# Service difficulty reports: N209PS

A list on [N209PS](https://openairdocs.org/aircraft/N209PS.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 2 · 91 reports

- [SDR VNAA2020032511101](https://openairdocs.org/sdr/VNAA2020032511101.md): Apu · failed · Mar 22, 2020 · N209PS · Cndair CL6002B19 · APU Core Engine
  > NOTICED HEAVY SMOKE COMING OUT OF APU INLET WHEN PWR/FUEL PBA PRESSED IN. INSPECTED. NO FIRE DAMAGE NOTED. REMOVED AND REPLACED APU. OPS CHECK GOOD.
- [SDR VNAA2019122081102](https://openairdocs.org/sdr/VNAA2019122081102.md): Battery · discharged · Dec 18, 2019 · N209PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK 4 ILLUMINATE FOR A FEW SECONDS THEN EXTINGUISH. R/R NUMBER 4 EMERGENCY LIGHT BATTERY PACK IAW CRJ-200 AMM 33-51-04-000/400-801 OPS CHECK GOOD
- [SDR VNAA201910121103](https://openairdocs.org/sdr/VNAA201910121103.md): Transducer · failed · Oct 11, 2019 · N209PS · Cndair CL6002B19 · Landing Gear Brake System
  > JUST AS THEY STARTED THEIR TAKE OFF RUN, AT APPROX 20-30KTS CREW RECEIVED ANTI SKID OUTBOARD CAUTION MESSAGE. THEY ABORTED THE TAKE OFF AND SAFELY TAXI OFF OF THE RUNWAY AND CONTACTED MAINTENANCE. THEY WERE UNABLE TO CORRECT THE ISSUE AND RETURNED TO THE GATE.
- [SDR VNAA2019091511104](https://openairdocs.org/sdr/VNAA2019091511104.md): Control Handle · faulty · Sep 15, 2019 · N209PS · Cndair CL6002B19 · Landing Gear Selector
  > DURING INITIAL CLIMB, THE AIRCRAFT'S LANDING GEAR WOULD NOT RETRACT. THE CREW DECLARED AN EMERGENCY AND DECIDED TO DIVERT TO IAD. AS THE CREW WAS BEING VECTORED TO IAD, THE GEAR THEN DID RETRACT. THE CREW WAS ABLE TO RE-EXTEND LANDING GEAR FOR THE LANDING. THE
- [SDR VNAA2019091511101](https://openairdocs.org/sdr/VNAA2019091511101.md): Hydraulic System · low · Sep 15, 2019 · N209PS · Cndair CL6002B19 · Hydraulic System, Main
  > ON CLIMB OUT FROM BUF, CREW RECEIVED A GEAR DISAGREE MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. EMERGENCY WAS DECLARED. FLIGHT LANDED WITH OUT FURTHER INCIDENT AND TAXIED BACK TO GATE. DEFERRED LANDING GEAR RETRACTION SYSTEM. SERVICED #1, 2, 3 HYDRAALICS
- [SDR VNAA2019040111101](https://openairdocs.org/sdr/VNAA2019040111101.md): Battery Pack · failed · Apr 1, 2019 · N209PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY BATTERY WILL NOT STAY ON. REMOVED AND REPLACED 4 BATTERY PACKS IAW CRJ 200 AMM 33-51-04-000/400-801 OPS CK GOOD. #1 P/N AD2013-1A S/N 69914, #2 S/N 122491, #3 S/N 89779, #4 S/N 187402
- [SDR VNAA2018110711102](https://openairdocs.org/sdr/VNAA2018110711102.md): Proximity Sensor · out of adjust · Nov 7, 2018 · N209PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKEOFF, THE CREW REPORTED A GEAR DISAGREE, THE NLG WOULD NOT RETRACT, BOTH MAINS RETRACTED WITHOUT ISSUE. WE DEFERRED THE LANDING GEAR RETRACTION SYSTEM AND THE AIRCRAFT FLEW ON TO CLT. ADJUSTED PROX SENSOR PS13 IAW CRJ 200 AMM OPS CHECK GOOD.
