# Service difficulty reports: N218PS

A list on [N218PS](https://openairdocs.org/aircraft/N218PS.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 3 · 121 reports

- [SDR SWIA2026070176357](https://openairdocs.org/sdr/SWIA2026070176357.md): Solenoid Valve · odor · Jul 1, 2026 · N218PS · Cndair CL6002B19 · APU Engine Fuel and Control
  > DURING 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-
- [SDR SWIA2026061276220](https://openairdocs.org/sdr/SWIA2026061276220.md): Windshield · sparks · Jun 12, 2026 · N218PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > WINDSHIELD 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 HEAT
- [SDR SWIA202510070920](https://openairdocs.org/sdr/SWIA202510070920.md): Coupling · leaking · Sep 20, 2025 · N218PS · Cndair CL6002B19 · Pneumatic Indicating System
  > RIGHT 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 RT
- [SDR SWIA202509220001](https://openairdocs.org/sdr/SWIA202509220001.md): Warning Message · illuminated · Sep 20, 2025 · N218PS · Cndair CL6002B19 · Pneumatic System
  > RIGHT 14TH DUCT WARNING MESSAGE WHEN CLIMBING THROUGH ABOUT 8000FT. RAN QRH. MESSAGE CLEARED. RETURNED TO ORD. (FLIGHT 5610) OPEN.
- [SDR SWIA2025092200018](https://openairdocs.org/sdr/SWIA2025092200018.md): Clamp · damaged · Sep 18, 2025 · N218PS · Cndair CL6002B19 · Cabin Cooling System
  > RIGHT 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 3086354
- [SDR SWIA2025091900008](https://openairdocs.org/sdr/SWIA2025091900008.md): Duct · warning message · Sep 18, 2025 · N218PS · Cndair CL6002B19 · Pneumatic System
  > R 10TH DUCT WARNING MSG DURING CLIMB AT 3500FT, APPLIED THE QRH MSG DISAPPEARED, RETURNED TO KORD WITH NO FURTHER ISSUE. (FLIGHT 5215 - FILED OPEN)
- [SDR SWIA2025091800017](https://openairdocs.org/sdr/SWIA2025091800017.md): Bleed Valve · warning message · Sep 17, 2025 · N218PS · Cndair CL6002B19 · Compressor Bleed Valve
  > R 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 SYS
- [SDR SWIA202405280025](https://openairdocs.org/sdr/SWIA202405280025.md): Landing Gear · warning message · May 25, 2024 · N218PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON 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.
- [SDR SWIA202310130009](https://openairdocs.org/sdr/SWIA202310130009.md): Unknown · cracked · Oct 9, 2023 · N218PS · Cndair CL6002B19 · Flight Compartment Windows
  > TRANSFER 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 OF
- [SDR SWIA20230807006](https://openairdocs.org/sdr/SWIA20230807006.md): Unknown · warning message · Aug 6, 2023 · N218PS · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR 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 INDICA
- [SDR SWIA202304260001](https://openairdocs.org/sdr/SWIA202304260001.md): Unknown · gouged · Apr 20, 2023 · N218PS · Cndair CL6002B19 · Cargo/Baggage Doors
  > COMPLY 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 SK
- [SDR SWIA202304210001](https://openairdocs.org/sdr/SWIA202304210001.md): Unknown · gouged · Apr 20, 2023 · N218PS · Cndair CL6002B19 · Doors
  > COMPLY 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 PROGRESS
- [SDR SWIA2023012500019](https://openairdocs.org/sdr/SWIA2023012500019.md): Windshield · cracked · Jan 19, 2023 · N218PS · Cndair CL6002B19 · Flight Compartment Windows
  > L 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.
- [SDR SWIA202264049](https://openairdocs.org/sdr/SWIA202264049.md): None · corroded · Jan 8, 2022 · N218PS · Cndair CL6002B19 · Wing Structure
  > L/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 A
- [SDR SWIA202164044](https://openairdocs.org/sdr/SWIA202164044.md): None · corroded · Dec 20, 2021 · N218PS · Cndair CL6002B19 · Doors
  > CARGO 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 51-42-06
- [SDR SWIA202164056](https://openairdocs.org/sdr/SWIA202164056.md): None · damaged · Dec 7, 2021 · N218PS · Cndair CL6002B19 · Ailerons
  > INSTALL 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
- [SDR SWIA202164030](https://openairdocs.org/sdr/SWIA202164030.md): None · worn · Nov 12, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > REPLACE 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 COMPLET
- [SDR SWIA202164029](https://openairdocs.org/sdr/SWIA202164029.md): None · damaged · Nov 4, 2021 · N218PS · Cndair CL6002B19 · Fuselage Structure (General)
  > 2 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
- [SDR SWIA202164043](https://openairdocs.org/sdr/SWIA202164043.md): None · corroded · Sep 28, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RIGHT 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 CRJ2
- [SDR SWIA202164055](https://openairdocs.org/sdr/SWIA202164055.md): None · damaged · Sep 20, 2021 · N218PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > REPLACE 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 71-14-01
- [SDR SWIA202164054](https://openairdocs.org/sdr/SWIA202164054.md): None · mislocated · Sep 17, 2021 · N218PS · Cndair CL6002B19 · Fuselage Structure (General)
  > UPPER 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-AG1132-5AUG2022
- [SDR SWIA202164035](https://openairdocs.org/sdr/SWIA202164035.md): None · gouged · Sep 15, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT 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 53-01-11-400-802
- [SDR SWIA202164034](https://openairdocs.org/sdr/SWIA202164034.md): None · gouged · Sep 15, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT 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 53-01-11-400-802
- [SDR SWIA202164028](https://openairdocs.org/sdr/SWIA202164028.md): None · corroded · Sep 14, 2021 · N218PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > L/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 0.07
