# Service difficulty reports: N873AS

A list on [N873AS](https://openairdocs.org/aircraft/N873AS.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 · 207 reports

- [SDR SWIA20241101029](https://openairdocs.org/sdr/SWIA20241101029.md): Attach Angle · cracked · Oct 29, 2024 · N873AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAXS DOOR ATTACH ANGLE CRACKED AT RIVET HOLE JUST AFT OF THE DOOR CABLE PULLEY (FILED CLOSED) PER REO 601R-52-11-513, REV -C, DATE: 2020-10-22 REPAIRED PAX DOOR STAIRS AFT DRAG ANGLE. COMPLETED TASK CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR. SEE CP
- [SDR SWIA2024080500002](https://openairdocs.org/sdr/SWIA2024080500002.md): Windshield · cracked · Aug 2, 2024 · N873AS · Cndair CL6002B19 · Flight Compartment Windows
  > FO WINDSHIELD BEGAN DELAMINATING RAN THE QRH AND AFTER TURNING OFF THE WINDSHIELD HEAT THE OUTER PANE SPIDER WEB CRACKED. (FLIGHT 4764 - FILE CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28634584 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLA
- [SDR SWIA2024062600006](https://openairdocs.org/sdr/SWIA2024062600006.md): Angle · cracked · Jun 6, 2024 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE IN LINE WITH STRINGER 10R BETWEEN FS625.30 AND 640.00 HAS APPROX 1.5" CRACK STARTING FROM AFT EDGE GOING FORWARD ON FUSELAGE SKIN FLAT SIDE AND APPROX. CENTERLINE OF FLAT. (FILED CLOSED) REMOVED AND REPLACED ANGLE IN LINE WITH STRINGER 10R BETWEEN FS
- [SDR SWIA2024062600604](https://openairdocs.org/sdr/SWIA2024062600604.md): Access Panel · failed · Jun 4, 2024 · N873AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING FUEL TANK ACCESS HOLE #7 (WS116.366) HAS 5 AREAS (MARKED) THAT HAVE EDDY CURRENT INDICATION GREATER THAN 50%. (FILED CLOSED) BLENDED 5 AREAS ON RH WING FUEL TANK ACCESS HOLE #7 (WS116.366) PANEL LANDING, IN REF. TO REO 601R-57-21-030, REV. L, DATED
- [SDR SWIA202406260531](https://openairdocs.org/sdr/SWIA202406260531.md): Pressure Blkhd · cracked · May 31, 2024 · N873AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R, INTERCOSTAL CRACKED. (FILED CLOSED) REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH
- [SDR SWIA2024062600529](https://openairdocs.org/sdr/SWIA2024062600529.md): Nut Plate · corroded · May 29, 2024 · N873AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORROSION AROUND 2 NUTPLATES ON RH PRESSURE FLOOR SILL AT FS 449.85 (FILED CLOSED) BLENDED AND TREATED CORROSION AROUND NUTPLATE ON RH PRESSURE FLOOR SILL AT FS 449.85 IN REF TO REO 601R-53-41-666, REV C. DATED 2012-11-06. REMOVED AND REPLACED AFFECTED NU
- [SDR SWI20240626000551](https://openairdocs.org/sdr/SWI20240626000551.md): Pressure Blkhd · cracked · May 29, 2024 · N873AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK FOUND ON FWD FACE OF THE FWD PRESSURE BULHEAD. EXTENDING IN TWO DIRECTIONS FROM A RIVET HOLE LOCATED 14.75 INCHES LEFT OF BL 0.0 AND 9.00 INCHES UP FROM WL 79.50 (FILED CLOSED) REPAIRED CRACK FOUND ON FWD FACE OF THE FWD PRESSURE BULHEAD. EXTENDING
- [SDR SWIA2022122967053](https://openairdocs.org/sdr/SWIA2022122967053.md): Panel · cracked · Dec 28, 2022 · N873AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RH FLAP CANOE PANEL 692BB BRACKET AFFIXED TO THE HINGE ARM IS CRACKED. (FILED CLOSED) INSTALLED NEW RH FLAP CANOE PANEL 692BB HINGE ARM BRACKET IN REF TO CRJ-200 SRM 51-42-10.
