# Service difficulty reports: N244PS, cancelled Dec 9, 2025

A list on [N244PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N244PS-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 · 90 reports

- [SDR VNAA2022012011101](https://openairdocs.org/sdr/VNAA2022012011101.md): Fairing · bent · Dec 30, 2019 · N244PS · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > UPPER FWD CORE COWL HINGE NOT PINNED CORRECTLY. NO. 2 ENGINE EXHAUST NOZZLE FAIRINGÏ¿½S ACCESS PANEL WAS FOUND TO BE BENT AND TWISTED. PLACED ON TEMP REPAIR REFERENCE EA25-2019-321 FOR DETAILS. C/W PERMANENT REPAIR. R+R RH ENGINE EXHAUST NOZZLE ASSY IAW CRJ200
- [SDR VNAA2019103011102](https://openairdocs.org/sdr/VNAA2019103011102.md): Inverter · failed · Oct 30, 2019 · N244PS · Cndair CL6002B19 · Emergency Lighting
  > R/H OVERWING EMERGENCY "EXIT: SIGN NOT WORKING. R/R INVERTER FOR RH OVERWING LOWER EMERGENCY EXIT SIGN. OPS CHECK GOOD.
- [SDR VNAA2019092711103](https://openairdocs.org/sdr/VNAA2019092711103.md): Cable · frayed · Sep 27, 2019 · N244PS · Cndair CL6002B19 · Passenger/Crew Doors
  > DOOR SUPPORT WHEEL CABLE ON AFT SIDE OF PAX DOOR IS HEAVILY FRAYED REMOVED AND REPLACED MAIN CABIN DOOR LOWER SUPPORT WHEEL CABLE NO FURTHER DEFECTS NOTED AT THIS TIME
- [SDR VNAA2019062211102](https://openairdocs.org/sdr/VNAA2019062211102.md): Ring · worn · Jun 22, 2019 · N244PS · Cndair CL6002B19 · Turbine Engine Oil System
  > RIGHT ENGINE OIL PRESSURE MSG IN FLIGHT. O/S MX SERVICED RT ENGINE WITH 6.0 QTS. GOING TO PROCEED WITH OIL CONSUMPTION RUN. FAILED OIL CONSUMPTION RUN..75QTS AFTER 20 MINUTES. R/R RT ENG IDG, ATS, STARTER CARBON SEALS AND MATING RING. CONSUMPTION CHECK GOOD.
- [SDR VNAA2019100217101](https://openairdocs.org/sdr/VNAA2019100217101.md): Sign · inoperative · Mar 17, 2019 · N244PS · Cndair CL6002B19 · Emergency Lighting
  > RH EXTERNAL MIDDLE OVERWING EMERGENCY LIGHT INOP. PERFORMED OPS CHECK ON RH EMRGENCY EXIT LOWER SIGN. IAW CRJ200 AMM 33-51-00-710-801. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2019031211101](https://openairdocs.org/sdr/VNAA2019031211101.md): Windshield · cracked · Mar 12, 2019 · N244PS · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT AFTER DEPARTURE FROM DCA FLIGHT 5484 GOT A SHATTERED CA WINDSHIELD AT ABOUT FL098 A EMERGENCY WAS DECLARED BY THE CREW WHEN RETURNING BACK TO DCA. THEY DID DENIED EMERGENCY EQUIPMENT TO STAND BY. THE AIRCRAFT WAS ABLE TO TAXI TO THE GATE UNDER ITS OWN PO
- [SDR VNAA2018110899912](https://openairdocs.org/sdr/VNAA2018110899912.md): Fitting · cracked · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > WINDSHIELD CNTR POST R/H BOTTOM FITTING CRACKED FROM LOWER FASTENER HOLE TO EDGE OF FITTING. C/A:REMOVED UNSERVICEABLE CENTER POST IAW CRJ 200 SRM 51-42-21. RECEIVED NEW CENTER POST RH BOTOTM FITTING. LOCATED AND DRILLED CENTER POST RH BOTTOM FITTING PN IAW C
- [SDR VNAA2018110899911](https://openairdocs.org/sdr/VNAA2018110899911.md): Support Bracket · broken · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > SUPPORT BRACKET AND CLIP FOR LH UPPER STANG FAIRING IS BROKEN ON PYLON TRACK. C/A: REMOVED AND REPLACED SUPPORT ASSY IAW CRJ200 SRM 51-42-06.
