# Service difficulty reports: N250PS, cancelled Dec 9, 2025

A list on [N250PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N250PS-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 · 89 reports

- [SDR VNAA2020031921101](https://openairdocs.org/sdr/VNAA2020031921101.md): Flashlight · inoperative · Mar 16, 2020 · N250PS · Cndair CL6002B19 · Emergency Equipment
  > FWD FA FLASHLIGHT INOP. MX REMOVED AND REPLACED FWD FA FLASHLIGHT. OPS CHECK GOOD.
- [SDR VNAA2020031101101](https://openairdocs.org/sdr/VNAA2020031101101.md): Tube · cracked · Mar 8, 2020 · N250PS · Cndair CL6002B19 · Engine Anti-Icing System
  > UNCOMMANDED DECELERATION OF RH ENGINE IN FLIGHT APROX 8% N1. MAINTENANCE FOUND THE T2 ANTI ICE TUBE ASSY CRACKED, REMOVED AND AND REPLACED THE TUBE ASSY OPS CHECK GOOD.
- [SDR VNAA2020030511101](https://openairdocs.org/sdr/VNAA2020030511101.md): Bpsu · out of rig · Mar 2, 2020 · N250PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > ON FINAL APPROACH INTO LGA, THE CREW PULLED FLAPS FROM 8-20, BUT FLAPS DID NOT MOVE, AND A FLAP FAILURE MESSAGE APPEARED. THE CREW EXECUTED A GO AROUND, AND DECIDED TO DIVERT TO JFK TO LAND ON A LONGER RUNWAY. THE CREW DID DECLARE AN EMERGENCY. THE AIRCRAFT LA
- [SDR VNAA2020021261102](https://openairdocs.org/sdr/VNAA2020021261102.md): Engine · oscillates · Jan 26, 2020 · N250PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AT 27000 FEET RIGHT ENGINE N1 OSCILLATED BETWEEN 81 TO 88 SLOWED THE PLANE AND IT STEADIED OUT. CONTINUED THE FLIGHT. PERFORMED ENG. RUN & CHECK N1 SPEED-CONTROL AMP. CHK. FOUND OK AND NO N1 OSCILLATION AT THIS TIME.
- [SDR VNAA2019123091101](https://openairdocs.org/sdr/VNAA2019123091101.md): Wire · disconnected · Dec 29, 2019 · N250PS · Cndair CL6002B19 · Light System Wiring
  > EXIT SIGN EMERGENCY LIGHT BY PAX DOOR INOP. FOUND WIRE UNPLUGGED. CONNECTED THE WIRE IAW AMM 33-51-10-400-801. OPS CHECK GOOD.
- [SDR VNAA2019121011101](https://openairdocs.org/sdr/VNAA2019121011101.md): Sensor · dirty · Dec 10, 2019 · N250PS · Cndair CL6002B19 · Engine Controls
  > AT 800 FT AFTER TAKEOFF, THE CREW OBSERVED AND FELT THE RH N1 SURGE. CREW LEVELED OFF AT 5000 FT, RAN QRH, AND RETURNED TO THE FIELD. THE CREW DID NOT DECLARE AN EMERGENCY BUT ATC DID ROLL THE FIRETRUCKS. DEFERRED RH ENG SPEED CONTROL SYSTEM. MX CLEANED T2 SE
- [SDR VNAA2019082097111](https://openairdocs.org/sdr/VNAA2019082097111.md): Pump · failed · Aug 17, 2019 · N250PS · Cndair CL6002B19 · Turbine Engine Oil System
  > ON CLIMB OUT AT FL100 ENGINE 1 OIL TEMP READ OUT FLASHED RED INDICATING HIGH OIL TEMP. CREW REQUESTED LEVEL OFF WITH ATC, BACKED ENGINE POWER DOWN AND RAN THE QRH. QRH INSTRUCTED TO SHUT DOWN ENGINE AND LAND AT NEAREST SUITABLE. CREW DECLARED AN EMERGENCY W
- [SDR VNAA2019073011101](https://openairdocs.org/sdr/VNAA2019073011101.md): Power Supply · failed · Jul 30, 2019 · N250PS · Cndair CL6002B19 · Emergency Lighting
  > CENTER AISLE EMERGENCY EXIT/FWD SIGN LIGHT INOP. R&R EMERGENCY BATTERY SUPPLY. IAW CRJ200 AMM 33-51-04-000/400-801. OPS CHECK GOOD.
