# Service difficulty reports: N877AS

A list on [N877AS](https://openairdocs.org/aircraft/N877AS.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 · 292 reports

- [SDR SWIA2025060000001](https://openairdocs.org/sdr/SWIA2025060000001.md): Cabin Pressure · warning message · Jun 1, 2025 · N877AS · Cndair CL6002B19 · Cabin Pressure Control System
  > CABIN ALT WARNING MESSAGE POPPED UP AND BOTH PILOTS GOT ON O2. COMPLIED WITH PROCEDURES (MEMORY ITEMS, QRC, QRH.) LANDED UNEVENTFUL. (FLIGHT 5956 - FILED CLOSED)CLEANED AND STOWED BOTH PILOT AND COPILOT O2 MASKS, CREW O2 PRESSURE OKAY FOR DISPATCH
- [SDR SWIA2025065000001](https://openairdocs.org/sdr/SWIA2025065000001.md): Acm · faulted · Jun 1, 2025 · N877AS · Cndair CL6002B19 · Cabin Cooling System
  > LH PACK HI TEMP MSG POPPED UP AND DISAPPEARED FROM CAS CLIMBING THROUGH FL180. CA CHECKED ECS PAGE AND NOTICED LEFT PACK WAS NO LONGER BEING SUPPLIED 10TH STAGE BLEED AIR. WE LEVELED OFF CABIN ALT CAUTION MESSAGE POPPED UP AND CA NOTICED CABIN ALT SLOWLY CLIMB
- [SDR SWIA20250601](https://openairdocs.org/sdr/SWIA20250601.md): Oxygen Mask · deployed · Jun 1, 2025 · N877AS · Cndair CL6002B19 · Passenger Oxygen System
  > PAX OXY DEPLOYED. DEFERRED ALL PASSENGER O2 MASKS IN CABIN INCLUDING FA AFTER BEING DISCHARGED IN FLIGHT PER 35-20-1A. NO MX REQUIRED. (FA MASK IS USED AND STOWED FOR ACCESS TO FLIGHT DECK). PLACARD INSTALLED
- [SDR SWIA20250527014](https://openairdocs.org/sdr/SWIA20250527014.md): Door · out of alignment · May 14, 2025 · N877AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR RESTRAINT NETTING AFT FITTING PLATE NOT ALIGNING WITH THE FLOOR BOARD PANEL. (FILED CLOSED)REMOVED AND REINSTALLED CARGO DOOR RESTRAINT NETTING AFT FITTING PLATE SO THAT IT ALIGNS WITH THE FLOOR BOARD PANEL WITH REFERENCE TO SRM 51-42-06 AND SRM 5
- [SDR SWIA202505270005](https://openairdocs.org/sdr/SWIA202505270005.md): Floor Panel · dented · May 5, 2025 · N877AS · Cndair CL6002B19 · Fuselage Floor Panel
  > DENT TO PRESSURE FLOOR SILL / PANEL ASSEMBLY LOCATED APPROXIMATELY FS 542.00 AND RBL 45.00 (FILED CLOSED)COMPLIED WITH REO 601R-53-41-3313 DATED: 2025-05-11 REV: -- REPAIR FOR DENT WITH BLEND TO PRESSURE FLOOR SILL PANEL BETWEEN FS540.25-FS544.00 AND RBL36.00
- [SDR SWI2025F00667](https://openairdocs.org/sdr/SWI2025F00667.md): Pressure Deck · corroded · Apr 20, 2025 · N877AS · Cndair CL6002B19 · Fuselage Main, Structure
  > LH PRESSURE FLOOR HAS SEVERAL SPOTS OF SURFACE CORROSION BETWEEN FS461.00 TO FS513.00 ON LBL44.00. (FILED CLOSED)BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL ASSY BETWEEN FS461.00 TO FS513.00 ON LBL44.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAIN
- [SDR SWI2025F00666](https://openairdocs.org/sdr/SWI2025F00666.md): Floor Support · corroded · Apr 20, 2025 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL BETWEEN FS 529.00 TO FS 544.00 AND RBL 44.00 HAS SURFACE CORROSION. (FILED CLOSED)BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL ASSY BETWEEN FS 529.00 TO FS 544.00 AND RBL 44.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING
- [SDR SWIA202505270420](https://openairdocs.org/sdr/SWIA202505270420.md): Fitting · corroded · Apr 20, 2025 · N877AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR RESTRAINT NETTING AFT FITTING PLATE HAS SURFACE CORROSION. (FILED CLOSED)REMOVED AND REPLACED CARGO DOOR RESTRATINT NETTING AFT FITTING PLATE WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-33
- [SDR SWIA202264903](https://openairdocs.org/sdr/SWIA202264903.md): None · failed · Feb 18, 2022 · N877AS · Cndair CL6002B19 · Horizontal Stabilizer, Attach Fittings
  > DURING INSTALL OF HORIZONTAL STABILIZER INSUFFICIENT CLEARANCE WAS FOUND ON RH SIDE OF STEADY T FITTING AND SLIDER BLOCKS. ALLOWABLE CLEARANCE IS 0.005" - 0.017". MEASURED 0.000" CLEARANCE. REF TASK CARD 55-300-1000-SKY STEP 4. D. (5) AND FIGURE 403 SHEET 2.
