# Service difficulty reports: N259PS, cancelled Dec 9, 2025

A list on [N259PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N259PS-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 · 75 reports

- [SDR SWIA202157575](https://openairdocs.org/sdr/SWIA202157575.md): Cabin Air Sys · odor · Apr 15, 2021 · N259PS · Cndair CL6002B19 · Air Distribution System
  > DURING DESCENT, AFTER APU START AND BLEED SWAP, STRONG SMELL OF RAW JET FUEL. PERFORMED OPS CHECK OF APU IN REF TO AMM 49-10-00 AND RAN BOTH PACKS IN REF TO AMM 21-00-00 AND COULD NOT DUPLICATE SMELL OF JET FUEL COMING THROUGH PACKS. AIRCRAFT OK FOR CONTINUE
- [SDR VNAA202004079993](https://openairdocs.org/sdr/VNAA202004079993.md): Drag Angle · cracked · Apr 7, 2020 · N259PS · Bombdr CL6002D15 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED IAE EA 70-2020-057
- [SDR VNAA202004079992](https://openairdocs.org/sdr/VNAA202004079992.md): Support Bracket · cracked · Apr 7, 2020 · N259PS · Bombdr CL6002D15 · Passenger/Crew Doors
  > PAX DOOR MOTOR BOTTOM SUPPORT BRACKET CRACKED. INSTALLED NEW PAX DOOR MOTOR BOTTOM SUPPORT BRACKET NEW SERVICEABLE IAW CRJ-200 SRM 51-42-06.
- [SDR VNAA202004079991](https://openairdocs.org/sdr/VNAA202004079991.md): Frame · cracked · Apr 7, 2020 · N259PS · Bombdr CL6002D15 · Fuselage Main, Frame
  > FRAME 654.00 TO BE CRACKED AT THE OUTBOARD MOST HOLE COMMON TO THE HYDRAULIC SUPPORT BRACKET AT STRINGER. REPAIRED FRAME IAW CRJ200 SRM 53-00-15 REF. 53-00-15 PG 208
- [SDR VNAA2020020751103](https://openairdocs.org/sdr/VNAA2020020751103.md): Engine · failed · Feb 5, 2020 · N259PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON ROLL OUT THE CREW NOTICED A SEVERE VIBRATION, LOW ENG OIL PRESSURE, AND RH ENG OVER HEAT MSG. THE AC BEHIND THEM SAW FLAMES EXITING THE RH ENG T/O WAS ABORTED, FIRE BOTTLES WERE NOT USED. FIRE TRUCKS MET THE PLANE ON THE TAXI WAY TO INSPECT, THEY DID NOT E
- [SDR VNAA2019061521101](https://openairdocs.org/sdr/VNAA2019061521101.md): Unknown · odor · Jun 12, 2019 · N259PS · Cndair CL6002B19 · Air Distribution System
  > CREW REPORTED STRONG FUEL SMELL IN FLT. PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM WITH ENGINES AND APU. NO FUEL SMELL NOTED.
- [SDR VNAA2019061011101](https://openairdocs.org/sdr/VNAA2019061011101.md): Pulley Bracket · cracked · Jun 10, 2019 · N259PS · Cndair CL6002B19 · Passenger/Crew Doors
  > DURING SCHEDULED MAINTENANCE, THE PULLEY BRACKET FOR THE PASSENGER DOOR SUPPORT WHEEL MECHANISM WAS FOUND WITH A CRACK. THE CRACK EMANATES FROM THE UPPER EDGE OF THE BRACKET AT A BEND RADIUS, / MEASURING 1.0Ï¿½ LONG. SEE FIGURE 1 FOR DETAILS. THE CUSTOMER REQU
- [SDR VNAA2019052711102](https://openairdocs.org/sdr/VNAA2019052711102.md): Light · inoperative · May 27, 2019 · N259PS · Cndair CL6002B19 · Emergency Lighting
  > LOWER EMERGENCY FLOOR LIGHT WILL NOT ILLUMINATE. REMOVED/REPLACED LIGHT. IAW CRJ200 AMM 33-51-10-000/400-801. OPS CHECK GOOD.
- [SDR VNAA2019050811101](https://openairdocs.org/sdr/VNAA2019050811101.md): Gearbox · failed · May 8, 2019 · N259PS · Cndair CL6002B19 · Power Lever
  > MX DIVERSION DUE TO RH THRUST REVERSER UNLOCK MSG. EMERGENCY DECLARED AND TRUCKS ROLLED. PLANE LANDED SAFELY AND MX DEFERRED RH THRUST REVERSER. SUPPLEMENTAL INFORMATION. MX REPLACED THE RH THROTTLE GEARBOX AND THROTTLE LOCKOUT SWITCH. OPS CHECK GOOD.
