# Service difficulty reports: N878AS

A list on [N878AS](https://openairdocs.org/aircraft/N878AS.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 · 227 reports

- [SDR SWIA202501071206](https://openairdocs.org/sdr/SWIA202501071206.md): Floor Support · corroded · Dec 6, 2024 · N878AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH CABIN FLOOR SILL AT RBL 41.75 AND BETWEEN FS559.00 TO FS559.00 + 16 HAS SURFACE CORROSION ON TOP SURFACE. (FILED CLOSED) REPAIRED LH CABIN FLOOR SILL AT RBL 41.75 AND BETWEEN FS559.00 TO FS559.00 + 16 WITH REFERENCE TO REO 601R-53-51-697 REV -- DATED
- [SDR SWIA202401071129](https://openairdocs.org/sdr/SWIA202401071129.md): Floor Support · corroded · Nov 29, 2024 · N878AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH CABIN FLOOR SILL AT RBL 41.75 AND BETWEEN FS559.00 +16 TO FS559.00 +48 HAS SURFACE CORROSION ON TOP SURFACE. (FILED CLOSED) REPAIRED THE RH CABIN FLOOR SILL AT RBL 41.75 AND BETWEEN FS559.00 +16 TO FS559.00 +48 IN REFERENCE WITH REO 601R-53-51-696 R
- [SDR SWI2025010700040](https://openairdocs.org/sdr/SWI2025010700040.md): Floor Support · corroded · Nov 25, 2024 · N878AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SEVERAL SPOTS OF CORROSION ON THE RH PRESSURE FLOOR SILL AT FS429.00, FS478.00, FS501.00, FS512.00, (2 SPOTS) AT FS518.00, FS524.00, FS531.00, FS537.00, FS542.00, FS548.00 (FILED CLOSED) REPAIRED RH PRESSURE FLOOR SILL AT FS429.00, FS478.00,
- [SDR SWIA2025010741125](https://openairdocs.org/sdr/SWIA2025010741125.md): Floor Support · corroded · Nov 25, 2024 · N878AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SEVERAL SPOTS OF CORROSION ON THE LH PRESSURE FLOOR SILL AT FS 478.00, FS507.00, FS509.00, FS518.00, FS522.00, FS530.00, FS536.00, FS542.00, AND FS548.00. (FILED CLOSED) REPAIRED LH PRESSURE FLOOR SILL AT FS 478.00, FS507.00, FS509.00, FS5
- [SDR SWIA20250106124](https://openairdocs.org/sdr/SWIA20250106124.md): Intercostal · cracked · Nov 24, 2024 · N878AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT SIDE OF FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 15L, INTERCOSTAL CRACKED. (FILED CLOSED) REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 15L WITH REFERENCE TO SRM 51-42-
- [SDR SWI2024F01285](https://openairdocs.org/sdr/SWI2024F01285.md): Pressure Blkhd · cracked · Nov 24, 2024 · N878AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R, INTERCOSTAL CRACKED. OPEN
- [SDR SWIA2024112501284](https://openairdocs.org/sdr/SWIA2024112501284.md): Pressure Blkhd · cracked · Nov 24, 2024 · N878AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 15L, INTERCOSTAL CRACKED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20241121](https://openairdocs.org/sdr/SWIA20241121.md): Track · cracked · Nov 21, 2024 · N878AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR, FWD TRACK, LOWER CHANNEL IS CRACKED (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR FWD TRACK AFT LOWER CHANNEL WITH REFERENCE TO SRM 51-42-06 AND SRM 53-61-23. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
