 559+112 AND BETWEEN STR 26L AND STR 26R, REF CRJ-200-SRM 51-21-0
- [SDR SWIA202055439](https://openairdocs.org/sdr/SWIA202055439.md): Skin · corroded · Nov 28, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL SKIN AT BETWEEN FS 559+32 AND FS 559+48 AND BETWEEN STR 26L AND STR 26R, LOCATIONS MARKED. C-CHECK RO 1/16/2021. REPAIRED DAMAGE ON EXTERNAL SKIN AT BETWEEN FS 559+32 AND FS 559+48 AND BETWEEN STR 26L AND STR 26R, IAW REO 601R-53-51-538
- [SDR SWIA202055438](https://openairdocs.org/sdr/SWIA202055438.md): Skin · corroded · Nov 28, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL SKIN AT APPROXIMATELY FS 559+16 AND BETWEEN STR 26L AND STR 26R, MARKED. C-CHECK RO 1/16/2021. REPAIRED CORROSION ON EXTERNAL SKIN AT FS 559+16 AND BETWEEN STR 26L AND STR 26R, REF REO 601R-53-51-538 REV- DATED 2020-12-07. COMPLIED WIT
- [SDR SWIA202055437](https://openairdocs.org/sdr/SWIA202055437.md): Doubler · corroded · Nov 28, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Structure
  > SERVICE DOOR SURROUND LOWER DOUBLER HAS CORROSION AT FS 319. C-CHECK RO 1/16/2021. REMOVED CORROSION FROM SERVICE DOOR SURROUND LOWER DOUBLER. STRUCTURALLY ACCEPTABLE, REF REO601R-53-21-3368 REV- 2020-12-05 AND CRJ200 SRM 51-21-06. COMPLIED WITH 51-900-100
- [SDR SWIA202055436](https://openairdocs.org/sdr/SWIA202055436.md): Attach Bracket · corroded · Nov 28, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > SERVICE DOOR SURROUND BRACKET ATTACHING TO ANGLE AT FS 319 (LOWER SILL AREA) HAS CORROSION. C-CHECK RO 1/16/2021. REMOVED CORRODED ANGLE AND REPLACED WITH NEW ANGLE, PER CRJ 200 DWG 601R38303 REV AR & CRJ 200 SRM 51-42-21 & 51-42-06. C/W SKY CARD 51-900-100
- [SDR SWIA202055435](https://openairdocs.org/sdr/SWIA202055435.md): Plate · corroded · Nov 28, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Structure
  > PLATE ON FRAME AT FS 310 HAS CORROSION ABOVE SERRATED PLATE FOR PASSENGER DOOR FORWARD ANCHOR FITTING. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW FABRICATED GUSSET PLATE P/N 601R31109-97 AT FS 310, REF CRJ-200 SRM 51-42-06 AND DRAWING 601R31109 REV F.
- [SDR SWIA202055471](https://openairdocs.org/sdr/SWIA202055471.md): Anchor Fitting · corroded · Nov 27, 2020 · N868AS · Cndair CL6002B19 · Passenger/Crew Doors
  > SERRATED PLATE FOR PASSENGER DOOR FORWARD ANCHOR FITTING HAS CORROSION ABOVE AND BELOW ANCHOR FITTING. C-CHECK RO 1/16/2021. REMOVED AND REPLACED WITH NEW SERRATED PLATE FOR PASSENGER DOOR FORWARD ANCHOR FITTING, REF CRJ 200 AMM 52-11-17-400-804.
