# Service difficulty reports: N875AS

A list on [N875AS](https://openairdocs.org/aircraft/N875AS.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 6 · 256 reports

- [SDR SWIA202265441](https://openairdocs.org/sdr/SWIA202265441.md): None · overheated · Apr 22, 2022 · N875AS · Cndair CL6002B19 · Ice/Rain Protection System
  > WING OVHT WARNING MESSAGE IN CLIMB, FOLLOW QRH, MESSAGE DIDN€™T CLEAR. / FA REPORTS CABIN SMELLS LIKE RUBBER BURNING. (FLIGHT 5735 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24708232 WITH THE FOLLOWING CORRECTIVE ACTION: "FOR RUBBER
- [SDR SWIA202265201](https://openairdocs.org/sdr/SWIA202265201.md): None · cracked · Feb 10, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > RH BEAM INTERCOSTAL FOUND CRACKED ON RBL9 AND BETWEEN FS559.00+64 - FS559.00+80. (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH BEAM INTERCOSTAL P/N 601R31117-35 AT RBL9 AND BETWEEN FS559.00+64-FS559.00+80 WITH A NEW IDENTICAL UNIT IAW CRJ200 SRM 51-42-06 A
- [SDR SWIA202265200](https://openairdocs.org/sdr/SWIA202265200.md): None · nicked · Feb 8, 2022 · N875AS · Cndair CL6002B19 · Stabilizer Position Indicating
  > * FOUND TWO NICKS ON THE LH TRUNNION OF THE HSTA ATTACH FITTINGS.(AREA MARKED) (C-CHECK RO 3-25-22) BLENDED DAMAGES ON LH TRUNNION OF THE HSTA ATTACH FITTINGS REF CRJ200 SRM 51-12-00. WITHIN LIMITS, RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-55-31-3
- [SDR SWIA202265211](https://openairdocs.org/sdr/SWIA202265211.md): None · damaged · Feb 2, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > CANN FLIGHT OBSERVERS LOWER SEAT RAIL P/N: 15981-1 FOR USE ON N929SW / SN: 7703. (C-CHECK RO 3-25-22) REMOVED AND REPLACED FLIGHT OBSERVER LOWER SEAT RAIL P/N 15981-1 REF CRJ 200 AMM 25-12-01-400-801
- [SDR SWIA202265199](https://openairdocs.org/sdr/SWIA202265199.md): None · corroded · Feb 1, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Stairs
  > CORROSION FOUND UNDERNEATH GIRT BAR FITTINGS AT SERVICE DOOR LOWER THRESHOLD FS319.70 TO FS349.00 STR17R (C-CHECK RO 3-25-22) REMOVED LOWER THESHOLD ANGLE REF CRJ 200 SRM 51-42-06 AND 51-42-36, INSTALLED LOWER THESHOLD ANGLE REF CRJ 200 SRM 51-42-06, REF
- [SDR SWIA202265198](https://openairdocs.org/sdr/SWIA202265198.md): None · corroded · Jan 31, 2022 · N875AS · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > R/H ELEVATOR FITTING LOCATED @ BL15.25 NEEDS TO BE REPLACED DUE TO CORROSION IN THE BEARING BORE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED R/H ELAVATOR FITTING ASSY( BEARING INCLUDED) @ ES 15-25 P/N 600-24043-1 REF CRJ 200 SRM 51-42-06 AND CRJ 200 DWG
- [SDR SWIA202265197](https://openairdocs.org/sdr/SWIA202265197.md): None · damaged · Jan 30, 2022 · N875AS · Cndair CL6002B19 · Wing, Center Box
  > DEFECTS NOTED IN THE RH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE RH WING DRAIN LOCATED BETWEEN WS0.00 + THE RH BOOST PUMP AND BETWEEN STR5 - STR7. (C-CHECK RO 3-25-22) REPAIRED DEFECTS IN THE RH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE R
- [SDR SWIA202265196](https://openairdocs.org/sdr/SWIA202265196.md): None · damaged · Jan 30, 2022 · N875AS · Cndair CL6002B19 · Wing, Center Box
  > DEFECTS NOTED IN THE LH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE LH WING DRAIN LOCATED BETWEEN WS0.00 + THE LH BOOST PUMP AND BETWEEN STR5 - STR7. (C-CHECK RO 3-25-22) REPAIRED DEFECTS IN THE LH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE L
- [SDR SWIA202265195](https://openairdocs.org/sdr/SWIA202265195.md): None · corroded · Jan 26, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > BRACKET COMMON TO PAX DOOR INTERCOSTAL DD6 FOUND CORRODED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR BRACKET P/N 601R8084-2 WITH A SERVICEABLE UNIT IAW CRJ200 SRM 51-42-06 REVISION 38: JUL 10/2019 AND BOMBARDIER DRAWING 601R31702 REV. -N. COMPLIE
- [SDR SWIA202265194](https://openairdocs.org/sdr/SWIA202265194.md): None · gouged · Jan 22, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE RH WING AILERON HINGE FITTING WING SIDE #4 HINGE KEEPER BOLT HOLE ON OUTBD SIDE IS GOUGED. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE ON RH WING AILERON HINGE FITTING WING SIDE #4 HINGE REF CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. RECEIVED AND C