- [SDR VNAA2019020199913](https://openairdocs.org/sdr/VNAA2019020199913.md): Floorbeam · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > R/H FS484.00 ANGLES @ RBL27 & RBL36 ARE CRACKED. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11, & 51-42-21
- [SDR VNAA2019020199912](https://openairdocs.org/sdr/VNAA2019020199912.md): Floorbeam · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > L/H FS484.00 ANGLES @ LBL27 & LBL36 ARE CRACKED. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11, & 51-42-21
- [SDR VNAA2019020199911](https://openairdocs.org/sdr/VNAA2019020199911.md): Floor Support · corroded · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLES AND CUPS AT PAX DOOR SILL ARE CORRODED FROM F.S. 310 TO F.S. 349. C/A: REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT ANGLES AND CUPS REF CRJ 200 SRM 51-42-06, 51-42-13 & 51-42-21.
- [SDR VNAA2019020199910](https://openairdocs.org/sdr/VNAA2019020199910.md): Seat Track · corroded · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 AND RBL9 FS364-399 FLOOR SEAT TRACK SEGMENTS HAVE CORROSION. C/A: REMOVED AND REPLACED TRACK SEGMENT IAW BOMBARDIER REO 601R-53-00-485.
- [SDR VNAA2019020199909](https://openairdocs.org/sdr/VNAA2019020199909.md): Seat Track · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 AND RBL9 FS399-409+120 FLOOR SEAT TRACK SEGMENTS HAVE CORROSION. C/A: REMOVED AND REPLACED TRACK SEGMENT IAW BOMBARDIER REO 601R-53-00-485.
- [SDR VNAA2019020199908](https://openairdocs.org/sdr/VNAA2019020199908.md): Stiffener · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR ASSIST MOTOR CRACKED AT WEB SIDE ATTACH POINT. C/A: REMOVED AND REPLACED PAX DOOR SIDE PANEL STIFFENER REF CRJ 200 SRM 51-42-15.
- [SDR VNAA2019020199907](https://openairdocs.org/sdr/VNAA2019020199907.md): Frame · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333.0 FRAME IS CRACKED BETWEEN STRINGER 0 AND STRINGER 1L. C/A: REMOVED AND REPLACED FRAME IAW CRJ 200SRM 51-40-11,51-42-21 AND 51-42-06.
- [SDR VNAA2019020199906](https://openairdocs.org/sdr/VNAA2019020199906.md): Trunnion · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE (FWD LOOKING AFT) HAS AN INDICATION AT 5TH FASTENER HOLE FROM THE FWD EDGE OF STEEL STRAP AT 55% FSH, FAILED NDT. C/A: REPAIRED L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2938 R
- [SDR VNAA2019020199905](https://openairdocs.org/sdr/VNAA2019020199905.md): Trunnion · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > L/H LOWER WING PLANK MLG TRUNNIION FASTENER HOLE (FWD LOOKING AFT) HAS AN INDICATION AT 2ND FASTENER HOLE FROM THE FWD EDGE OF STEEL STRAP AT 60% FSH FAILED NDT. C/A: REPAIRED L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2938 R
- [SDR VNAA2019020199904](https://openairdocs.org/sdr/VNAA2019020199904.md): Trunnion · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > FOUND INDICATION ON R/H TRUNNION 7TH HOLE FROM AFT TO STRAP 90% FSH APPROX. 0.5 UP THE TRUNNION FAILS NDT. C/A: REPAIRED R/H TRUNNION DAMAGED FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2939 REV.--DATED 2019-01-24.
- [SDR VNAA2019020199903](https://openairdocs.org/sdr/VNAA2019020199903.md): Trunnion · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > FOUND INDICATION ON R/H TRUNNION 4TH HOLE FROM AFT OF STRAP 60% FSH APPROX. 0.75 UP THE TRUNNION FAILS NDT. C/A: REPAIRED R/H TRUNNION DAMAGED FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2939 REV.--DATED 2019-01-24.