- [SDR VNAA2018100911101](https://openairdocs.org/sdr/VNAA2018100911101.md): Warning System · false activation · Oct 8, 2018 · N209PS · Cndair CL6002B19 · APU Oil System
  > THE CREW RECEIVED AN APU OIL TEMP CAUTION WITH THE NR 2 IDG ON DEFERRAL. THE AIRCRAFT DIVERTED AND DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE APU OIL LEVEL AND DELTA P WITH NO DEFECTS. OPERATIONAL CHECK GOOD. / 209
- [SDR VNAA2018071711101](https://openairdocs.org/sdr/VNAA2018071711101.md): Shutoff Valve · leaking · Jul 17, 2018 · N209PS · Cndair CL6002B19 · APU Engine Fuel and Control
  > FUEL SMELL FROM BOTH PACKS AT FL18. R&R APU SOV, OPS AND LEAK CK GOOD.
- [SDR VNAA2018060599909](https://openairdocs.org/sdr/VNAA2018060599909.md): Strap · corroded · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT & RT FLOORBEAM STRAP AT BS 559 BETWEEN RBL 27 AND RBL 43 WAS CORRODED. REPLACED THE STRAP.
- [SDR VNAA2018060599908](https://openairdocs.org/sdr/VNAA2018060599908.md): Support Fitting · cracked · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT MLG LOWER WING PLANK HAD AN INDICATION 100% FSH AT THE LOWER EDGE OF THE MOST AFT FASTENER HOLE, INBD. FAILED NDT. REPAIRED THE DAMAGE IAW REO 601R-57-21-2793
- [SDR VNAA2018060599907](https://openairdocs.org/sdr/VNAA2018060599907.md): Floorbeam · corroded · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 27, FLOORBEAM ANGLE HAD CORROSION AT BS 615. REPLACED THE FLOORBEAM ANGLE.
- [SDR VNAA2018060599906](https://openairdocs.org/sdr/VNAA2018060599906.md): Seat Track · corroded · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED FROM BS 559+80 TO 621. REPLACED THE SEAT TRACK.
- [SDR VNAA2018060599905](https://openairdocs.org/sdr/VNAA2018060599905.md): Seat Track · corroded · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. REPLACED THE SEAT TRACK.
- [SDR VNAA2018060599904](https://openairdocs.org/sdr/VNAA2018060599904.md): Bulkhead Web · cracked · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB, BS 621, RBL 18.00, WL 110 HAD MULITPLE INDICATIONS NOTED, APPROXIMATELY 4 INCHES LONG, 50% FSH. FAILED NDT INSPECTION. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.
- [SDR VNAA2018060599903](https://openairdocs.org/sdr/VNAA2018060599903.md): Stringer · corroded · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L WAS CRACKED AT BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03.
- [SDR VNAA2018060599902](https://openairdocs.org/sdr/VNAA2018060599902.md): Stringer · corroded · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L WAS CRACKED AT BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03.
- [SDR VNAA2018060590002](https://openairdocs.org/sdr/VNAA2018060590002.md): Floor Support · corroded · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT WAS CORRODED, BS 574 TO 621 ON UPPER AND LOWER SURFACE. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-61-1574, REV B.
- [SDR VNAA2018060599901](https://openairdocs.org/sdr/VNAA2018060599901.md): Floorbeam · corroded · Jun 2, 2018 · N209PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM ANGLE WAS CORRODED AROUND 2 EA FASTENER HOLES, BETWEEN LBL 9 AND RBL 9. FABRICATED AND FIT A NEW FLOORBEAM ANGLE IAW REO 601R-53-11-926.
- [SDR VNAA2017102211101](https://openairdocs.org/sdr/VNAA2017102211101.md): Wire Harness · malfunctioned · Oct 22, 2017 · N209PS · Cndair CL6002B19 · Landing Gear System Wiring
  > DURING CRUISE, AT 27,000 FEET, GEAR INDICATIONS APPEARED ON THE EICAS WITH AMBER DASHED LINES FOR NOSE GEAR FLUCTUATING THEN CAME ON SOLID RED THEN GEAR DISAGREE MESSAGE APPEARED ON EICAS CREW REPORTED GEAR RETRACTION HAD BEEN NORMAL, AND AFTER FOLLOWING QRH T
- [SDR VNAA201710110001](https://openairdocs.org/sdr/VNAA201710110001.md): Priority Valve · failed · Oct 11, 2017 · N209PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISSAGREE MESSAGE AFTER TAKE OFF. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. MX R & R THE NLG PRIORITY VALVE OPS CHECKED GOOD.
