N854AS

Service difficulty reports · 270

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 = 'N854AS' AND registry_match = 'registration'
  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 SWIA2024021900011Engine · damagedAFTER TAKEOFF DURING CLIMBOUT RECEIVED R FIRE FAIL CAUTION MESSAGE. SHORTLY AFTER THAT, RECEIVED R ENG FIRE WARNING MESSAGE WITH THE FIRE PUSH ILLUMINATED. NO LOSS OF ENGINE POWER, ITT WAS NORMAL. CHECKED SYNOPTIC PAGES, HYDRAULIC PUMP 2A WAS RED. BY THE TIME Feb 11, 2024 · N854AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2024021200001Fire Warning · illuminatedAFTER TAKEOFF DURING CLIMBOUT RECEIVED R FIRE FAIL CAUTION MESSAGE. SHORTLY AFTER THAT, RECEIVED R ENG FIRE WARNING MESSAGE WITH THE FIRE PUSH ILLUMINATED. NO LOSS OF ENGINE POWER, ITT WAS NORMAL. CHECKED SYNOPTIC PAGES, HYDRAULIC PUMP 2A WAS RED. BY THE TIME Feb 11, 2024 · N854AS · Cndair CL6002B19 · Fire DetectionSDR SWIA20230907831Unknown · dentedTRANSFER FROM EAML 1202516 : -1 AREA OF DENT DAMAGE TO EXISTING DOUBLERS REPAIR (GREO601R-53-21-180, REF) ON SKIN PANEL (DWG: 601R31062, REF) LOCATED BETWEEN STR 15 €“ STR 16 AND AT FS310.00. DENT AFFECTS ENTIRE STACKUP OF REPAIR AND MEASURES 0.5€? (L) X 0.2Aug 31, 2023 · N854AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202266457None · smokePAX IN 11D SAW WHITE/GREY SMOKE COMING FROM SIDE WALL/FLOOR ON T/O WAS NOT REPORTED UNTIL JUST PRIOR TO LANDING. A FEW PAX AROUND THE AREA ALSO SMELLED ODOR BUT DID NOT SEE SMOKE (FLIGHT #5122 FILED CLOSED) PERFORMED AN OPERATIONAL CHECK OF THE AIR CONDITIOSep 12, 2022 · N854AS · Cndair CL6002B19 · Air Conditioning SystemSDR SWIA202265047None · bentAFT RIB ON THE LH INBOARD FLAP IS BENT AT PREVIOUS SKIN REPAIR (MARKED) (C-CHECK RO 3/14/2022) REMOVED PREVIOUS SKIN REPAIR AND REPLACED WITH NEW DOUBLER, FILLER AND ANGLE REF CRJ200 SRM 57-52-00 REPAIR NO. 3 / COMPLIED WITH TASK CARD 51-900-1003-SKYFeb 4, 2022 · N854AS · Cndair CL6002B19 · AileronsSDR SWIA202265046None · cracked: DURING FLOOR SUPPORT ANGLE REMOVAL FROM FLOOR BEAM AT FS280, LBL9-RBL9, IT WAS FOUND FLOOR BEAM VERTICAL ATTACH ANGLE CRACKED AT FS280.00, LBL9 (C-CHECK RO 3/14/2022) REMOVED DAMAGED FLOOR BEAM VERTICAL ATTACH ANGLE AT FS280.00, LBL9 AND REPLACED BY A Feb 4, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265045None · elongatedENLOGATED HOLE ON FLANGE ANGLE ON RIGHTHAND HORIZONTAL TIP (C-CHECK RO 3/14/2022) REMOVED AND REPLACED RIGHTHAND HORIZONTAL TIP UPPER FLANGE ANGLE IAW CRJ 200 SRM 51-42-06 / CRJ SRM 51-42-15 AND DRAWING # 601R23037 REV -B. (SEE CONTINUATION SHEET FOR FURJan 29, 2022 · N854AS · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous StructureSDR SWIA202265044None · gougedIN MAIN CABIN AT CABIN AT FS319.00 AT STRINGER8R BRACKET HAS GOUGES (C-CHECK RO 3/14/2022) REMOVED GOUGES ON BRACKET IN MAIN CABIN AT FS319.00 AT STRINGER8R IAW CRJ 200 SRM 51-12-00 / EVALUATED BRACKET IN MAIN CABIN AT FS319.00 AT STGR8R FOUND TO BE OUTJan 27, 2022 · N854AS · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA202265043None · crackedCOPILOTS WIDOW SIDE POST THE LOWER FITTING IS CRACKED (MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED CO PILOTS WINDOW SIDE POST LOWER ATTACH FITTING P/N 601R33235-4. INSTALLED REF BOMBARDIER DWG 601R33007 REV -U AND CRJ 200 SRM 51-42-21. COMPLIED Jan 26, 2022 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265042None · crackedCOMPLY WITH AD 2008-06-10/04 REPAIR OF CRACKS IN FRAME REINFORCEMENT DOUBLER ONLY DUE BEFORE FURTHER FLIGHT. (C-CHECK RO 3/14/2022) COMPLIED WITH PARAGRAPH (H)(2) OF THIS AD FOR ANY CRACK FOUND IN THE FRAME REINFORCEMENT DOUBLER ONLY, BY DOING THE FRAMEJan 25, 2022 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202265041None · corroded*RIGHT WING LOWER WING PLANK ACCESS HOLE 650BB HAS COROSION. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM RIGHT WING LOWER WING PLANK AROUND THE MATING SURFACE OF WING PANEL 650BB REF BOMBARDIER REO 601R-57-21-030 REV -L DATED 2014-02-05. EVALUATED ANDJan 18, 2022 · N854AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202265093None · gougedCENTER HINGE FITTINGS FOR THE RH AILERON HAS GOUGES (MARKED) (C-CHECK RO 3/14/2022) BLENDED RH AILERON CENTER HINGE FITTINGS TO A SMOOTH CONTOUR. REF: CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS REF REF CRJ 200 SRM 57-51-14 FIGURE 101.RECIEVED REO 601Jan 17, 2022 · N854AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265088None · corroded*IN MAIN CABIN, ON INTERCOSTAL BETWEEN FRAME FS349 AND FS364, AND BETWEEN STR17L AND STR16L, SIDEWALL SUPPORT BRACKET IS CORRODED. (MARKED) (C-CHECK RO 3/14/2022) FOUND SIDEWALL SUPPORT BRACKET BETWEEN FS 349 AND FS 364 AND BETWEEN STR 17L AND 16L OUT OJan 13, 2022 · N854AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202265087None · corroded*IN MAIN CABIN, AT FS349 NEAR STR15L, SIDE SEAT BRACKET CORRODED. (MARKED) (C-CHECK RO 3/14/2022) FOUND CORROSION ON BRACKET AT FS 349 NEAR STR 15L OUT OF LIMITS REF CRJ 200 SRM 53-00-00 AND INSTALLED NEW BRACKET REF CRJ 200 SRM 51-42-06.Jan 13, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265074None · corroded*RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS449.85 THRU FS499.00 HAS PITTING AND CORRODED AROUND SCREWS. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON R/H SIDE SEAT RAIL BETWEEN FS449.85 TO FS499.00 . REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REF:Jan 13, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265073None · corroded*IN MAIN CABIN, AT FS349 NEAR STR15L INTERCOSTAL, TIE AT INTERCOSTAL TO FRAME IS CORRODED. (MARKED) (C-CHECK RO 3/14/2022) FOUND CORROSION AT FS 349 NEAR STR 15L GUSSET TIE OUT OF LIMITS REF CRJ 200 SRM 53-00-00 USING DIGITAL CALIPARS TUC 9393 CAL DUE 31Jan 13, 2022 · N854AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202265072None · crackedSTIFFENER ON LWR LH AFT FS621.0 BULKHEAD CRACKED (MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED STIFFENER ON LWR LH AFT FS621.0 BULKHEAD WITH NEW P/N 601R36008-51 REF CRJ200 SRM 51-42-06Jan 12, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202265091None · chafed*PASSENGER DOOR, AT UPPER END OF DOOR, AT AFT EDGE OF FWD DOOR CAP, CHAFING ON STRUCTURE AND FASTENER HEAD. (MARKED) (C-CHECK RO 3/14/2022) BLENDED OUT CHAFING ON STRUCTURE ON PASSENGER DOOR, AT UPPER END OF DOOR, AT AFT EDGE OF FWD DOOR CAP. REF: CRJ-2Jan 11, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265040None · dented*PASSENGER DOOR, ON INNER SKIN/STEP SUPPORT STRUCTURE, DENT ON INSIDE SKIN AT ACCESS HOLE FOR COUNTER BALANCE PULLEY MOUNT BOLT. (MARKED) (C-CHECK RO 3/14/2022) REPAIED PASSENGER DOOR, ON INNER SKIN/STEP SUPPORT STRUCTURE REF REO 601R-52-11-2915 REV-- DJan 11, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265090None · corroded*AFT CARGO FLOOR SUPPORT ANGLE BETWEEN LBL 27 €“ 36, ATTACHED TO