- [SDR VNAA2018110899910](https://openairdocs.org/sdr/VNAA2018110899910.md): Cascade · cracked · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Engine Thrust Reverser
  > UPPER CENTER CASCADE CRACKED ON LH THRUST REVERSER ASSY MARKED WITH TAPE. C/A: REMOVED L/H TR UPPER CENTER CASCADE IAR CRJ200 AMM 78-33-01-000-801. INSTALLED L/H TR UPPER CENTER CASCADE IAW CRJ200 AMM 78-33-01-400-801.
- [SDR VNAA2018110899909](https://openairdocs.org/sdr/VNAA2018110899909.md): Angle · cracked · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS.280 CROSSBEAM IS CORRODED BETWEEN LBL9 AND RBL9. FOUND 4EA FS280 CLIPS TO BE CRACKED BETWEEN LBL9 AND RBL9. C/A: FABRICATED 4 EA F.S. 280 CLIPS REFERENCING REO 601R-53-11-926 FOR MATERIAL SPEC IAW CRJ200 SRM 51-24-36-AND 51-40-11 REF. JOB:27912111 OP:134 F
- [SDR VNAA2018110899908](https://openairdocs.org/sdr/VNAA2018110899908.md): Cargo Track · corroded · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT, SEAT TRACK @ RBL9, APPROX. F.S. 559.00+80 CORRODED. C/A: REMOVED AN REPLACED DAMAGED SEAT TRACK AT @FS559.00+80 LBL 9 NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802.
- [SDR VNAA2018110899907](https://openairdocs.org/sdr/VNAA2018110899907.md): Cargo Track · corroded · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT, SEAT TRACK @ LBL9, APPROX. F.S. 559.00+80 CORRODED. C/A: REMOVED AN REPLACED DAMAGED SEAT TRACK AT @FS559.00+80 LBL 9 NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802.
- [SDR VNAA2018110899906](https://openairdocs.org/sdr/VNAA2018110899906.md): Seat Track · corroded · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT LBL27, APPROX F.S. 559.00+80 CORRODED. C/A: REMOVED AND REPLACED DAMAGED SEAT TRACK AT F 559.00+80 LBL 27. INSTALLED NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802.
- [SDR VNAA2018110899905](https://openairdocs.org/sdr/VNAA2018110899905.md): Cargo Track · broken · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT TWO SEAT TRACK FILLERS BROKEN. K.LONG 10/22/18. C/A: INSTALLED 3 EACH NEW SERVICEABLE SEAT TRACK FILLERS P/N:601R38731-7, 601R38731-17 AND 601R38731-19 IAW CRJ200 AMM 20-21-00-910-801.
- [SDR VNAA2018110899904](https://openairdocs.org/sdr/VNAA2018110899904.md): Cargo Track · corroded · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT, SEAT TRACK @ RBL9, APPROX. F.S.559.00+112 CORRODED. C/A: REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK P/N: 601R38779-49 IAW CRJ200 AMM 53-01-11-000-802.
- [SDR VNAA2018110899903](https://openairdocs.org/sdr/VNAA2018110899903.md): Cargo Track · corroded · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT SEAT TRACK @ LBL9, APPROX. F.S. 559.00+112 CORRODED. C/A: REMOVED SEAT TRACK AND REPLACED SEAT TRACK, P/N 601R38779-S, IAW CRJ200 AMM 53-01-11-400-802
- [SDR VNAA2018110899902](https://openairdocs.org/sdr/VNAA2018110899902.md): Seat Track · corroded · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON RBL9 BETWEEN FS.559+16 TO FS.559+80 IS CORRODED. C/A: NSTALLED NEW SERVICEABLE SEAT TRACK ON RBL9 BETWEEN FS559.00+16 - FS559.00+80 IAW CRJ200 AMM 53-01-11-400-802.
- [SDR VNAA2018110899901](https://openairdocs.org/sdr/VNAA2018110899901.md): Door Frame · cracked · Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H OVERWING DOOR CUTOUT HAS CRACKED/ MISSING STRUCTUAL FILLER FOR DOOR SEAL LANDING. C/A: REPAIRED RH OVERWING DOOR CUTOUT MISSING STRUCTURAL FILLER IAW SRM 51-12-00 P14 STEP 9.
- [SDR VNAA2018111199901](https://openairdocs.org/sdr/VNAA2018111199901.md): Frame · cracked · Oct 11, 2018 · N244PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS718 FRAME IS CRACKED AT STGR 11R. C/A: REMOVED FRAME AT R/H FS718 AND COMPLETED INSTALLATION OF FRAME AT FS718 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.
