N244PS, cancelled Dec 9, 2025

Service difficulty reports · 90

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA2022012011101Fairing · bentUPPER 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 CRJ200Dec 30, 2019 · N244PS · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR VNAA2019103011102Inverter · failedR/H OVERWING EMERGENCY "EXIT: SIGN NOT WORKING. R/R INVERTER FOR RH OVERWING LOWER EMERGENCY EXIT SIGN. OPS CHECK GOOD.Oct 30, 2019 · N244PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2019092711103Cable · frayedDOOR 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 TIMESep 27, 2019 · N244PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2019062211102Ring · wornRIGHT 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.Jun 22, 2019 · N244PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2019100217101Sign · inoperativeRH 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.Mar 17, 2019 · N244PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2019031211101Windshield · crackedRIGHT 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 POMar 12, 2019 · N244PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2018110899912Fitting · crackedWINDSHIELD 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 CNov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2018110899911Support Bracket · brokenSUPPORT 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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR VNAA2018110899910Cascade · crackedUPPER 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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2018110899909Angle · crackedFS.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 FNov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2018110899908Cargo Track · corrodedAFT 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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018110899907Cargo Track · corrodedAFT 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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018110899906Seat Track · corrodedSEAT 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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018110899905Cargo Track · brokenAFT 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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018110899904Cargo Track · corrodedAFT 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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018110899903Cargo Track · corrodedAFT 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 53-01-11-400-802Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018110899902Seat Track · corrodedSEAT 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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018110899901Door Frame · crackedR/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.Nov 8, 2018 · N244PS · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA2018111199901Frame · crackedFS718 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.Oct 11, 2018 · N244PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA20191108101Windshield · crackedSUPPLEMENTAL INFORMATION: MX REPLACED FO WINDSHIELD. REMOVED & REPLACED RH WINDSHIELD HEAT CONTROLLER. OPS CHECK GOOD. P/N 1659-1 S/N 4643Aug 28, 2018 · N244PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2018083081101Windshield · failedTHE 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.Aug 28, 2018 · N244PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2018040111101Warning Message · false activationDECLARED 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.Apr 1, 2018 · N244PS · Cndair CL6002B19 · Pneumatic Distribution SystemSDR VNAA20170606MOC01Oil System · fluctuatesON 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.Jun 6, 2017 · N244PS · Cndair CL6002B19 · Engine Oil PressureSDR VNAA2017012400034Cover · brokenROW 1 EMERGENCY LIGHT COVER BROKEN. REPLACED THE TRACK COVER, STRAIGHTENED PINS ON FORWARD EMERGENCY TRACK LIGHTING CONNECTOR AND CONNECTED.Jan 24, 2017 · N244PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2017011600022Wire Harness · defectivePASSENGER DOOR LATCH CAUTION MESSAGE DURING FLIGHT. REMOVED AND REPLACED THE PASSENGER DOOR WIRE HARNESS, OPS CHECKED GOOD.Jan 16, 2017 · N244PS · Cndair CL6002B19 · Door System WiringSDR VNAA2016102900036Bulkhead Web · crackedBS 621 PRESSURE BULKHEAD WEB IS CRACKED IN 4 PLACES. MAINTENANCE PERFORMED A MAJOR REPAIR.Oct 29, 2016 · N244PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2016091300010Sensor · faultyRIGHT 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 AIRCRASep 13, 2016 · N244PS · Cndair CL6002B19 · Pneumatic SystemSDR VNAA2015090200002Anti-Ice Valve · failedCREW 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 Sep 2, 2015 · N244PS · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR VNAA2015090100001Pressure Switch · failedCREW 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.Sep 1, 2015 · N244PS · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR VNAA2015083100039Warning Message · false activationCREW 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 DAug 31, 2015 · N244PS · Cndair CL6002B19 · APU Oil SystemSDR VNAA2015010100001Connector · unsecureCREW 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.Jan 1, 2015 · N244PS · Cndair CL6002B19 · Light System WiringSDR VNAA2014121100003Stringer · crackedSTRINGER 3L FWD OF BS 379 HAS .500 INCH CRACK. REPAIRED THE STRINGER IAW SRM, 53-00-03, SPLICE REPAIR FIG 202, SHEET 1.Dec 11, 2014 · N244PS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR VNAA2014121900005Skin · dentedLEFT INBD GROUND SPOILER, INBD LOWER CORNER DENTED 5" LONG AND 2" WIDE. REPAIRED IAW EO CL600-2B19-57-L02986.Dec 4, 2014 · N244PS · Cndair CL6002B19 · SpoilersSDR VNAA2014061300011Pump · failedCREW 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 CLJun 13, 2014 · N244PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR VNAA2014050800006Control Unit · failedCREW 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 MAMay 8, 2014 · N244PS · Cndair CL6002B19 · Stabilizer Control SystemSDR VNAA2013092400011Oil System · low pressureCREW 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. Sep 24, 2013 · N244PS · Cndair CL6002B19 · Engine Oil Indicating SystemSDR VNAA2013082900018Skin · damagedDURING SCHEDULED MX, THE RT LOWER WING PLANK CHAFE DAMAGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.Aug 29, 2013 · N244PS · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA2013082900017Skin · damagedDURING SCHEDULED MX, THE LT LOWER WING PLANK CHAFE DAMAGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.Aug 29, 2013 · N244PS · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA2013062800019Control Unit · failedCREW 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 CHECKSJun 28, 2013 · N244PS · Cndair CL6002B19 · Stabilizer Control SystemSDR VNAA2013031800017Ring · damagedCREW 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 MMar 18, 2013 · N244PS · Cndair CL6002B19 · Exterior LightingSDR VNAA2013021000009Warning System · false activationCREW 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 PERFORFeb 10, 2013 · N244PS · Cndair CL6002B19 · AC Indicating SystemSDR VNAA2012050800010Display · dirtyCREW 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 (MMay 8, 2012 · N244PS · Cndair CL6002B19 · Central DisplaySDR VNAA2012050300004Radome · damagedCREW 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 FAIRINMay 3, 2012 · N244PS · Cndair CL6002B19 · Aerodynamic FairingsSDR VNAA2011112000001Bulkhead · crackedDURING 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.Nov 21, 2011 · N244PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2011111500011Floorbeam · crackedDURING 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.Nov 15, 2011 · N244PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2011102100019Transducer · malfunctionedCREW 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 TRANSDUCEROct 17, 2011 · N244PS · Cndair CL6002B19 · Engine Oil PressureSDR VNAA2011101900014Scavenge Pump · malfunctionedCREW 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 REPLACOct 13, 2011 · N244PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2011092900023Bpsu · failedCREW 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 ASep 25, 2011 · N244PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2011092800022Ecu · failedCREW 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 MAINTENANSep 23, 2011 · N244PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2011091900019Bpsu · failedCREW 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 CHECKSSep 14, 2011 · N244PS · Cndair CL6002B19 · Trailing Edge Flap Control System
Back to N244PS, cancelled Dec 9, 2025