BULKHEAD 621.00 (C-CHECK RO 3/14/2022) REMOVED CORROSION AFT CARGO FLOOR SUPPORT ANGLE BETWEEN LBL27-36 ATTACHED TO BULKHEAD FS 621.00 REF CRJ200 SRM 51-21-06 / ORIGINAL MATERIAL .094 IAW Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265086None · corroded*ON PASSENGER DOOR, LOWER LATCH MECHANISMTORQUE TUBE STOP BOLT HAS CORRODED HARDWARE AND NUTPLATE. (MARKED) (C-CHECK RO 3/14/2022) REMOVED CORRODED HARDWARE @ PAX DOOR LOWER TORQUE TUBE AND REPLACED WITH NEW STOP HARDWARE FOR STOP FITTING. REF CRJ200 Jan 10, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265085None · corroded*CORROSION ON STANDOFF ATTACHED TO RH FLOOR SILL BETWEEN FS 574.00 €“ 589.00, RBL 36 €“ 45 (C-CHECK RO 3/14/2022) REMOVED AND INSTALLED NEW STANDOFF AT RH FLOOR SILL BETWEEN FS574.00- 589.00 RBL45. REF. CRJ 200 SRM 51-45-00Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265084None · corroded*CORROSION ON 2EA STANDOFFS ATTACHED TO RH FLOOR SILL BETWEEN FS 409.00+112 €“ 409.00+128 (C-CHECK RO 3/14/2022) REMOVED AND REPLACED NEW STANDOFFS 2 EA ATTACHED TO RH FLOOR SILL BETWEEN FS 409.00+112 €“ 409.00+128 REF. CRJ 200 SRM 51-45-00Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265083None · corroded*CORROSION ON FLOOR SUPPORT BEAM AT FS 333.00 BETWEEN RBL 27 €“ 36 (C-CHECK RO 3/14/2022) REMOVED CORROSION ON FLOOR SUPPORT BEAM AT FS 333.00 BETWEEN RBL 27 TO 36 REF: CRJ-200 SRM 51-21-06 / FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-00. MEASURED Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265071None · corroded*CORROSION ON FLOOR SEAT TRACK RBL9 BETWEEN FS 349.00 €“ 409.00+128. AREAS MARKED (C-CHECK RO 3/14/2022) REMOVED AND REPLACED 2 EA. FLOOR SEAT RAILS FROM APPROX. FS 349.00 TO FS409+128 AT RBL 9.0 REF: CRJ-200 AMM 53-01-11-000-802 AND CRJ-200 AMM 53-01-Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265039None · corrodedRH PRESSURE FLOOR SILL FS409.0+128 TO FS559.0 HAS MULTIPLE AREAS OF CORROSION (MARKED) (C-CHECK RO 3/14/2022) REMOVED CORROSION R/H PRESSURE FLOOR SILL PANEL FS 409.0+128 TO FS 559.0 REF MHIRJ REO 601R-53-41-666 REV-C DATE-2012-11-06 / COMPLIED WITH REJan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265038None · corrodedLH PRESSURE FLOOR SILL FS409.0+128 TO FS559.0 HAS MULTIPLE AREAS OF CORROSION (MARKED) (C-CHECK RO 3/14/2022) REMOVED CORROSION L/H PRESSURE FLOOR SILL PANEL FS 409.0+128 TO FS 559.0 REF REO 601R-53-41-666 REV-C DATE-2012-11-06 .COMPLIED WITH REO 601R-Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265037None · corroded*CORROSION ON RH FLOOR SILL BETWEEN FS 559.00+80 €“ APPROX. 559.00+96 (C-CHECK RO 3/14/2022) BLENDED RH FLOOR SILL BETWEEN FS559.00+80 TO APPROX. FS559.00+96 IN LIMITS AND RESTORED REF CRJ200 SRM 51-42-15, CRJ200 SRM 51-21-06, CRJ200 SRM 53-51-43, CRJ20Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265036None · corroded*CORROSION ON RH FLOOR SILL BETWEEN FS 559.00 €“ APPROX 559.00+80 (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM RH FLOOR SILL BETWEEN FS559.00-559.00+80 IAW CRJ200 SRM 51-21-06-00 .INTERCOSTAL AT 559-559+16 FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265035None · corroded*CORROSION ON LH FLOOR SILL BETWEEN FS 559.00 €“ 559.00+80 (C-CHECK RO 3/14/2022) REPAIRED AFT CABIN LEFTHAND FLOOR SILL BETWEEN FS559.00 TO FS559.00+80 ON LEFTHAND SIDE IAW REO 601R-53-00-526 REV -- DATE 22-MAY-2013 STEPS. 