- [SDR VNAA2017090701101](https://openairdocs.org/sdr/VNAA2017090701101.md): Switch · faulty · Sep 7, 2017 · N209PS · Cndair CL6002B19 · Exterior Lighting
  > AFTER LANDING, CREW REPORTED SMOKE FROM AROUND THE STANDBY COMPASS AND THE FO WAS SHOCKED BY THE OVERHEAD PANEL. REMOVED AND REPLACED NOSE LANDING LIGHT SWITCH IAW CMM 33-41-07-OPS CHECKS GOOD AT THIS TIME.
- [SDR VNAA2017041700016](https://openairdocs.org/sdr/VNAA2017041700016.md): Proximity Switch · faulty · Apr 17, 2017 · N209PS · Cndair CL6002B19 · Door Warning System
  > SERVICE DOOR INDICATION SYSTEM INOPERATIVE. REMOVED AND REPLACED THE SERVICE DOOR OUTER HANDLE PROXIMITY SWITCH.
- [SDR VNAA2016070700010](https://openairdocs.org/sdr/VNAA2016070700010.md): Stiffener · cracked · Jul 7, 2016 · N209PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128 RBL 18 INBOARD AND OUTBOARD SIDE VERTICAL STIFFENERS CRACKED. MAINTENANCE PERFORMED A MAJOR REPAIR TO FS 409+128 RBL 18 INBOARD AND OUTBOARD VERTICAL STIFFENERS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.
- [SDR VNAA2016070400008](https://openairdocs.org/sdr/VNAA2016070400008.md): Frame · corroded · Jul 4, 2016 · N209PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 349 CORRODED BETWEEN STR 26L AND STR 26R. MAINTENANCE R & R FS 349 FRAME SEGMENT BETWEEN STR 26L AND STR 26R AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.
- [SDR VNAA2016070400007](https://openairdocs.org/sdr/VNAA2016070400007.md): Frame · corroded · Jul 4, 2016 · N209PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME, FS 319 CORRODED BETWEEN 25R AND 26R. MAINTENANCE R & R FS 319, FRAME SEGMENT BETWEEN STR 25R AND 26R AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.
- [SDR VNAA2016070400006](https://openairdocs.org/sdr/VNAA2016070400006.md): Frame · corroded · Jul 4, 2016 · N209PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME, FS 333 CORRODED BETWEEN 26L AND 25R. MAINTENANCE R & R FS 333 SEGMENT BETWEEN STR 26L AND 25R AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.
- [SDR VNAA2016070300004](https://openairdocs.org/sdr/VNAA2016070300004.md): Bulkhead · cracked · Jul 3, 2016 · N209PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB AROUND THE LINTEL ATTACHMENT FITTING FAILED NON-DESTRUCTIVE TESTING. MAINTENANCE PERFORMED A MAJOR REPAIR TO PRESSURE BULKHEAD WEB FS621, LINTEL INSTALLATION AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENA
- [SDR VNAA2016070300001](https://openairdocs.org/sdr/VNAA2016070300001.md): Stringer · corroded · Jul 3, 2016 · N209PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 27, CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 319 AND FS 349. MAINTENANCE PERFORMED A SPLICE REPAIR TO STR 27 BETWEEN FS319 AND FS 349 IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.
- [SDR VNAA2016062900034](https://openairdocs.org/sdr/VNAA2016062900034.md): Floor Support · corroded · Jun 29, 2016 · N209PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR SUPPORT LBL 27, BS 569 TO 621 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTNENANCE.