- [SDR VNAA20191108101](https://openairdocs.org/sdr/VNAA20191108101.md): Windshield · cracked · Aug 28, 2018 · N244PS · Cndair CL6002B19 · Flight Compartment Windows
  > SUPPLEMENTAL INFORMATION: MX REPLACED FO WINDSHIELD. REMOVED & REPLACED RH WINDSHIELD HEAT CONTROLLER. OPS CHECK GOOD. P/N 1659-1 S/N 4643
- [SDR VNAA2018083081101](https://openairdocs.org/sdr/VNAA2018083081101.md): Windshield · failed · Aug 28, 2018 · N244PS · Cndair CL6002B19 · Flight Compartment Windows
  > THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD SHATTERED IN FLIGHT, AFTER THEY RECEIVED A WINDSHIELD HEAT CUATION MESSAGE. DECLARED AN EMERGENCY AND DIVERTED. THE AIRCRAFT LANDED WITHOUT INCIDENT.
- [SDR VNAA2018040111101](https://openairdocs.org/sdr/VNAA2018040111101.md): Warning Message · false activation · Apr 1, 2018 · N244PS · Cndair CL6002B19 · Pneumatic Distribution System
  > DECLARED AN EMERGENCY ON APPROACH FOR A 14TH STAGE BLEED AIR WARNING. MAINTENANCE INSPECTED LOOPS AND NO DEFECTS WERE FOUND, OPS CHECKED GOOD. NO ABNORMAL INDICATIONS FOUND.
- [SDR VNAA20170606MOC01](https://openairdocs.org/sdr/VNAA20170606MOC01.md): Oil System · fluctuates · Jun 6, 2017 · N244PS · Cndair CL6002B19 · Engine Oil Pressure
  > ON APPROACH, CREW DECLARED AN EMERGENCY DUE TO RT ENGINE OIL PRESSURE FLUCUATED AND JUST BEFORE TOUCHDOWN GOT A RT ENGINE OIL LOW PRESSURE WARNING MESSAGE.
- [SDR VNAA2017012400034](https://openairdocs.org/sdr/VNAA2017012400034.md): Cover · broken · Jan 24, 2017 · N244PS · Cndair CL6002B19 · Emergency Lighting
  > ROW 1 EMERGENCY LIGHT COVER BROKEN. REPLACED THE TRACK COVER, STRAIGHTENED PINS ON FORWARD EMERGENCY TRACK LIGHTING CONNECTOR AND CONNECTED.
- [SDR VNAA2017011600022](https://openairdocs.org/sdr/VNAA2017011600022.md): Wire Harness · defective · Jan 16, 2017 · N244PS · Cndair CL6002B19 · Door System Wiring
  > PASSENGER DOOR LATCH CAUTION MESSAGE DURING FLIGHT. REMOVED AND REPLACED THE PASSENGER DOOR WIRE HARNESS, OPS CHECKED GOOD.
- [SDR VNAA2016102900036](https://openairdocs.org/sdr/VNAA2016102900036.md): Bulkhead Web · cracked · Oct 29, 2016 · N244PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 PRESSURE BULKHEAD WEB IS CRACKED IN 4 PLACES. MAINTENANCE PERFORMED A MAJOR REPAIR.
- [SDR VNAA2016091300010](https://openairdocs.org/sdr/VNAA2016091300010.md): Sensor · faulty · Sep 13, 2016 · N244PS · Cndair CL6002B19 · Pneumatic System
  > RIGHT ENGINE 14TH STAGE BLEED WARNING MESSAGE. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RIGHT HAND PYLON SENSING ELEMENT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRA
- [SDR VNAA2015090200002](https://openairdocs.org/sdr/VNAA2015090200002.md): Anti-Ice Valve · failed · Sep 2, 2015 · N244PS · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > CREW REPORTED RT COWL ANTI-ICE CAUTION MESSAGE. CREW RAN QRH, MESSAGE PERSISTED IN FLIGHT WITH COWL ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT ENGINE COWL ANTI-ICE VALVE AND PERFORMED CHECKS
- [SDR VNAA2015090100001](https://openairdocs.org/sdr/VNAA2015090100001.md): Pressure Switch · failed · Sep 1, 2015 · N244PS · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > CREW REPORTED RT COWL ANTI-ICE CAUTION MESSAGE IN FLIGHT WITH ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT COWL ANTI-ICE PRESSURE SWITCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015083100039](https://openairdocs.org/sdr/VNAA2015083100039.md): Warning Message · false activation · Aug 31, 2015 · N244PS · Cndair CL6002B19 · APU Oil System
  > CREW REPORTED APU OIL PRESSURE CAS MESSAGE DURING CRUISE FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED APU OIL LEVEL AS FULL AND OIL PRESSURE SENSOR CONNECTOR. NO DEFECT FOUND. CHECKS PERFORMED BY MAINTENANCE IAW AMM. COULD NOT D
- [SDR VNAA2015010100001](https://openairdocs.org/sdr/VNAA2015010100001.md): Connector · unsecure · Jan 1, 2015 · N244PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED ROW 6-8 EMERGENCY LIGHTS AND EMERGENCY DOOR LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND SECURED CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014121100003](https://openairdocs.org/sdr/VNAA2014121100003.md): Stringer · cracked · Dec 11, 2014 · N244PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L FWD OF BS 379 HAS.500 INCH CRACK. REPAIRED THE STRINGER IAW SRM, 53-00-03, SPLICE REPAIR FIG 202, SHEET 1.