- [SDR SWIA202264902](https://openairdocs.org/sdr/SWIA202264902.md): None · corroded · Feb 15, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/H PRESSURE FLOOR SILL HAS AREAS OF CORROSION AT F.S. 519.00 AND 522.00. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3008 REV.--, DATED 2022-01-26 AND MHIRJ REO
- [SDR SWIA202264901](https://openairdocs.org/sdr/SWIA202264901.md): None · corroded · Feb 15, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION AT F.S. 501.00 AND F.S. 507.00. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3008 REV.--, DATED 2022-01-26 AN
- [SDR SWIA202264900](https://openairdocs.org/sdr/SWIA202264900.md): None · corroded · Feb 14, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION BETWEEN F.S. 524.00 AND 544.00. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012/11/06, MHIRJ REO 601R-53-41-3006 REV.--, DATED 2022/02/26 AN
- [SDR SWIA202264899](https://openairdocs.org/sdr/SWIA202264899.md): None · corroded · Feb 14, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > L/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION BETWEEN F.S. 439.00 AND 449.85. (C CHECK RO 3/11/2022) REPAIRED L/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3010 REV.--, DATED 2022-01-26 AN
- [SDR SWIA202264898](https://openairdocs.org/sdr/SWIA202264898.md): None · corroded · Feb 14, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > L/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION BETWEEN F.S. 424.00 AND F.S. 439.00 (C CHECK RO 3/11/2022).REPAIRED L/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3010 REV.--, DATED 2022-01-
- [SDR SWIA202264971](https://openairdocs.org/sdr/SWIA202264971.md): None · corroded · Feb 1, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CROSSBEAM ATTACH FITTING AT F.S. 349 LBL42 CORRODED! (C CHECK RO 3/11/2022) REMOVED AND REPLACED CROSSBEAM ATTACH FITTING AT F.S 349 LBL 42 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.
- [SDR SWIA202264970](https://openairdocs.org/sdr/SWIA202264970.md): None · cracked · Jan 24, 2022 · N877AS · Cndair CL6002B19 · Doors
  > FOUND PAX DOOR AFT WEB DRAG ANGLE TO BE CRACKED IN PREVIOUS REPAIR AREA. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR AFT WEB DRAG ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-13
- [SDR SWIA202264897](https://openairdocs.org/sdr/SWIA202264897.md): None · corroded · Jan 24, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > F.S. 280 CROSSBEAM WEB CORRODED. (C CHECK RO 3/11/2022) REMOVED OLD AND INSTALLED NEW SERVICEABLE F.S. 280 CROSSBEAM WEB IAW SRM 51-42-06 REV 38B DATED 25 NOV 2020 AND SRM 51-40-11 REV 38B DATED 25 NOV 2020. BOMBARDIAR REO 601R-53-11-993REV-- DATED 11 APR
- [SDR SWIA202264949](https://openairdocs.org/sdr/SWIA202264949.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)
  > F.S.280 J ANGLE IS CORRODED BETWEEN LBL 11 AND RBL 11 (C CHECK RO 3/11/2022) REMOVED OLD AND DRILLED UP/INSTALLED NEW SERVICEABLE F.S. 280 J-ANGLEIAW CRJ200 SRM 51-40-11 AND 51-42-06, REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
- [SDR SWIA202264946](https://openairdocs.org/sdr/SWIA202264946.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK SEGMENT RBL 9 BETWEEN F.S.364 TO F.S.399 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED SEAT TRACK AT RBL 9 FROM F.S. 364.00 - F.S. 399.00 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202264944](https://openairdocs.org/sdr/SWIA202264944.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK SEGMENT LBL 9 BETWEEN F.S.364 TO F.S.399 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED SEAT TRACK SEGMENT LBL 9 F.S. 364.00 - 399.00 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202264896](https://openairdocs.org/sdr/SWIA202264896.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S.349 FLOOR BEAM UPPER FLANGE IS CORRODED AT APPROX. RBL 42 (C CHECK RO 3/11/2022) REMOVED DAMAGED SECTION OF FLOOR BEAM AT FS 349 AND INSTALLED A NEW SECTION IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-42-13 REV.38B, DATED 11/25/2020 WITH REO 601R-53-21-