- [SDR SWIA2022122967052](https://openairdocs.org/sdr/SWIA2022122967052.md): Panel · cracked · Dec 28, 2022 · N873AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RH FLAP CANOE PANEL 692BB IS CRACKED ON THE FWD LEADING EDGE. (FILED CLOSED) REMOVED AND REPLACED RH FLAP FAIRING 692BB IN REFERENCE TO CRJ 200 AMM 57-55-03
- [SDR SWIA202266621](https://openairdocs.org/sdr/SWIA202266621.md): None · warning message · Oct 21, 2022 · N873AS · Cndair CL6002B19 · Auto Flight System
  > MACH TRIM AND STAB TRIM CAUTION MESSAGES ON TAKEOFF. WOULD NOT RE-ENGAGE NORMALLY. SELECTED STAB TRIM DISCONNECT BUTTON. BOTH TRIMS ENGAGED AFTERWARDS. (FLIGHT #4312 FILED CLOSED) COMPLIED WITH FAULT ISOLATION PROCEDURE FOR STAB TRIM MACH TRIM CAUTION MESS
- [SDR SWIA202265164](https://openairdocs.org/sdr/SWIA202265164.md): None · smoke · Mar 25, 2022 · N873AS · Cndair CL6002B19 · Fire Protection System
  > RECEIVED SMOKE CARGO WARNING AND SMOKE TOILET CAUTION MESSAGE AT AROUND 10,000. RAN QRH INCLUDING DISCHARGING BOTH CARGO FIRE BOTTLES. WITNESSED WHITE SMOKE IN CABIN AND ON FLIGHT DECK. (FLIGHT 4300 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP
- [SDR SWIA202157914](https://openairdocs.org/sdr/SWIA202157914.md): Hinge Box · corroded · Apr 5, 2021 · N873AS · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H WING, OUTBD FLAP, OUTBD FLAP HINGE BOX, HAS CORRODE HARDWARE ON BUTE DOOR COMPRESSION SPRING AND BOLTS AT SAFETY PLATES 6 PLACES (MARKED) (C-CHECK RO 4/25/2021) REMOVED AND REPLACED WITH NEW R/H WING, OUTBD FLAP, OUTBD FLAP HINGE BOX, HARDWARE ON
- [SDR SWIA202157891](https://openairdocs.org/sdr/SWIA202157891.md): Bracket · cracked · Mar 29, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FRONT TENSIONER BRACKET LOCATED AT FS.621.00 BULKHEAD FOUND CRACKED. (C-CHECK RO 4/25/2021) REPLACED CARGO DOOR FRONT TENSIONER BRACKET LOCATED AT FS621.00 BULKHEAD REF. DWG 601R35055 REV-M AND CRJ200 SRM 51-42-06. LEAK CHECK GOOD. COMPLIED
- [SDR SWIA202157913](https://openairdocs.org/sdr/SWIA202157913.md): Attach Fitting · corroded · Mar 22, 2021 · N873AS · Cndair CL6002B19 · Trailing Edge Flaps
  > * R/H FORWARD FLAP HINGE BOX ATTACH LUG ON WING AT WS178.00 HAS 2 CORRODED BOLTS, MARKED. (C-CHECK RO 4/25/2021) REPLACED CORRODED HARDWARE AT RH FWD FLAP HINGE BOX ATTACH LUG ON WING AT WS178.00 REF. CRJ200 AMM 57-21-37-400-801. LEAK CHECK GOOD
- [SDR SWIA202157912](https://openairdocs.org/sdr/SWIA202157912.md): Attach Fitting · corroded · Mar 22, 2021 · N873AS · Cndair CL6002B19 · Trailing Edge Flaps
  > * R/H FORWARD FLAP HINGE BOX ATTACH LUG ON WING AT WS220.00 HAS 2 CORRODED BOLTS, MARKED. (C-CHECK RO 4/25/2021) REPLACED CORRODED HARDWARE AT RH FWD FLAP HINGE BOX ATTACH LUG ON WING AT WS220.00 REF. CRJ200 AMM 57-21-37-400-802. LEAK CHECK GOOD
- [SDR SWIA202157911](https://openairdocs.org/sdr/SWIA202157911.md): Attach Fitting · corroded · Mar 22, 2021 · N873AS · Cndair CL6002B19 · Trailing Edge Flaps
  > * R/H FORWARD FLAP HINGE BOX ATTACH LUG ON WING AT WS264.00 HAS A CORRODED BOLT, MARKED. (C-CHECK RO 4/25/2021) REPLACED CORRODED HARDWARE AT RH FWD FLAP HINGE BOX ATTACH LUG ON WING AT WS264.00 REF. CRJ200 AMM 57-21-37-400-803. LEAK CHECK GOOD
- [SDR SWIA202157910](https://openairdocs.org/sdr/SWIA202157910.md): Attach Fitting · corroded · Mar 22, 2021 · N873AS · Cndair CL6002B19 · Trailing Edge Flaps
  > * L/H FORWARD FLAP HINGE BOX ATTACH LUG ON WING AT WS264.00 HAS A CORRODED BOLT, MARKED. (C-CHECK RO 4/25/2021) REPLACED CORRODED HARDWARE AT LH FWD FLAP HINGE BOX ATTACH LUG ON WING AT WS264.00 REF. CRJ200 AMM 20-21-00-910-801. LEAK CHECK GOOD
- [SDR SWIA202157909](https://openairdocs.org/sdr/SWIA202157909.md): Hinge Arm · corroded · Mar 21, 2021 · N873AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBD FLAP HIMNGE ARMS HAVE CORRODED HARDWARE (C-CHECK RO 4/25/2021) ORDERED AND RECIEVED NEW FROM STOCK 1 BUSHING, 1 BOLT, 6EA NUTS AND 6EA COTTER PINS. INSTALLATION OF NEW HARDWARE ACCOMPLISHED ON JOB 2754965 OP 5913 MX TRANS #21982154.
