N877AS

Service difficulty reports · 292

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Query with SQL
duckdb -csv -c "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'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2025060000001Cabin Pressure · warning messageCABIN 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 DISPATCHJun 1, 2025 · N877AS · Cndair CL6002B19 · Cabin Pressure Control SystemSDR SWIA2025065000001Acm · faultedLH 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 CLIMBJun 1, 2025 · N877AS · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA20250601Oxygen Mask · deployedPAX 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 INSTALLEDJun 1, 2025 · N877AS · Cndair CL6002B19 · Passenger Oxygen SystemSDR SWIA20250527014Door · out of alignmentCARGO 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 5May 14, 2025 · N877AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202505270005Floor Panel · dentedDENT 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 RBL36.00May 5, 2025 · N877AS · Cndair CL6002B19 · Fuselage Floor PanelSDR SWI2025F00667Pressure Deck · corrodedLH 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 REMAINApr 20, 2025 · N877AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2025F00666Floor Support · corrodedRH 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 Apr 20, 2025 · N877AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202505270420Fitting · corrodedCARGO 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-33Apr 20, 2025 · N877AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202264903None · failedDURING 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. Feb 18, 2022 · N877AS · Cndair CL6002B19 · Horizontal Stabilizer, Attach FittingsSDR SWIA202264902None · corrodedR/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 REOFeb 15, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264901None · corrodedR/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 ANFeb 15, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264900None · corrodedR/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 ANFeb 14, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264899None · corrodedL/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 ANFeb 14, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264898None · corrodedL/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-Feb 14, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264971None · corrodedCROSSBEAM 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.Feb 1, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202264970None · crackedFOUND 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 51-42-13Jan 24, 2022 · N877AS · Cndair CL6002B19 · DoorsSDR SWIA202264897None · corrodedF.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 APRJan 24, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202264949None · corrodedF.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 PERFORMEDJan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202264946None · corrodedSEAT 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.Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202264944None · corrodedSEAT 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.Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202264896None · corrodedF.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-Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202264895None · corrodedANGLE 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 WORJan 13, 2022 · N877AS · Cndair CL6002B19 · DoorsSDR SWIA202264893None · corrodedF.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. BOMBJan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202264889None · corrodedF.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 0Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202264887None · corrodedF.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 20Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202264885None · corrodedF.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 51-900Jan 13, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202264883None · crackedAFTER 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 WJan 11, 2022 · N877AS · Cndair CL6002B19 · DoorsSDR SWIA202264881None · crackedSTRINGER 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.Jan 11, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA202264941None · crackedOBLIQUE 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 Jan 10, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202264976None · corrodedFOUND 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 57-2Jan 8, 2022 · N877AS · Cndair CL6002B19 · Aileron TabsSDR SWIA202264969None · corrodedLH 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-Jan 6, 2022 · N877AS · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA202264968None · corrodedRH 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 97579Jan 6, 2022 · N877AS · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA202264967None · corrodedPASSENGER 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.Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202264966None · corrodedPASSENGER 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.Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202264879None · crackedLEFT 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.Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202264878None · corrodedLH 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 CHJan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202264876None · corrodedRH 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. REJan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202264874None · corrodedPASSENGER 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 ATJan 6, 2022 · N877AS · Cndair CL6002B19 · DoorsSDR SWIA202264872None · gougedPASSENGER 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 ATTACJan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202264870None · corrodedTOP 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-Jan 6, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264939None · corrodedFLOOR 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.Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202264935None · corrodedFLOOR 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 53-01-11-400-802Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202264868None · gougedRH 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-33Jan 5, 2022 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202264866None · gougedLH 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 CJan 5, 2022 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202264864None · corrodedTOP 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 IAJan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264862None · corrodedTOP 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-Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264860None · corrodedTOP 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 SKJan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264858None · corrodedRH 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 51-900-1003Jan 5, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264978None · corrodedLH 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 2022-01Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264856None · corrodedRH 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 RJan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
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