N254PS, cancelled Dec 9, 2025

Service difficulty reports · 92

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 = 'N254PS' AND deregistration_id = 'N254PS-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 VNAA2020030611101Unknown · malfunctionedR/H PACK FAIL IN FLIGHT WITH LH PACK ON DEFERRAL. PERFORMED OPS CHECK OF RH PACK IAW CRJ 200 AMM 21-51-00-710-801. OPS CHECK GOOD AT THIS TIME.Mar 4, 2020 · N254PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA2020013021102Control Unit · failedJUST GETTING READY TO START APPROACH FOR CHA AT ABOUT 3000 FT. SET FLAPS TO 8 DEGREES AND GOT A FLAP FAIL CAUTION MESSAGE. CREW BROKE OFF APPROACH, RAN QRH, THEN MADE DECISION TO DIVERT TO TYS DUE TO RUNWAY LENGTH AND A WET RUNWAY. LANDED TYS WITHOUT INCIDENT.Jan 27, 2020 · N254PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2018111211102Strut · contaminatedGEAR DISAGREE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD SERVICED NLG STRUT SUSPECTED AIR IN THE SYSTEM.Nov 12, 2018 · N254PS · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR VNAA2018102811102Sensor · out of limitsTHE CREW RECEIVED A NOSE GEAR DISAGREE AFTER TAKEOFF. THEY RAN THE QRH WHICH TOLD THEM TO LAND AT THE NEAREST SUITABLE AIRPORT. THEY RETURNED TO SHV AFTER BURNING OFF SOME FUEL. FOUND NGL WOW SENSOR TO BE OUT OF LIMITS. ADJUSTED SENSOR IAW CRJ200AMM. OPS CHECOct 28, 2018 · N254PS · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA2018102599915Door Sill · corrodedGALLEY SVC DOOR/LOWER SILL ANGLE CORRODED IN THREE LOCATIONS. C/A:. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE LOWER SILL ANGLE IAW SRM 51-40-11, 51-42-06, 51-42-13 AND 51-42-21.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2018102599914Angle · crackedRT SIDE FS625 OBLIQUE ANGLE IS CRACKED. C/A: REMOVED AND REPLACED RT OBLIQUE ANGLE PN 601-35012-52 IAW SRM 51-42-06.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2018102599913Floorbeam · corrodedDISCREPANCY: CARGO FLOORBEAM IS CORRODED LT SIDE FS 589.00 BETWEEN LBL 9 AND LBL 18. CORRECTIVE ACTION: REMOVED CORROSION FROM FLOORBEAM CAP STRIP AND FOUND CAP STRIP TO BE OUT OF LIMITS, REMOVED AND REPLACED FLOORBEAM CAP STRIP IAW SRM 51-40-11 (TR51-42), 51-Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2018102599912Floorbeam · corrodedDISCREPANCY: LBL 27 FLOORBEAM IS CORRODED BETWEEN FS 589 - FS 605 CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM CAP IAW REO 601R-53-61-6742 REV -- DATED 2018/10/16.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2018102599911Seat Track · corrodedDISCREPANCY: RBL9 SEAT TRACK IS CORRODED AT VARIOUS LOCATIONS FROM FS 559 TO FS 559+80. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK @ RBL 9 FS 559-55-+80 IAW AMM 53-01-11-000/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018102599910Seat Track · corrodedDISCREPANCY: LBL 9 SEAT TRACK IS CORRODED AT VARIOUS LOCATIONS FROM FS 559-FS559+80 CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018102599909Bulkhead · crackedDISCREPANCY: FS621 REAR PRESSURE BULKHEAD WEB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA @ LBL 27 WL 106.25 TO WL 137.25 AT 50% FSH, FAILED NDT INSPECTION. CORRECTIVE ACTION: REPAIRED REAR PRESSURE BULKHEAD AT LBL 27 IAW REO'S 601R-5Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018102599908Strap · damagedDISCREPANCY: WHILE PERFORMING TRUNNION SB 601R-57-046 REV C, FOUND 1EA HOLE TO BE PREVIOUSLY OVERSIZED AT MOST AFT HOLE ON STEEL STRAP, LEFT SIDE. CORRECTIVE ACTION: REPAIRED DAMAGED HOLE IAW REO 601R-57-21-2879 REV -- DATED 2018/10/16.