- [SDR SWIA202265193](https://openairdocs.org/sdr/SWIA202265193.md): None · chafed · Jan 22, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE RH WING AILERON HINGE FITTING WING SIDE #3 HINGE IS CHAFFED IN 2EA LOCATIONS. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGES ON RH WING AILERON HINGE FITTING WING SIDE #3 HINGE REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIE
- [SDR SWIA202265192](https://openairdocs.org/sdr/SWIA202265192.md): None · gouged · Jan 22, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE LH WING AILERON HINGE FITTING WING SIDE #3 HINGE INBD LUG IS GOUGED. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE ON LH WING AILERON HINGE FITTING WING SIDE #3 HINGE REF CRJ200 SRM 51-12-00. FOUND TO BE WITHIN LIMITS. REF REO 601R-57-51-989 REV--,
- [SDR SWIA202265232](https://openairdocs.org/sdr/SWIA202265232.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > *THE RH INBD GROUND HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED CORRODED CASTLE NUTS, WASHERS AND COTTER PINS ON R/H INBOARD GROUND SPOILER HINGE ATTACHMENT OUTBOARD AND INBOARD HINGE IAW CRJ200 27-65-01-400-801 STEPS 2.B.(9)
- [SDR SWIA202265231](https://openairdocs.org/sdr/SWIA202265231.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > *THE RH INBD GROUND PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED R/H INBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE AND REPLACED WITH NEW IAW CRJ200 AMM 27-63-01-400-801 STEPS 2.B.(2)
- [SDR SWIA202265230](https://openairdocs.org/sdr/SWIA202265230.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > *THE RH OUTBD GROUND HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H OUTBOARD GROUND SPOILER HINGE ATTACHMENT CASTLE NUT, WASHER AND COTTER PIN REMOVED FROM INBOARD AND OUTBOARD HINGE AND REPLACED WITH NEW IAW CRJ200 AMM 27-65-01-400-801 STEPS 2.B
- [SDR SWIA202265229](https://openairdocs.org/sdr/SWIA202265229.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control System
  > *THE RH FLIGHT SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H FLIGHT SPOILER HARDWARE FOR HINGE ATTACHMENT REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-64-05-400-801 STEPS 2.B. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22
- [SDR SWIA202265228](https://openairdocs.org/sdr/SWIA202265228.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control System
  > *THE RH FLIGHT SPOILER PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H FLIGHT SPOILER PCU LOWER ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-62-01-400-801 STEPS 2. A THROUGH B / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DU
- [SDR SWIA202265227](https://openairdocs.org/sdr/SWIA202265227.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > THE RH SPOILERON HINGES'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H SPOILERON HINGE ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-64-01-400-801 STEPS 2.B. AND C. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22
- [SDR SWIA202265226](https://openairdocs.org/sdr/SWIA202265226.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control System
  > * THE RH SPOILERON PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H SPOILERON PCU LOWER ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-62-01-400-801 STEPS 2. A. THROUGH B. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/
- [SDR SWIA202265225](https://openairdocs.org/sdr/SWIA202265225.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control System
  > * THE LH SPOILERON HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW HARDWARE ON L/H SPOILERON, REF. CRJ-200 AMM 27-64-01-400-801. SEE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202265224](https://openairdocs.org/sdr/SWIA202265224.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control System
  > * THE LH SPOILERON PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED SURFACE CORROSION FROM L/H SPOILERON HARDWARE, REF. CRJ-200 SRM 51-21-06 STEPS 7. A. [1] (A)-(B).