- [SDR SWIA202157890](https://openairdocs.org/sdr/SWIA202157890.md): Shear Tie · damaged · Mar 18, 2021 · N873AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLANGE REPAIR ANGLE COMMON TO FRAME FS.589 AND SKIN BETWEEN STGR 25L & STGR 26L REMOVED TO FOM ON CAMP 22452578 JOB 2754961 OP 222 HAS SHORT ED ON 1EA FASTENER HOLE ON LOWER FLANGE (C-CHECK RO 4/25/2021) FABRICATED AND INSTALLED REPAIR ANGLE ON FS589.0
- [SDR SWIA202157908](https://openairdocs.org/sdr/SWIA202157908.md): Angle · corroded · Mar 15, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE PN 600-32004-113 @ FS 333 BETWEEN ST 25L AND ST 25R FOUND CORRODED AFTER REMOVAL TO FOM. (C-CHECK RO 4/25/2021) ANGLE PN 600-32004-113 ORIGINAL MATERIAL THICKNESS IS.050" / --REMAINING MATERIAL THICKNESS IS.039" / --MATERIAL REMOVED IS.011" /
- [SDR SWIA202157916](https://openairdocs.org/sdr/SWIA202157916.md): Frame · corroded · Mar 13, 2021 · N873AS · Cndair CL6002B19 · Fuselage Main, Frame
  > *FRAME, FS310, NOTED CORROSION BETWEEN STGR24L AND STGR25R (MARKED) (C-CHECK RO 4/25/2021) REMOVED CORROSION ON FRAME FS 310 BETWEEN ST 24L AND ST 25R REF CRJ 200 SRM 51-21-06 / ORIGINAL MATERLAL THICKNESS=0.063, REF: CRJ 200, SRM 53-21-15, MATERIAL REM
- [SDR SWIA202157907](https://openairdocs.org/sdr/SWIA202157907.md): Floorbeam · corroded · Mar 13, 2021 · N873AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *COCKPIT FLOOR SUPPORT ANGLE AT FS280, BETWEEN LBL12 AND RBL12 HAS CORROSION AND CHAFING. (MARKED) (C-CHECK RO 4/25/2021) REMOVED AND REPLACED FWD COCKPIT FLOOR SUPPORT ANGLE AT FS280, BETWEEN LBL12 AND RBL12 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-
- [SDR SWIA202157897](https://openairdocs.org/sdr/SWIA202157897.md): Support · cracked · Mar 13, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *SUPPORT AT APPROX FS 469 FOR RH UPPER WING TO FUSELAGE FAIRING 162EL HAS CRACK. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED ANGLE SUPPORT FAIRING SIDE ACCES PN 601R31037-62 AT FS469.00 RH UPPER WING UNDER FUSELAGE FAIRING 162EL. REF. CRJ 200 SRM 51-42-
- [SDR SWIA202157896](https://openairdocs.org/sdr/SWIA202157896.md): Support · cracked · Mar 13, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *SUPPORT AT APPROX FS 461.5 FOR RH UPPER WING TO FUSELAGE FAIRING 162EL HAS CRACK. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED ANGLE SUPPORT FAIRING SIDE ACCESS PN 601R31037-42 AT FS461.5 RH UPPER WING TO FUSELAGE FAIRING 162EL. REF. CRJ 200 SRM 51-42-0
- [SDR SWIA202157895](https://openairdocs.org/sdr/SWIA202157895.md): Support · cracked · Mar 13, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *SUPPORT AT APPROX FS 476 FOR LH UPPER WING TO FUSELAGE FAIRING 161DL HAS CRACK. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED CRACK BRACKET WITH NEW BRACKET, LOCATED AT APPROX FS476, L/H UPPER WING TO FAUSELAGE FAIRING 161DL. REF: CRJ 200, SRM 51-41-02,
- [SDR SWIA202157894](https://openairdocs.org/sdr/SWIA202157894.md): Support · cracked · Mar 13, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *SUPPORT AT APPROX FS 469 FOR LH UPPER WING TO FUSELAGE FAIRING 161DL HAS CRACK. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED CRACKED BRACKET WITH NEW BRACKET, LOCATED AT APPROX FS469, L/H UPPER WING TO FUSELAGE FAIRING 161DL. REF: CRJ 200, SRM 51-41-02,
- [SDR SWIA202157889](https://openairdocs.org/sdr/SWIA202157889.md): Floor Support · corroded · Mar 13, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *RBL9 FLOOR BEAM, BETWEEN APPROX. FS409+4 TO FS409+122 HAS CORROSION. (MARKED) (C-CHECK RO 4/25/2021) NO CORROSION FOUND AT RBL9 FLOOR BEAM FROM FS409+4 TO FS409+5 AND FROM FS409+118 TO FS409+122. REMOVED AND REPLACED THE FLOOR BEAM CAP RBL9 BETWEEN FS4
