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 SWIA202265082None · corroded*FLOOR SUPPORT ANGLE ATTACHED TO PAX DOOR LWR SILL HAS LOOSE AND CORRODED FASTENERS. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED FLOOR SUPPORT ANGLE ATTACHED TO PAX DOOR LWR SILL CORRODED FASTENERS AND NUTPLATES. REF: CRJ-200 SRM 51-42-10.Jan 7, 2022 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265023None · corroded*PAX DOOR FWD HANDRAIL SUPPORT ARM POCKET ATTACHED TO FLOOR SUPPORT ANGLE HAS CORROSION. (C-CHECK RO 3/14/2022) BLENDED OUT CORROSION ON THE PAX DOOR FWD HANDRAIL BRACKET REF CRJ 200 SRM 51-21-06. OUT OF LIMITS REF CRJ 200 SRM 53-00-00 / REMOVED AND INSTJan 7, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265021None · corroded*PAX DOOR LWR SILL HAS CORROSION AT THE AFT END. (C-CHECK RO 3/14/2022) BLENDED OUT CORROSION ON AFT END OF LOWER SILL AT PAX DOOR SURROUND REF CRJ 200 SRM 51-21-06 / FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-00. MEASURED THICKNESS .056. ORIGINAL TJan 7, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265019None · worn*CARGO DOOR AFT DOOR TRACK IS WORN AT THE TOP ENDS. (C-CHECK RO 3/14/2022) FOUND THE CARGO DOOR TRACK OUT OF LIMITS REF CRJ SRM 200 53-00-00 FIG 101. REMOVED AND INSTALLED NEW CARGO DOOR AFT DOOR TRACK AND RESTORED FINISH. REF: CRJ200 SRM 51-42-06, CRJ2Jan 7, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265089None · gouged*RIGHT WING FUSELAGE ATTACHMENT FITTING AT BL45 AND FS 513 HAS A SMALL GOUGE ON THE INBD SIDE. (IN WHEEL WELL AREA) (C-CHECK RO 3/14/2022) BLENDED DAMAGED AREA OF THE R/H WING FUSELAGE ATTACHMENT FITTING AT BL45 COMMON TO FS 513 INBD. SIDE (WHEEL WELL ARJan 6, 2022 · N854AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265081None · corroded*ON PAX DOOR, ON UPPER TORQUE TUBE, CORRODED HARDWARE AFT OF STOP FITTING. (MARKED) (C-CHECK RO 3/14/2022) PAX DOOR, ON UPPER TORQUE TUBE, INSTALLED NEW HARDWARE AFT OF STOP FITTING 2 NEW BOLTS, 2 WASHERS AND 2 NUTS PER THE CRJ 200 AMM 20-21-00-910-801Jan 6, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265080None · corroded*ON PAX DOOR, AT UPPER TORQUE TUBE, STOP FITTING HARDWARE IS CORRODED. (MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED PAX DOOR CORRODED HARDWARE FOR THE STOP FITTING INCLUDED STOP BOLT REF: CRJ-200 SRM TASK 51-41-02. ADJUSTMENT CHECK GOOD. OPS CJan 6, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265015None · elongated*PASSENGER DOOR HINGE ON THE FUSELAGE SIDE HAS ELONGATED HOLES. FOUND OUT OF LIMITS WITH GO-NOGO TOOL #G670-521104-101. (C-CHECK RO 3/14/2022) REPLACED PASSENGER DOOR HINGE ON THE FUSELAGE SIDE REF CRJ200 SRM 53-21-23, REO 601R-53-21-656 REV. -A DATED 20Jan 6, 2022 · N854AS · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA202265079None · cracked*ANGLE INSIDE RH AFT EQUIPMENT BAY HAS A POSSIBLE CRACK. FS 625.30.STGR 15R. FLAGGED AND MARKED (C-CHECK RO 3/14/2022) REMOVED AND REPLACED ANGLE BRACKET IN R/H AFT EQUIPMENT BAY AT FS625.30 STGR 15R WITH NEW P/N 601-35012-54 REF CRJ 200 SRM 51-42-06 ANJan 5, 2022 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265098None · seizedRH AILERON CENTER HINGE FITTING LOWER INBD BOLT IS SEIZED (C-CHECK RO 3/14/2022) REMOVED RH AILERON CENTER BOLT STOP FITTING TO F.O.M REF CRJ200 SRM 