- [SDR SWIA202265223](https://openairdocs.org/sdr/SWIA202265223.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE LH FLIGHT SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED HARDWARE FROM THE LH FLIGHT SPOILER HINGES REF CRJ200 AMM 27-64-05-000-801 PGS 401-407. INSTALLED NEW HARDWARE FOR THE LH FLIGHT SPOILER HINGES REF CRJ200 AMM 27-6
- [SDR SWIA202265222](https://openairdocs.org/sdr/SWIA202265222.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE LH FLIGHT SPOILER PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REPLACED LH FLIGHT SPOILER PCU'S CORRODED HARDWARE REF CRJ200 AMM 27-64-05-000-801 AND AMM 27-64-05-400-801. REPLACED 2 SCREWS,1 SPLIT WASHER, 1 NUT, 3 WASHERS.
- [SDR SWIA202265221](https://openairdocs.org/sdr/SWIA202265221.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE LH OUTBD GROUND SPOILER BONDING JUMPER HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER BONDING JUMPER ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 2 EA NUTS AND 2 EA SCREWS. IAW CRJ200 AMM 27
- [SDR SWIA202265220](https://openairdocs.org/sdr/SWIA202265220.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE LH OUTBD GROUND SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER HINGE ATTACHMENT HARDWARE TO INCLUDE 3 EA NUTS AND COTTER PINS. ONLY REPALCED ONE NUT AT A TIME IAW CRJ200 AMM 27-65-01-400-801 P
- [SDR SWIA202265219](https://openairdocs.org/sdr/SWIA202265219.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE LH OUTBD GROUND SPOILER PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 3 EA NUTS, 1 EA BOLT, 2 EA WASHERS AND COTTER PINS. ONLY REPALCED
- [SDR SWIA202265218](https://openairdocs.org/sdr/SWIA202265218.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE LH INBD GROUND SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H INBOARD GROUND SPOILER HINGE ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 3 EA NUTS AND COTTER PINS. ONLY REPALCED ONE NUT AT A TIME. IAW
- [SDR SWIA202265217](https://openairdocs.org/sdr/SWIA202265217.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing Structure
  > * THE LH INBD GROUND SPOILER PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) L/H INBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-63-01-400-801 STEPS 2.B.(2)
- [SDR SWIA202265214](https://openairdocs.org/sdr/SWIA202265214.md): None · corroded · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Ailerons
  > * THE LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE IS CORRODED AROUND NUTPLATE HOLES. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE AT LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE REF. CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REC
- [SDR SWIA202265210](https://openairdocs.org/sdr/SWIA202265210.md): None · chafed · Jan 21, 2022 · N875AS · Cndair CL6002B19 · Ailerons
  > * THE LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE IS CHAFFED. (MARKED) (C-CHECK RO 3-25-22) BLENDED CHAFFING ON LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH
- [SDR SWIA202265234](https://openairdocs.org/sdr/SWIA202265234.md): None · corroded · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Doors
  > PAX DOOR. UPPER STOP BOLT FITTING CORRODED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED BRACKET ASSY P/N 601R38921-13 WITH A NEW SERVICEABLE UNIT IAW CRJ200 SRM 51-42-14.