- [SDR SWIA202157888](https://openairdocs.org/sdr/SWIA202157888.md): Floor Support · corroded · Mar 13, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *RIGHT SIDE FLOOR SILL HAS CORROSION, BETWEEN APPROX. FS310 TO FS319(MARKED) (C-CHECK RO 4/25/2021) REMOVED AND REPLACED RH FLOOR SILL BETWEEN FS 310 AND FS319 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-45-00, CRJ200 SRM 51-42-21 AND DWG 601R31148 REV-J. CO
- [SDR SWIA202157915](https://openairdocs.org/sdr/SWIA202157915.md): Strap · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * CORROSION ON STRAP AT FS559+80 BETWEEN RBL9 AND RBL 27. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PLATE P/N 601R32215-43 CRJ200 SRM 51-42-06
- [SDR SWIA202157906](https://openairdocs.org/sdr/SWIA202157906.md): Anchor Fitting · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Passenger/Crew Doors
  > *PASSENGER DOOR €“ AFT ANCHOR FITTING, FS349.00, AND HARDWARE ARE CORRODED. (MARKED) (C-CHECK RO 4/25/2021) PASSENGER DOOR- AFT ANCHOR FITTING FS349.00 REMOVED AND REPLACED, NEW HARDWARE INSTALLED, OPERATIONAL TEST COMPLIED WITH NO DEFECTS NOTED AT THI
- [SDR SWIA202157905](https://openairdocs.org/sdr/SWIA202157905.md): Plate · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > *PASSENGER DOOR €“ AFT ANCHOR FITTING AT FS349.00 SERRATED MOUNT PLATE IS CORRODED. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED CORRODED AFT ANCHOR FITTING SERRATED MOUNT PLATE AT FS349.00 PAX DOOR FRAME REF CRJ-200 SRM 51-41-02 WITH A NEW PLATE P/N 60
- [SDR SWIA202157904](https://openairdocs.org/sdr/SWIA202157904.md): Strap · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * CORROSION ON STRAP BETWEEN RBL9 AND RBL27 AT FS559+48. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PLATE P/N 601R32215-43 CRJ200 SRM 51-42-06
- [SDR SWIA202157903](https://openairdocs.org/sdr/SWIA202157903.md): Seat Track · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * LBL27 SEAT TRACK CORRODED BETWEEN FS559+78 AND FS559+95. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED NEW FABRICATED SEAT TRACK P/N 601R 38779-9 PO# T58082 ON LBL 27.0 FROM FS 559+78 TO FS 559+95. REF. BOMBARDIER REO 601R-53-00-485 REV D DATED 2018-01-
- [SDR SWIA202157902](https://openairdocs.org/sdr/SWIA202157902.md): Seat Track · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * LBL9 SEAT TRACK CORRODED BETWEEN FS559+86 AND FS559+95. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED NEW FABRICATED SEAT TRACK P/N 601R 38779-13 PO# T58082 ON LBL 9.0 FROM FS 559+86 TO FS 559+95. REF. BOMBARDIER REO 601R-53-00-485 REV D DATED 2018-01-2
- [SDR SWIA202157901](https://openairdocs.org/sdr/SWIA202157901.md): Seat Track · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * RBL27 SEAT TRACK CORRODED BETWEEN FS559+78 AND FS559+95. (C-CHECK RO 4/25/2021) FABRICATED AND REPLACED CORRODED SEAT TRACK PER REO 601R-53-00-485, REV -D, DATED 2018-01-29, SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202157900](https://openairdocs.org/sdr/SWIA202157900.md): Seat Track · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * RBL9 SEAT TRACK CORRODED BETWEEN FS559+86 AND FS559+95. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED NEW FABRICATED SEAT TRACK P/N 601R 38779-13 PO# T55899 ON RBL 9.0 FROM FS 559+86 TO FS 559+95. REF. BOMBARDIER REO 601R-53-00-485 REV D DATED 2018-01-2