51-42-21. SEE INSTALL OF NEW HARDWARE ON CAMP#23855597 JOB#2738280 OP#519Jan 4, 2022 · N854AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265078None · corroded*LH HORIZONTAL STAB/ELEVATOR #3 HINGE HAS CORRODED BUSHING (C-CHECK RO 3/14/2022) REMOVED AND INSTALLED NEW BUSHING ON LH H-STAB/ELEVATOR #3 HINGE. REF - CRJ 200 AMM 27-34-01-400-801. / BUSHING P/N NAS43HT3-21Jan 4, 2022 · N854AS · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202265077None · corroded*RH HORIZONTAL STAB/ELEVATOR #3 HINGE HAS CORRODED BUSHING (C-CHECK RO 3/14/2022) REMOVED AND INSTALLED NEW BUSHING ON RH H-STAB/ELEVATOR #3 HINGE. REF - CRJ 200 AMM 27-34-01-400-801. / BUSHING P/N NAS43HT3-21Jan 4, 2022 · N854AS · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202265060None · chafed*CREW ESCAPE HATCH HINGE ARM HAS A CORNER CHAFFED & CORRODED (MARKED) (C-CHECK RO 3/14/2022) REMOVED AND INSTALLED NEW CREW ESCAPE HATCH HINGE ARMS. REF. CRJ200 CMM 52-22-01 STEPS 2. A. (3) (A) - (C). PAGE 3001 AND CRJ200 CMM 52-22-01 STEPS 3. A. (2) (A)Jan 4, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265013None · gouged*LH OVERWING EMERGENCY EXIT DOOR CUTOUT HAS BOTTOM HINGE FITTINGS (X2) GOUGED/DAMAGED (MARKED) (C-CHECK RO 3/14/2022) REMOVED GOUGES ON BOTTOM HINGE FITTINGS FORWARD AND AFT FROM RIGHT HAND OVERWING EMERGENCY EXIT DOOR CUTOUT AFTER EVALUATED, DAMAGE FOUNJan 4, 2022 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202265011None · chafedANGLE ON THE VERTICAL FRONT SPAR TO FUSELAGE SPLICE STRAP IS CHAFFED (MARKED) (C-CHECK RO 3/14/2022) REPLACED ANGLE ON THE VERTICAL FRONT SPAR TO FUSELAGE SPLICE STRAP REF DWG 600-21108 REV. C, CRJ200 SRM 51-42-21, CRJ200 SRM 51-41-02. COMPLIED WITH 51-9Jan 4, 2022 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265097None · failedL/H INBOARD GROUND SPOILER HAS EXCESSIVE PLAY, FAILED BACKLASH CHECK. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED THE LH INBOARD GROUND SPOILER LINK AND ATTACHMENT HARDWARE REF CRJ-200 AMM 27-65-01-400-801. BACKLASH AND OP TEST CHECKED GOOD.Jan 3, 2022 · N854AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265096None · failedLH ELEVATOR #2 PCU BEARING FAILED BACKLASH CHECK. LIMIT: 0.210, READING: 0.289. (C-CHECK RO 3/14/2022) / REMOVED AND REPLACED LEFT ELEVATOR #2 SPHEICAL BEARING REF CRJ 200 AMM 27-33-01-400-801. BACKLASH CHECK GOOD REF CRJ 200 AMM 27-31-00-220-804. COMPJan 2, 2022 · N854AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265095None · failedLH ELEVATOR #3 PCU BEARING FAILED BACKLASH CHECK. LIMIT 0.210, READING 0.320. (C-CHECK RO 3/14/2022) / REMOVED AND REPLACED LEFT ELEVATOR #3 PCU BEARING REF CRJ 200 AMM 27-33-01-400-801. BACKLASH CHECK GOOD REF CRJ 200 AMM27-31-00-220-804. OPS CHECK GOOJan 2, 2022 · N854AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265094None · failedLH ELEVATOR #3 PCU FAILED BACKLASH CHECK. LIMIT: 0.800 READINGS 0.965 AND 0.965. (C-CHECK RO 3/14/2022) / REMOVED AND REPLACED LEFT ELEVATOR #3 PCU HARDWARE AT ELEVATOR REF CRJ 200 AMM 27-33-01-400-801. BACKLASH CHECK GOOD REF CRJ 200 AMM 27-31-00-220-8Jan 2, 2022 · N854AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265009None · cracked*LH MLG WHEEL WELL BAT RIB AT APPROX. LBL45 HAS POSSIBLE CRACK (C-CHECK RO 3/14/2022) REMOVED AND REPLACED LH MLG WHEEL WELL BATT RIB AT APPROX. LBL45 IAW CRJ-200 SRM 51-42-21 REV.