- [SDR SWIA202164027](https://openairdocs.org/sdr/SWIA202164027.md): None · corroded · Sep 14, 2021 · N218PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > L/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.
- [SDR SWIA202164026](https://openairdocs.org/sdr/SWIA202164026.md): None · corroded · Sep 14, 2021 · N218PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/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"
- [SDR SWIA202164025](https://openairdocs.org/sdr/SWIA202164025.md): None · corroded · Sep 14, 2021 · N218PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/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 THIC
- [SDR SWIA202164033](https://openairdocs.org/sdr/SWIA202164033.md): None · gouged · Sep 12, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > F/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 /
- [SDR SWIA202164032](https://openairdocs.org/sdr/SWIA202164032.md): None · gouged · Sep 12, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > F/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-
- [SDR SWIA202164031](https://openairdocs.org/sdr/SWIA202164031.md): None · gouged · Sep 12, 2021 · N218PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > F/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-
- [SDR SWIA202164042](https://openairdocs.org/sdr/SWIA202164042.md): None · cracked · Sep 11, 2021 · N218PS · Cndair CL6002B19 · Fuselage Main, Keel
  > FS 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 IDENTIFIE
- [SDR SWIA202164041](https://openairdocs.org/sdr/SWIA202164041.md): None · corroded · Sep 2, 2021 · N218PS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > R/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 DA
- [SDR SWIA202164024](https://openairdocs.org/sdr/SWIA202164024.md): None · dented · Aug 22, 2021 · N218PS · Cndair CL6002B19 · Fuselage Structure (General)
  > THERE'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 B
- [SDR SWIA202164045](https://openairdocs.org/sdr/SWIA202164045.md): None · broken · Aug 21, 2021 · N218PS · Cndair CL6002B19 · Galley Doors
  > SERVICE 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 52-41-00
- [SDR SWIA202164040](https://openairdocs.org/sdr/SWIA202164040.md): None · corroded · Aug 20, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > L/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-OCT21
- [SDR SWIA202164039](https://openairdocs.org/sdr/SWIA202164039.md): None · corroded · Aug 20, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > L/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 22
- [SDR SWIA202164038](https://openairdocs.org/sdr/SWIA202164038.md): None · corroded · Aug 20, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > I/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 2022
- [SDR SWIA202164048](https://openairdocs.org/sdr/SWIA202164048.md): None · corroded · Aug 17, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > R/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 51-21-06
- [SDR SWIA202164037](https://openairdocs.org/sdr/SWIA202164037.md): None · corroded · Aug 17, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > R/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
- [SDR SWIA202164036](https://openairdocs.org/sdr/SWIA202164036.md): None · corroded · Aug 17, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > L/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 WRE
- [SDR SWIA202164053](https://openairdocs.org/sdr/SWIA202164053.md): None · damaged · Aug 12, 2021 · N218PS · Cndair CL6002B19 · Ailerons
  > REMOVE 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 / TORQ
- [SDR SWIA202164052](https://openairdocs.org/sdr/SWIA202164052.md): None · damaged · Aug 12, 2021 · N218PS · Cndair CL6002B19 · Ailerons
  > REMOVE 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.
- [SDR SWIA202164050](https://openairdocs.org/sdr/SWIA202164050.md): None · damaged · Aug 12, 2021 · N218PS · Cndair CL6002B19 · Ailerons
  > REMOVE 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 C
- [SDR SWIA202164047](https://openairdocs.org/sdr/SWIA202164047.md): None · worn · Jun 2, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > REMOVE 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 COMPLETE
- [SDR SWIA202164046](https://openairdocs.org/sdr/SWIA202164046.md): None · worn · Jun 2, 2021 · N218PS · Cndair CL6002B19 · Wing Structure
  > REMOVE 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
- [SDR VNAA2020022871102](https://openairdocs.org/sdr/VNAA2020022871102.md): Unknown · pressure loss · Feb 27, 2020 · N218PS · Cndair CL6002B19 · Cabin Pressure Control System
  > ON 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 CPCP
- [SDR VNAA2020010431103](https://openairdocs.org/sdr/VNAA2020010431103.md): Warning Message · false activation · Jan 3, 2020 · N218PS · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > CREW 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 T
- [SDR VNAA2019112899901](https://openairdocs.org/sdr/VNAA2019112899901.md): Skin · cracked · Nov 28, 2019 · N218PS · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK 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.
- [SDR VNAA2019011511102](https://openairdocs.org/sdr/VNAA2019011511102.md): Control Unit · unknown · Jan 15, 2019 · N218PS · Cndair CL6002B19 · Flight Control System
  > SUPPLEMENTAL INFORMATION: MX C/W FUNCTIONAL CHECK OF HSTCU IAW CRJ200 AMM. FUNCTIONAL CHECK GOOD. OPS CHECK GOOD. OCF CHECK GOOD.
- [SDR VNAA2019011501101](https://openairdocs.org/sdr/VNAA2019011501101.md): Warning System · activated · Jan 15, 2019 · N218PS · Cndair CL6002B19 · Stabilizer Position Indicating
  > AS 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.

Next page: https://openairdocs.org/aircraft/N218PS/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 = 'N218PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N218PS/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.