- [SDR SWIA202157893](https://openairdocs.org/sdr/SWIA202157893.md): Support Beam · cracked · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > *CARGO DOOR €“ FORWARD CARGO DOOR TRACK SUPPORT BEAM ANGLE IS CRACKED FS574.00. (MARKED) (C-CHECK RO 4/25/2021) REMOVED BROKEN FORWARD CARGO DOOR TRACK SUPPORT BEAM ANGLE CLIP, AND INSTALLED NEW CLIP REF. CRJ200 SRM 51-42-21.
- [SDR SWIA202157887](https://openairdocs.org/sdr/SWIA202157887.md): Attach Fitting · cracked · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > * CRACKED CLIP FOR CABLE GUIDE BRACKET AT FS484 RBL36. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED EXISTING REPAIR CLIP FOR CABLE GUIDE BRACKET AT FS484 RBL36 REF REO 601R-53-41-059, REV-C, DATED 2020-03-11. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAIL
- [SDR SWIA202157886](https://openairdocs.org/sdr/SWIA202157886.md): Floor Support · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * CORROSION ON LBL9 FLOOR BEAM CAP BETWEEN FS559+10 AND FS569 AT MULTIPLE LOCATIONS. (C-CHECK RO 4/25/2021) REMOVED CORROSION FROM THE LBL9 FLOOR BEAM CAP BETWEEN FS559+10 AND FS569 REF. CRJ200 SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. REMO
- [SDR SWIA202157885](https://openairdocs.org/sdr/SWIA202157885.md): Floor Support · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * CORROSION ON RBL9 FLOOR BEAM CAP BETWEEN FS559+10 AND FS569 AT MULTIPLE LOCATIONS. (C-CHECK RO 4/25/2021) REMOVED CORROSION ON THE RBL9 FLOOR BEAM CAP BETWEEN FS559+10 AND FS569 REF. CRJ200 SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. REMOVE
- [SDR SWIA202157884](https://openairdocs.org/sdr/SWIA202157884.md): Floor Support · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * MULTIPLE SPOTS OF CORROSION ON LH FLOOR SILL BETWEEN FS559+16 AND FS559+84. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED NEW LH FLOOR SILL P/N 601R31133-77 BETWEEN FS 559+16 AND FS 559+84 REF CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-4
- [SDR SWIA202157883](https://openairdocs.org/sdr/SWIA202157883.md): Floor Support · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RBL 27 FLOOR BEAM CAP HAS CORROSION BETWEEN FS559+64 AND FS559+83. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED WITH NEW FABRICATED FLOOR BEAM CAP AT RBL 27 BETWEEN FS 559+10 AND FS 569 REF DWG 601R31119 REV -H, DWG 601R31030 REV -P, DWG 601R31005 REV
- [SDR SWIA202157882](https://openairdocs.org/sdr/SWIA202157882.md): Floor Support · corroded · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * LBL 9 FLOOR BEAM CAP OUTBOARD FLANGE HAS SPOTS OF CORROSION BETWEEN FS589 AND FS621. (C-CHECK RO 4/25/2021) REMOVED CORROSION ON LBL 9 FLOOR BEAM CAP OUTB`D FLANGE BETWEEN FS 589 AND FS 621 REF CRJ200 SRM 51-21-06 / ORIGINAL MATERIAL THICKNESS OF FLOO
- [SDR SWIA202157881](https://openairdocs.org/sdr/SWIA202157881.md): Bulkhead Web · gouged · Mar 12, 2021 · N873AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD FACE OF FS 621 AFT PRESS BLKHD - APROX 11 EA SCREW STARTS / GOUGES INTO BASE METAL AND RIVETS AS MARKED (C-CHECK RO 4/25/2021) COMPLIED AND REPAIRED FWD FACE OF FS621 AFT PRESSURE BULKHEAD, REF. BOMBARDIER REO 601R-53-61-1240 REV-D DATED 2016-10-31
- [SDR SWIA202157892](https://openairdocs.org/sdr/SWIA202157892.md): Bracket · cracked · Mar 10, 2021 · N873AS · Cndair CL6002B19 · Galley Doors
  > * SERVICE DOOR STOP BOLT SWITCH BRACKET CRACKED MARKED (C-CHECK RO 4/25/2021) REPLACED BRACKET, HARDWARE, AND HELICOIL INSERTS PER CRJ200SRM 51-42-02 AND 51-42-21. OPS CHECKS GOOD.