-38 JUL10/09 DWG 600-10204 REV-M COMPLIED WITH 51-900-1003-SKYJan 2, 2022 · N854AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202165076None · corrodedRIGHT WING O/B GROUND SPOILER HAS CORRODED HARDWARE AT CENTER HINGE FITTING (C-CHECK RO 3/14/2022) REPLACED CORRODED HARDWARE WITH NEW HARDWARE ON RH WING OUTBOARD GROUND SPOILER AT CENTER HINGE FITTING. REF. CRJ200 AMM 27-65-01-400-801. OP TEST GOOD. SDec 29, 2021 · N854AS · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202165075None · corrodedLEFT WING O/B GROUND SPOILER HAS CORRODED HARDWARE AT CENTER HINGE FITTING (C-CHECK RO 3/14/2022) REPLACED CORRODED HARDWARE WITH NEW HARDWARE ON LH WING OUTBOARD GROUND SPOILER AT CENTER HINGE FITTING. REF. CRJ200 AMM 27-63-01-400-801. OP TEST GOOD. SEEDec 29, 2021 · N854AS · Cndair CL6002B19 · Wing StructureSDR SWIA202165059None · chafedRIGHT I/B FLAP VANE SKIN IS CHAFFED ON L/E JUST O/B OF O/B VANE ACTUATOR (C-CHECK RO 3/14/2022) DAMAGE FOUND ON R/H I/B FLAP VANE L/E WEAR PLATE, NO DAMAGE NOTED UNDER WEAR PLATE ON L/E SKIN. REMOVED AND REPLACED WEAR PLATE REF. CRJ 200 SRM 51-42-13-001-Dec 29, 2021 · N854AS · Cndair CL6002B19 · AileronsSDR SWIA202165058None · chafedRIGHT I/B FLAP VANE SKIN IS CHAFFED ON L/E JUST O/B OF MID VANE ACTUATOR (C-CHECK RO 3/14/2022) DAMAGE FOUND ON R/H I/B FLAP VANE L/E WEAR PLATE, NO DAMAGE NOTED UNDER WEAR PLATE ON L/E SKIN. REMOVED AND REPLACED WEAR PLATE REF. CRJ 200 SRM 51-42-13-001-Dec 29, 2021 · N854AS · Cndair CL6002B19 · AileronsSDR SWIA202165057None · chafedRIGHT I/B FLAP VANE SKIN IS CHAFFED ON L/E JUST I/B OF I/B VANE ACTUATOR (C-CHECK RO 3/14/2022) REMOVED AND INSTALLED NEW SKIN CAP ON R/H I/B FLAP VANE SKIN COMMON TO L/E JUST I/B OF I/B VANE ACTUATOR, REF: CRJ-200 SRM 51-42-13Dec 29, 2021 · N854AS · Cndair CL6002B19 · AileronsSDR SWIA202165007None · damagedTOP PLATE FOR 1EA NUTPLATE ON THE RIGHT HORIZONTAL TIP HAS DAMAGE (MARKED) (C-CHECK RO 3/14/2022) REPAIRED TOP PLATE ON RIGHTHAND HORIZONTAL TIP IAW REO 601R-55-11-712 REV -- DATE 2022-02-01 STEPS. 1-9. (SEE CONTINUATION SHEET FOR FURTHER DETAILS) COMPLIDec 29, 2021 · N854AS · Cndair CL6002B19 · Horizontal Stabilizer, Tab StructureSDR SWIA202165005None · corrodedRH HORIZONAL STAB LE ERODED. (C-CHECK RO 3/14/2022) REMOVED EROSION ON RH HORIZONAL STAB LE, REF. CRJ200 SRM 51-12-00 / COMPLIED WITH REO 601R-55-12-716 REV -- DATE 2022-01-20Dec 29, 2021 · N854AS · Cndair CL6002B19 · Horizontal Stabilizer, Tab StructureSDR SWIA202165004None · chafed* CARGO DOOR EXTERIOR HANDLE HOUSING CHAFED (MARKED). (C-CHECK RO 3/14/2022) REMOVED AND REPLACED CARGO DOOR HANDLE HOUSING WITH NEW HOUSING REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-21-16 AND DWG. 601R35027 REV K SEE CONTINUATION FOR DETAILS. COMPLIED WITDec 28, 2021 · N854AS · Cndair CL6002B19 · DoorsSDR SWIA202165003None · gouged* EXTERIOR SKIN GOUGED FWD OF CARGO DOOR AT APROX. FS.,574.00 STR15L (MARKED). (C-CHECK RO 3/14/2022) REPAIRED GOUGED EXTERIOR SKIN FWD OF CARGO DOOR AT APPROX. FS.,574.00 STR15L BY COMPLYING WITH REO 601R-53-61-7789 REV -- DATED 2022-01-11, DISPOSITIONDec 28, 2021 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202165002None · dented* DENT ON LEFT SIDE OF A/C AT APROX. FS265.00 