- [SDR VNAA2018022799908](https://openairdocs.org/sdr/VNAA2018022799908.md): Attach Angle · cracked · Feb 27, 2018 · N259PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RBL 27 POST ON AFT SIDE OF FS621 BULKHEAD HAS AN INDICATION NOTED AT THE FWD END OF LOWER ENGINE BEAM ATTACH ANGLE FOOTPRINT.700" LONG BY 80% FSH. FAILED NDT. COMPLETED REPAIR TO FS 621 RBL 27 ENGINE BEAM ATTACH ANGLE IAW REO 601R-53-61-1285 REV E DATED 2016-
- [SDR VNAA2018022799907](https://openairdocs.org/sdr/VNAA2018022799907.md): Bulkhead · cracked · Feb 27, 2018 · N259PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 RPB WEB HAS AN AREA OF MULTIPLE INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA AR RBL27 WL86 TO WL109; AT BL0 WL 107.5 TO WL111.5; AT LBL18 WL131 1.000" LONG;AT LBL18 WL110 1.000" LONG; AT LBL27 WL102 TO WL105.5.;AT LBL36 WL79 1.000" LONG; AT LBL36 WL
- [SDR VNAA2018022799906](https://openairdocs.org/sdr/VNAA2018022799906.md): Frame · corroded · Feb 27, 2018 · N259PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 574 FRAME IS CORRODED ON FWD SIDE BETWEEN STGRS 27-26R. REMOVED AND INSTALLED FS 574 FRAME P/N 601R36024-61 IAW SRM 51-42-21 AND 51-42-06.
- [SDR VNAA2018022799905](https://openairdocs.org/sdr/VNAA2018022799905.md): Frame · corroded · Feb 27, 2018 · N259PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 364 FRAME HAS CORROSION ON FWD FLANGE BETWEEN STGR 27R-26R. INSTALLED NEW SERVICEABLE FRAME PN 601R-32007-15, IAW SRM 51-42-06-51-42-2 LOCATED AND DRILLED IAW SRM 51-40-11.
- [SDR VNAA2018022799904](https://openairdocs.org/sdr/VNAA2018022799904.md): Intercostal · corroded · Feb 27, 2018 · N259PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ON FWD SIDE OF AVIONICS DOOR SURROUND IS CORRODED ON LOWER FLANGE, FS364 STGR 27L. NO DAMAGE ALLOWED IN THAT AREA PER SRM. INSTALLED INTERCOSTAL FWD OF FS 364 STGR 27L IAW SRMS 51-42-06 AND 51-42-21. 2. LOCATED AND DRILLED UP INTERCOSTAL FWD OF FS
- [SDR VNAA2018022799903](https://openairdocs.org/sdr/VNAA2018022799903.md): Seat Track · corroded · Feb 27, 2018 · N259PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 AND RBL 9 FLOOR SEAT TRACK SEGMENTS ARE CORRODED FROM FS 364 TO FS 409+112. INSTALLED NEW SERVICEABLE SEAT TRACK PN 601R31032-15 IAW AMM 53-01-11-400-802.
- [SDR VNAA2018022799902](https://openairdocs.org/sdr/VNAA2018022799902.md): Seat Track · corroded · Feb 27, 2018 · N259PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 AND RBL 9 FLOOR SEAT TRACK SEGMENTS ARE CORRODED FROM FS 559 TO FS 559+80. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802 AT LBL9 AND RBL9. FABRICATED NEW SERVICEABLE FLOOR SEAT RAIL AT FS559.00 TO 559+80 IAW REO 601R-53-00-485.
- [SDR VNAA2018022799901](https://openairdocs.org/sdr/VNAA2018022799901.md): Bracket · corroded · Feb 27, 2018 · N259PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CLIPS AT FS 316 AND FS 342 LT ARE CORRODED. REMOVED CORROSION ON LT FLOOR SUPPORT CLIPS CORROSION DETERMIND TO BE OUT OF LIMITS IAW SRM 51-21-06 DUE TO CORROSION AROUND FASTENER HOLES. REMOVED AFT SUPPORT CLIP & BRACKET IAW SRM 51-42-06 LOCATED,
- [SDR VNAA2016032200024](https://openairdocs.org/sdr/VNAA2016032200024.md): Skin · cracked · Mar 22, 2016 · N259PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN AT BS 235 HAS A CRACK AT STR 26L AND 26R. REPAIRED SKIN AT FS 235 FROM STR 26R TO STR 26L IAW REO.