- [SDR SWIA202264895](https://openairdocs.org/sdr/SWIA202264895.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Doors
  > ANGLE IS CORRODED ATTACHING TO SERVICE DOOR SILL CAP ANGLE AT APPROX. F.S.319 (C CHECK RO 3/11/2022) REMOVED AND REPLACED ANGLE ATTACHING TO SERVICE DOOR SILL CAP ANGLE AT F.S. 319.00 IAW CRJ-200 SRM 51-42-21 AND 51-40-11. REF ATTACHED CONTINUATION FOR WOR
- [SDR SWIA202264893](https://openairdocs.org/sdr/SWIA202264893.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > F.S.280 LOWER WEB DOUBLER AT APPROX. RBL 12 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED OLD AND INSTALLED NEW SERVICABLE F.S.280 LOWER WEB DOUBLER AT APPROX. RBL 12 IAW SRM 51-42-06 REV 38B DATED 25 NOV 2020 AND SRM 51-40-11 REV 38B DATED 25 NOV 2020. BOMB
- [SDR SWIA202264889](https://openairdocs.org/sdr/SWIA202264889.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > F.S.280 LOWER WEB DOUBLER AT APPROX.LBL 12 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED OLD AND INSTALLED NEW SERVICEABLE F.S. 280 LOWER DOUBLER AT LBL 12 IAW CRJ200 SRM 51-40-11 AND 51-42-06 REV 38B 25 NOV 2020,BOMBARDIAR REO 601R-53-11-991 REV -- DATED 0
- [SDR SWIA202264887](https://openairdocs.org/sdr/SWIA202264887.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S.280 CROSSBEAM UPPER FLANGE IS CORRODED BETWEEN RBL 9 AND LBL18 (C CHECK RO 3/11/2022) REMOVED OLD DAMAGED AND LOCATED, DRILLED AND SHOT NEWFS 280 CROSS BEAM UPPER FLANGE BETWEEN RBL9 AND RBL 8 IAW SRM 51-42-06 AND SRM 51-40-11 REV 38 B DATED 25 NOV 20
- [SDR SWIA202264885](https://openairdocs.org/sdr/SWIA202264885.md): None · corroded · Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S.349 FLOOR BEAM UPPER FLANGE IS CORRODED AT APPROX. LBL 42. (C CHECK RO 3/11/2022) FS 349.00 CROSSBEAM REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 601R-53-21-3524 REV -- DATED 2022-02-24 WITH NEGLIGABLE CHANGE TO WEIGHT AND BALANCE, M-337 AND TASK CARD 51-900
- [SDR SWIA202264883](https://openairdocs.org/sdr/SWIA202264883.md): None · cracked · Jan 11, 2022 · N877AS · Cndair CL6002B19 · Doors
  > AFTER THE REMOVAL OF THE PAX DOOR INNER SKIN FOUND AFT INTERCOSTAL DD7 TO BE CRACKED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED THE PAX DOOR DD7 AFT INTERCOSTAL IAW CRJ-200 SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO W
- [SDR SWIA202264881](https://openairdocs.org/sdr/SWIA202264881.md): None · cracked · Jan 11, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, Keel
  > STRINGER 3L IS CRACKED BETWEEN F.S. 364.00 AND 379.00. (C CHECK RO 3/11/2022) REMOVED DAMAGED SECTION OF CRACKED STRINGER, FABRICATED REPLACEMENT STRINGER SECTION AND INSTALLED IAW CRJ 200 SRM 53-00-03. REF CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202264941](https://openairdocs.org/sdr/SWIA202264941.md): None · cracked · Jan 10, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)
  > OBLIQUE ANGLES BETWEEN F.S. 621.00 AND F.S. 625.00, STRINGER 14L AND STRINGER 14R ARE CRACKED. (C CHECK RO 3/11/2022) REPLACE WITH NEW 2 EA OBLIQUE ANGLES BETWEEN F.S. 621.00 AND F.S. 625.00 ON STRINGER 14L AND 14R. ALL NEW HARDWARE INSTALLED. NEW OBLIQUE
- [SDR SWIA202264976](https://openairdocs.org/sdr/SWIA202264976.md): None · corroded · Jan 8, 2022 · N877AS · Cndair CL6002B19 · Aileron Tabs
  > FOUND 2EA. BOLTS AND ALL NUTS TO BE UNSERVICEABLE AT W.S. 178.00, 220.00 AND 264.00 REQUIRE REPLACEMENT. (C CHECK RO 3/11/2022) REMOVED AND REPLACED ALL UNSERVICEABLE LH OB FLAP HINGE BOX HARDWARE AT W.S. 178, W.S. 220, AND W.S. 264.00 IAW CRJ-200 AMM 57-2