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR VNAA2018102599907Strap · damagedDISCREPANCY: WHILE PERFORMING TRUNNION SB 601R-57-046 REV C, FOUND 1EA HOLE TO BE PREVIOUSLY OVERSIZED AT MOST AFT HOLE ON STEEL STRAP, RIGHT SIDE. CORRECTIVE ACTION: REPAIRED DAMAGED HOLE IAW REO 601R-57-21-2878 REV -- DATED 2018/10/16.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR VNAA2018102599906Angle · crackedDISCREPANCY: AFT CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IAW SRM 51-42-21.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR VNAA2018102599905Tie Down · corrodedDISCREPANCY: 5 CARGO TIE DOWNS ARE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED 5 EA ANCHOR PLATES IAW SRM 51-41-02.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Cargo CompartmentsSDR VNAA2018102599904Cargo Track · corrodedDISCREPANCY: RBL9 CARGO SEAT TRACK IS CORRODED AT FS 559+112. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK AT RBL9 FS559+112 IAW AMM 53-01-11-000-802/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018102599903Cargo Track · corrodedDISCREPANCY: CARGO SEAT TRACK IS CORRODED AT LBL18 FROM FS559+80 TO FS559+96. CORRECTIVE ACTION: REMOVED AND REPLACED CARGO SEAT TRACK AT LBL18 FROM FS559+80 TO FS559+96 IAW AMM 53-01-11-400-802.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018102599902Cargo Track · corrodedDISCREPANCY: CARGO SEAT TRACK IS CORRODED AT LBL9 BETWEEN FS559+80 AND 559+96. CORRECTIVE ACTION: REMOVED AT REPLACED CARGO SEAT TRACK AT LBL9 BTWN FS559+80 AND 559+96 IAW AMM 53-01-11-000-802/400-802 AND REO 601R-53-00-485 REV C DATED 2017-12-18.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018102599901Fitting · crackedDISCREPANCY: RT INBOARD CLIP AT F.S. 484 IS CRACKED CORRECTIVE ACTION: REMOVED AND REPLACED 601R31171-9 CLIP IAW SRM 53-41-43 AND 51-42-21.Oct 25, 2018 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017090611101Landing Gear · malfunctionedAFTER TAKE OFF, THE CREW TRIED TO RETRACT THE LANDING GEAR AND RECEIVED A GEAR DISAGREE WARNING MESSAGE. THE MAIN GEAR DISPLAYED UP AND LOCKED, BUT THE NOSE GEAR WAS STILL SHOWING DOWN AND GREEN. FOLLOWED THE QRH AND SELECTED THE GEAR MANUAL RELEASE AND ALLSep 6, 2017 · N254PS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR VNAA2017040500005Proximity Sensor · malfunctionedPASSENGER DOOR AMBER MESSAGE IN FLIGHT. REMOVED AND REPLACED PROXIMITY SENSOR PS9MB.Apr 5, 2017 · N254PS · Cndair CL6002B19 · Door Warning SystemSDR VNAA2017022400031Latch · stickingCAN NOT LATCH MAIN CABIN DOOR. CLEANED AND LUBRICATED LATCH. OPERATIONAL CHECK GOOD.Feb 24, 2017 · N254PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2017021400022Switch · inoperativeCABIN ALTITUDE AND OVERBOARD COOL CAUTION MESSAGE IN FLIGHT. AIRCRAFT WAS NOT PRESSURIZING. REMOVED AND REPLACED PASSENGER DOOR SWITCH S102MB.Feb 14, 2017 · N254PS · Cndair CL6002B19 · DoorsSDR VNAA2016101400046Bulkhead · crackedFS 621 REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATION AT LBL27.50, WL130. MAINTENANCE REPAIRED BULKHEAD WEB AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Oct 14, 2016 · N254PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2016101400045Strap · corrodedCORROSION ON TOP SIDE OF STRAP AT FS 559, LBL30. MAINTENANCE REMOVED AND REPLACED STRAP AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Oct 14, 2016 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2016101300016Bulkhead Web · crackedBS 621 REAR PRESSURE BULKHEAD WEB CRACKED AT LBL 27.50 AT TOP OF CARGO DOOR AFT TRACK. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW REO.Oct 13, 2016 · N254PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2016101300015Strap · corrodedCORROSION FOUND ON TOP SIDE OF STRAP AT BS 559 NEAR LBL 30. MAINTENANCE REMOVED AND REPLACED STRAP IAW SRM.Oct 13, 2016 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2016040800009Warning Light · false activationCREW REPORTED A "STEERING INOPERATIVE" MESSAGE IN FLIGHT. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, COMPLIED WITH SYS RESET AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.Apr 8, 2016 · N254PS · Cndair CL6002B19 · Steering UnitSDR VNAA2016011100009Control Lever · failedCREW REPORTED FLAPS FAIL MESSAGE DURING CLIMBOUT. FLAPS AT 8 DEGREES DURING TAKEOFF. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM IAW FIM, R & R FLAP LEVER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jan 11, 2016 · N254PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2015111100005Flap System · malfunctionedCREW REPORTED FLAP FAIL AT 30 DEGREES ON FINAL APPROACH. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FIM AND DETERMINED SYS OPERATED NORMALLY AND THAT CAUSE OF DISCREPANCY WAS OPERATOR ERROR. MAINTENANov 11, 2015 · N254PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2015072100023Battery Pack · dischargedEMERGENCY LIGHT HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 3 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jul 21, 2015 · N254PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2015072100022Battery Pack · dischargedEMERGENCY LIGHT HAD BEEN LT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 1 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jul 21, 2015 · N254PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2015072100021Battery Pack · dischargedEMERGENCY LIGHT HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 2 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jul 21, 2015 · N254PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2015072100020Battery Pack · dischargedEMERGENCY LIGHTS HAD BEEN LEFT ON. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHTS BATTERY PACK NR 4 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jul 21, 2015 · N254PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2015021700013Smoke Detector · false activationCREW REPORTED SMOKE LAV CAUTION MESSAGE AT 2,500 FT. ALARM IN LAV WENT OFF WITH F/A SMELLING SMOKY SMELL. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LAV SMOKE DETECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Feb 17, 2015 · N254PS · Cndair CL6002B19 · Smoke DetectionSDR VNAA2015021700012Coalescer Bag · odorCREW REPORTED SMOKE LAV CAUTION MESSAGE AT 2,500 FT ALARM IN LAV WENT OFF WITH F/A SMELLING SMOKY SMELL. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT COALESCER BAG AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Feb 17, 2015 · N254PS · Cndair CL6002B19 · Humidity Control SystemSDR VNAA2015010600006Adc · failedCREW REPORTED CAPTAIN’S PRIMARY FLIGHT DISPLAY (PFD) LOST AIRSPEED, ALTITUDE AND NAVIGATION DATA IN FLIGHT. MACH TRIM ALSO DISCONNECTED AND AUTOPILOT DISENGAGED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT. R & R NR 1 AIR DATAJan 6, 2015 · N254PS · Cndair CL6002B19 · Air Data ComputerSDR VNAA201412020001Fuel Nozzle · leakingDURING START OF APU, THE CREW REPORTED A FUEL ODOR IN COCKPIT. MAINTENANCE TROUBLSHOT FUEL ODOR AND FOUND TOP FUEL NOZZLE/FUEL LINE