- [SDR SWIA202265233](https://openairdocs.org/sdr/SWIA202265233.md): None · cracked · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Doors
  > PAX DOOR. AFT DRAG ANGLE SUSPECTED CRACK BY THE MOTOR ASSIST PULLEY. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE P/N 601R31772-6 WITH A NEW UNIT IAW CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-14.
- [SDR SWIA202265191](https://openairdocs.org/sdr/SWIA202265191.md): None · corroded · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *IN MAIN CABIN, ON PRESSURE FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559, AND RBL9, HAS CORROSION ON MULTIPLE AREAS OF UPPER SURFACE. (MARKED) (C-CHECK RO 3-25-22) PERFORMED REPAIR ON FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559.00
- [SDR SWIA202265190](https://openairdocs.org/sdr/SWIA202265190.md): None · gouged · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Doors
  > PAX DOOR CUT-OUT FRAME AFT ROLLER ATTACHMENT GOUGED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED THE PAX DOOR AFT ROLLER BRACKET REF AMM 53-21-23-400-801 REV 64 SEP 10/2021 AND DWG 600-31469 REV A. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. CHECKS G
- [SDR SWIA202265189](https://openairdocs.org/sdr/SWIA202265189.md): None · corroded · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *IN MAIN CABIN, ON PRESSURE FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559, AND LBL9, HAS CORROSION ON MULTIPLE AREAS OF UPPER SURFACE. (MARKED) (C-CHECK RO 3-25-22) PERFORMED REPAIR ON FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559.00
- [SDR SWIA202265188](https://openairdocs.org/sdr/SWIA202265188.md): None · gouged · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Structure (General)
  > PAX. DOOR. CUT-OUT FRAME FS310.00 GOUGED JUST BELOW UPPER PIN STOP. (C-CHECK RO 3-25-22) PERFORMED REPAIR TO PAX DOOR SEAL STRIKER I.A.W. ALL STEPS OF REO 601R-53-22-033 REV-D DATE 2014/02/17 REPAIR TYPE IV. COMPLIED WITH TASK CARD 51-900-1003-SKY. OPS CH
- [SDR SWIA202265187](https://openairdocs.org/sdr/SWIA202265187.md): None · corroded · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *IN MAIN CABIN, L/H PRESSURE FLOOR SILL MEMBER, FROM APPROXIMATELY 409+128 TO FS559, NEAR STR17L, HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED CORROSION FROM L/H PRESSURE FLOOR SILL FS 409+128-FS 559 STR 17L PER CRJ 200 SRM 51-2
- [SDR SWIA202265186](https://openairdocs.org/sdr/SWIA202265186.md): None · corroded · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > PAX DOOR, INTERCOSTAL DD6 AFT END CORRODED. DISCREPANCY VIEWED THRU ACCESS HOLE 832GR. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR DD6 INTERCOSTAL P/N 601R31902-323 WITH A SERVICEABLE UNIT IAW CRJ200 SRM 51-42-06 REVISION 38: JUL 10/2019 AND BOMBAR
- [SDR SWIA202265185](https://openairdocs.org/sdr/SWIA202265185.md): None · corroded · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *IN MAIN CABIN, AT APPROXIMATELY FS409+30 TO FS409+128, AND NEAR LBL6-LBL8, FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED MAIN CABIN FLOOR BEAM CAP AT APPROXIMATELY FS409+30 TO FS409+128, AND NEAR LBL6-LBL
- [SDR SWIA202265184](https://openairdocs.org/sdr/SWIA202265184.md): None · corroded · Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *IN MAIN CABIN, ON FLOOR BEAM AT APPROXIMATELY FS409+16 TO FS409+128, AND BETWEEN RBL6 TO RBL8, FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED FLOOR BEAM CAP AT FS409+16 TO FS409+128, AND BETWEEN RBL6 T