- [SDR SWIA202055434](https://openairdocs.org/sdr/SWIA202055434.md): Support Beam · cracked · Nov 27, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR SURROUND TRACK SUPPORT BEAM AT FS 621 LOWER BRACKET CRACKED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED CARGO DOOR LOWER TRACK SUPPORT BRACKET, REF CRJ-200-SRM 51-24-21 AND BOMBARDIER DRAWING 601R35050 REV AC. COMPLIED WITH 51-900-1003-SKY. SEE
- [SDR SWIA202055433](https://openairdocs.org/sdr/SWIA202055433.md): Hinge Fitting · out of tolerance · Nov 27, 2020 · N868AS · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL OF LT ELEVATOR HINGE FITTING BEARING BORE WAS FOUND TO BE OUT OF TOLERANCE, REPLACE HINGE FITTING ASSEMBLY. P/N 600-24043-1. C-CHECK RO 1/16/2021. INSTALLED NEW HINGE FITTING ASSEMBLY P/N 600-24043-1 ON LT ELEVATOR, REF CRJ200 SRM 51-42-06, SRM
- [SDR SWIA202055432](https://openairdocs.org/sdr/SWIA202055432.md): Splice Angle · cracked · Nov 27, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CRACK ON INBOARD SPLICE ANGLE AT STR 3L JUST AFT OF FS 280. C-CHECK RO 1/16/2021. REPLACED SPLICE ANGLE AT STR 3L AT FS 280, REF CRJ-200-SRM 51-42-06 AND DWG PL 600-31057 REV P. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202055486](https://openairdocs.org/sdr/SWIA202055486.md): Skin · dented · Nov 25, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL SKIN BETWEEN FS 349.00-333.00 AT STGR 26R. C-CHECK RO 1/16/2021. REPAIRED FUSELAGE EXTERNAL SKIN BETWEEN FS 349.00-333.00, AT STGR 26R, REF REO 601R-53-21-3373 REV- DATED 2020-12-14 AND REO 601R-51-00-309 REV -A DATED 2017-08-23. LEAK CHEC
- [SDR SWIA202055431](https://openairdocs.org/sdr/SWIA202055431.md): Skin · dented · Nov 25, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL SKIN BETWEEN FS 310.00-310.00, STGR 25R-24R. C-CHECK RO 1/16/2021. REPAIRED EXTERNAL SKIN BETWEEN FS 310.00-310.00, STGR 25R-24R, REF REO 601R-53-21-3367 REV - DATED 2020-12-10. COMPLIED WITH 51-900-1003-SKY. SEE CONTIUATION CARD FOR DETAI
- [SDR SWIA202055430](https://openairdocs.org/sdr/SWIA202055430.md): Skin · scratched · Nov 25, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SCRATCH ON EXTERNAL SKIN BELOW FWD POTABLE WATER SERVICING PORT CUTOUT BETWEEN FS 349.00-364.00, 20R-19R. C-CHECK RO 1/16/2021. BLENDED SCRATCH ON EXTERNAL SKIN BELOW FWD POTABLE WATER SERVICING PORT CUTOUT BETWEEN FS 349.00-364.0 12R-19R, REF CRJ-200-SRM 51
- [SDR SWIA202055429](https://openairdocs.org/sdr/SWIA202055429.md): Intercostal · corroded · Nov 25, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON AVIONICS BAY CUTOUT INTERCOSTAL LOWER FLANGE BETWEEN 26 L AND 27 L FROM FS 394.00 TO FS 409.00. C-CHECK RO 1/16/2021. BLENDED CORROSION FROM AVIONICS BAY CUTOUT INTERCOSTAL LOWER FLANGE BETWEEN 26 L AND 27 L FROM FS 394.00 TO FS 409.00, RE
- [SDR SWIA202055481](https://openairdocs.org/sdr/SWIA202055481.md): Retainer · worn · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 3 EA FAIRING 193AB RETAINERS ARE WORN BEYOND PERMISSIBLE DIMENSIONS, RETAINERS ARE ATTACHED TO FUSELAGE SIDE, FLAGGED. C-CHECK RO 1/16/2021. REMOVED WORN RETAINERS AND INSTALLED 3 EA NEW RETAINERS WITH NEW NUTPLATES (P/N: 601R31036-10, 601R31036-11, 601R3103
- [SDR SWIA202055470](https://openairdocs.org/sdr/SWIA202055470.md): Floor Support · corroded · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM CAP HAS CORROSION AT MULTIPLE AREAS ON THE INBOARD FLANGE RBL 9, FS 559.00+11-FS 569.00, MARKED. C-CHECK RO 1/16/2021. REMOVED CORROSION ON FLOOR BEAM CAP IN MULTIPLE AREAS ON INBOARD FLANGE RBL 9 FS 559.00+11-FS 569.00, REF CRJ200 SRM 51-21-06.
