# Service difficulty reports: N863AS, cancelled Jan 25, 2023

A list on [N863AS, cancelled Jan 25, 2023](https://openairdocs.org/deregistered/N863AS-2023-01-25.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 · 168 reports

- [SDR SWIA202265531](https://openairdocs.org/sdr/SWIA202265531.md): None · delaminated · Apr 24, 2022 · N863AS · Cndair CL6002B19 · Window/Windshield System
  > RH WINDOW DELAMINATION ON EDGE WITH VERTICAL LENGTH OF 8" AND HORIZONTAL LENGTH OF 4". (FLIGHT 5848 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24721877 WITH THE FOLLOWING CORRECTIVE ACTION: " REPLACED RH SIDE WINDOW IN REFERENCE TO CRJ2
- [SDR SWIA202052767](https://openairdocs.org/sdr/SWIA202052767.md): Heat Shield · cracked · Sep 23, 2020 · N863AS · Cndair CL6002B19 · APU Exhaust System
  > APU HEAT SHIELD HAS A CRACK AT THE 6 O' POSITION. FILED CLOSED (9/23/2020). REMOVED AND REPLACED APU EXHAUST HEAT SHIELD, IN REF TO CRJ200 AMM.
- [SDR SWIA2020071451337](https://openairdocs.org/sdr/SWIA2020071451337.md): Seat Track · corroded · Jun 26, 2020 · N863AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK AT RBL9 FROM FS559.00+3-FS559.00+85 IS CORRODED. (C-CHECK) RO 7/10/2020 REMOVED CORROSION ON CABIN FLOOR SEAT TRACK AT RBL9 FROM FS559.00+3-FS559.00+85. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW SEAT TRACK P/N 601R31032-9. SEAT TRA
- [SDR SWIA2020071451322](https://openairdocs.org/sdr/SWIA2020071451322.md): Strap · corroded · Jun 18, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION FOUND ON STRAP AT FS 333, BETWEEN STR 25L AND 26L. (C-CHECK) RO 7/10/2020 REPAIRED DAMAGED AREA PER REO. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA2020071451321](https://openairdocs.org/sdr/SWIA2020071451321.md): Skin · dented · Jun 18, 2020 · N863AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BETWEEN FS589-FS605, STR 21L-22L IS DENTED. (C-CHECK) RO 7/10/2020 DRESSED OUT DENT ON FUSELAGE SKIN BETWEEN FS589-FS605, STR 21L-22L REF REO. EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO FASTENER PROXIMITY REF SRM. SUBMITTED TO ENGINEERING
- [SDR SWIA2020071451320](https://openairdocs.org/sdr/SWIA2020071451320.md): Skin · dented · Jun 18, 2020 · N863AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BETWEEN FS700-FS718, STR 14L-15L IS DENTED. (C-CHECK) RO 7/10/2020 HAND DRESSED DENTS (2EA) ON THE FUSELAGE SKIN BETWEEN FS700-FS718, STR 14L-15L REF REO. AFT DENT FOUND TO BE WITHIN LIMITS. FWD DENT FOUND TO BE OUT OF LIMITS REF SRM. SUBMITT
- [SDR SWIA2020071451319](https://openairdocs.org/sdr/SWIA2020071451319.md): Skin · dented · Jun 18, 2020 · N863AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BETWEEN FS589-FS605, STR 24R-26R IS DENTED. (C-CHECK) RO 7/10/2020 HAND DRESSED DENTS (3EA) LOCATED AT FUSELAGE SKIN BETWEEN FS589-FS605, STR 24R-26R REO. ALL THREE DENTS FOUND TO BE OUT OF LIMITS DUE TO DENTS IN ADJACENT PANELS IN THE CIRCUMFE
- [SDR SWIA2020071451318](https://openairdocs.org/sdr/SWIA2020071451318.md): Frame · chafed · Jun 15, 2020 · N863AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS654.5 IS CHAFED THROUGH JUST FORWARD OF THE APU EXHAUST PORT. (C-CHECK) RO 7/10/2020 REPAIRED FRAME AT FS654.5 JUST FORWARD OF THE APU EXHAUST PORT REF REO. SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA2020071451336](https://openairdocs.org/sdr/SWIA2020071451336.md): Seat Track · corroded · Jun 14, 2020 · N863AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT FS 559+80 - FS 574.0 RBL 9 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED CARGO TIE DOWN TRACKS AT FS559.00+80 - FS574.00 RBL 9 DUE TO CORROSION FOUND TO BE OUT OF LIMITS REF AMM.