- [SDR VNAA2019020199902](https://openairdocs.org/sdr/VNAA2019020199902.md): Angle · cracked · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS409+128 BLO RH VERTICAL POST ANGLE HAS AN INDICATION.15" LONG BY 80% FSH IN THE UPPER AFT RADIUS WL69. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11,51-42-22 AND 51-42-06.
- [SDR VNAA2019020199901](https://openairdocs.org/sdr/VNAA2019020199901.md): Seal Depressor · corroded · Feb 1, 2019 · N250PS · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR LOWER SEAL SURROUND CORRODED. C/A: REMOVED AND REPLACED PAX DOOR LOWER SEAL SURROUND IAW CRJ 200 SRM 51-40-11 AND 51-42-06.
- [SDR VNAA2018091711101](https://openairdocs.org/sdr/VNAA2018091711101.md): Loop · contaminated · Sep 10, 2018 · N250PS · Cndair CL6002B19 · Pneumatic Indicating System
  > CREW RECEIVED A L 10TH DUCT RED MSG. RAN THE QRH AND CAUTION DID NOT CLEAR. DECLARED AN EMERGENCY AND LANDED IN GSO. CLT MX GOING TO GSO WITH PARTS. CLT MX FOUND LOOPS SUBMERGED IN WATER IN AFT EQUIP BAY, CLEANED OUT WATER/LOOPS, CHECK GOOD.
- [SDR VNAA2018021611102](https://openairdocs.org/sdr/VNAA2018021611102.md): Warning Message · activated · Feb 16, 2018 · N250PS · Cndair CL6002B19 · Ice/Rain Protection System
  > THE CREW RECEIVED AN ANTI-ICE DUCT SYSTEM MESSAGE. THE CREW RAN THE QRH AND DECLARED AN EMERGENCY TO CLIMB OUT OF ICING CONDITIONS. THE CREW CONTINUED TO THEIR DESTINATION AND LANDED WITHOUT INCIDENT. OPEN.
- [SDR VNAA2017082911102](https://openairdocs.org/sdr/VNAA2017082911102.md): Controller · malfunctioned · Aug 29, 2017 · N250PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > AFTER DEPARTURE, THE CREW RECEIVED A LEFT WINDSHIELD HEAT CAUTION MESSAGE AND NOTICED A SLIGHT ODOR. THE QUICK REFERENCE HANDBOOK WAS FOLLOWED AND CYCLED SYSTEM. AFTER CYCLING THE SYSTEM THE CREW OBSERVED SMOKE AND TURNED THE WINDSHIELD HEAT OFF. THE AIRCRAFT
- [SDR VNAA2017082811102](https://openairdocs.org/sdr/VNAA2017082811102.md): Unknown · odor · Aug 28, 2017 · N250PS · Cndair CL6002B19 · Cabin Cooling System
  > BURNING ODOR FROM LEFT PACK ON GROUND. PERFORMED AN OPS CHECK OF THE LT PACK, OPS CHECKED GOOD.
- [SDR VNAA2017012300030](https://openairdocs.org/sdr/VNAA2017012300030.md): Skin · damaged · Jan 23, 2017 · N250PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN AT BS 235 BETWEEN STRINGERS 26L AND 26R DAMAGED. PERFORMED A MAJOR REPAIR.
- [SDR VNAA2016071800018](https://openairdocs.org/sdr/VNAA2016071800018.md): Control Unit · malfunctioned · Jul 18, 2016 · N250PS · Cndair CL6002B19 · Overheat Detection
  > LEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FIRE AND OVERHEAT CONTROL UNIT AND PERFORMED CHECKS IAW AMM.
- [SDR VNAA2016071800017](https://openairdocs.org/sdr/VNAA2016071800017.md): Overheat Sensor · out of position · Jul 18, 2016 · N250PS · Cndair CL6002B19 · Overheat Detection
  > LEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED JETPIPE SENSING ELEMENTS AND FOUND LOOP-A SENSING ELEMENT TOUCHING A CLAMP. MAINTENANCE REPOSITIONED LOOP AND PERFORMED CHECKS IAW AMM.
