N218PS

Service difficulty reports · 121

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 = 'N218PS' 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 SWIA2026070176357Solenoid Valve · odorDURING CRUISE, SMELL OF FUEL IN COCKPIT. FA REPORTED SMELL OF FUEL IN THE CABIN. SMELLED STRONGER TOWARD THE REAR OF CABIN. (FLIGHT 5137) FOUND APU FUEL SHUT OFF SOLENOID VALVE LEAKING. REMOVED AND REPLACED THE APU FUEL SHUT OFF SOLENOID VALVE REF AMM 49-31-Jul 1, 2026 · N218PS · Cndair CL6002B19 · APU Engine Fuel and ControlSDR SWIA2026061276220Windshield · sparksWINDSHIELD HEAT SPARKED FROM TOP GROUNDING BLOCK. LIGHT SMOKE AND CAUTION MESSAGE. RAN QRH AND MESSAGE PERSISTED. (FLIGHT 5136) FOUND TO BE THAT THE PILOT'S PERSONAL SUNSCREEN MADE CONTACT WITH THE TERMINALS AND TRIPPED THE BREAKER. RESET THE WINDSHIELD HEATJun 12, 2026 · N218PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR SWIA202510070920Coupling · leakingRIGHT 14TH DUCT WARNING MESSAGE WHEN CLIMBING THROUGH ABOUT 8000FT. RAN QRH. MESSAGE CLEARED. RETURNED TO ORD. (FLIGHT 5610) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30875407, SEE THE FOLLOWING CPS FOR MX PERFORMED:CP 30882896 FOR REPLACEMENT OF THE RTSep 20, 2025 · N218PS · Cndair CL6002B19 · Pneumatic Indicating SystemSDR SWIA202509220001Warning Message · illuminatedRIGHT 14TH DUCT WARNING MESSAGE WHEN CLIMBING THROUGH ABOUT 8000FT. RAN QRH. MESSAGE CLEARED. RETURNED TO ORD. (FLIGHT 5610) OPEN.Sep 20, 2025 · N218PS · Cndair CL6002B19 · Pneumatic SystemSDR SWIA2025092200018Clamp · damagedRIGHT 10TH DUCT WARNING MSG DURING CLIMB AT 3500FT. APPLIED QRH, MSG DISAPPEARED, RETURNED TO KORD WITH NO FURTHER ISSUE. (FLIGHT 5215) SEE CP 30863533 FOR 10TH STAGE LEAK CHECK. SEE CP 30863951 FOR ACM COMPRESSOR INLET DUCT CLAMP REPLACEMENT SEE CP 3086354Sep 18, 2025 · N218PS · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA2025091900008Duct · warning messageR 10TH DUCT WARNING MSG DURING CLIMB AT 3500FT, APPLIED THE QRH MSG DISAPPEARED, RETURNED TO KORD WITH NO FURTHER ISSUE. (FLIGHT 5215 - FILED OPEN)Sep 18, 2025 · N218PS · Cndair CL6002B19 · Pneumatic SystemSDR SWIA2025091800017Bleed Valve · warning messageR 14TH STAGE BLED AIR DUCT MASTER WARNING N CLIMB OUT (FLIGHT 5038) PERFORMED VISUAL INSPECTION OF THE RH 14TH STAGE BLEED DUCTS REFERENCING APPLICABLE STEPS OF AMM 36-12-00. NO DEFECTS NOTED AT THIS TIME. PERFORMED LEAK TEST OF THE 10TH STAGE BLEED AIR SYSSep 17, 2025 · N218PS · Cndair CL6002B19 · Compressor Bleed ValveSDR SWIA202405280025Landing Gear · warning messageON DEPARTURE OUT OF RIW WE BROUGHT THE GEAR UP AT 230 KTS AND GOT GEAR DISAGREE. SLOWED THE AIRPLANE DOWN AND THE MESSAGE EXTINGUISHED. RAN QRH. NO ISSUES BRINGING GEAR DOWN ON LANDING. (FLIGHT 5130 FILED CLOSED) UPON ARRIVAL TROUBLESHOT REF CRJ FIM 32-60-07.May 25, 2024 · N218PS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA202310130009Unknown · crackedTRANSFER FROM EAML 1226325 : HAD ARCING ON THE CAPTAIN€™S SIDE WINDSHIELD DURING CRUISE. DURING THE DESCENT THE WINDSHIELD STARTED CRACKING ON THE OUTSIDE. ALL APPLICABLE QRHS WERE COMPLIED WITH. (FLIGHT 5060 - FILED CLOSED) SEE CP 27284480 FOR REMOVAL OFOct 9, 2023 · N218PS · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA20230807006Unknown · warning messageGEAR DISAGREE WARNING MSG POSTED SHORTLY