1-7 (SEE CONTINUATION SHEET FJan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265034None · corroded*CORROSION ON LH FLOOR SILL BETWEEN FS 349.00 €“ AFT OF 409.00 (C-CHECK RO 3/14/2022) REPAIRED FORWARD CABIN FLOOR SILL ON LEFTHAND SIDE BETWEEN FS349.00 TO FS409.00 IAW REO 601R-53-00-530 REV -A DATE 2014-10-07 STEPS.1-9 (SEE CONTINUATION SHEET FOR FURJan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265033None · corroded*CORROSION ON LH FLOOR SILL SUPPORT AT FS 349.00 (C-CHECK RO 3/14/2022) REPAIRED FORWARD CABIN FLOOR SILL SUPPORT ON LEFTHAND SIDE AT FS349.00 IAW REO 601R-53-00-530 REV -A DATE 2014-10-07 STEPS.1-9 (SEE CONTINUATION SHEET FOR FURTHER DETAILS)Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265032None · corroded*CORROSION ON FLOOR SUPPORT BEAM AT FS 349.00, APPROX. LBL36 (C-CHECK RO 3/14/2022) REMOVED CORROSION AT FLOOR SUPPORT BEAM AT FS 349.00 APPROX. LBL 36 REF: CRJ-200 SRM 51-21-06 / NOMINAL THICKNESS OF 0.063" REF CRJ 200 SRM 53-21-15 FIGURE 5. REMAINING TJan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265031None · corroded*CORROSION ON LH FLOOR SILL DOUBLER BETWEEN FS 310.00 €“ 295.00 (C-CHECK RO 3/14/2022) REPAIRED FORWARD CABIN FLOOR SILL DOUBLER BETWEEN FS295.00 TO FS310.00 ON LEFTHAND SIDE IAW REO 601R-53-00-530 REV -A DATE 2014-10-07 STEPS. 1-9 (SEE CONTINUATION SHEJan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265030None · corroded*CORROSION ON STOWAGE AFT OTBD FLOOR MOUNT DOUBLER LBL 36 (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM AFT OTBD FLOOR MOUNT DOUBLER LBL 36 REF: CRJ-200 SRM 51-21-06. FOUND TO BE IN LIMITS REF CRJ200 SRM 53-00-00, SEE CONTINUATION CARD FOR DETAILS OF WORJan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265029None · damagedCOMPLY WITH AD 2002-03-14/10 REPAIR OF RIGHT SIDE LOWER WING PLANK DUE BEFORE FURTHER FLIGHT. (C-CHECK RO 3/14/2022) COMPLIED WITH PARAGRAPH (B) OF AD 2002-03-14 BY REPAIRING CRACK ON THE RIGHT SIDE LOWER WING PLANK BEFORE FURTHER FLIGHT PER A METHOD APPJan 10, 2022 · N854AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202265028None · corroded*CORROSION ON FS 280.00 FWD FLOOR BEAM ANGLE BETWEEN RBL 9 €“ LBL 9 (C-CHECK RO 3/14/2022) REPLACED FLOOR SUPPORT ANGLE P/N600-34017-351 ON FLOOR BEAM AT FS280.00 BETWEEN LBL9 AND RBL9 PER REF CRJ200 SRM 51-42-06 AND DRAWING 600-34017 REV AD / COMPLIED Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265027None · corroded*CORROSION ON RH FLOOR SILL BETWEEN FS 295.00 €“ 310.00 (C-CHECK RO 3/14/2022) BLENDED RH FLOOR SILL BETWEEN FS295 TO FS310 IN LIMITS AND RESTORED REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-21-06, CRJ200 SRM 53-21-43, CRJ200 SRM 51-25-16, CRJ200 SRM 51-42-1Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265026None · corroded*CORROSION ON RH FLOOR SILL DOUBLER BETWEEN FS 310.00 €“ 319.00 (C-CHECK RO 3/14/2022) BLENDED CORROSION ON RH FLOOR SILL DOUBLER BETWEEN FS 310.00-319.00 PER REF CRJ 200 SRM 51-12-00 / FOUND TO BE OUT OF LIMITS / REMOVED AND INSTALLED NEW RH FLOOR SILJan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265025None · corroded*CORROSION ON RH FLOOR SILL SUPPORT AFT OF FS 349.00 (C-CHECK RO 3/14/2022) BLENDED CORROSION ON RH FLOOR SILL AFT OF FS 349.00 PER REO 601R-53-00-530 REV -A DATE 2014-10-07 . FOUND TO BE IN LIMITS REF REO 601R-53-00-530 REV -A DATE 2014-10-07. COMPLIED Jan 10, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265070None · damaged*RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS544.00 THRU FS559.00+80 HAS PITTING AND SCRATCH'S. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON R/H SIDE SEAT RAIL BETWEEN FS544.00 TO FS559.00+80 REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REF: CRJ-200Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265069None · damaged*RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS499.00 THRU FS544.00 HAS PITTING AND SCRATCH'S. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON R/H SIDE SEAT RAIL BETWEEN FS499.00 TO FS544.00. REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REF: CRJ-200 SRM Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265068None · corroded*RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS409.00+112 THRU FS449.85 HAS PITTING AND CORRODED AROUND SCREWS. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON SIDE SEAT RAIL BETWEEN FS409.00+112 TO FS449.85 ON RIGHTHAND SIDE IAW CRJ 200 SRM 51-21-06. FOUND TO BE Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265067None · corroded*RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS409.00+16 THRU FS409.112 HAS PITTING AND CORRODED AROUND SCREWS. (C-CHECK RO 3/14/2022) REMOVED CORROSION ON SIDE SEAT RAIL BETWEEN FS409.00+16 TO FS409+112 ON RIGHT HAND SIDE IAW CRJ 200 SRM 51-21-06. FOUND TO BEJan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265066None · corroded* RIGHT SIDE SEAT RAIL STRUCTURE APPROX FS364.00 THRU FS409.00 HAS PITTING AND CORRODED AROUND SCREWS. (C-CHECK RO 3/14/2022) REPLACED RIGHT SIDE SEAT RAIL STRUCTURE APPROX. FS364.00 TO FS409.00 REF REO 601R-53-00-055 REV.-C DATED 2017-03-21 ALL STEPS COJan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265065None · corroded*LEFT SIDE SEAT RAIL STRUCTURE AFT OF FS499.00 HAS MULTIBLE AREA'S CHAFING AND GOUGES. (C-CHECK RO 3/14/2022) FOUND LH SIDE SEAT RAIL FROM FS 499 TO FS 599 OUT OF LIMITS REF CRJ 200 SRM 53-21-49 AND INSTALLED NEW SIDE SEAT RAIL REF CRJ 200 AMM 53-01-11-4Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265064None · corroded*LEFT HAND SIDE SEAT RAIL CORRODED IN MULTIPLE AREA'S APPROX FS449.85 THRU FS499.00. (C-CHECK RO 3/14/2022) .REMOVED CORROSION FROM L/H SIDE SEAT RAIL FROM APPROX. FS449.85 THRU FS499.00 REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REF: CRJ-200 Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265063None · corroded*LEFT HAND SIDE SEAT RAIL CORRODED IN MULTIPLE AREA'S APPROX FS409.00+112 THRU FS449.85. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM LH SIDEWALL SEAT RAIL FS409.00+112 TO FS449.85 BY BLENDING IAW CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS PER SRM 5Jan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265062None · corroded*LEFT HAND SIDE SEAT RAIL CORRODED IN MULTIPLE AREA'S APPROX FS409.00+16 THRU FS409.00+112. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM LH SIDEWALL SEAT RAIL FS409.00+16 TO FS409.00+112 BY BLENDING IAW CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS PERJan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265061None · corroded*LEFT HAND SIDE SEAT RAIL CORRODED IN MULTIPLE AREA'S FS364.00 THRU FS409.00+16. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM LH SIDEWALL SEAT RAIL FS364.00 TO FS409.00+16 BY BLENDING IAW CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS PER SRM 53-21-49 REJan 9, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
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