- [SDR SWIA2024061200011](https://openairdocs.org/sdr/SWIA2024061200011.md): Strut · failed · Jun 11, 2024 · N878AS · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > NOSE GEAR DISAGREE ON DEPARTURE RAN QRH GEAR WAS DOWN AND THREE GREEN (FLIGHT 5082 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28370699 WITH THE FOLLOWING CORRECTIVE ACTION: "REF. CP 28370769 FOR REPLACEMENT OF LEAKING NLG NITROGEN CHARGING V
- [SDR SWIA20240425](https://openairdocs.org/sdr/SWIA20240425.md): Warning Message · false activation · Apr 25, 2024 · N878AS · Cndair CL6002B19 · Overheat Detection
  > TROUBLESHOOT WING OVHT WARNING MSG AT NEXT MX OVENIGHT DUE TO REPEAT. MCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 5719 FILED CLOSED)APR 25, 2024 STATION: ORD--PERFORMED OPS CHECK OF THE WING ANTI ICE INDICATION AND CONTROL SYSTEM IN NORMAL AND STANDBY MODE I
- [SDR SWIA202263752](https://openairdocs.org/sdr/SWIA202263752.md): Bracket · damaged · Jan 9, 2022 · N878AS · Cndair CL6002B19 · Main Landing Gear
  > NOSE DOOR OPEN WARNING MSG AND GEAR DISAGREE WARNING MSG UPON GEAR RETRACTION. MAIN GEAR RETRACTED, NOSE GEAR INDICATED DN. / PERFORMED QRH PROCEDURE(S). (FLIGHT# 4033 - FILED CLOSED) REMOVED AND REPLACED NLG OLEO SENSOR BRACKET WITH A SERVICABLE UNIT. R
- [SDR SWIA2021083160635](https://openairdocs.org/sdr/SWIA2021083160635.md): Landing Gear · unwanted extend · Aug 30, 2021 · N878AS · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR DISAGREE WARNING ON RAISING GEAR AFTER TEN MINUTES BELOW 200 KIAS PER MEL 20-14-1A? NOSE GEAR RETURNED TO THE DOWN LOCKED POSITION WITH GEAR HANDLE UP. COMPLIED WITH QRH PROCEDURE, GEAR LOWERED DOWN AND LOCKED SAFELY, AND LANDED NEAREST SUITABLE AIRFIELD.
- [SDR SWIA2021072659743](https://openairdocs.org/sdr/SWIA2021072659743.md): Selector Valve · leaking · Jul 22, 2021 · N878AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON APPROACH TO BTM€¦.HYDRAULIC 3 LO PRESS CAUTION (FLIGHT 4273) PLEASE REFERENCE AML 691078 PLEASE REFERENCE AML 691079 PLEASE REFERENCE AML 691082 PLEASE REFERENCE AML 691083 PLEASE REFERENCE AML 691087 PLEASE REFERENCE AML 691088 P
- [SDR SWIA2021072159639](https://openairdocs.org/sdr/SWIA2021072159639.md): Connector · corroded · Jun 5, 2021 · N878AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD AND AFT BRACKET CONNECTOR HAS CORROSION (C-CHECK RO 7/18/2021) REMOVED AND REPLACED 2EA NEW PAX DOOR BRACKET CONNECTORS FWD AND AFT, P/N 601R31771-1. CRJ-200 SRM 51-42-06 AND CRJ-200 DWG 601R31527 REV €ŒAM€? COMPLIED WITH 51-900-1003-S
- [SDR SWIA2021072159663](https://openairdocs.org/sdr/SWIA2021072159663.md): Attach Angle · gouged · May 22, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 310 STGR 5L - AFT CORNER CLEAT SECURING INTERCOSTAL TO FRAME GOUGED TO BARE METAL SEVERAL PLACES (C-CHECK RO 7/18/2021) REMOVED AND INSTALLED NEW FABRICATED CLEAT AT FS310.00 STGR5L ON INTERCOSTAL AFT CORNER OF FRAME. REF. BOMBARDIER DWG # 601R31096