- [SDR VNAA2016021900025](https://openairdocs.org/sdr/VNAA2016021900025.md): Light · inoperative · Feb 19, 2016 · N209PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED ROW 1 FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED, R & R ROW 1 EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2016021700021](https://openairdocs.org/sdr/VNAA2016021700021.md): Sensor · failed · Feb 17, 2016 · N209PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > CREW REPORTED RECEIVING A FLAP FAIL MESSAGE AT FL 290. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE BRAKE AND POSITIONING SENSOR UNIT. MAINTENANCE PERFORMED CHECKS IAW THE AM
- [SDR VNAA2015122800017](https://openairdocs.org/sdr/VNAA2015122800017.md): Connector · broken · Dec 28, 2015 · N209PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING STRIP FROM ROW 9 AFT INOPERATIVE. MAINTENANCE INSPECTED, REPLACED BROKEN PIN CONNECTION AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015080500009](https://openairdocs.org/sdr/VNAA2015080500009.md): Shutoff Valve · failed · Aug 5, 2015 · N209PS · Cndair CL6002B19 · Pneumatic Distribution System
  > CREW REPORTED LT PACK DID NOT PRESSURIZE AND LT PRESSURE REGULATING SHUTOFF VALVE DID NOT WORK AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R TENTH STAGE SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEAS
- [SDR VNAA2014031300013](https://openairdocs.org/sdr/VNAA2014031300013.md): Lamp · inoperative · Mar 13, 2014 · N209PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED EXTERIOR, LT OVERWING AFT EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED, REPLACED LAMPS AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2014011100007](https://openairdocs.org/sdr/VNAA2014011100007.md): Radome · damaged · Jan 11, 2014 · N209PS · Cndair CL6002B19 · Aerodynamic Fairings
  > CREW REPORTED LIGHTNING STRIKE TO NOSE OF ACFT DURING FLIGHT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R RADOME.
- [SDR VNAA2013122200013](https://openairdocs.org/sdr/VNAA2013122200013.md): Windshield · cracked · Dec 22, 2013 · N209PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED CRACKED WINDSHIELD. MAINTENANCE TROUBLESHOT, R & R THE LEFT WINDSHIELD USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013101700006](https://openairdocs.org/sdr/VNAA2013101700006.md): Control Unit · failed · Oct 17, 2013 · N209PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED WOW INPUT INOPERATIVE CAUTION MESSAGE ON INITIAL TAKEOFF ROLL AND NOSE WHEEL STEERING INOPERATIVE. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MX TROUBLESHOT, R & R PSEU (PROXIMITY SENSOR ELECTRONIC UNIT) AND PERFORMED CHECKS IAW AMM. ACFT REL
- [SDR VNAA2013071300011](https://openairdocs.org/sdr/VNAA2013071300011.md): Connector · dirty · Jul 13, 2013 · N209PS · Cndair CL6002B19 · Landing Gear System Wiring
  > STEERING INOPERATIVE MESSAGE AS ACFT TOOK RUNWAY FOR DEPARTURE. PULLED OFF RUNWAY AND RETURNED TO GATE. MX INSPECTED, REMOVED, CLEANED AND REINSTALLED NOSE WHEEL STEERING CONNECTORS AND PERFORMED CHECKS USING AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013070200002](https://openairdocs.org/sdr/VNAA2013070200002.md): Light · damaged · Jul 2, 2013 · N209PS · Cndair CL6002B19 · Exterior Lighting
  > DURING APPROACH, A LIGHTNING STRIKE TO ACFT. ACFT LANDED WITHOUT INCIDENT. MX TROUBLESHOT, R & R THE UPPER TAIL NAVAGATION LIGHT ASSY, AND STATIC WICKS IAW ACFT MANUALS. CHECKS WERE PERFOMED IAW THE ACFT MANUALS AND ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013063000020](https://openairdocs.org/sdr/VNAA2013063000020.md): Radome · damaged · Jun 30, 2013 · N209PS · Cndair CL6002B19 · Aerodynamic Fairings
