# Service difficulty reports: N237PS, cancelled Dec 9, 2025

A list on [N237PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N237PS-2025-12-09.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 · 61 reports

- [SDR VNAA2019122531102](https://openairdocs.org/sdr/VNAA2019122531102.md): Reflector · bent · Dec 23, 2019 · N237PS · Cndair CL6002B19 · Emergency Equipment
  > FLOOR REFLECTIVE STRIP WAS FOUND BENT OUT OF PLACE. MAINTENANCE REMOVED AND REPLACED EMERENCY LIGHT FLOOR STRIP TRACK. AND OPERATIONS CHECKED GOOD.
- [SDR VNAA2019121711101](https://openairdocs.org/sdr/VNAA2019121711101.md): Engine · smoke · Dec 17, 2019 · N237PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AFTER PUSHBACK WHEN THE FO STARTED THE RH ENG LOTS OF SMOKE CAME OUT AND WAS BLOWING PAST THE COCKPIT AND FUMES FILLED THE CABIN AND COCKPIT AND CAPTAIN STATED HE NEVER SEEN THAT MUCH SMOKE ON START UP. CREW FELT THERE MIGHT BE AN ISSUE SO START ABORTED, RETUR
- [SDR VNAA2019040231101](https://openairdocs.org/sdr/VNAA2019040231101.md): Coalescer Bag · odor · Mar 3, 2019 · N237PS · Cndair CL6002B19 · Air Distribution System
  > STRONG SMELL OF SMOKE IN COCKPIT AND CABIN AFTER ENGINE SHUTDOWN AT GATE. GROUND CREW NOTICED SMOKE DURING TAXI. REMOVED AND REPLACED LH AND RH COALESCERS BAGS IAW CRJ 200 AMM 21-51-13-040-801. APU OPS CHECK GOOD. THIS CLEARS MEL."
- [SDR VNAA2018080899906](https://openairdocs.org/sdr/VNAA2018080899906.md): Floor Support · corroded · Aug 8, 2018 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION AROUND FASTENER HOLES ON THE LT PRESSURE FLOOR SUPPORT, BS 409+128 AND 559. COMPLIED WITH A REPAIR IAW REO 601R-53-41-666, & REO 601R-53-41-2350.
- [SDR VNAA2018080899905](https://openairdocs.org/sdr/VNAA2018080899905.md): Strap · corroded · Aug 8, 2018 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR STRAP WAS CORRODED AT BS 559 BETWEEN RBL 27 AND RBL 36. LOCATED AND DRILLED A NEW STRAP IAW SRM 51-40-11.
- [SDR VNAA2018080899904](https://openairdocs.org/sdr/VNAA2018080899904.md): Bulkhead Web · cracked · Aug 8, 2018 · N237PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB AT BS 621 HAD MULTIPLE INDICATIONS AT BL 0, WL 112, TWO INCHES LONG, 70% FSH, FAILED NDT. PERFORMED A MAJOR REPAIR TO THE WEB IAW REO 601R-53-61-1285, REV E.
- [SDR VNAA2018080899903](https://openairdocs.org/sdr/VNAA2018080899903.md): Seat Track · corroded · Aug 8, 2018 · N237PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BETWEEN BS 409 TO 409+128, LBL 9 WAS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802.
- [SDR VNAA2018080899902](https://openairdocs.org/sdr/VNAA2018080899902.md): Seat Track · corroded · Aug 8, 2018 · N237PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FROM BS 394 - 409+128, RBL 9 WAS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802.
- [SDR VNAA2018080899901](https://openairdocs.org/sdr/VNAA2018080899901.md): Seat Track · corroded · Aug 8, 2018 · N237PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FROM BS 364 TO 394, RBL 9 WAS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND 53-01-11-400-802.