- [SDR VNAA2014121900005](https://openairdocs.org/sdr/VNAA2014121900005.md): Skin · dented · Dec 4, 2014 · N244PS · Cndair CL6002B19 · Spoilers
  > LEFT INBD GROUND SPOILER, INBD LOWER CORNER DENTED 5" LONG AND 2" WIDE. REPAIRED IAW EO CL600-2B19-57-L02986.
- [SDR VNAA2014061300011](https://openairdocs.org/sdr/VNAA2014061300011.md): Pump · failed · Jun 13, 2014 · N244PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED, NR 1 HYD SYSTEM FAILED IN FLIGHT WITH NO PRESSURE AND NO FLUID LEVELS. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED REPAIR TO PRESSURE LINE FROM NR 1 ENGINE DRIVEN PUMP AFTER FINDING LINE CHAFED THROUGH AT CL
- [SDR VNAA2014050800006](https://openairdocs.org/sdr/VNAA2014050800006.md): Control Unit · failed · May 8, 2014 · N244PS · Cndair CL6002B19 · Stabilizer Control System
  > CREW REPORTED STAB CHANNEL ONE INOPERATIVE MESSAGE DURING FLIGHT. ENGAGED SYSTEM AND BOTH STAB TRIM AND MACH TRIM WENT INOPERATIVE. CREW FOLLOWED QRH TO RE-ENGAGE SYSTEMS. STABILIZER CHANNEL, 1 INOPERATIVE MESSAGE OCCURRED AGAIN, FOLLOWED BY STAB TRIM AND MA
- [SDR VNAA2013092400011](https://openairdocs.org/sdr/VNAA2013092400011.md): Oil System · low pressure · Sep 24, 2013 · N244PS · Cndair CL6002B19 · Engine Oil Indicating System
  > CREW REPORTED LT ENGINE OIL PRESSURE AMBER DURING TAKEOFF ABOVE 80 KTS AND FOR FIRST 3 MINUTES AFTER TAKEOFF. MAXIMUM PSI OBSERVED WAS 150 PSI. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MX INSPECTED, R & R LT ENGINE AND PERFORMED CHECKS IAW AMM.