- [SDR SWIA202265209](https://openairdocs.org/sdr/SWIA202265209.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > * THE RH SIDE SEAT TRACK FROM APPROX FS409+16 TO FS409+112 HAS MULTIPLE LOCATIONS OF CORROSION (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH SIDE SEAT TRACK AT FS409+16 TO FS409+112 REF CRJ200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR SWIA202265208](https://openairdocs.org/sdr/SWIA202265208.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > * THE RH SIDE SEAT TRACK FROM APPROX FS364 TO FS409+16 HAS MULTIPLE LOCATIONS OF CORROSION (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH SIDE SEAT TRACK FROM FS364 TO FS409+16 REF CRJ200 AMM 53-01-11-000-802 STEPS 1-3.A AND AMM 53-01-11-400-802 S
- [SDR SWIA202265207](https://openairdocs.org/sdr/SWIA202265207.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > * THE LH SIDE SEAT TRACK FROM APPROX FS409+16 TO FS409+112 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LH SIDE SEAT TRACK FROM FS409+16 TO 409+112 REF CRJ200 AMM 53-01-11-000-802 STEPS 1-3.A AND AMM 53-01-11-40
- [SDR SWIA202265206](https://openairdocs.org/sdr/SWIA202265206.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > * THE LH SIDE SEAT TRACK FROM APPROX FS364 TO FS409+16 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LH SIDE SEAT TRACK FROM FS364 TO FS409+16 REF CRJ200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802 TORQUE SCREWD
- [SDR SWIA202265205](https://openairdocs.org/sdr/SWIA202265205.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > * THE LH SIDE SEAT RAIL RETAINER TRIM FROM APPROX FS364 TO FS409.00+16 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LEFT SEAT RAIL RETAINER AND SEAT RAIL FROM APPROX FS364 TO FS409+16 IAW CRJ200 AMM 53-01-11-00/4
- [SDR SWIA202265183](https://openairdocs.org/sdr/SWIA202265183.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *GUSSET COMMON TO FS409 FRAME AND INTERCOSTAL AT STR25R HAS CORROSION (MARKED). (C-CHECK RO 3-25-22) REPLACED GUSSET REF DRAWING #601R31049 REV:-F, CRJ200 SRM 51-42-21-00 REV: 38B DATED: 25 NOV 2020. FOR ALL WORK ACCOMPLISHED SEE CONTINUE CARD. COMPLIED
- [SDR SWIA202265182](https://openairdocs.org/sdr/SWIA202265182.md): None · damaged · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, Frame
  > *FRAME AT FS394 HAS GOUGE DAMAGE ON TOPSIDE RADIUS OF THE UPPER FLANGE AT STR27 (MARKED). (C-CHECK RO 3-25-22) BLENDED FRAME AT FS394 UPPER FLANGE AT STR27 PER REF: CRJ-200 SRM 51-12-00, FOUND TO BE WITH IN LIMITS REF CRJ 200 SRM 53-00-00. RESTORED FINISH
- [SDR SWIA202265181](https://openairdocs.org/sdr/SWIA202265181.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON FLOOR SILL ATTACHING ANGLE RBL 45 BETWEEN FS 605.00 €“ 621.00 (C-CHECK RO 3-25-22) REMOVED CORROSION FROM FLOOR SILL ATTACHING ANGLE RBL45 F.S.605-621.00 IAW REO 601R-53-61-4690 REV.-- DATED 2012-10-24 FOUND TO BE WITHIN LIMITS.
- [SDR SWIA202265180](https://openairdocs.org/sdr/SWIA202265180.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON FLOOR SUPPORT BEAM AT FS 589.00 BETWEEN RBL 27 €“ RBL 36 (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT FS 589.00 BETWEEN RBL 27 €“ RBL 36 REF CRJ200 SRM 51-42-06 REV 38 JUL 10/2019 AND BOMBARDIER DWG 601R35031 REV -
- [SDR SWIA202265179](https://openairdocs.org/sdr/SWIA202265179.md): None · corroded · Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 9 €“ RBL 18 (C-CHECK RO 3-25-22) REMOVED CORROSION ON FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 9 €“ RBL 18 IAW CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NEW FLOOR

Next page: https://openairdocs.org/aircraft/N875AS/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 = 'N875AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N875AS/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.