- [SDR SWIA2020071451335](https://openairdocs.org/sdr/SWIA2020071451335.md): Seat Track · corroded · Jun 14, 2020 · N863AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SMALL PIECE OF SEAT TRACK AT FS 559+112-FS 574.0 LBL 27 HAS CORROSION. (C-CHECK) RO 7/10/2020 FABRICATED NEW SEAT TRACK USING N126-2075, PO TX3728 PER REO.
- [SDR SWIA2020071451317](https://openairdocs.org/sdr/SWIA2020071451317.md): Seat Track · corroded · Jun 14, 2020 · N863AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CAP RBL 27 AT FS 559+112 TO JUST AFT OF FS 559.0 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED SEAT TRACK CAP AT RBL27 FROM FS559.00-FS559.00+112. COMPLIED WITH ALL STEPS OF THE REPAIR. REF REO AND DRAWING. COMPLIED WITH CARD.
- [SDR SWIA2020071451316](https://openairdocs.org/sdr/SWIA2020071451316.md): Seat Track · corroded · Jun 14, 2020 · N863AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SUPPORT CAP RBL 9 JUST FWD OF FS 574.0 TO FS 621.0 HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVE CORROSION FROM SEAT TRACK SUPPORT CAP ON RBL 9 FWD OF FS 574 - FS 621.0 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REO. INSTALLED NEW REPLACEMENT
- [SDR SWIA2020071451315](https://openairdocs.org/sdr/SWIA2020071451315.md): Seat Track · corroded · Jun 14, 2020 · N863AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SUPPORT CAP FROM FS 559.0 TO FS 574.0 RBL 9 HAS CORROSION. (C-CHECK) RO 7/10/2020. REMOVED AND REPLACED SEAT TRACK SUPPORT CAP FROM FS559.00 TO FS574.00 RBL 9. COMPLIED WITH ALL STEPS OF THE REPAIR. REF REO AND DRAWING. COMPLIED WITH TASK CARD.
- [SDR SWIA2020071451314](https://openairdocs.org/sdr/SWIA2020071451314.md): Door Sill · corroded · Jun 13, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LEFT HAND FLOOR SILL AT FS 349. (C-CHECK) RO 7/10/2020 REPAIRED LT FLOOR SILL AT FS 349 REF REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020071451313](https://openairdocs.org/sdr/SWIA2020071451313.md): Panel · corroded · Jun 12, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT PRESSURE FLOOR SILL PANEL HAS SEVERAL AREA OF CORROSION BETWEEN FS 499 AND FS 559. (C-CHECK) RO 7/10/2020 REPAIRED THE RT PRESSURE FLOOR SILL PANEL BETWEEN FS 499 AND FS 559 REF REO. REFERENCE THE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020071451312](https://openairdocs.org/sdr/SWIA2020071451312.md): Strap · corroded · Jun 12, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRAP AT FS 559 HAS CORROSION BETWEEN APPROXIMATE LBL33 AND LBL44. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM. NDT MEASURED THICKNESS AND FOUND PART TO BE OUT OF LIMITS, SEE CONTINUATION FOR DETAILS. REMOVED AND REPLACED FLOOR STRAP, 601R3125, AND HA
- [SDR SWIA2020071451311](https://openairdocs.org/sdr/SWIA2020071451311.md): Panel · corroded · Jun 12, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL PANEL HAS SEVERAL AREA OF CORROSION BETWEEN FS 409+112 AND FS 559. (C-CHECK) RO 7/10/2020 REPAIRED THE LT PRESSURE FLOOR SILL PANEL BETWEEN FS 409.00+112 AND FS 559.00. REF REO REFERENCE THE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020071451310](https://openairdocs.org/sdr/SWIA2020071451310.md): Intercostal · corroded · Jun 12, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > THE PAX DOOR INTERCOSTAL DD5 AFT HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL AFT DD5 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR INTERCOSTAL DD5 AFT REF
- [SDR SWIA2020071451309](https://openairdocs.org/sdr/SWIA2020071451309.md): Hinge Bracket · chafed · Jun 11, 2020 · N863AS · Cndair CL6002B19 · Rudder Structure
  > RUDDER LOWER CENTER HINGE BRACKET ON VERTICAL STABILIZER IS CHAFED ON TOP SURFACE JUST FORWARD OF THE SPHERICAL BEARING. (C-CHECK) RO 7/10/2020 BLENDED CHAFE ON RUDDER LOWER CENTER HINGE BRACKET TOP SURFACE TO A SMOOTH CONTOUR (20:1 TRANSITION). REF SRM. BLE
- [SDR SWIA2020071451308](https://openairdocs.org/sdr/SWIA2020071451308.md): Hinge Bracket · chafed · Jun 11, 2020 · N863AS · Cndair CL6002B19 · Rudder Structure
  > RUDDER UPPER CENTER HINGE BRACKET ON VERTICAL STABILIZER IS CHAFED ON TOP SURFACE JUST FORWARD OF THE SPHERICAL BEARING. (C-CHECK) RO 7/10/2020 BLENDED CHAFE ON UPPER HINGE BRACKET TOP SURFACE TO A SMOOTH CONTOUR (20:1 TRANSITION). REF SRM. BLEND MEASURES.