- [SDR VNAA2013082900018](https://openairdocs.org/sdr/VNAA2013082900018.md): Skin · damaged · Aug 29, 2013 · N244PS · Cndair CL6002B19 · Wing, Plate/Skin
  > DURING SCHEDULED MX, THE RT LOWER WING PLANK CHAFE DAMAGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013082900017](https://openairdocs.org/sdr/VNAA2013082900017.md): Skin · damaged · Aug 29, 2013 · N244PS · Cndair CL6002B19 · Wing, Plate/Skin
  > DURING SCHEDULED MX, THE LT LOWER WING PLANK CHAFE DAMAGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013062800019](https://openairdocs.org/sdr/VNAA2013062800019.md): Control Unit · failed · Jun 28, 2013 · N244PS · Cndair CL6002B19 · Stabilizer Control System
  > CREW REPORTED STAB TRIM CAUTION MESSAGE AND RUNAWAY DURING CLIMB. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED HSTCU (HORIZONTAL STABILIZER TRIM CONTROL UNIT), CLEANED MACH TRIM SWITCH AND PERFORMED CHECKS
- [SDR VNAA2013031800017](https://openairdocs.org/sdr/VNAA2013031800017.md): Ring · damaged · Mar 18, 2013 · N244PS · Cndair CL6002B19 · Exterior Lighting
  > CREW REPORTED POSSIBLE LIGHTNING STRIKE IN FLIGHT AT 17,000 FEET. AIRCRAFT IN CLEAN CONFIGURATION. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REMOVED AND REPLACED LOWER TAIL NAV LIGHT LENS RING DUE TO MULTIPLE M
- [SDR VNAA2013021000009](https://openairdocs.org/sdr/VNAA2013021000009.md): Warning System · false activation · Feb 10, 2013 · N244PS · Cndair CL6002B19 · AC Indicating System
  > CREW REPORTED GEN 2 AMBER CAS MESSAGE ON CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING FIM (FAULT ISOLATION MANUAL). MAINTENANCE FOUND IDG (INTEGRATED DRIVE GENERATOR) OIL LEVEL FULL, INSPECTED WIRING AND PERFOR
- [SDR VNAA2012050800010](https://openairdocs.org/sdr/VNAA2012050800010.md): Display · dirty · May 8, 2012 · N244PS · Cndair CL6002B19 · Central Display
  > CREW REPORTED CAPTAIN’S PFD DISPLAY TEMP MESSAGE AND FIRST OFFICER’S PFD AND MFD DISPLAY TEMP MESSAGES DURING FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED FLIGHT DISPLAY DUCTS, PFD’S (PRIMARY FLIGHT DISPLAY) AND MFD (M
- [SDR VNAA2012050300004](https://openairdocs.org/sdr/VNAA2012050300004.md): Radome · damaged · May 3, 2012 · N244PS · Cndair CL6002B19 · Aerodynamic Fairings
  > CREW REPORTED TOP STATIC WICK ON LEFT WINGLET MISSING, WITH SOME BURN DAMAGE VISIBLE. CREW ALSO REPORTED POSSIBLE LIGHTNING STRIKE DAMAGE TO TAIL CONE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REMOVED AND REPLACED RADOME AND LEFT WINGLET TIP FAIRIN
- [SDR VNAA2011112000001](https://openairdocs.org/sdr/VNAA2011112000001.md): Bulkhead · cracked · Nov 21, 2011 · N244PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE FS 621 BULKHEAD WEB WAS FOUND CRACKED. THE FS 621.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011111500011](https://openairdocs.org/sdr/VNAA2011111500011.md): Floorbeam · cracked · Nov 15, 2011 · N244PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011102100019](https://openairdocs.org/sdr/VNAA2011102100019.md): Transducer · malfunctioned · Oct 17, 2011 · N244PS · Cndair CL6002B19 · Engine Oil Pressure
  > CREW REPORTED LEFT ENGINE LOW OIL PRESSURE 40 TO 22 PSI AT ALL POWER SETTINGS AFTER DEPARTURE FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE TRANSDUCER
- [SDR VNAA2011101900014](https://openairdocs.org/sdr/VNAA2011101900014.md): Scavenge Pump · malfunctioned · Oct 13, 2011 · N244PS · Cndair CL6002B19 · Turbine Engine Oil System
  > CREW REPORTED LEFT OIL PRESSURE DROPPED FROM 70 PSI TO 48 PSI ON TAKEOFF ROLL ON DEPARTURE FROM CLT. LEFT HAND OIL PRESSURE DROPPED TO 39 PSI AT 2,000 FEET. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLAC
- [SDR VNAA2011092900023](https://openairdocs.org/sdr/VNAA2011092900023.md): Bpsu · failed · Sep 25, 2011 · N244PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL AMBER CAS MESSAGE IN FLIGHT EN ROUTE FROM CAK TO CLT. CREW DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING A
- [SDR VNAA2011092800022](https://openairdocs.org/sdr/VNAA2011092800022.md): Ecu · failed · Sep 23, 2011 · N244PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL CAUTION MESSAGE AT ZERO DEGREES ON DESCENT INTO SDF. AIRCRAFT LANDED IN SDF WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENAN
- [SDR VNAA2011091900019](https://openairdocs.org/sdr/VNAA2011091900019.md): Bpsu · failed · Sep 14, 2011 · N244PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL CAUTION MESSAGE IN FLIGHT ON DESCENT INTO CLT. CREW COMPLETED QRH AND AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED RIGHT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS

Next page: https://openairdocs.org/deregistered/N244PS-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 = 'N244PS' AND deregistration_id = 'N244PS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N244PS-2025-12-09/reports

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