- [SDR SWIA2021072159638](https://openairdocs.org/sdr/SWIA2021072159638.md): Hinge Arm · gouged · May 19, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H INBD FLAP - OTBD HINGE ARM ASSY - HINGE BOX ASSY ATTACHMENT HOLE BOSS AND SURROUNDING AREA SHOWS DEEP GOUGES AND IMPACT DAMAGE SEVERAL PLACES (C-CHECK RO 7/18/2021) REPAIRED R/H INBD FLAP - OTBD HINGE ARM ASSY - HINGE BOX ASSY ATTACHMENT HOLE BOSS A
- [SDR SWIA2021072159637](https://openairdocs.org/sdr/SWIA2021072159637.md): Window Post · cracked · May 19, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H WINDSHIELD SUPPORT POST BRACKET ATTACH CLIP (LOWER) CRACK FOUND IN RADIUS. (C-CHECK RO 7/18/2021) INSTALLED NEW R/H WINDSHIELD SUPPORT POST BRACKET ATTACH CLIP IAW CRJ200 SRM 51-42-21. AND DWG 601R34032 REV -V. COMPLETED SKYWEST TASK CARD 51-900-
- [SDR SWIA2021072159636](https://openairdocs.org/sdr/SWIA2021072159636.md): Stringer · cracked · May 19, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *STGR 3L CRACKED AFT OF FS 379.00 (C-CHECK RO 7/18/2021) REMOVED AND REPAIRED STR 3L AFT OF FS379 REF DWG 601R31016, REV-D, DWG 601R31522 REV-R, CRJ200 SRM 53-00-03, REO 601R-53-21-3453, REV--, DATED 2021-05-31. NO LEAKS NOTED. SEE CONTINUE CARD FOR DET
- [SDR SWIA2021072159635](https://openairdocs.org/sdr/SWIA2021072159635.md): Floorbeam · cracked · May 18, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND CRACKED FLOOR BEAM AT FS 589 DURING REMOVAL OF FLOOR BEAM CAP AT LBL9 (C-CHECK RO 7/18/2021) REMOVED AND REPLACED LBL9, FS589, BEAM WEB P/N 600-35031-307, BOMBARDIER ENG DWG 600-35031 REV Y BOMBARDIER REO 601R-53-61-3780 REV A DATED 2011-07-15 CO
- [SDR SWIA2021072159634](https://openairdocs.org/sdr/SWIA2021072159634.md): Skin · dented · May 17, 2021 · N878AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > * AFT CARGO DOOR DENTED ON UPPER EDGE (MARKED). (C-CHECK RO 7/18/2021) REPAIRED AFT CARGO DOOR AT UPPER EDGE REF REO 601R-52-31-353, REV--, DATED 2021-07-12. ALL OPS CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH ATTACHED TASK 51-900-1003-SKY
- [SDR SWIA2021072159633](https://openairdocs.org/sdr/SWIA2021072159633.md): Vane · gouged · May 15, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > * LH INBOARD FLAP. INBOARD VANE ACTUATOR HAS GOUGES IN SKIN ON THE OUTBOARD RIB, OUTBOARD SIDE (BEHIND PANEL 584AB) MARKED (C-CHECK RO 7/18/2021) BLEND WAS PERFORMED TO A SMOOTH CONTOUR, REMAINING THICKNESS IS NOT LESS THEN REPORTED, NO DEFECTS NOTED, R
- [SDR SWIA2021072159632](https://openairdocs.org/sdr/SWIA2021072159632.md): Floorbeam · cracked · May 15, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CLIP CRACKED OTBD OF RBL 9 AT FS 280 CROSSBEAM (C-CHECK RO 7/18/2021) REMOVED AND REPLACED OUTBD CLIP AT RBL 9 FS 280 CROSSBEAM REF. CRJ-200 SRM 51-42-21 AND REO 601R-53-11-926 REV -B DATED 2006/05/10 REFERENCE FOR FABRICATION OF CLIP AND FASTENER CAL
- [SDR SWIA2021072159631](https://openairdocs.org/sdr/SWIA2021072159631.md): Floorbeam · cracked · May 15, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CLIP CRACKED OTBD OF LBL9 AT FS280 CROSSBEAM (MARKED) (C-CHECK RO 7/18/2021) REMOVED AND REPLACED OUTBD CLIP OF LBL9 FS 280 CROSSBEAM REF. CRJ-200 SRM 51-42-21 AND REO 601R-53-11-926 REV -B DATED 2006/05/10 REFERENCE FOR FABRICATION OF CLIP AND FASTENE