- [SDR VNAA2016070400005](https://openairdocs.org/sdr/VNAA2016070400005.md): Air Filter · faulty · Jul 4, 2016 · N250PS · Cndair CL6002B19 · Air Distribution System
  > LEFT HIGH PRESSURE CAUTION MESSAGE AT 8000 FEET. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT 10TH STAGE PRESSURE SHUTOFF VALVE INLET FILTER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVIC
- [SDR VNAA2016062300025](https://openairdocs.org/sdr/VNAA2016062300025.md): Strip · missing · Jun 23, 2016 · N250PS · Cndair CL6002B19 · Emergency Lighting
  > ROW EMERGENCY LIGHTS COLOR STRIPPING MISSING. MAINTENANCE INSPECTED, REINSTALLED PHOTOLUMINESCENT FLOOR MARKING AND COVER, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2015091000014](https://openairdocs.org/sdr/VNAA2015091000014.md): Windshield · delaminated · Sep 10, 2015 · N250PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED SEVERE DELAMINATION ON LT FORWARD WINDSHIELD AND WINDSHIELD ARCING. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015091000015](https://openairdocs.org/sdr/VNAA2015091000015.md): Controller · failed · Sep 10, 2015 · N250PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > CREW REPORTED SEVERE DELAMINATION ON LT FORWARD WINDSHIELD AND WINDSHIELD ARCING. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015062800041](https://openairdocs.org/sdr/VNAA2015062800041.md): Hose · leaking · Jun 28, 2015 · N250PS · Cndair CL6002B19 · Hydraulic System, Main
  > ON APPROACH, CREW REPORTED HYD SYS NR 3 LOW PRESSURE MESSAGE CAME ON WHEN LANDING GEAR SELECTED DOWN. CREW LANDED AND USING DIFFERENTIAL BRAKING, TAXIED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND LEAK ON AFT SIDE OF ALTERNATING CURRENT MOTOR PUMP, ACMP, 3B.
- [SDR VNAA2015062800040](https://openairdocs.org/sdr/VNAA2015062800040.md): Hose · leaking · Jun 28, 2015 · N250PS · Cndair CL6002B19 · Hydraulic System, Main
  > ON APPROACH, CREW REPORTED HYDRAULIC SYSTEM NR 3 LOW PRESSURE MESSAGE CAME ON WHEN LANDING GEAR SELECTED DOWN. CREW LANDED AND USING DIFFERENTIAL BRAKING, TAXIED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND LEAK ON AFT SIDE OF ALTERNATING CURRENT MOTOR PUMP, A
- [SDR VNAA2015032600026](https://openairdocs.org/sdr/VNAA2015032600026.md): Structure · corroded · Mar 26, 2015 · N250PS · Cndair CL6002B19 · Fuselage Main, Structure
  > IN PASSENGER COMPARTMENT AT PASSENGER DOOR CUTOUT ON FS 310.00 AND FS 349.00, THE PASSENGER DOOR COUNTER BALANCE ANCHOR FITTING SERATED PLATES HAVE EXFOLIATION CORROSION. REMOVED CORRODED PLATES AND INSTALLED NEW SERVICABLE PLATES IAW AMM 52-11-17-400-804.