AND STR20L (MARKED). (C-CHECK RO 3/14/2022) REPAIRED DENTS ON LEFT SIDE OF A/C AT APPROX. FS265.00 AND STR20L BY COMPLYING WITH REO 601R-51-00-309 REV -A DATED 2017-08-23 , DISPOSITION STEPS 1-12 (DENT #2) ANDec 28, 2021 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202165102None · wornREMOVE & REINSTALL RH AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON IAW AMM 27-15-01-000-801. COMPLY WITH TASK CARD 27-900-1001-SKY (C-CHECK RO 3/14/2022) REMOVED & INSTALLED NENov 18, 2021 · N854AS · Cndair CL6002B19 · Wing StructureSDR SWIA202165101None · wornREMOVE & REINSTALL LH AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON IAW AMM 27-15-01-000-801. COMPLY WITH TASK CARD 27-900-1001-SKY (C-CHECK RO 3/14/2022) REMOVED & REINSTALLED Nov 18, 2021 · N854AS · Cndair CL6002B19 · Wing StructureSDR SWIA202165100None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3/14/2022) REMOVED AND REPLACED BUSHINGS WITH 15 EA NEW BUSHINGS RIGHT AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804. HARDWARE REPLNov 18, 2021 · N854AS · Cndair CL6002B19 · Wing StructureSDR SWIA202165099None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3/14/2022) REMOVED AND REPLACED BUSHINGS ON LEFT AILERON WING AFT SPAR WITH 15 EA NEW BUSHINGS REF CRJ 200 AMM 20-26-00-910-804. HARDWARE RENov 18, 2021 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202165001None · damagedCOMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK RO 3/14/2022) COMPLIED WITH REO 601R-53-41-1116 REV - C DATED 2017-03-09 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & Nov 18, 2021 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202162018None · failedD: ON APPROACH, LOWERED LANDING GEAR AND GOT HYD3 LO PRESS FOLLOWED BY GEAR DISAGREE. WENT AROUND, AND GOT 3 GREEN GEAR INDICATION. REVIEWED THE QRH, THEN LOWERED THE GEAR. GOT SAME ERRORS. TURNED 3B FROM AUTO TO ON AND HYD 3 LO PRESS WENT AWAY. SHOWED 29Oct 31, 2021 · N854AS · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202165056None · corrodedRBL 27.00 FLOOR BEAM BETWEEN FS. 605 TO 621 HAS CORROSION (C-CHECK RO 3/14/2022) REMOVED CORROSION AT RBL 27.00 FLOOR BEAM BETWEEN FS. 605 TO 621 FOUND TO BE OUT OF LIMITS. REPAIRED IAW REO 601R 53-61-7585 REV -- DATED 2021-03-01. ALL STEPS COMPLIED WITFeb 16, 2021 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202165055None · corrodedRBL 27.00 FLOOR BEAM APPROX BETWEEN FS. 559+96 TO 559+112 HAS CORROSION (C-CHECK RO 3/14/2022) REMOVED CORROSION ON RBL 27.0 FLOOR BEAM CAP FROM FS 559+96 TO FS 559+122 , FOUND OUT OF LIMIT PER REO 601R-53-00-005 REV B DATED 2011-01-06. REPLACED WITH NEFeb 16, 2021 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202165054None · corroded* CORROSION AND PITTING , GOUGES AT FS 621.0 FLOOR RAIL FITTINGS WHERE SEAT RAIL BEAM ATTACHES / 4 SEPERATE LOCATIONS. MARKED (C-CHECK RO 3/14/2022) REMOVED AND REPLACED 4EA FLOOR RAIL FITTINGS COMMON TO FS621.00 REF REO 601R-53-61-3780 REV -A DATED 2011Feb 16, 2021 · N854AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202165053None · corrodedRH PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FROM APPROX. FS.409+128 TO APPROX. FS559+16 (MARKED) (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM RH PRESSURE FLOOR SILL FROM APPROX FS409+128 TO