- [SDR SWIA2020071451307](https://openairdocs.org/sdr/SWIA2020071451307.md): Retainer · corroded · Jun 10, 2020 · N863AS · Cndair CL6002B19 · Service Doors
  > UPON PROVIDED ACCES TO TREATMANT OF CORROSION DAMAGE ON SERVICE DOOR SEAL LWR AFT CORNER RETAINER FOUND CORROSION DAMAGE AT DOOR FRAME LWR AFT PAN SECTION. (C-CHECK) RO 7/10/2020 REMOVED CORROSION DAMAGE FROM SERVICE DOOR LWR AFT FRAME PAN SECTION REF SRM. O
- [SDR SWIA2020071451306](https://openairdocs.org/sdr/SWIA2020071451306.md): Fitting · cracked · Jun 10, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT STR14R, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW CLIP AT STGR 14R BETWEEN FS621 AND FS625 REF SRM AND REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020071451305](https://openairdocs.org/sdr/SWIA2020071451305.md): Fitting · cracked · Jun 10, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP AT STR14L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW CLIP AT STGR 14L BETWEEN FS621 AND FS625 REF CSRM AND REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020071451304](https://openairdocs.org/sdr/SWIA2020071451304.md): Intercostal · cracked · Jun 10, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL / CLIP COMMON TO THE SKIN AT STR14L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED CLIP/INTERCOSTAL COMMON TO THE OUTER SKIN AT STR 14L BETWEEN FS 621 AND 625 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020071451325](https://openairdocs.org/sdr/SWIA2020071451325.md): Stop Fitting · cracked · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR PULL-IN LEVER TORQUE TUBE STOP FITTING CORRODED AND APPEARS CRACKED. (C-CHECK) RO 7/10/2020 REPLACED PASSENGER DOOR LOWER TORQUE TUBE STOP FITTING P/N 601R38923-3 AND RELATED HARDWARE, REF AMM, PERFORMED OPERATIONAL TEST OF THE PASSENGER DOOR,
- [SDR SWIA2020071451324](https://openairdocs.org/sdr/SWIA2020071451324.md): Bracket · cracked · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR SUPPORT WHEEL SYSTEM CABLE BRACKET AT BOTTOM OF STAIRS APPEARS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED CRACKED SUPPORT WHEEL CABLE BRACKET ASSY ON AFT SIDE OF BOTTOM STEP AND INSTALLED NEW BRACKET ASSY P/N 601R317186-1 REF SRM.
- [SDR SWIA2020071451323](https://openairdocs.org/sdr/SWIA2020071451323.md): Drag Angle · cracked · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR SUSPECT CRACK AT THE AFT STAIR DRAG ANGLE. (C-CHECK) RO 7/10/2020 REPLACED THE CRACKED AFT STAIR DRAG ANGLE REF SRM.