AFTER TAKEOFF AND DURING INITIAL TURNOUT. AIRSPEED APPROX 160 KIAS AND ALTITUDE AROUND 600 AGL. LEFT MAIN GEAR SHOWED A RED INDICATION. GEAR MANUAL RELEASE HANDLE WAS PULLED PER QRH AND ALL GEAR RETURNED TO GREEN INDICAAug 6, 2023 · N218PS · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202304260001Unknown · gougedCOMPLY WITH PERMANENT REPAIR OF GOUGE DAMAGE TO CARGO DOOR OUTER SKIN UPPER EDGE BETWEEN FS589.00 - FS605.00 PER REO 601R-52-31-404. THIS IS CLASSIFIED AS A MAJOR REPAIR. FORM M-337 INITIATED. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF CARGO DOOR OUTER SKApr 20, 2023 · N218PS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202304210001Unknown · gougedCOMPLY WITH PERMANENT REPAIR OF GOUGE DAMAGE TO CARGO DOOR OUTER SKIN UPPER EDGE BETWEEN FS589.00 - FS605.00 PER REO 601R-52-31-404. THIS IS CLASSIFIED AS A MAJOR REPAIR. FORM M-337 INITIATED. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSApr 20, 2023 · N218PS · Cndair CL6002B19 · DoorsSDR SWIA2023012500019Windshield · crackedL WSHLD CRACKED ACROSS HALF THE WINDOW. (FILED CLOSED)REMOVED, AND REPLACED LEFT WINDSHIELD AS REQUIRED REF AMM AMM 56-11-01, SEE CARD 56-220-1000-SKY OPS AND LEAK CHECKS GOOD.Jan 19, 2023 · N218PS · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA202264049None · corrodedL/H FLIGHT SPOILER I/B PCU FAILS BACKLASH CHECK. TROUBLESHOOT & REPAIR AS REQUIRED PER MM & COMPLETE BACKLASH CHECK OF FLIGHT SPOILER I/B PCU (C CHECK RO 1/20/22) REMOVED AND REPLACED LOWER MOUNTING HARDWARE AT LH FLIGHT SPOILER INBOARD PCU IAW CRJ 200 AJan 8, 2022 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164044None · corrodedCARGO DOOR KICKPLATE AFT HINGE SECTION HAS CORROSION (C CHECK RO 1/20/22) REMOVED AND REPLACED HINGE ON CARGO DOOR KICKPLATE AFT HINGE SECTION IAW CRJ 200 SRM 51-40-11 AND SRM 51-42-06Dec 20, 2021 · N218PS · Cndair CL6002B19 · DoorsSDR SWIA202164056None · damagedINSTALL SERVICEABLE FLAP L/H I/B (C CHECK RO 1/20/22) REMOVED L/H I/B UNSERVICEABLE FLAP AND REPLACED WITH SERVICEABLE FLAP IAW CRJ 200 AMM 27-54-01-000-801 AND CRJ 200 AMM 27-54-01-400-801. REMOVED AND REPLACED L/H I/B FLAP #1 AND #2 ACTUATORS IAW CRJ Dec 7, 2021 · N218PS · Cndair CL6002B19 · AileronsSDR SWIA202164030None · wornREPLACE I/B BUSHINGS ON I/B R/H GROUND SPOILER (C CHECK RO 1/20/22) REPLACED INBOARD BUSHING ON INBOARD RH GROUND SPOILER IAW CRJ 200 AMM 20-26-00 AND REO 601R-57-51-982 REV -A DATED 2022-01-19 ANALASIS TO DETERMIN ADDITIONAL REQUIREMENTS WILL BE COMPLETNov 12, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164029None · damaged2 DAMAGED HOLES ON R/H CHECK PANEL (C CHECK RO 1/20/22) OPENED UP (2) HOLES AND INSTALLED FREEZE PLUG BUSHINGS IAW CRJ200 BOMBARDIER REO 601R-53-11-162. REV. D. DATE: 2019-02-05. / BUSHINGS FABRICATED BY OUTSIDE VENDOR SEE ATTACHED INVOUIC # 12684CURRENT Nov 4, 2021 · N218PS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202164043None · corrodedRIGHT SIDE SEAT RAILS FROM FS 349.00 TO FS 559+80 HAVE AREAS OF CORROSION & SURFACE WEAR IN VARIOUS SPOTS (C CHECK RO 1/20/22) REMOVED RIGHT HAND SEAT RAILS FROM 349.00 TO 559.00+80. EVALUATED CONDITION OF EACH RAIL. CLEANED CORROSION AS REQUIRED IAW CRJ2Sep 28, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164055None · damagedREPLACE DOUBLE GROMMET ON LOWER L/H NOSE COWLING (C CHECK RO 1/20/22) REMOVED & REPLACED DOUBLE GROMMET ON LOWER L/H NOSE COWLING. .INSTALLATION COMPLETE, IAW CRJ 200 CMM 71-14-01Sep 20, 2021 · N218PS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202164054None · mislocatedUPPER FORWARD ROLLER ON CARGO DOOR IS MISSING THE ROLLING PART (C CHECK RO 1/20/22) / REPLACED UPPER FORWARD ROLLER ASSEMBLY ON CARGO DOOR IAW CRJ 200 AMM 52-31-00 / TORQUE WRENCH-AG1132-5AUG2022Sep 17, 2021 · N218PS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202164035None · gougedSEAT TRACK RBL9 FROM FS559 TO FS559+80 MULTIPLE GOUGES AND CORROSION MARKED IN RED GREASE PENCIL (C CHECK RO 1/20/22) REMOVED UNSERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FROM F/S 559 TO F/S 559+80 RBL9 IAW CRJ 200 AMM 53-01-11-400-802Sep 15, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164034None · gougedSEAT TRACK LBL9 FROM FS559 TO FS559+80 MULTIPLE GOUGES AND CORROSION MARKED IN RED GREASE PENCIL (C CHECK RO 1/20/22) REMOVED UNSERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FROM F/S 559 TO F/S 559+80 LBL9 IAW CRJ 200 AMM 53-01-11-400-802Sep 15, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164028None · corrodedL/H LONGERON PRESSURE FLOOR ANGLE FS409+128 TO FS559 CORROSION AS MARKED (C CHECK RO 1/20/22) CORROSION DAMAGE ON L/H LONGERON PRESSURE FLOOR ANGLE FS409+128 TO FS559 REMOVED, ORIGINAL THICKNESS 0.080", DAMAGE REMOVED WAS 0.008", REMAINING THICKNESS 0.07Sep 14, 2021 · N218PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164027None · corrodedL/H LONGERON PRESSURE FLOOR SILL PANEL FS409+128 TO FS559 CORROSION AS MARKED (C CHECK RO 1/20/22) CORROSION DAMAGE ON L/H PRESSURE FLOOR SILL PANEL FS409+128 TO FS 559 REMOVED, ORIGINAL THICKNESS 0.055", DAMAGE REMOVED WAS 0.011", REMAINING THICKNESS 0.Sep 14, 2021 · N218PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164026None · corrodedR/H LONERON PRESSURE FLOOR ANGLE FS409+128 TO FS559 CORROSION AS MARKED (C CHECK RO 1/20/22) CORROSION DAMAGE ON R/H LONGERON PRESSURE FLOOR ANGLE FS409+128 TO FS559 REMOVED, ORIGNAL THICKNESS 0.080", DAMAGE REMOVED WAS 0.003", REMAINING THICKNESS 0.077"Sep 14, 2021 · N218PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164025None · corrodedR/H LONGERON PRESSURE FLOOR SILL PANEL FS409+128 TO FS559 CORROSION AS MARKED (C CHECK RO 1/20/22) CORROSION DAMAGE ON R/H LONGERON PRESSURE FLOOR SILL PANEL FS409+128 TO FS559 REMOVED, ORIGINAL THICKNESS 0.055", DAMAGE REMOVED WAS 0.004", REMAINING THICSep 14, 2021 · N218PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164033None · gougedF/S 370 TO F/S 409+ 116 RBL 9 SEAT TRACK MULTIPLE AREAS OF GOUGES & COROSION MARKED IN RED GREASE PENCIL- EVAL (C CHECK RO 1/20/22) REMOVED USERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FORM F/S 370 TO 409+116 RBL 9 IAW CRJ 200 AMM 53-01-11 / Sep 12, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164032None · gougedF/S 409+ 128 TO F/S 559 LBL 9 SEAT TRACK MULTIPLE AREAS OF GOUGES & CORROSION MARKED IN RED GREASE PENCIL- EVAL (C CHECK RO 1/20/22) REMOVED UNSERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FROM F/S 409+128 TO F/S 559 LBL9 IAW CRJ 200 AMM 53-01-Sep 12, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164031None · gougedF/S 409+ 128 TO F/S 559 RBL 9 SEAT TRACK MULTIPLE AREAS OF GOUGES & CORROSION MARKED IN RED GREASE PENCIL- EVAL (C CHECK RO 1/20/22) REMOVED UNSERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FROM F/S 409+128 TO F/S 559 RBL9 IAW CRJ 200 AMM 53-01-Sep 12, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164042None · crackedFS 628 STR 15 & 16L CRACKED FOUND DURING NDT INSPECTION OF FS 625 SPLICE SPAR & WEB INSPECTION (C CHECK RO 1/20/22) REMOVED AND REPLACED FS 628 STR 15L AND 16L ANGLES IAW CRJ200 SRM 51-24-38, SRM 51-42-21 FABRICATED REPLACEMENT PARTS, PARTS IDENTIFIESep 11, 2021 · N218PS · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA202164041None · corrodedR/H HORIZONTAL REAR SPAR RBL 16 & RBL 95 GROUND STUDS CORRODED 2 EACH FLAGGED (C CHECK RO 1/20/22) REMOVED & REPLACED RH HORIZONTAL REAR SPAR RBL 16 AND RBL 95 GROUND STUDS IAW CRJ200 AMM 51-80-00. / CALIBRATED TOOL USE . TORQUE WRENCH AV7326, CAL DUE DASep 2, 2021 · N218PS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/RibSDR SWIA202164024None · dentedTHERE'S DENT ON LOWER SKIN AT FS 589 BETWEEN STGR 26, 25 AND STGER 24 (C CHECK RO 1/20/22) REPAIRED FUSELAGE SKIN BETWEEN FS574.00 - FS621.00 STR24R- 24L. IAW REO601R-53-61-7719 REV-- DATED 2021-10-16 AND CRJ200 SRM 53-00-31. AIRCRAFT NOT TO BE OPERATED BAug 22, 2021 · N218PS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202164045None · brokenSERVICE DOOR FORWARD FROM TOP STOP BROKEN (C CHECK RO 1/20/22) REMOVED AND REPLACED SERVICE DOOR STOP AND ADJUSTED THE SCREW IAW CRJ 200 AMM 52-41-00Aug 21, 2021 · N218PS · Cndair CL6002B19 · Galley DoorsSDR SWIA202164040None · corrodedL/H FLIGHT SPOILER I/B & O/B ACTUATOR HINGE BOLTS NUTS CORROSION (C CHECK RO 1/20/22) REMOVED AND REPLACED CORRODED FASTENERS ON L/H FLIGHT SPOILER I/B & O/B ACTUATOR HINGE IAW CRJ 200 AMM 27-64-05 / TORQUE WRENCH-AV5920-OCT21Aug 20, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164039None · corrodedL/H FLIGHT SPOILER I/B HINGE BOLT KEEPER BOLTS CORRODED (C CHECK RO 1/20/22) REPLACED L/H FLIGHT SPOILER I/B HINGE BOLT KEEPER BOLTS IAW CRJ 200 AMM 27-64-05 USING TORQUE WRENCH AG1132 CAL DUE AUG 22, SAFETY CABLE GUN AV6061 CAL DUE JUN 22Aug 20, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164038None · corrodedI/B GROUND SPOILER O/B HINGE BOLT NUT CORRODED (C CHECK RO 1/20/22) REMOVED AND REPLACED O/B HINGE BOLT NUT ON THE I/B GROUND SPOILER IAW CRJ200 AMM 27-65-01. / TORQUE WRENCH AG1132 CAL DUE: AUG 2022Aug 20, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164048None · corrodedR/H WING SPOILERON, GROUNDING STRAPS ON CENTER AND I/B HINGE FITTINGS HAVE CORRODED HARDWARE (C CHECK RO 1/20/22) REMOVED CORROSION FROM ATTACHING HARD WEAR IAW CRJ 200 SRM 51-21-06Aug 17, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164037None · corrodedR/H FLIGHT SPOILER AT CENTER HINGE FITTING WS 191.44 WS 183.00 & I/B SPAR WS 162.49 LOCK BOLTS PLATES SCREWS ARE CORRODED TOTAL 8 SCREWS FLAGGED (C CHECK RO 1/20/22) R/H FLIGHT SPOILER AT CENTER HINGE FITTING WS 191.44 WS 183.00 & I/B SPAR WS 162.49 LOCK Aug 17, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164036None · corrodedL/H AILERON FLUTTER DAMPNER ATTACH CLEVIS CORROSION LOWER EDGES OF LEGS (C CHECK RO 1/20/22) REMOVED AND INSTALLED NEW CLEVIS TO L/H AILERON FLUTTER DAMPENER IAW CRJ 200 AMM 27-15-05 / CALIBRATED TOOLING: TORQUE WRENCH AV 7334 CAL. DUE