  > CREW REPORTED A LIGHTNING STRIKE TO AIRCRAFT. AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RADOME, RADAR ANTENNA, AND STATIC WICKS PER AIRCRAFT MANUALS. CHECKS WERE PERFOMED PER THE AIRCRAFT MAN
- [SDR VNAA2013050700003](https://openairdocs.org/sdr/VNAA2013050700003.md): Door Seal · defective · May 7, 2013 · N209PS · Cndair CL6002B19 · Passenger/Crew Doors
  > CREW REPORTED PASSENGER DOOR SQUEALING. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE DOOR SEAL PER AIRCRAFT MANUALS. CHECKS WERE PERFOMED PER THE AIRCRAFT MANUALS AND AIRCRAFT WAS RELEASED FOR SERV
- [SDR VNAA2013041200006](https://openairdocs.org/sdr/VNAA2013041200006.md): Modulating Valve · failed · Apr 12, 2013 · N209PS · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > CREW REPORTED WING OVERHEAT WARNING MESSAGE IN FLIGHT WITH WING ANTI-ICE SELECTED IN STANDBY MODE. NORMAL MODE WAS ON DEFERRAL PER MEL. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED LEFT MODULATING AND SHU
- [SDR VNAA2013031600011](https://openairdocs.org/sdr/VNAA2013031600011.md): Wire Harness · broken · Mar 16, 2013 · N209PS · Cndair CL6002B19 · Door System Wiring
  > CREW REPORTED PASSENGER DOOR WARNING AND SERVICE DOOR CAUTION MESSAGES AT 800 FEET AGL AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CARGO DOOR WIRING HARNESS BROKEN (CARGO DOOR INDICATION HAD PREVIOUSLY B
- [SDR VNAA2012062500009](https://openairdocs.org/sdr/VNAA2012062500009.md): Ballast · defective · Jun 25, 2012 · N209PS · Cndair CL6002B19 · Passenger Compartment Lighting
  > CREW REPORTED SLIGHT BURNING SMELL IN AREA OF ROWS 1-3. MAINTENANCE INSPECTED, REMOVED AND REPLACED BALLAST AND BULBS FOR BOARDING LIGHTS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2012062300006](https://openairdocs.org/sdr/VNAA2012062300006.md): Power Unit · malfunctioned · Jun 23, 2012 · N209PS · Cndair CL6002B19 · Passenger Compartment Lighting
  > CREW REPORTED STRONG ODOR COMING FROM AROUND ROW 3, POSSIBLY BURNING PLASTIC. MAINTENANCE INSPECTED AND FOUND POWER UNIT DIMMER AT ROW 4A/C TO HAVE STRONG BURNING SMELL. MAINTENANCE REMOVED AND REPLACED POWER UNIT AND PERFORMED CHECKS USING AIRCRAFT MAINTENA
- [SDR VNAA2012052800022](https://openairdocs.org/sdr/VNAA2012052800022.md): Transceiver · faulty · May 28, 2012 · N209PS · Cndair CL6002B19 · Weather Radar System
  > CREW REPORTED WEATHER RADAR ON CAPTAIN’S AND FIRST OFFICER’S MFD (MULTIFUNCTION DISPLAY) WILL NOT DISPLAY IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED WEATHER RADAR RECEIVER / TRANSMITTER AND AN
- [SDR VNAA2012030200016](https://openairdocs.org/sdr/VNAA2012030200016.md): Apu · failed · Feb 28, 2012 · N209PS · Cndair CL6002B19 · APU Core Engine
  > CREW REPORTED SMOKE LAV CAS MESSAGE ON TAXI IN, ACCOMPANIED BY STRONG SMELL OF SMOKE. CREW STOPPED AIRCRAFT SHORT OF JETBRIDGE AND PASSENGERS EVACUATED AIRCRAFT THROUGH PASSENGER DOOR. MAINTENANCE INSPECTED LAVATORY AND FOUND NO EVIDENCE OF FIRE OR SMOKE. M
- [SDR VNAA2011110900002](https://openairdocs.org/sdr/VNAA2011110900002.md): Engine · malfunctioned · Nov 4, 2011 · N209PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CREW REPORTED RIGHT ENGINE OIL PRESSURE WARNING MESSAGE AND RIGHT ENGINE OIL INDICATION READ ZERO ON DESCENT INTO PHL. CREW COMPLIED WITH QRH AND SHUT DOWN RIGHT ENGINE. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REP
- [SDR VNAA2011110300032](https://openairdocs.org/sdr/VNAA2011110300032.md): Control Unit · failed · Oct 30, 2011 · N209PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL AT 20 DEGREES DURING APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AI

Next page: https://openairdocs.org/aircraft/N209PS/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 = 'N209PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N209PS/reports

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