- [SDR SWIA2020071451303](https://openairdocs.org/sdr/SWIA2020071451303.md): Intercostal · cracked · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP COMMON TO THE SKIN AT STR13L, FS621-FS625, IS CRACKED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED CLIP/INTERCOSTAL COMMON TO THE OUTER SKIN AT STR13L BETWEEN FS621 AND 625 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020071451302](https://openairdocs.org/sdr/SWIA2020071451302.md): Former · corroded · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORMER AT FS329.50 BETWEEN DD5 AND DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR FORMER AT FS329.50 BETWEEN INTERCOSTAL DD5 AND DD6 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. WET INSTALLED AND FILL
- [SDR SWIA2020071451301](https://openairdocs.org/sdr/SWIA2020071451301.md): Intercostal · corroded · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR MIDDLE INTERCOSTAL AT DD2 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD2 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR MID INTERCOSTAL DD2 REF S
- [SDR SWIA2020071451300](https://openairdocs.org/sdr/SWIA2020071451300.md): Intercostal · corroded · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR MIDDLE INTERCOSTAL AT DD3 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD3 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMTS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR MID INTERCOSTAL DD3 RE
- [SDR SWIA2020071451299](https://openairdocs.org/sdr/SWIA2020071451299.md): Intercostal · corroded · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR MIDDLE INTERCOSTAL AT DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL MID DD4 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR MID INTERCOSTAL DD4 R
- [SDR SWIA2020071451298](https://openairdocs.org/sdr/SWIA2020071451298.md): Intercostal · corroded · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT INTERCOSTAL AT DD4 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED THE CORROSION FROM THE PAX DOOR INTERCOSTAL AFT DD4 REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. WET INSTALLED AND FILLET SEALED THE PAX DOOR AFT INTERCOSTAL DD4 REF
- [SDR SWIA2020071451297](https://openairdocs.org/sdr/SWIA2020071451297.md): Intercostal · corroded · Jun 9, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR CLIP FOR FWD INTERCOSTAL AT DD6, AND AT APPROX FS320 CORRODED. (C-CHECK) RO 7/10/2020 REMOVED AND INSTALLED NEW PAX DOOR CLIP / CLEAT COMMON TO INTERCOSTAL FWD DD6 AT APPROX FS320 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020071451334](https://openairdocs.org/sdr/SWIA2020071451334.md): Skin · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN IS CORRODED AT APPROX FS559+96-559+112, STR26L-26R. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM 51-21-06. FOUND TO BE OUT OF LIMITS. NO ALLOWABLE DAMAGE IN DISCREPANT AREA. SUBMITTED TO ENGINEERING AND RECIEVED DISPOSITION OF REO. COMP
- [SDR SWIA2020071451333](https://openairdocs.org/sdr/SWIA2020071451333.md): Skin · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN IS CORRODED AT APPROX FS559+44, STR25L-25R. (C-CHECK) RO 7/10/2020 BLENDED CORROSION ON EXTERNAL SKIN AT FS 559+44 BETWEEN STR 25L-25R REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. REPAIRED EXTERNAL SKIN AT FS 559+44 BETWEEN STR 25L
- [SDR SWIA2020071451332](https://openairdocs.org/sdr/SWIA2020071451332.md): Fastener · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Spoilers
  > RT INBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED THE RT INBD GROUND SPOILER ACTUATOR LINK HARDWARE REF AMM. ALL CHECKS GOOD.
- [SDR SWIA2020071451331](https://openairdocs.org/sdr/SWIA2020071451331.md): Fastener · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Spoilers
  > RT OUTBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED RT OTBD GROUND SPOILER LINK HARDWARE REF AMM. ALL CHECKS GOOD.
- [SDR SWIA2020071451330](https://openairdocs.org/sdr/SWIA2020071451330.md): Fastener · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Spoilers
  > LT INBOARD GROUND SPOILER ACTUATOR LINK HAS CORRODED HARDWARE. (C-CHECK) RO 7/10/2020 REMOVED AND REPLACED LT I/B GROUND SPOILER ACTUATOR LINK HARDWARE IAW AMM. OPS CHECK GOOD.
- [SDR SWIA2020071451329](https://openairdocs.org/sdr/SWIA2020071451329.md): Floor Support · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SURROUND STRUCTURE: UPPER FLOOR SUPPORT ANGLE HAS CORROSION. (C-CHECK) RO 7/10/2020 REMOVED 2 EACH SOLID FASTENERS WITH CORROSION AT THE SERVICE DOOR SURROUND STRUCTURE UPPER FLOOR SUPPORT ANGLE REFERENCE SRM, INSTALLED NEW SOLID FASTENERS AND AP