- [SDR VNAA2017092511102](https://openairdocs.org/sdr/VNAA2017092511102.md): Switch · malfunctioned · Sep 25, 2017 · N237PS · Cndair CL6002B19 · Engine Cranking
  > WHILE IN CRUISE, CREW RECEIVED A NO STARTER CUTOUT MESSAGE. THE CREW RAN THE QRH WHICH ADVISED THEM TO LAND AT THE NEAREST SUITABLE AIRPORT. DECLARED AN EMERGENCY AND DIVERTED AND LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE SWAPPED SPEED SWITCHES, CHECK GO
- [SDR VNAA2016072500026](https://openairdocs.org/sdr/VNAA2016072500026.md): Bulkhead Web · cracked · Jul 25, 2016 · N237PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD WEB CRACKED AT LBL 27.50, 0.100 LONG AT TOP OF CARGO DOOR AFT TRACK. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE FS 621 PRESSURE BULKHEAD WEB, LBL 27.50 AT TOP OF CARGO DOOR AFT TRACK IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK M
- [SDR VNAA2016072400023](https://openairdocs.org/sdr/VNAA2016072400023.md): Stringer · cracked · Jul 24, 2016 · N237PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED AT BS 379. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE STRINGER IAW AMM.
- [SDR VNAA2016072300022](https://openairdocs.org/sdr/VNAA2016072300022.md): Floor Support · corroded · Jul 23, 2016 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT HAND FLOOR SUPPORT CAP CORRODED LBL 27 BETWEEN BS 589 - 605. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW AMM.
- [SDR VNAA2016072300021](https://openairdocs.org/sdr/VNAA2016072300021.md): Floor Support · corroded · Jul 23, 2016 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT CORRODED RBL 45 BETWEEN BS 559+80 AND 621. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW AMM.
- [SDR VNAA2016072100019](https://openairdocs.org/sdr/VNAA2016072100019.md): Frame · corroded · Jul 21, 2016 · N237PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 349 CORRODED BETWEEN STR 26L AND 26R. MAINTENANCE R & R FS 349 FRAME SEGMENT BETWEEN STR 26L AND 26R IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.
- [SDR VNAA2016060600008](https://openairdocs.org/sdr/VNAA2016060600008.md): Switch · out of position · Jun 6, 2016 · N237PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > MASTER WARNING NOSE DOOR OPEN AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RETURNED NOSE DOOR SWITCH TO NORMAL POSITION AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016031400018](https://openairdocs.org/sdr/VNAA2016031400018.md): Switch · failed · Mar 14, 2016 · N237PS · Cndair CL6002B19 · Engine Thrust Reverser
  > CREW REPORTED LT THRUST REVERSER UNLOCK AMBER CAUTION MESSAGE AND THAT EMERGENCY STOW DID NOT WORK. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT STOW MICROSWITCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2016031400017](https://openairdocs.org/sdr/VNAA2016031400017.md): Drive Unit · failed · Mar 14, 2016 · N237PS · Cndair CL6002B19 · Engine Thrust Reverser
  > CREW REPORTED LT THRUST REVERSER UNLOCK AMBER CAUTION MESSAGE AND THAT EMERGENCY STOW DID NOT WORK. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT POWER DRIVE UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2016022000028](https://openairdocs.org/sdr/VNAA2016022000028.md): Wire · broken · Feb 20, 2016 · N237PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED EMERGENCY FLOOR LIGHT NOT OPERATING FROM ROW 8 TO 13. MAINTENANCE INSPECTED, INSTALLED NEW CONNECTOR ON LIGHTING WIRE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015032100025](https://openairdocs.org/sdr/VNAA2015032100025.md): Tire · failed · Mar 21, 2015 · N237PS · Cndair CL6002B19 · Tire