- [SDR VNAA2014071200006](https://openairdocs.org/sdr/VNAA2014071200006.md): Sensor · malfunctioned · Jul 12, 2014 · N250PS · Cndair CL6002B19 · Pneumatic Distribution System
  > CREW REPORTED LT 14TH DUCT RED WARNING MESSAGE WHILE DESCENDING THROUGH 14,000 FT. CREW COMPLIED WITH QRH. MESSAGE DID NOT EXTINGUISH IMMEDIATELY, BUT DID EXTINGUISH SHORTLY BEFORE LANDING. DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE TROUBLESHOT,
- [SDR VNAA2013062800018](https://openairdocs.org/sdr/VNAA2013062800018.md): Downlock Sensor · faulty · Jun 28, 2013 · N250PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED TRIPLE CHIME AND GEAR DISAGREE AMBER NOSEWHEEL INDICATION ON DESCENT. CREW PERFORMED MANUAL GEAR EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED NOSE LANDING GEAR NUMBER TWO (2) DOWNLOCK SENSOR AND PERFORMED G
- [SDR VNAA2013052700016](https://openairdocs.org/sdr/VNAA2013052700016.md): Bulkhead · cracked · May 27, 2013 · N250PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE FS 621 PRESSURE BULKHEAD HAD INDICATION OF CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013052700015](https://openairdocs.org/sdr/VNAA2013052700015.md): Structure · damaged · May 27, 2013 · N250PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE FS 589.0 TO FS 605.0 DAMGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013042400017](https://openairdocs.org/sdr/VNAA2013042400017.md): Light · inoperative · Apr 24, 2013 · N250PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING AT SEATS 4F/D REPORTED INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING AT SEAT 4F/D AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2013042300016](https://openairdocs.org/sdr/VNAA2013042300016.md): Battery Pack · discharged · Apr 23, 2013 · N250PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED EMERGENCY LIGHTS ON THE FLOOR BETWEEN ROWS TWO (2) TO FIVE (5) INTERMITTENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) EMERGENCY LIGHT BATTERY PACK AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FO
- [SDR VNAA2013031800013](https://openairdocs.org/sdr/VNAA2013031800013.md): Seal · leaking · Mar 18, 2013 · N250PS · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > CREW REPORTED RIGHT 14TH DUCT RED MESSAGE DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RIGHT ENGINE 14TH STAGE DUCT COUPLING FROM ENGINE TO PYLON TO BE LEAKING. MAINTENANCE REMOVED AND REPLACED E-SEALS A
- [SDR VNAA2013022700017](https://openairdocs.org/sdr/VNAA2013022700017.md): Engine · failed · Feb 27, 2013 · N250PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CREW REPORTED A HIGH ITT AND VIBRATION WITH LOSS OF POWER IN NR 2 ENGINE. CREW RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE NR 2 ENGINE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT
- [SDR VNAA2012091600018](https://openairdocs.org/sdr/VNAA2012091600018.md): Bulkhead · cracked · Sep 23, 2012 · N250PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE FOUND FS 202.75 PRESSURE BULKHEAD WEB CRACKED. FS 202.75 PRESSURE BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012082100016](https://openairdocs.org/sdr/VNAA2012082100016.md): Windshield · cracked · Aug 21, 2012 · N250PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED THE RIGHT WINDSHIELD CRACKED. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE RIGHT WINDSHIELD USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL CHECKS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTE
- [SDR VNAA2011091500013](https://openairdocs.org/sdr/VNAA2011091500013.md): Fairing · damaged · Sep 11, 2011 · N250PS · Cndair CL6002B19 · Trailing Edge Flaps
  > AT PHL, CREW REPORTED RIGHT WING AFT INBOARD FLAP FAIRING HAD BURN MARK / FRAYING AREA. MAINTENANCE INSPECTED AIRCRAFT AND REPAIRED LIGHTNING STRIKE DAMAGE TO RIGHT WING AFT INBOARD FLAP FAIRING. MAINTENANCE REPAIRED DAMAGED PAINT ON LEFT LOWER AFT WINGLET A
- [SDR VNAA2011082500013](https://openairdocs.org/sdr/VNAA2011082500013.md): Connector · loose · Aug 20, 2011 · N250PS · Cndair CL6002B19 · Door System Wiring
  > CREW REPORTED RANDOM GEAR HORN IN FLIGHT. RED GEAR DISAGREE MESSAGE AND RED NOSE DOOR OPEN MESSAGE REPORTED AFTER SELECTING GEAR DOWN ON APPROACH TO MOB. AIRCRAFT LANDED IN MOB WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, TIGHTENED PROXIMITY SENSOR CABLE CONN
- [SDR VNAA2011081000006](https://openairdocs.org/sdr/VNAA2011081000006.md): Post · cracked · Aug 7, 2011 · N250PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE VERTICLE POST FS718.0 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011081000005](https://openairdocs.org/sdr/VNAA2011081000005.md): Post · cracked · Aug 7, 2011 · N250PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE VERTICLE POST FS 409+128 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011081000004](https://openairdocs.org/sdr/VNAA2011081000004.md): Angle · corroded · Aug 7, 2011 · N250PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DURING SCHEDULED MAINTENANCE THE FLOORBEAM CAP ANGLE BETWEEN FS 574 AND FS 608 AT LBL 27 WAS FOUND CORRODED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N250PS-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 = 'N250PS' AND deregistration_id = 'N250PS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N250PS-2025-12-09/reports

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