- [SDR VNAA2016030500006](https://openairdocs.org/sdr/VNAA2016030500006.md): Circuit Breaker · tripped · Mar 5, 2016 · N259PS · Cndair CL6002B19 · Door Warning System
  > CREW REPORTED RECEIVING A PASSENGER DOOR, SERVICE DOOR AND CARGO DOOR EICAS INDICATION ON CLIMBOUT AT 6,000 FT. THEY RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESET CIRCUIT BREAKERS AND PERFORMED CHECKS IAW THE AMM. THE ACFT WA
- [SDR VNAA2016021400018](https://openairdocs.org/sdr/VNAA2016021400018.md): Circuit Breaker · tripped · Feb 14, 2016 · N259PS · Cndair CL6002B19 · Door Warning System
  > CREW REPORTED WHEN CLIMBING OUT AT 87,000 FT, THEY RECEIVED A PASSENGER MASTER WARNING, A SERVICE OUTER HANDLE CAUTION AND CARGO DOOR CAUTION. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESET CIRCUIT BREAKER AND PERFORME
- [SDR VNAA2015122900018](https://openairdocs.org/sdr/VNAA2015122900018.md): Apu · oil consumption · Dec 29, 2015 · N259PS · Cndair CL6002B19 · APU Oil System
  > CREW REPORTED APU OIL TEMPERATURE AND PRESSURE AMBER MESSAGES SHORTLY AFTER DEPARTURE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, SERVICED APU OIL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015121600013](https://openairdocs.org/sdr/VNAA2015121600013.md): Electronic Unit · failed · Dec 16, 2015 · N259PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED GEAR DISAGREE ON SHORT FINAL AFTER GETTING 3 GREEN INDICATIONS. NOSE GEAR INDICATION CHANGED TO RED. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R PROXIMITY SENSOR ELECTRONIC UNIT AND PE
- [SDR VNAA2015121600012](https://openairdocs.org/sdr/VNAA2015121600012.md): Proximity Sensor · failed · Dec 16, 2015 · N259PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED GEAR DISAGREE ON SHORT FINAL AFTER GETTING 3 GREEN INDICATIONS. NOSE GEAR INDICATION CHANGED TO RED. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT NOSE DOWNLOCK PROXIMITY SENSOR AND
- [SDR VNAA2015121600011](https://openairdocs.org/sdr/VNAA2015121600011.md): Wire Harness · damaged · Dec 16, 2015 · N259PS · Cndair CL6002B19 · Landing Gear System Wiring
  > CREW REPORTED GEAR DISAGREE ON SHORT FINAL AFTER GETTING 3 GREEN INDICATIONS. NOSE GEAR INDICATION CHANGED TO RED. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT NOSE DOWNLOCK HARNESS AND PERFORMED
- [SDR VNAA2015112300013](https://openairdocs.org/sdr/VNAA2015112300013.md): Connector · stripped · Nov 23, 2015 · N259PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED EMERGENCY EXIT IN-FLOOR LIGHTING NOT WORKING FROM ROW 9 TO 13. MAINTENANCE INSPECTED, FOUND AFT CONNECTORS STRIPPED, R & R CONNECTORS AND PINS, AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015012500031](https://openairdocs.org/sdr/VNAA2015012500031.md): Wire · loose · Jan 25, 2015 · N259PS · Cndair CL6002B19 · Flight Control System Wiring
  > CREW REPORTED STABILIZER TRIM DISCONNECTED AND WOULD NOT RESET. CREW RETURNED TO FIELD AND LANDED SAFELY. MAINTENANCE TROUBLESHOT, INSPECTED YOKE TRIM DISCONNECT SWITCHES AND FOUND LOOSE WIRE ON CAPTAIN’S DISCONNECT SWITCH. MAINTENANCE RESOLDERED WIRE TO DIS
- [SDR VNAA2014112500010](https://openairdocs.org/sdr/VNAA2014112500010.md): Windscreen · cracked · Nov 19, 2014 · N259PS · Cndair CL6002B19 · Flight Compartment Windows
  > FLT LEVEL 25,000 F/O WIND SCREEN STARTED TO CRACK AND SPARK. ACFT RETURNED TO DAY AND LANDED WITH NO INCIDENT. R & R RT WINDSHEILD IAW AMM 56-01-400. OPS AND LEAKED CHECK GOOD.
- [SDR VNAA2014111800011](https://openairdocs.org/sdr/VNAA2014111800011.md): Skin · dented · Nov 16, 2014 · N259PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND DAMAGE TO SKIN BELOW CARGO DOOR, BS 603 - 621 BETWEEN STRINGERS 20 - 23L.