- [SDR SWIA202055469](https://openairdocs.org/sdr/SWIA202055469.md): Strap · corroded · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR STRAP CORRODED RBL 29-RBL 43 FS 559.00, MARKED. C-CHECK RO 1/16/2021. REMOVED CORROSION ON 3 EA AREAS STRAP FLOOR RBL 29-RBL 43, FS 559.00, REF CRJ200 SRM 51-21-06 ORIGINAL MATERIAL THICKNESS IS.050", LOWEST REMAINING THICKNESS IS.043", MATERIAL RE
- [SDR SWIA202055468](https://openairdocs.org/sdr/SWIA202055468.md): Seat Track · corroded · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL HAS MULTIPLE AREAS OF CORROSION FS 409.00+4-FS 409.00+126 LBL 9, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED SEAT RAIL FS 409.00+4-FS 409.00+126 LBL 9, REF CRJ-200 AMM 53-01-11-400-802 AND REO 601R-53-00-485 REV D DATED 2018-01-29 AND CRJ-20
- [SDR SWIA202055467](https://openairdocs.org/sdr/SWIA202055467.md): Seat Track · corroded · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION AT FORWARD END, LBL 9 FS 364.00-FS 398.00, MARKED. C-CHECK RO 1/16/2021. REMOVED OUT OF LIMITS SEAT TRACK, FABRICATE NEW LBL SEAT RAIL P/N 601R31032 FROM FS 364.00 TO FS 398.00 USING EXTRUSION 20276-288-0-0A, PO T55899, REF REO 601R-
- [SDR SWIA202055466](https://openairdocs.org/sdr/SWIA202055466.md): Seat Track · corroded · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS CORROSION AT MULTIPLE AREAS, RBL 9 FS 364.00-FS 398.00, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CORRODED SEAT RAIL WITH NEW SEAT RAIL AT RBL 9, BETWEEN FS 364.00 TO FS 398.00, REF CRJ-200 SRM 51-21-06, CRJ-200 SRM 53-21-19, REO 601R
- [SDR SWIA202055428](https://openairdocs.org/sdr/SWIA202055428.md): Floorbeam · corroded · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM CAP HAS CORROSION AT MULTIPLE AREAS ON THE INBOARD FLANGE LBL 9, FS 559.00+11-FS 569.00, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FLOOR BEAM AT FS 559+11 TO FS 569 AT LBL 9, REF REO 601R-53-51-540 REV - DATED 2020-12-18, DWG 601R31032 RE
- [SDR SWIA202055427](https://openairdocs.org/sdr/SWIA202055427.md): Floorbeam · corroded · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM CAP HAS CORROSION AT MULTIPLE AREAS ON THE OUTBOARD FLANGE RBL 9, FS 559.00+32-FS 559.00+112, MARKED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW FLOOR BEAM CAP AT RBL 9, FS 559.00+32-FS 559.00+112, REF CRJ-200-SRM 51-42-34,CRJ-200 SRM 51-42-2
- [SDR SWIA202055426](https://openairdocs.org/sdr/SWIA202055426.md): Floor Support · corroded · Nov 24, 2020 · N868AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL CORRODED AT MULTIPLE LOCATIONS, FS 559.00+85-FS 559.00+116, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT FLOOR SILL P/N 601R31133-102S, REF CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31026 REV F. COMPLIED WITH 51-9

Next page: https://openairdocs.org/deregistered/N868AS-2023-10-02/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 = 'N868AS' AND deregistration_id = 'N868AS-2023-10-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N868AS-2023-10-02/reports

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