  > ON POST FLIGHT INSPECTION, CREW REPORTED TREAD SEPARATION FROM RT INBD MAIN TIRE. MAINTENANCE INSPECTED AND R & R NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES. MAINTENANCE ALSO R & R THE FOLLOWING DUE TO DAMAGE CAUSED BY THE TREAD SEPARATION FROM THE NR 3 TIRE: RT INB
- [SDR VNAA2015030900018](https://openairdocs.org/sdr/VNAA2015030900018.md): Light · inoperative · Mar 9, 2015 · N237PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED EMERGENCY EXIT GLOW STRIPS PEELING UP FROM FLOOR ROW 11. MAINTENANCE INSPECTED, R & R EMERGENCY FLOOR ESCAPE PATH LAMP STRIP AT SEAT 12 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015021600011](https://openairdocs.org/sdr/VNAA2015021600011.md): Transducer · failed · Feb 16, 2015 · N237PS · Cndair CL6002B19 · Engine Oil Pressure
  > CREW REPORTED LT ENGINE OIL PRESSURE DROP ON CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT ENGINE OIL PRESSURE TRANSDUCER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014121200004](https://openairdocs.org/sdr/VNAA2014121200004.md): Light · failed · Dec 12, 2014 · N237PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED, R & R THE EMERGENCY LIGHT STRIP AT ROW 1 D/F AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014091800006](https://openairdocs.org/sdr/VNAA2014091800006.md): Floor Support · corroded · Sep 18, 2014 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE, THE FLOOR SUPPORT BETWEEN BS 310 - 349 LBL 45, FOUND CORRODED. R & R 1 IAW SRM 51-42-06, 51-42-21 AND 51-40-11.
- [SDR VNAA2014091800005](https://openairdocs.org/sdr/VNAA2014091800005.md): Seat Track · corroded · Sep 18, 2014 · N237PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DURING SCHEDULED MAINTENANCE, THE SEAT TRACK FROM BS 559 +110 - 565, LBL9, WAS FOUND CORRODED AT THE ATTACHMENT HOLES. R & R THE SEAT TRACK IAW AMM 20-21-00-910-801.
- [SDR VNAA2014091800004](https://openairdocs.org/sdr/VNAA2014091800004.md): Skin · dented · Sep 18, 2014 · N237PS · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP PANEL HAS A LARGE DENT ON INBD BOTTOM SIDE APPROXIMATELY 3" WIDE X 0.30" DEPTH. PERFORMED REPAIR TO RT INBD FLAP LOWER SKIN PANEL IAW AMM AND RETURNED TO SERVICE.
- [SDR VNAA2014051800012](https://openairdocs.org/sdr/VNAA2014051800012.md): Sign · inoperative · May 18, 2014 · N237PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED LOWER LEFT EMERGENCY EXIT LIGHTED SIGN WAS OUT. MAINTENANCE INSPECTED, R & R LOWER LT EMERGENCY EXIT LIGHTED SIGN AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014051700011](https://openairdocs.org/sdr/VNAA2014051700011.md): Engine · surges · May 17, 2014 · N237PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CREW REPORTED LT ENGINE BEGAN TO SURGE IN POWER IMMEDIATELY AFTER TAKEOFF, DROPPING AND SPIKING UP TO 5 PERCENT N1. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED GROUND ENGINE RUN AND FOUND LT ENGINE N1 SURGING ABOVE 80 PERCENT N1
- [SDR VNAA2013111100007](https://openairdocs.org/sdr/VNAA2013111100007.md): Control Handle · failed · Nov 11, 2013 · N237PS · Cndair CL6002B19 · Landing Gear Selector
  > AFTER TAKEOFF, CREW REPORTED GEAR DID NOT RETRACT WITH PARKING BRAKE SHUTOFF VALVE FAIL AND INBD ANTI-SKID CAS MESSAGES. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT, R & R LANDING GEAR CONTROL HANDLE AND PERFORMED CHECKS IAW AMM. ACFT RELEA