- [SDR VNAA2014071500008](https://openairdocs.org/sdr/VNAA2014071500008.md): Switch · failed · Jul 15, 2014 · N259PS · Cndair CL6002B19 · Stabilizer Control System
  > CREW REPORTED F/O STAB TRIM WOULD NOT TRIM DOWN IN FLIGHT AND PROBLEM SEEMED TO BE INTERMITTENT. CAPTAIN’S SIDE WORKED FINE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R F/O PITCH TRIM SWITCH AND PERFORMED CHECKS IAW AMM.
- [SDR VNAA2014062500021](https://openairdocs.org/sdr/VNAA2014062500021.md): Wire · sheared · Jun 25, 2014 · N259PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED FLOOR EMERGENCY LIGHTS AFT OF ROW 8 DID NOT ILLUMINATE. MAINTENANCE INSPECTED AND FOUND WIRES SHEARED OFF AT PIGTAIL ADJACENT TO LAVATORY. MAINTENANCE REPAIRED WIRING AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014061000009](https://openairdocs.org/sdr/VNAA2014061000009.md): Step · corroded · Jun 10, 2014 · N259PS · Cndair CL6002B19 · Service Doors
  > DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND ON BOTTOM OF THE SERVICE DOOR STEP PLATE. THE AREA WAS INSPECTED, R & R SERVICE DOOR STEP PLATE USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014061000008](https://openairdocs.org/sdr/VNAA2014061000008.md): Seat Track · corroded · Jun 10, 2014 · N259PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND ON 4 SEAT TRACK SEGMENTS BETWEEN 559+80 AND FS 559+112. THE AREA WAS INSPECTED, R & R SEAT TRACKS USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014061000007](https://openairdocs.org/sdr/VNAA2014061000007.md): Beam · corroded · Jun 10, 2014 · N259PS · Cndair CL6002B19 · Fuselage Main, Structure
  > DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON TRASVERSE BEAM PLATE BETWEEN LBL 9 AND LBL 27 AT FS 589. THE AREA WAS INSPECTED, R & R TRANSVERSE BEAM PLATE USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014061000006](https://openairdocs.org/sdr/VNAA2014061000006.md): Stringer · cracked · Jun 10, 2014 · N259PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED MAINTENANCE, STRINGER 3L AT BS 379 WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014050300005](https://openairdocs.org/sdr/VNAA2014050300005.md): Pitot Tube · obstructed · May 3, 2014 · N259PS · Cndair CL6002B19 · Pitot/Static System
  > CREW REPORTED BIRD STRIKE TO PITOT TUBE ON F/O SIDE AND TO NOSE CONE WHILE ON APPROACH. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION AND FOUND DEBRIS IN RT PITOT TUBE. MAINTENANCE R & R RT PITOT TUBE AND PERFORMED CHECK
- [SDR VNAA2014032300014](https://openairdocs.org/sdr/VNAA2014032300014.md): Switch · failed · Mar 23, 2014 · N259PS · Cndair CL6002B19 · Ice/Rain Protection System
  > CREW REPORTED LT ANTI-ICE DUCT MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THERMAL SWITCHES IN LT INBD L/E DUE TO ERRATIC CONTINUITY AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2014022100017](https://openairdocs.org/sdr/VNAA2014022100017.md): Skin · damaged · Feb 21, 2014 · N259PS · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > CREW REPORTED POSSIBLE LIGHTNING STRIKE ON DESCENT. CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R LT HORIZONTAL STABILIZER TIP AND REPAIRED LT HORIZONTAL TIP SPAR EXTENSION AND RIB DUE TO LIGHTNING STRIKE DAMAGE. MA
- [SDR VNAA2013062400016](https://openairdocs.org/sdr/VNAA2013062400016.md): Warning System · false activation · Jun 24, 2013 · N259PS · Cndair CL6002B19 · Engine Thrust Reverser
  > CREW REPORTED RIGHT AND LEFT REVERSER UNSAFE AMBER MESSAGE ON TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MESSAGE OCCURRED TWO (2) TIMES ON LANDING WITH REVERSER NOT ARMED. MAINTENANCE TROUBLESHOT USING AIRCRAFT FIM (FAULT ISOLATION MANUAL)
- [SDR VNAA2013032600020](https://openairdocs.org/sdr/VNAA2013032600020.md): Windshield · cracked · Mar 26, 2013 · N259PS · Cndair CL6002B19 · Flight Compartment Windows
  > CAPTAIN’S WINDSHIELD CRACKED IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED CAPTAIN’S WINDSHIELD AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2013031800016](https://openairdocs.org/sdr/VNAA2013031800016.md): Antenna · damaged · Mar 18, 2013 · N259PS · Cndair CL6002B19 · Emergency Locator Beacon
