N257PS, cancelled Dec 9, 2025

Service difficulty reports · 61

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 = 'N257PS' AND deregistration_id = 'N257PS-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 VNAA202003119995Door Sill · corrodedAFT CARGO DOOR FLOOR SILL CORRODED IN MULTIPLE LOCAITONS FROM FS 574 - 621 UNDER FLOORBOARD 281LLF. 03/02/20 (ROSEM) M/A: 1. N/A. C/A: 1. FOUND AFT CARGO DORO FLOOR SILL TO BE OUT OF LIMITS IAW CRJ 200 53-0-00 SRM. MTC 03/03/20 M/A: 2. REMOVED THE AFT CARGO DOMar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202003119994Door Sill · corrodedLH PRESSURE FLOOR SILL HAS 3 AREAS OF CORROSION FS449-FS473. 02/20/20 (AS) M/A: 1. N/A C/A: 1. REMOVED CORROSION @ L/H PRESSURE FLOOR SILL BETWEEN FS 409+129 AND FS 559, PRESSURE FLOOR ANGLE 409+128-559 IAW REO 601R-53-41-666, REV.C DATED 2012-11-06. 2/20/20 MMar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202003119993Door Sill · corrodedRH PRESSURE FLOOR SILL HAS 9 AREAS OF CORROSION BETWEEN FS428 AND FS530. 02/20/20 (AS) M/A: 1. N/A C/A: 1. REMOVED CORROSION @ R/H PRESSURE FLOOR SILL AND FLOOR ANGLE IAW REO 601R-53-41-666, REV.C DATED 2012-11-06. 2/20/20 M/A: 2. REPAIR AREAS REQUIRE NDT TO Mar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202003119992Bulkhead · crackedFOUND REAR PRESSURE BUCKHEAD HAS INDICATIONS NOTED AT BLOO WL112-110 5090 FSH AND LBL18 WL141-142.510090FSH BOTH AREAS FAILED NOT INSPECTIONS. 2/17/20 (TK) M/A: 1. REMOVE AFT CARGO DOOR PULLEY BRACKET IAW CRJ200 SRM 51-42-06. 2/20/20 C/A: 1. REINSTALLED AFT CAMar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Main, BulkheadSDR VNAA202003119991Skin · corrodedCORROSION FOUND ON OUTER SKIN UNDER FWD WATER DRAIN MAST. 2/15/20 (PCC) M/A: 1. CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ200 SRM 53-00-31. 2/15/20 C/A: 1. REMOVED CORROSION IAW CRJ200 SRM 51-21-06. 2/15/20 M/A: 2. UT INSPECTION REQUIRED TO DETERMINE REMAININMar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA2019110761102Warning Message · false activationAPU FIRE RED WARNING MESSAGE IN FLIGHT. DEFERRED APU. PER FIM VISABLY INSPECTED APU FIRE LOOP NO DEFECTS NOTED PERFORMED OPS CHECK OF APU FIRE-DETECTION SYSTEM IAW CRJ 200 AMM OPS CHECK GOOD AT THIS TIME. THIS CLEARS MEL.Nov 6, 2019 · N257PS · Cndair CL6002B19 · Fire DetectionSDR VNAA2019071811101Battery · dischargedEMERGENCY LIGHTS WON'T STAY ON. R&R ALL 4 EMERGENCY POWER SUPPLY BATTERIES IAW CRJ 200 AMM 33-51-04-000/400-801. OPS CHECK GOOD AT THIS TIME. S/N 169577, 121949, 103966, 126070Jul 18, 2019 · N257PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2019060911101Inverter · failedLH LOWER EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LH FLOOR LEVEL FLOOD EXIT SIGN IAW CRJ 200 AMM 33-51-10-000/400-801 REMOVED AND REPLACED #2 INVERTER IAW CRJ 200 AMM 33-51-07-000/400-801 OPS CHECK GOODJun 9, 2019 · N257PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2018102211102Exhaust Valve · malfunctionedDURING CLIMB CREW RECEIVED AN OVERBOARD COOL AMBER MSG. AFTER RUNNING THE QRH THE MSG STILL PERSISTED. CREW DECIDED TO CONTINUE TO CLT PRESSURIZED AND DECLARED AN EMERGENCY INTO CLT. MAINTENANCE DEFERRED OVERBOARD EXHAUST VALVE AND INBOARD EXHAUST VALVE.Oct 22, 2018 · N257PS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2018011499912Trunnion · crackedONE INDICATION NOTED IN FASTENER HOLE OTBD OF MLG CUT OUT ON RT SIDE 5TH HOLE GOING FWD FROM AFT HOLE IN STEEL STRAP ON O/B AFT