- [SDR VNAA2013110200001](https://openairdocs.org/sdr/VNAA2013110200001.md): Target · loose · Nov 2, 2013 · N237PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED GEAR DISAGREE AND LT MAIN WOULD NOT RETRACT. CREW RETURNED TO FIELD AND LANDED SAFELY. MX INSPECTED, FOUND LT UPLOCK PROXIMITY SENSOR TARGET LOOSE, TIGHTENED UPLOCK SENSOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013071800009](https://openairdocs.org/sdr/VNAA2013071800009.md): Controller · failed · Jul 12, 2013 · N237PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > CREW REPORTED LT WINDSHIELD CRACKED AT 33,000 FT. CREW DIVERTED AND LANDED SAFELY. MX INSPECTED, R & R LT WINDSHIELD AND LT WINDSHIELD TEMP CONTROLLER AND PERFORMED CHECKS USING AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2012122500015](https://openairdocs.org/sdr/VNAA2012122500015.md): Anti-Ice Valve · failed · Dec 25, 2012 · N237PS · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > CREW REPORTED LEFT COWL ANTI ICE VALVE WOULD NOT OPEN. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TOUBLESHOT, REMOVED, REPLACED, AND OPERATION CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012090300018](https://openairdocs.org/sdr/VNAA2012090300018.md): Bulkhead · cracked · Aug 28, 2012 · N237PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE PRESSURE BULKHEAD AT 202.75 HAS A 2 INCH CRACK. THE FS 202.75 PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012081700009](https://openairdocs.org/sdr/VNAA2012081700009.md): Door · not closed · Aug 13, 2012 · N237PS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE AFTER DEPARTURE. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT AND FOUND AFT CARGO DOOR NOT FULLY CLOSED. MAINTENANCE CLOSED DOOR AND PERFORMED OPERATIONAL CHECKS USING AIRCRAFT
- [SDR VNAA2012080800003](https://openairdocs.org/sdr/VNAA2012080800003.md): Throttle Cable · broken · Aug 8, 2012 · N237PS · Cndair CL6002B19 · Power Lever
  > AT 7,000 FEET ON CLIMBOUT, CREW REPORTED LEFT ENGINE DID NOT RESPOND TO THRUST LEVER COMMANDS. CREW FOLLOWED QRH AND SHUT DOWN NUMBER ONE ENGINE. BRINGING THRUST LEVER TO SHUT OFF DID SHUT DOWN ENGINE SUCCESSFULLY. CREW RETURNED TO FIELD AND LANDED WITHOUT
- [SDR VNAA2011112100018](https://openairdocs.org/sdr/VNAA2011112100018.md): Reservoir · failed · Nov 21, 2011 · N237PS · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > CREW REPORTED HYDRAULIC NR 2 LOW PRESSURE IN LEVEL FLIGHT. CREW DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE NR 2 RESERVOIR USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR
- [SDR VNAA2011080300039](https://openairdocs.org/sdr/VNAA2011080300039.md): Post · cracked · Jul 30, 2011 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE LEFT AND RIGHT VERTICLE POST FS409+128 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011080300038](https://openairdocs.org/sdr/VNAA2011080300038.md): Sill · corroded · Jul 30, 2011 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE LEFT AND RIGHT PRESSURE FLOOR SILL AT FS 559.0 HAD AREAS OF CORROSION ON THE FLOOR SILL ANGLE. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011080300037](https://openairdocs.org/sdr/VNAA2011080300037.md): Sill · corroded · Jul 30, 2011 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE LEFT PRESSURE FLOOR SILL AT FS 513.0 HAD AREAS OF CORROSION AROUND FASTENER NUT PLATE. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011080300036](https://openairdocs.org/sdr/VNAA2011080300036.md): Sill · corroded · Jul 30, 2011 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE LEFT PRESSURE FLOOR SILL FROM FS424.0 TO 449.85 HAD AREAS OF CORROSION AROUND FASTENER NUT PLATES. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011080300035](https://openairdocs.org/sdr/VNAA2011080300035.md): Structure · dented · Jul 30, 2011 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE A PROTRUDING DENT BETWEEN FS 574.0 AND FS 589.0. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011080300034](https://openairdocs.org/sdr/VNAA2011080300034.md): Beam · damaged · Jul 30, 2011 · N237PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED AND CORRODED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011070400028](https://openairdocs.org/sdr/VNAA2011070400028.md): Ahrs · failed · Jun 29, 2011 · N237PS · Cndair CL6002B19 · Integrated Flight System