- [SDR SWIA2021072159630](https://openairdocs.org/sdr/SWIA2021072159630.md): Skin · dented · May 15, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > L/H INBD FLAP - APROX WS 75 - SEVERAL DENTS ON BOTTOM FLAP SKIN BEHIND MLG OTBD TIRE (C-CHECK RO 7/18/2021) REPLACED L/H INBD FLAP SKIN WITH FABRICATED SKIN REF MHIRJ EO 601R14008 SNIEO S12 2021-06-14 AND EO 601R14002 SNIEO S23 2021-06-14, DWG 601R140
- [SDR SWIA2021072159673](https://openairdocs.org/sdr/SWIA2021072159673.md): Window Post · cracked · May 14, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Structure
  > * FLIGHT DECK WINDSHIELD STRUCTURE HAS POSSIBLE HAIR LINE CRACK ON LOWER CAPITAINS SIDE POST FITTING AREA IS MARKED WITH RED CHINA MARKER AN FLAGGED (C-CHECK RO 7/18/2021) INSTALLED NEW FLIGHT DECK WINDSHIELD LOWER CAPITAINS SIDE POST FITTING REF CRJ2
- [SDR SWIA2021072159662](https://openairdocs.org/sdr/SWIA2021072159662.md): Fastener · corroded · May 14, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > * LEFT WING I/B TRAILING EDGE HAS CORRODED FASTENERS AT APPROX W/S 139 ON BUMP STOP BRACKET (C-CHECK RO 7/18/2021) REMOVED AND REPLACED LH WING I/B TRAILING EDGE CORRODED FASTENERS AT APPROX W/S 139 ON BUMP STOP BRACKET. IAW CRJ 200 SRM 51-41-04. TUC55
- [SDR SWIA2021072159661](https://openairdocs.org/sdr/SWIA2021072159661.md): Fastener · corroded · May 14, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > * LEFT WING I/B TRAILING EDGE HAS CORRODED FASTENERS AT APPROX W/S 104 ON BUMP STOP BRACKET (C-CHECK RO 7/18/2021) REMOVED AND REPLACED LH WING I/B TRAILING EDGE CORRODED FASTENERS AT APPROX W/S 104 ON BUMP STOP BRACKET. IAW CRJ 200 SRM 51-41-04. TUC55
- [SDR SWIA2021072159660](https://openairdocs.org/sdr/SWIA2021072159660.md): Fastener · corroded · May 14, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBOARD TRAILING EDGE STOP ASSY @WS 56.30 HAVE CORRODED FASTENERS. MARKED (C-CHECK RO 7/18/2021) REMOVED CORRODED HARDWARE FROM RIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY NEW 1EA WASHER AND NEW 1EA NUT @WS56.30 REF CRJ200 SRM 51-41-02
- [SDR SWIA2021072159659](https://openairdocs.org/sdr/SWIA2021072159659.md): Nut · corroded · May 14, 2021 · N878AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > RIGHT WING INBOARD TRAILING EDGE @WS 98.009 & WS 104.00 HAS CORRODED CASTLE NUTS AT 2 LOCATIONS. MARKED (C-CHECK RO 7/18/2021) REMOVED RIGHT WING INBOARD TRAILING EDGE 2 CASTLE NUTS @WS 98.009 & WS 104.00 AND INSTALLED 2EA NEW CASTLE AND 2 NEW COTTER P
- [SDR SWIA2021072159658](https://openairdocs.org/sdr/SWIA2021072159658.md): Stop · corroded · May 14, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBOARD TRAILING EDGE STOP ASSY @WS 104.00 HAS CORRODED FASTENERS. MARKED (C-CHECK RO 7/18/2021) REMOVED AND REPLACED WITH NEW. NEW HARDWARE INCLUDES 2 FASTENERS AND 2 WASHERS. PER CRJ 200 AMM 51-41-02.