- [SDR SWIA202264969](https://openairdocs.org/sdr/SWIA202264969.md): None · corroded · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Elevator, Plate/Skin
  > LH ELEVATOR HINGE MOUNTING HARDWARE IS CORRODED AT ALL 4 ATTACH POINTS. NEED TO REMOVE AND REPLACE HINGE HARDWARE. (C CHECK RO 3/11/2022) REMOVED AND REPLACED ALL CORRODED HARDWARE FOR THE LEFT ELEVATOR AT THE 4 ATTACH HINGE POINTS IW CRJ200 AMM 27-34-01-
- [SDR SWIA202264968](https://openairdocs.org/sdr/SWIA202264968.md): None · corroded · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Elevator, Plate/Skin
  > RH ELEVATOR HINGE MOUTING HARDWARE IS CORRODED AT ALL 4 ATTACH POINTS, NEED TO REMOVE AND REPLACE ALL HINGE HARDWARE. (C CHECK RO 3/11/2022) RECEIVED NEW SERVICEABLE HARDWARE FOR RIGHT ELEVATOR HINGE MOUNTING POINTS. REFERENCE CUSTOMER # 7579721, JOB 97579
- [SDR SWIA202264967](https://openairdocs.org/sdr/SWIA202264967.md): None · corroded · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > PASSENGER DOOR AFT FIXED STAIR PANEL IS CORRODED AROUND FASTENERS IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR AFT WEB IAW CRJ 200 SRM 51-42-13.
- [SDR SWIA202264966](https://openairdocs.org/sdr/SWIA202264966.md): None · corroded · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > PASSENGER DOOR FWD FIXED STAIR PANEL IS CORRODED AROUND FASTENERS IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR FWD WEB IAW CRJ 200 SRM 51-42-13.
- [SDR SWIA202264879](https://openairdocs.org/sdr/SWIA202264879.md): None · cracked · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, Frame
  > LEFT WINDSHIELD LOWER OB SIDEPOST FITTING IS CRACKED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LEFT WINDSHIELD LOWER O/B SIDEPOST FITTING IAW CRJ200 SRM 51-40-11 AND 51-42-21.
- [SDR SWIA202264878](https://openairdocs.org/sdr/SWIA202264878.md): None · corroded · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)
  > LH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED THE LH OVERWING EXIT INTERCOSTAL IAW CRJ-200 SRM 51-42-06. LEAK CHECK IS GOOD AT THIS TIME. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED. NO CH
- [SDR SWIA202264876](https://openairdocs.org/sdr/SWIA202264876.md): None · corroded · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)
  > RH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IS CORRODED (C CHECK RO 3/11/2022) REPLACED RH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06 REV 38B DATED 11/25/2020, COMPLIED WITH 51-900-1003-SKY, NO CHANGE TO WEIGHT AND BALANCE. RE
- [SDR SWIA202264874](https://openairdocs.org/sdr/SWIA202264874.md): None · corroded · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Doors
  > PASSENGER DOOR SILL ANGLE CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE IAW CRJ-200 SRM 51-42-21, 51-40-11, 51-42-06 AND 51-42-13. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE. REF AT
- [SDR SWIA202264872](https://openairdocs.org/sdr/SWIA202264872.md): None · gouged · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)
  > PASSENGER DOOR OUTER SKIN GOUGED ON LOWER FWD EDGE. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR FWD SEAL RETAINER IAW CRJ-200 SRM 51-42-13 AND 51-42-06. COMPLETED FORM M-337 AND TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REF ATTAC
- [SDR SWIA202264870](https://openairdocs.org/sdr/SWIA202264870.md): None · corroded · Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > TOP OF FLOOR BEAM AT LBL9 FROM FS 409.00 TO FS 409.00+120 IS CORRODED IN MULITPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED CORRODED FLOOR BEAM AT LBL9 F.S.409.00 - 409+120 AND INSTALLED NEW SERVICEABLE FLOOR BEAM IAW CRJ-200 SRM 51-42-21, 51-42-22, 51-42-