- [SDR SWIA2020071451327](https://openairdocs.org/sdr/SWIA2020071451327.md): Plate · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR SURROUND STRUCTURE: AFT ANCHOR, SERRATED MOUNTING PLATE HAS CORROSION ON ITS OUTBOARD SIDE. (C-CHECK) RO 7/10/2020 REMOVED DAMAGED SERRATED MOUNTING PLATE FROM PASSENGER DOOR AFT ANCHOR FITTING AND INSTALLED NEW P/N 600-3801-6 REF AMM, PERFORME
- [SDR SWIA2020071451296](https://openairdocs.org/sdr/SWIA2020071451296.md): Skin · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN IS CORRODED AT APPROX FS559+34, STR26L. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM 51-21-06. FOUND REMAINING MATERIAL TO BE OUT OF LIMITS, REF SRM. SUBMITTED TO ENGINEERING, WHO APPROVED A DISPOSTION FOR BLENDED CORROSION DAMAGE TO FUSE
- [SDR SWIA2020071451295](https://openairdocs.org/sdr/SWIA2020071451295.md): Floor Support · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE: LOWER FLOOR SUPPORT ANGLE HAS CORROSION AROUND FASTENERS. (C-CHECK) RO 7/10/2020 REMOVED CORROSION FROM PAX DOOR FLOOR SUPPORT LWR ANGLE FLANGE (NEXT TO DOOR AFT HAND RAIL LINK MOUNTING BRACKET) PER SRM. ORIGINAL THICKNESS=
- [SDR SWIA2020071451294](https://openairdocs.org/sdr/SWIA2020071451294.md): Retainer · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR: LOWER SEAL RETAINER IS CORRODED. (C-CHECK) RO 7/10/2020 REMOVED CORROSION DAMAGE FROM SERVICE DOOR SILL LWR AFT CORNER RETAINER REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMTS REF SRM. INSTALLED NEW SVC DOOR SILL LWR AFT RETAINER ANGLE P/N 6041
- [SDR SWIA2020071451293](https://openairdocs.org/sdr/SWIA2020071451293.md): Angle · corroded · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR INTERNAL STRUCTURE: CLIP INSIDE LIGHTENING CUT-OUT JUST AFT OF THE INNER HANDLE ACCESS AREA HAS CORROSION. (C-CHECK) RO 7/10/2020 BLENDED CORROSION, REF SRM. FOUND TO BE OUT OF LIMITS. FABRICATED AND REPLACED ANGLE CLIP, P/N: 601R38304-49 REF D
- [SDR SWIA2020071451292](https://openairdocs.org/sdr/SWIA2020071451292.md): Skin · gouged · Jun 8, 2020 · N863AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL STRUCTURE: HAS LIGHT GOUGING, AND SOME CORROSION, ON THE RIVET TAILS AND STRUCTURE BELOW THE HANDLE MECHANISM. (C-CHECK) RO 7/10/2020 ORDER AND RECEIVED NEW CARGO DOOR DUE TO INNER SKIN BEING OUT OF LIMITS SEE 21093161 JOB 2748791 OP 184 F
- [SDR SWIA2020071451291](https://openairdocs.org/sdr/SWIA2020071451291.md): Skin · dented · Jun 7, 2020 · N863AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING, LOWER WING PLANK, INBD OF WS50 AND FORWARD OF THE WING TANK ACCESS HOLES, APPEARS TO BE DENTED. (C-CHECK) RO 7/10/2020 REPAIRED LT LOWER WING PLANK INBOARD OF WS50 AND FORWARD OF THE WING TANK ACCESS HOLE REF MHIRJ REO. SEE CONTINUATION CARD FOR
- [SDR SWIA2019050145817](https://openairdocs.org/sdr/SWIA2019050145817.md): Uplock Roller · failed · May 1, 2019 · N863AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE NOSE GEAR DID NOT GO DOWN. CYCLED GEAR HANDLE PER QRH AND ALL GEAR DOWN AND LOCKED. (FLT#5529) FO: 05/01/2019 CLOSED REMOVED AND REPLACED NLG UPLOCK ROLLER AND BRACKET WITH SERVICEABLE UNITS IAW AMM. OPS CHECK GOOD AT THIS TIME. PERFORMED FULL ST
- [SDR SWIA2019050145818](https://openairdocs.org/sdr/SWIA2019050145818.md): Uplock Roller · slow · May 1, 2019 · N863AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > EXTENDED GEAR AT 180 KTS, RECEIVED GEAR DISAGREE WARNING MESSAGE. AFTER ABOUT 20 SECONDS, THE GEAR INDICATED DOWN BEFORE WE COULD EVEN START THE QRH PROCEDURE. (FLT#5574) CLOSED REMOVED AND REPLACED NLG UPLOCK ROLLER AND BRACKET WITH SERVICEABLE UNITS. OPS CHE
- [SDR SWIA2019040545663](https://openairdocs.org/sdr/SWIA2019040545663.md): Line · leaking · Mar 23, 2019 · N863AS · Cndair CL6002B19 · Turbine Engine Oil System
  > ENGINE TWO LOW OIL PRESSURE IN FLIGHT. ENGINE SHUT DOWN IN FLIGHT ACCOMPLISHED. (FLT#5223) REMOVED AND REPLACED OIL SUPPLY LINE IAW AMM. NO LEAKS NOTED AFTER ENGINE RUNS.

Next page: https://openairdocs.org/deregistered/N863AS-2023-01-25/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 = 'N863AS' AND deregistration_id = 'N863AS-2023-01-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N863AS-2023-01-25/reports

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