- [SDR SWIA2021072159657](https://openairdocs.org/sdr/SWIA2021072159657.md): Hinge Fitting · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY @ WS 139.924 STOP ASSY HAS CORRODED FASTENERS. MARKED (C-CHECK RO 7/18/2021) REMOVED CORRODED HARDWARE FROM RIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY AND INSTALLED NEW 1EA WASHER AND NEW 1EA NUT
- [SDR SWIA2021072159656](https://openairdocs.org/sdr/SWIA2021072159656.md): Hinge Fitting · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY @ WS 139.924 HAS A CORRODED CASTLE NUT. MARKED (C-CHECK RO 7/18/2021) REMOVED CORRODED HARDWARE FROM RIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY AND INSTALLED NEW HARDWARE 1EA NEW NUT AND1 NEW WASHER
- [SDR SWIA2021072159655](https://openairdocs.org/sdr/SWIA2021072159655.md): Seat Track · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *CORROSION SCRATCHES AND GOUGES NOTED ON FLOOR SEAT RAIL AT LBL9 AT APPROX. FS364.00-409.00 (MARKED) (C-CHECK RO 7/18/2021) INSTALLED NEW FLOOR SEAT RAIL AT LBL9 AT APPROX. FS364.00-409.00 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159654](https://openairdocs.org/sdr/SWIA2021072159654.md): Seat Track · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *CORROSION SCRATCHES AND GOUGES NOTED ON FLOOR SEAT RAIL AT RBL9 AT APPROX. FS364.00-399.00 (MARKED) (C-CHECK RO 7/18/2021) REMOVED CORROSION, SCRATCHES AND GOUGES ON FLOOR SEAT RAIL AT RBL9 FS364.00-FS399.0 REF. CRJ200 SRM 51-12-00 & CRJ200 SRM 51-21-0
- [SDR SWIA2021072159653](https://openairdocs.org/sdr/SWIA2021072159653.md): Seat Track · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *R/H SIDE SEAT RAIL HAS CORROSION, SCRATCHES AND GOUGES AT MULTIPLE SPOTS AT APPROX. FS544.00-FS559.00+80 (MARKED) (C-CHECK RO 7/18/2021) / INSTALLED NEW R/H SIDE SEAT RAIL FS544.00-FS559.00+80 REF CRJ-200 AMM 53-01--11-400-802
- [SDR SWIA2021072159652](https://openairdocs.org/sdr/SWIA2021072159652.md): Seat Track · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *R/H SIDE SEAT RAIL HAS CORROSION, SCRATCHES AND GOUGES AT MULTIPLE SPOTS AT APPROX. FS499.00-FS544.00 (MARKED) (C-CHECK RO 7/18/2021) INSTALLED NEW R/H SIDE SEAT RAIL FS499.00-FS544.00 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159651](https://openairdocs.org/sdr/SWIA2021072159651.md): Seat Track · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *R/H SIDE SEAT RAIL HAS CORROSION, SCRATCHES AND GOUGES AT MULTIPLE SPOT AT APPROX. FS409.00+112-FS449.85 (MARKED) (C-CHECK RO 7/18/2021) INSTALLED NEW R/H SIDE SEAT RAIL FS409.00+112-FS449.85 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159650](https://openairdocs.org/sdr/SWIA2021072159650.md): Seat Track · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSIONS,SCRATCHES AND GOUGES AT APPROX. FS544.00-FS559+80 (MARKED) (C-CHECK RO 7/18/2021) INSTALLED NEW L/H SIDE SEAT TRACK AT APPROX. FS544.00-FS559+80 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159649](https://openairdocs.org/sdr/SWIA2021072159649.md): Seat Track · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSIONS,SCRATCHES AND GOUGES AT APPROX. FS499.00-FS544.00 (MARKED) (C-CHECK RO 7/18/2021) INSTALLED NEW L/H SIDE SEAT RAIL FS499.00-FS544.00 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159629](https://openairdocs.org/sdr/SWIA2021072159629.md): Floorbeam · corroded · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *CORROSION NOTED ON FLOOR SUPPORT ANGLE FOR FLOOR PANEL #221ALF COMMON TO 280 CROSSBEAM FROM LBL9-RBL9 (C-CHECK RO 7/18/2021) REMOVED AND REPLACED CORRODED FLOOR SUPPORT ANGLE FOR FLOOR PANEL #221ALF COMMON TO FS 280 CROSSBEAM REF. CRJ-200 SRM 51-42-06
- [SDR SWIA2021072159628](https://openairdocs.org/sdr/SWIA2021072159628.md): Floorbeam · cracked · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CLIP CRACKED AT RBL 9 AT FS280 CROSS BEAM (MARKED) (C-CHECK RO 7/18/2021) REMOVED AND REPLACED INBD CLIP AT RBL 9 FS 280 CROSSBEAM REF. CRJ-200 SRM 51-42-21 AND REO 601R-53-11-926 REV -B DATED 2006/05/10 REFERENCE FOR FABRICATION OF CLIP AND FASTENER