- [SDR SWIA202264939](https://openairdocs.org/sdr/SWIA202264939.md): None · corroded · Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > FLOOR SEAT TRACK AT RBL9 FROM FS 559.00 TO FS 559.00+80 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED FLOOR SEAT TRACK RBL 9 F.S. 559.00 - 559+80 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202264935](https://openairdocs.org/sdr/SWIA202264935.md): None · corroded · Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > FLOOR SEAT TRACK AT LBL9 FROM FS 559.00 TO FS 559.00+80 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED DAMAGED SEAT TRACK AT LBL 9 FROM FS 559.00 TO 559.00+80 AND INSTALLED A NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802
- [SDR SWIA202264868](https://openairdocs.org/sdr/SWIA202264868.md): None · gouged · Jan 5, 2022 · N877AS · Cndair CL6002B19 · Wing Structure
  > RH AILERON #2 HINGE FITTING AT WS319 AFT WING SPAR IS GOUGED. (C CHECK RO 3/11/2022) REPAIRED RH AILERON #2 HINGE FITTING AT WS319 AFT WING SPAR IAW MHIRJ REO 601R-57-51-984, REV --, DATE: 2022-01-28, SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED. M-33
- [SDR SWIA202264866](https://openairdocs.org/sdr/SWIA202264866.md): None · gouged · Jan 5, 2022 · N877AS · Cndair CL6002B19 · Wing Structure
  > LH AILERON #3 HINGE FITTING AT WS323 AFT WING SPAR IS GOUGED. (C CHECK RO 3/11/2022) REPAIRED LH AILERON HINGE #3 FITTING AT W.S.323.00 AFT SPAR IAW MHIRJ REO 601R-57-51-985 REV - - DATED 2022-01-31. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO C
- [SDR SWIA202264864](https://openairdocs.org/sdr/SWIA202264864.md): None · corroded · Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > TOP OF PRESSURE FLOOR BEAM AT RBL9 FROM FS 559.00 TO FS 559.00+48 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005. REMOVED DAMAGED FLOOR BEAM AND INSTALLED A NEW FLOOR BEAM IA
- [SDR SWIA202264862](https://openairdocs.org/sdr/SWIA202264862.md): None · corroded · Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > TOP OF PRESSURE FLOOR BEAM AT RBL9 FROM FS 409.00+120 TO FS 461.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED PRESSURE FLOOR BEAM AT RBL 9.00 FROM F.S. 409.00+120 TO F.S. 461.00 I.A.W. MHIRJ REO 601R-53-41-3001 REV.A, DATED 2022-01-
- [SDR SWIA202264860](https://openairdocs.org/sdr/SWIA202264860.md): None · corroded · Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > TOP OF PRESSURE FLOOR BEAM AT LBL9 FROM 409.00+120 TO FS 461.00 IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED PRESSURE FLOOR BEAM AT LBL 9.00 FROM 409.00+120 TO F.S. 461.00 I.A.W. MHIRJ REO 601R-53-41-3002 REV.A, DATED 2022-01-25. COMPLIED WITH SK
- [SDR SWIA202264858](https://openairdocs.org/sdr/SWIA202264858.md): None · corroded · Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RH FLOOR SILL FROM FS 559.00 TO FS 559.00+32 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED FLOOR SILL I.A.W. BOMBARDIER CRJ200 SRM 51-42-06 AND 51-42-21 REV.38B, DATED 11/25/2020. COMPLIED WITH SKYWEST TASK CARD 51-900-1003
- [SDR SWIA202264978](https://openairdocs.org/sdr/SWIA202264978.md): None · corroded · Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LH PRESSURE FLOOR SILL PANEL FROM FS 484.00 TO FS 529.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED L/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-301 REV.--, DATED 2022-01
- [SDR SWIA202264856](https://openairdocs.org/sdr/SWIA202264856.md): None · corroded · Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RH PRESSURE FLOOR SILL PANEL FROM FS 529.00 TO FS 559.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL PANEL FROM F.S. 529.00 TO F.S. 559.00 I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ R

Next page: https://openairdocs.org/aircraft/N877AS/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 = 'N877AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N877AS/reports

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