  > AFTER TAKEOFF CAPT'S ED NR 1 SHOWED AMBER PTTCH & ROLL. ALSO, LOST ATT DATA. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CH
- [SDR VNAA2011030800003](https://openairdocs.org/sdr/VNAA2011030800003.md): Unknown · malfunctioned · Mar 6, 2011 · N237PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > CREW REPORTED GEAR DISAGREE (UP POSITION) DURING CLIMB AFTER DEPARTURE FROM AVL. GEAR WAS NOT IN TRANSIT AT THE TIME. CREW CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS ON THE LANDING GEAR EXTENSION / RETRACTION SYSTEM USING THE
- [SDR VNAA2010120900001](https://openairdocs.org/sdr/VNAA2010120900001.md): Detector · malfunctioned · Dec 2, 2010 · N237PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > WHILE ON APPROACH TO PHL, CREW REPORTED A FLAP FAIL CAUTION MESSAGE WHEN THE FLAP HANDLE WAS MOVED TO 30 DEGREES. FLAPS WERE STUCK AT 20 DEGREES. CREW LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE SKE
- [SDR VNAA2010071500009](https://openairdocs.org/sdr/VNAA2010071500009.md): Bulkhead · cracked · Jul 7, 2010 · N237PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING MAINTENANCE A CRACK WAS FOUND ON THE PRESSURE BULKHEAD FS 559 AND WEB CAP. MAINTENANCE REPAIRED AIRCRAFT USING AIRCRAFT MANUALS AND RELEASED AIRCRAFT FOR SERVICE.
- [SDR VNAA2009042600015](https://openairdocs.org/sdr/VNAA2009042600015.md): Structure · damaged · Apr 21, 2009 · N237PS · Cndair CL6002B19 · Elevator Miscellaneous Structure
  > CREW REPORTED A LIGHTNING STRIKE IN CLT. MAINTENANCE INSPECTED AND REPAIRED DAMAGE TO THE ELEVATOR PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR VNAA2009040600003](https://openairdocs.org/sdr/VNAA2009040600003.md): Wire Harness · failed · Apr 2, 2009 · N237PS · Cndair CL6002B19 · Engine Exhaust System Wiring
  > CREW REPORTED AFTER ENGINE START THE LEFT ENGINE ITT STABILIZED LOWER THAN NORMAL. AIRCRAFT RETURNED TO GATE IN CLT. MAINTENANCE REMOVED AND REPLACED THE LEFT ITT HARNESS PER THE MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA0808012](https://openairdocs.org/sdr/VNAA0808012.md): Gearbox · failed · Aug 23, 2008 · N237PS · Cndair CL6002B19 · Turbine Engine Accessory Drive
  > CREW REPORTED THE LT ENGINE FAILED ON CLIMBOUT. CREW ELECTED TO DIVERT TO IAD LANDING WITHOUT INCIDENT. MX INSPECTED ENGINE AND FOUND THE LT GEARBOX FAILED. GEARBOX WAS R&R. CHECKS WERE COMPLETED AND NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0807014](https://openairdocs.org/sdr/VNAA0807014.md): A/C Pack · failed · Jul 24, 2008 · N237PS · Cndair CL6002B19 · Cabin Cooling System
  > CREW REPORTED, THE LT PACK TEMP TO BE 113 DEG C AND UNCONTROLLABLE IN AUTO OR MANUAL. CREW ELECTED TO RETURN TO DTW LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LT AIR CYCLE MACHINE. CHECKS WERE ACCOMPLISHED WITH

Next page: https://openairdocs.org/deregistered/N237PS-2025-12-09/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 = 'N237PS' AND deregistration_id = 'N237PS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N237PS-2025-12-09/reports

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