- [SDR SWIA2021072159627](https://openairdocs.org/sdr/SWIA2021072159627.md): Floorbeam · cracked · May 13, 2021 · N878AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *CLIP CRACKED AT LBL9 AT FS280 CROSSBEAM (MARKED) (C-CHECK RO 7/18/2021) REMOVED AND REPLACED INBD CLIP AT LBL 9 FS 280 CROSSBEAM REF. CRJ-200 SRM 51-42-21 AND REO 601R-53-11-926 REV -B DATED 2006/05/10 REFERENCE FOR FABRICATION OF CLIP AND FASTENER C
- [SDR SWIA2021072159648](https://openairdocs.org/sdr/SWIA2021072159648.md): Seat Track · corroded · May 12, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSIONS,SCRATCHES AND GOUGES AT APPROX. FS449.85-FS499.00 (MARKED) (C-CHECK RO 7/18/2021) INSTALLED NEW L/H SIDE SEAT RAI FS449.85-FS499.00 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159647](https://openairdocs.org/sdr/SWIA2021072159647.md): Seat Track · corroded · May 12, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSIONS,SCRATCHES AND GOUGES AT APPROX. FS409.00+112-FS449.85 (MARKED) (C-CHECK RO 7/18/2021) INSTALLED NEW L/H SIDE SEAT RAIL FS409.00+112-FS449.85 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159646](https://openairdocs.org/sdr/SWIA2021072159646.md): Seat Track · corroded · May 12, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION,SCRATCHES AND GOUGES AT APPROX. FS409.00+16-FS409.00+112 (MARKED) (C-CHECK RO 7/18/2021) SEAT TRACK WAS FOUND TO BE OUT OF LIMITS, INSTALLED NEW L/H SIDE SEAT RAIL FS409.00+16-FS409.00+112 REF CRJ-200
- [SDR SWIA2021072159645](https://openairdocs.org/sdr/SWIA2021072159645.md): Seat Track · corroded · May 12, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION,SCRATCHES AND GOUGES AT APPROX. FS364.00-FS409.00+16 (MARKED) (C-CHECK RO 7/18/2021) REMOVED AND REPLACED L/H SIDE RAIL FROM FS364.00-FS409.00+16 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159644](https://openairdocs.org/sdr/SWIA2021072159644.md): Seat Track · corroded · May 12, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *MULTIPLE SPOTS OF CORROSION NOTED ON R/H SIDE SEAT RAIL AT APPROX. FS364.00--FS409.00+16 (MARKED) (C-CHECK RO 7/18/2021) INSTALLED NEW R/H SIDE SEAT RAIL AT APPROX FS364.00--FS409.00+16 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159643](https://openairdocs.org/sdr/SWIA2021072159643.md): Seat Track · corroded · May 12, 2021 · N878AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *MULTIPLE SPOTS OF CORROSION NOTED ON R/H SIDE SEAT RAIL AT APPROX. 409.00+16-409.00+112 (MARKED) (C-CHECK RO 7/18/2021) REMOVE OLD SIDE SEAT RAIL AND INSTALLED NEW R/H SIDE SEAT RAIL AT APPROX. 409.00+16-409.00+112 REF CRJ-200 AMM 53-01-11-400-802
- [SDR SWIA2021072159642](https://openairdocs.org/sdr/SWIA2021072159642.md): Intercostal · cracked · May 12, 2021 · N878AS · Cndair CL6002B19 · Aerodynamic Fairings
  > *LEFT HAND WING TO BODY FAIRING SUPPORT STRUCTURE ON INTERCOSTAL IS CRACKED FS449.85. (MARKED & FLAGGED) (C-CHECK RO 7/18/2021) INSTALLED NEW SUPPORT ANGLE REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, CRJ200 SRM 51-45-00 AND DWG 601R-31037 REV. F
- [SDR SWIA2021072159641](https://openairdocs.org/sdr/SWIA2021072159641.md): Support · cracked · May 12, 2021 · N878AS · Cndair CL6002B19 · Aerodynamic Fairings
  > *RIGHT HAND WING TO BODY FAIRING SUPPORT STRUCTURE ON INTERCOSTAL IS CRACKED JUST FORWARD OF FS473.15. (MARKED & FLAGGED) (C-CHECK RO 7/18/2021) INSTALLED NEW SUPPORT ANGLE REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13, CRJ200 SRM 51-45-00 AND DWG 601R-

Next page: https://openairdocs.org/aircraft/N878AS/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 = 'N878AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N878AS/reports

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