  > CREW REPORTED POSSIBLE LIGHTNING STRIKE IN FLIGHT AND THAT ADC 2 (AIR DATA COMPUTER) SEEMED TO BE INOPERATIVE AS A RESULT. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK ON ADC’S. NO DEFECTS FOUND. MAINTENANCE PERFORMED LIGHT
- [SDR VNAA1122120000016](https://openairdocs.org/sdr/VNAA1122120000016.md): Bulkhead · cracked · Nov 22, 2012 · N259PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE PARKING BRAKE CABLE PASS THRU AT THE FORWARD BULKHEAD WAS CRACKED. THE FORWARD BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012112200015](https://openairdocs.org/sdr/VNAA2012112200015.md): Bulkhead · cracked · Nov 22, 2012 · N259PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE REAR PRESSURE BULKHEAD WEB HAD AN INDICATION OF CRACKED. THE REAR PRESSURE BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012071500010](https://openairdocs.org/sdr/VNAA2012071500010.md): Bpsu · failed · Jul 15, 2012 · N259PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > CREW REPORTED FLAPS FAIL CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FO
- [SDR VNAA2011081800011](https://openairdocs.org/sdr/VNAA2011081800011.md): Blade · bent · Aug 15, 2011 · N259PS · Cndair CL6002B19 · Turbine Engine Compressor Section
  > CREW REPORTED POSSIBLE BIRD STRIKE ON TAKEOFF. NO VIBRATION INDICATION NOTED. AT CLT, MAINTENANCE INSPECTED, FOUND THREE (3) BENT BLADES IN RIGHT ENGINE FAN, REMOVED AND REPLACED THREE (3) SETS OF BLADES AND PERFORMED CHECKS USING MAINTENANCE MANUALS. AIRCR
- [SDR VNAA2011072700029](https://openairdocs.org/sdr/VNAA2011072700029.md): Tire · failed · Jul 24, 2011 · N259PS · Cndair CL6002B19 · Tire
  > CREW REPORTED AFTER LANDING THEY FOUND LEFT INBOARD TIRE FAILED AND DAMAGE TO LEFT FLAP. TIRE WAS REPLACED AND FLAP WAS REPAIRED. INSPECTION, REMOVAL, REPLACEMENTS, AND OPERATIONAL CHECKS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WA
- [SDR VNAA2011040500003](https://openairdocs.org/sdr/VNAA2011040500003.md): Bulkhead · cracked · Apr 3, 2011 · N259PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE FS 280 BULKHEAD WEB. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011022200009](https://openairdocs.org/sdr/VNAA2011022200009.md): Window · erratic · Feb 17, 2011 · N259PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED A RIGHT WINDOW HEAT CAS MESSAGE AFTER DEPARTURE FROM DAY. MESSAGE WOULD NOT RESET. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND FOUND ERRATIC RESISTANCE READINGS ON THE RIGHT WINDOW HEAT SENSORS.
- [SDR VNAA2011020100013](https://openairdocs.org/sdr/VNAA2011020100013.md): Transducer · failed · Jan 26, 2011 · N259PS · Cndair CL6002B19 · Stall Warning System
  > CREW REPORTED A STALL FAIL MESSAGE IN FLIGHT AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT AOA TRANSDUCER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE M
- [SDR VNAA2011012700008](https://openairdocs.org/sdr/VNAA2011012700008.md): Actuator · malfunctioned · Jan 22, 2011 · N259PS · Cndair CL6002B19 · Landing Gear Actuator
  > CREW REPORTED A GEAR DISAGREE MESSAGE 20+ SECONDS AFTER SELECTING THE GEAR UP ON TAKEOFF FROM ORF. AFTER THREE (3) MINUTES, THE GEAR RETRACTED. CREW RAN THE QRH FOR GEAR DISAGREE AND MANUALLY EXTENDED THE GEAR. CREW RETURNED TO ORF AND LANDED WITHOUT FURTHE
- [SDR VNAA2011011100001](https://openairdocs.org/sdr/VNAA2011011100001.md): Warning System · malfunctioned · Jan 6, 2011 · N259PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED NOSE GEAR DISAGREE AURAL AND WARNING MESSAGE ON TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FUNCTIONAL CHECKS OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM USING THE AIRCRAFT MAINTENANCE MANUA

Next page: https://openairdocs.org/deregistered/N259PS-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 = 'N259PS' AND deregistration_id = 'N259PS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N259PS-2025-12-09/reports

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