DEC. 21, TORQUE WREAug 17, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164053None · damagedREMOVE AND REINSTALL LH IB FLAP ASSY (C CHECK RO 1/20/22) REMOVED AND REPLACED L/H I/B FLAP ASSY IAW CRJ 200 AMM 27-54-01-000-801 AND 27-54-01-400-801 / CALIBRATED TOOLS: / TORQUE WRENCH AV1655 CAL DATE: DEC21 / TORQUE WRENCH AV2050 CAL DATE: JUN22 / TORQAug 12, 2021 · N218PS · Cndair CL6002B19 · AileronsSDR SWIA202164052None · damagedREMOVE AND REINSTALL LH OB FLAP ASSY (C CHECK RO 1/20/22) REMOVED AND INSTALLED NEW SERVICEABLE L/H O/B FLAP ASSY IAW CRJ 200 AMM 27-54-05-400-801. OPS CHECK GOOD NO DEFECTS NOTED. CALIBRATED TOOLS USED: TORQUE WRENCH AV7335 CAL DUE: MAR 22.Aug 12, 2021 · N218PS · Cndair CL6002B19 · AileronsSDR SWIA202164050None · damagedREMOVE AND REINSTALL RH IB FLAP ASSY (C CHECK RO 1/20/22) REMOVED AND INSTALLED SERVICEABLE R/H I/B FLAP ASSY IAW CRJ 200 AMM 27-54-01 AND TASK 27-900-1006-SKY. PERFORMED OPS CKECK IAW CRJ 200 AMM 27-54-00-710-801. OPS CHECK GOOD. / TORQUE WRENCH AG1132 CAug 12, 2021 · N218PS · Cndair CL6002B19 · AileronsSDR SWIA202164047None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C CHECK RO 1/20/22) REMOVED RH AILERON HINGE FITTING BUSHINGS LOCATED AT RH WING AFT SPAR. / REPLACEMENT BUSHINGS INSTALLED AND REAMING TO SIZE COMPLETEJun 2, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR SWIA202164046None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C CHECK RO 1/20/22) REMOVED LH AILERON HINGE FITTING BUSHINGS LOCATED AT LH WING AFT SPAR. REPLACEMENT BUSHINGS INSTALLED AND REAMING TO SIZE COMPLETE Jun 2, 2021 · N218PS · Cndair CL6002B19 · Wing StructureSDR VNAA2020022871102Unknown · pressure lossON CLIMBOUT THRU FL160 CREW RECEIVED A CABIN ALT PRESSURE MESSAGE. CREW OBSERVED CABIN ALT CLIMBING RAPIDLY. LEVELED OFF AND REQUEST DECENT TO ATC. EMERGENCY DECLARED AND DECENT MADE. ONCE BELOW 8000 FT THE CABIN RETURNED TO NORMAL PRESSURIZATION. CHECKED CPCPFeb 27, 2020 · N218PS · Cndair CL6002B19 · Cabin Pressure Control SystemSDR VNAA2020010431103Warning Message · false activationCREW RECEIVED PITOT HEAT BASE AMBER MSG. THEY RAN THEIR QRH AND DECIDED TO RETURN TO DCA WHERE THEY LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL CHECK OF THE AIR DATA SENOR HEATER CONTROLLER IAW CRJ200 AMM 30-31-15-710-801 AND OPS CHECKS FOUND GOOD AT THIS TJan 3, 2020 · N218PS · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR VNAA2019112899901Skin · crackedCRACK FOUND AT RH WING LOWER PLANK BETWEEN FUEL PANELS 640CB AND 640DB. C/A: REPAIRED THE RH WING LOWER PLANK AROUND DRAIN HOLE AT W.S. 85.5 BETWEEN STRINGER 14R-15R IAW BBD REO 610R-57-21-3206 REV --, DATED 2019-11-28.Nov 28, 2019 · N218PS · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA2019011511102Control Unit · unknownSUPPLEMENTAL INFORMATION: MX C/W FUNCTIONAL CHECK OF HSTCU IAW CRJ200 AMM. FUNCTIONAL CHECK GOOD. OPS CHECK GOOD. OCF CHECK GOOD.Jan 15, 2019 · N218PS · Cndair CL6002B19 · Flight Control SystemSDR VNAA2019011501101Warning System · activatedAS GEAR WAS SELECTED UP, THE CREW RECEIVED A STAB AND MACH TRIM AMBER CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENTS. THE AIRCRAFT IS CURRENTLY IN MAINTENANCE.Jan 15, 2019 · N218PS · Cndair CL6002B19 · Stabilizer Position Indicating
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