- [SDR SWIA202157899](https://openairdocs.org/sdr/SWIA202157899.md): Nut Plate · corroded · Mar 9, 2021 · N873AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > * RIGHT OVERWING EMER EXIT DOOR HAS NUT PLATES INSIDE BOTTOM OF DOOR CORRODED MARKED (C-CHECK RO 4/25/2021) REMOVED AND REPLACED 23EA NUT PLATES ON RIGHT OVERWING EMERGENCY EXIT DOOR INSIDE BOTTOM OF DOOR. REF CRJ 200 SRM 51-45-00 TOOL # TUC 5657 CAL D
- [SDR SWIA202157898](https://openairdocs.org/sdr/SWIA202157898.md): Nut Plate · corroded · Mar 9, 2021 · N873AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > * LEFT OVERWING EMER EXIT DOOR NUT PLATES CORRODED UNDER TOP PLATE ACCESS COVER MARKED (C-CHECK RO 4/25/2021) REMOVED AND REPLACED 15EA NEW NUT PLATES AND SCREWS AT LEFT OVERWING EMER EXIT DOOR UNDER TOP PLATE ACCESS COVER REF CRJ200 SRM 51-45-00 AND
- [SDR SWIA202157880](https://openairdocs.org/sdr/SWIA202157880.md): Bracket · gouged · Mar 9, 2021 · N873AS · Cndair CL6002B19 · Ailerons
  > * FOUND GOUGE ON RH AILERON FRONT SPAR RETAINER BRACKET(AREA FLAGGED). (C-CHECK RO 4/25/2021) REMOVED AND REPLACED RH AILERON FRONT SPAR RETAINER BRACKET REF CRJ200 SRM 51-42-21 AND CRJ200 SRM 51-45-00 AND DWG CC670-13082 REV-B. COMPLIED WITH ATTACHED
- [SDR SWIA202157879](https://openairdocs.org/sdr/SWIA202157879.md): Skin · corroded · Mar 9, 2021 · N873AS · Cndair CL6002B19 · Ailerons
  > * FOUND SURFACE COROSSION ON THE LOWER SKIN PANEL OF THE LH AILERON(AREA MARKED) (C-CHECK RO 4/25/2021) REPLACED CORRODED LH AILERON LOWER SKIN PANEL (CENTER LOWER FIXED SKIN PANEL WITH A NEW PANEL P/N 601R13031-147S REF CRJ-200 SRM 51-42-06 AND DWG # 6
- [SDR SWIA202157878](https://openairdocs.org/sdr/SWIA202157878.md): Rib · cracked · Mar 8, 2021 · N873AS · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > * L/H ENGINE PYLON RIB AT FS 605.00 CRACKED AT LOWER OBD CORNER. (C-CHECK RO 4/25/2021) REPAIRED L/H ENGINE PYLON RIB AT FS605.00 REF. MHIRJ REO 601R-54-61-127 REV -- DATED 2021-03-10. THRUST REVERSER OPERATIONAL TEST GOOD. COMPLIED WITH 51-900-1003-SKY

Next page: https://openairdocs.org/aircraft/N873AS/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 = 'N873AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N873AS/reports

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