CHAFED AND INDICATION OF FIRE. R & R APU, OPS AND LEAKED CHECK GOOD. ACFT RELEASED FOR SERVICE.Dec 2, 2014 · N254PS · Cndair CL6002B19 · APU Engine Fuel and ControlSDR VNAA2014120200001Line · chafedWHILE STARTING THE APU, THE CREW REPORTED A FUEL ODOR IN COCKPIT. MAINTENANCE TROUBLESHOT FUEL ODOR AND FOUND TOP FUEL NOZZLE AND NOZZLE FUEL LINE CHAFED. R & R APU, OPS AND LEAKED CHECK GOOD. ACFT RELEASED FOR SERVICE.Dec 2, 2014 · N254PS · Cndair CL6002B19 · APU Engine Fuel and ControlSDR VNAA2014112600016Door Sill · corrodedCARGO DOOR SILL IS CORRODED AROUND NUTPLATES BS 574 - 621. REMOVED AND REPLACED THE CORRODED DOOR SILL IAW REO 601-53-61-1574, REV B.Nov 26, 2014 · N254PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2014112600015Floorbeam · damagedRBL 9 FLOORBEAM HAS ELONGATED HOLE AST FS 559 + 34 ON OTBD SIDE WITH SCREW STILL STUCK IN HOLE. REPAIRED FLOORBEAM AT FS 559+34, RBL 9 IAW SRM 53-00-43, REV 32, REPAIR 1, FIGURE 203, SHEET 2.Nov 26, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2014112600014Stringer · crackedSTRINGER 3L IS CRACKED .750" LONG AT FS 379.00. REPAIRED CRACKED STRINGER 3L AT FS 379.0 IAW REO 601R-53-21-2582 AND SRM 53-00-03.Nov 26, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR VNAA2014112600013Attach Fitting · damagedPASSENGER DOOR ATTACHMENT STRUCTURE FOR STOP PANEL 832 ET FASTENER HOLE ENLARGED. REPAIRED DAMAGED NUTPLATE AND BOTTOM ROW OF PANEL 832 ET STEP STRUCTURE IAW EO NR CL600-2B19-52-L02946.Nov 26, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA201411170007Stiffener · crackedTHE RIGHT INLET INTERNAL STIFFENER AT 11 O'CLOCK FWD MOST HOLE IS CRACKED. CUT AND REMOVED THE DAMAGE PART OF THE INLET INTERNAL STIFFENER. FABRICATED A REPAIR ANGLE, APPROXIMATELY 3.5" LONG AND INSTALLED ANGLE.Nov 26, 2014 · N254PS · Cndair CL6002B19 · Engine Air Intake SystemSDR VNAA201411170006Stringer · crackedSTRINGER 3L IS CRACKED .750' LONG AT BS 379.Nov 17, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR VNAA2014111700005Bulkhead · crackedFS 202.75 HAS EVIDENCE OF CRACK ON FWD AND AFT SIDE OF BULKHEAD AROUND PARKING BRAKE CABLE HOLE.Nov 17, 2014 · N254PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2014100200002Target · out of rigCREW REPORTED GEAR DISAGREE WARNING MESSAGE DURING FLIGHT. LEFT GEAR SHOWED DASHES. MANUAL RELEASE WORKED NORMALLY. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND PROXIMITY SENSOR ELECTRONIC UNIT FLAGGING LEFT LANDING GEAR UPOct 2, 2014 · N254PS · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA2014061500013Carbon Seal · leakingCREW REPORTED LT ENGINE OIL PRESSURE RED WARNING MESSAGE AT FL320. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND IDG CARBON SEAL LEAKING. MAINTENANCE R & R LT ENGINE IDG CARBON SEAL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FORJun 15, 2014 · N254PS · Cndair CL6002B19 · AC Generator-AlternatorSDR VNAA2014051500009Structure · damagedCREW REPORTED POSSIBLE LIGHTNING STRIKE ON LT SIDE OF ACFT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R THE LOWER VHF ANTENNA AND STATIC WICKS ON HORIZONTAL STABILIZER. REPAIR PERFORMED FOR BURN MARK ON LT SIDE AFT TAIL CONE. MAINTENANCE PERMay 15, 2014 · N254PS · Cndair CL6002B19 · Fuselage Structure (General)SDR VNAA2014020400002Feeder Cable · damagedCREW REPORTED AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT POWER STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Feb 4, 2014 · N254PS · Cndair CL6002B19 · Light System Wiring
Back to N254PS, cancelled Dec 9, 2025