APPROX FS559+16 BLENDED WITHIN LIMITS REF REO 601R-5Feb 15, 2021 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202165052None · corrodedLH PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FROM APPROX. FS.409+128 TO APPROX. FS.559+16 (MARKED) (C-CHECK RO 3/14/2022) BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL FROM APPROX. FS.409+128 TO APPROX. FS.559+16 REF REO 601R-53-41-666 REV -CFeb 15, 2021 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202165051None · corrodedLH PRESSURE FLOOR SILL ANGLE FROM APPROX. FS.424 TO APPROX. FS473 HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 3/14/2022) BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL ANGLE FROM APPROX. FS.424 TO APPROX. FS.473 REF REO 601R-53-41-666 REV -C DAFeb 15, 2021 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202165050None · corrodedRH PRESSURE FLOOR ANGLE AT FS.424.00 HAS CORROSION (MARKED) (C-CHECK RO 3/14/2022) BLENDED RH PRESSURE FLOOR SILL ANGLE AT FS424. MINIMUM REMAINING THICKNESS OF 0.077" IS WITHIN LIMITS. RESTORED FINISH TO REPAIR AREA. REF REO 601R-53-41-666 REV -C DATFeb 15, 2021 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202165049None · corrodedLH FLOOR SILL AT APPROX. FS409+120 TO FS409+128 HAS CORROSION (C-CHECK RO 3/14/2022) BLENDED CORROSION ON THE LH FLOOR SILL AT APPROX. FS.409+120 TO FS.409+128 REF CRJ 200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS. RECEIVED REPAIR FOR AREA REF REO 601R-53-3Feb 15, 2021 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202165048None · corrodedCORROSION AROUND NUTPLATE HOLE ON RH PRESSURE FLOOR SILL AT FS424.00 (C-CHECK RO 3/14/2022) BLENDED CORROSION FROM R/H PRESSURE FLOOR SILL AT FS424.00 TO A SMOOTH CONTOUR. REMAINING MATERIAL WITHIN LIMITS. REF REO 601R-53-41-666 REV -C DATED 2012-11-06. Feb 14, 2021 · N854AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202054675Smoke Detector · false activationSMOKE TOILET CAUTION MESSAGE JUST PRIOR TO LANDING. NO SMOKE OBSERVED. MESSAGE EXTINGUISHED AFTER APPROXIMATELY 5 MINUTES. QRH PROCEDURE EMER 2-14 COMPLIED WITH. FLIGHT 5529-FILED CLOSED. REVERSED MAINTENANCE, PER EMER 2-14. PERFORMED TROUBLESHOOTING FORDec 14, 2020 · N854AS · Cndair CL6002B19 · Smoke DetectionSDR SWIA2019112246780Line · unsecureRECEIVED A DIFF PRESS WARNING MESSAGE AT FL330. INITIATED AN EMERGENCY DECENT,AND DECLARED AN EMERGENCY. PERFORMED QRH PROCEDURE FOR DIFF PRESS, WE WERE UNABLE TO CONTROL PRESSURIZATION IN MANUAL MODE. CABIN ALTITUDE CONTINUALLY DECREASED. WE DIVERTED TO KMCI.Nov 22, 2019 · N854AS · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR SWIA2018040944495Skin · damagedLEFT ELEVATOR HAS A DAMAGED LEADING EDGE AT EACH HINGE POINT. REPAIRED THE ELEVATOR IAW REO.Mar 21, 2018 · N854AS · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA2018040944499Skin · dentedLEFT INBD FLAP UPPER SKIN DENTED, 59 INCHES FROM THE INBD EDGE AND 1 INCH FROM TRAILING EDGE OF FLAP. REPAIRED IAW SRM.Mar 5, 2018 · N854AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201844497Channel · dentedDENT IN RUDDER TRAILING EDGE CHANNEL APPROXIMATELY 10 INCHES? FROM THE BOTTOM, BETWEEN RS 54 & 66. REPAIRED IAW REO.Feb 21, 2018 · N854AS · Cndair CL6002B19 · Rudder Structure
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