SIDE OF HOLE .550 INCH UP FROM LOWER SURFACE OF STEEL STRAP EXTENDING UP .100 INCH. PERFORMED EDDY CURRENT INSPECTION AT THE RT MLG Jan 14, 2018 · N257PS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR VNAA2018011499911Trunnion · crackedONE INDICATION NOTED IN FASTENER HOLE O/B OF MLG CUT OUT ON LT SIDE FIRST HOLE AFT OF STEEL STRAP. ON AFT SIDE OF HOLE .300 INCH UP FROM LOWER SURFACE OF PLANK EXTENDING UP .100 INCH. REPAIRED THE TRUINNION IAW REO 601R-57-21-2704 REV.Jan 14, 2018 · N257PS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR VNAA2018011499910Bulkhead Web · crackedREAR PRESSURE BULKHEAD WEB HAS CRACK INDICATIONS, LBL 27.5, WL 130. ONE INCH IN LENGTH. CUT OUT DAMAGE IAW REO 601R-53-61-1541, REV F. PERFORMED AN EDDY CURRENT OF REWORKED AREA IAW REO 601R-53-61-1541, REV F. NO INDICATIONS NOTED. REPAIRED IAW REO 6Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018011499909Bulkhead Web · crackedREAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 9.5, WL 109, ONE INCH IN LENGTH. CUT OUT DAMAGE IAW REO 601R-53-61-1285, REV E. PERFORMED EDDY CURRENT OF REWORKED AREAS IAW REO 601R-53-61-1285 REV E, NO INDICATIONS NOTED. REPAIRED Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018011499908Bulkhead Web · crackedREAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 76, ONE INCH LONG. CUT OUT DAMAGE IAW REO 601R-53-61-1285, REV E, SHEET 13, SECTION 5D. THE CUTOUT IS OUTSIDE OF REO 601R-53-61-1285 REPAIR SCOPE. PERFORMED EDDY CURRENT ON REWORKEDJan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018011499907Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED ADJACENT TO POWER ASSIST PULLEY BRACKET. REPAIRED THE DRAG ANGLE IAW EO 2B19-52-L05444A, PART B, AND REO 601R-52-11-513 REV B.Jan 14, 2018 · N257PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2018011499906Frame · crackedFRAME CRACKED AT BS 718, STRINGER 11L. REMOVED AND INSTALLED A NEW FRAME SECTION IAW SRM 51-42-06 & 51-23-16.Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2018011499905Frame · crackedFRAME CRACKED AT BS 718, STRINGER 11R. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, AND SRM 51-40-11.Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2018011499903Angle · crackedFLOORBEAM AT BS 484, LBL27 HAS A CRACKED ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA20180114999Seat Track · corrodedCORROSION ON LEFT SEAT TRACK FWD AND AFT OF BS 409 + 128 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-055, REV C.Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018011499902Seat Track · corrodedCORROSION ON RT SEAT TRACK FWD AND AFT OF BS 409 + 128 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-055, REV C.Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018011499901Angle · crackedAFT EQUIPMENT BAY LEFT BS 621 - 625 OBLIQUE ANGLE CRACKED. REMOVED AND REPLACED THE OBLIQUE ANGLE IAW SRM 51-42-21.Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017070911101Connector · dirtyCREW RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE AT FLIGHT LEVEL 290. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITH OUT INCIDENT. FOUND NO EVIDENCE OF FIRE OR SMOKE. MAINTENANCE CLEANED THE CONNECTOR PLUGS ON THE FIRE BOTTLES AND PREFORMED AN OPS CHECK OFJul 9, 2017 · N257PS · Cndair CL6002B19 · Fire Protection System WiringSDR VNAA2016081800020Control Lever · faultyFLAPS FAILED DURING APPROACH AT 30 DEGREES AND 160 KNOTS. LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLAP CONTROL LEVER AND PREFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Aug 18, 2016 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2016081100009Inverter · inoperativeEMERGENCY FLOOR TRACK LIGHTING OUT AFTER ROW 5 TO THE BACK SIDEWALL. MAINTENANCE R & R THE NR 3 INVERTER IAW AMM AND THE NR 4 POWER SUPPLY BATTERY FOR THE EMERGENCY LIGHTS IAW AMM, OPS CHECK GOOD.Aug 11, 2016 · N257PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2016081100008Inverter · inoperativeRIGHT LOWER FLOODLIGHT INOPERATIVE. MAINTENANCE R & R THE NR 3 INVERTER IAW AMM, OPS CHECK GOOD.Aug 11, 2016 · N257PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2016060400005Controller · inoperativeCAPTAIN SIDE WINDSHIELD SHATTERED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT WINDSHIELD AND WINDSHIELD TEMP CONTROLLER. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND TJun 4, 2016 · N257PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR VNAA2016060400004Windshield · crackedCAPTAIN SIDE WINDSHIELD SHATTERED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT WINDSHIELD AND WINDSHIELD TEMP CONTROLLER. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND TJun 4, 2016 · N257PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2016041600017A/C Pack · malfunctionedDURING CLIMBOUT, THE CREW RECEIVED A RT PACK FAULT AND RT PACK HIGH PRESSURE WHEN COMPLYING WITH MEL PROCEDURES FOR THE LT PACK. MAINTENANCE INTEROGATED AND FOUND NO RELATED FAULTS FOR THE RT PACK AND COULD NOT DUPLICATE THE ISSSUE. MAINTENANCE PERFORMED CHECApr 16, 2016 · N257PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA2016030300003Plate · corrodedPASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE CORRODED. R & R PASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE, PN 600-38061-11 IAW AMM 52-11-17-400-804.Mar 3, 2016 · N257PS · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA2016030200002Angle · corrodedPAX DOOR UPPER SILL ANGLE CORRODED BETWEEN BS 310 AND 349. REPAIRED PAX DOOR UPPER SILL ANGLE, PN 601R31527-221 IAW SRM 51-42-10, 51-42-21, AND 51-42-06.Mar 2, 2016 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2016030200001Floor Support · corrodedRIGHT PRESSURE FLOOR SILL STRAP CORRODED BEYOND LIMITS AT FS 513.00. R & R RT PRESSURE SILL STRAP IAW SRM 51-42-16, 51-42-22, AND 51-77-00.Mar 2, 2016 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2016021400017Connector · damagedCREW REPORTED BACK HALF OF FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT, REPAIRED AFT CONNECTOR ON EMERGENCY LIGHT STRIP AND PERFORMED CHECKS IAW AMM. THE ACFT WAS RELEASED FOR SERVICE.Feb 14, 2016 · N257PS · Cndair CL6002B19 · Light System WiringSDR VNAA2015111100004Wire · disconnectedCREW REPORTED FLOOR EMERGENCY LIGHTS HAD A DISCONNECTED WIRE AND AFT HALF OF LIGHTS BEYOND ROW NINE INOPERATIVE. MAINTENANCE INSPECTED, SPLICED IN WIRE SPLICE CONNECTORS ON ROW 13 EMERGENCY FLOOR LIGHTS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICENov 11, 2015 · N257PS · Cndair CL6002B19 · Light System WiringSDR VNAA2015050700001Sensor · failedCREW REPORTED ANTI-ICE DUCT WARNING MESSAGE DURING CLIMB. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FUSELAGE SENSING ELEMENT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.May 7, 2015 · N257PS · Cndair CL6002B19 · Detection SystemSDR VNAA2014102800016Light · brokenCREW REPORTED ENTRY LIGHT BROKEN. MAINTENANCE INSPECTED, R & R ENTRY FLOOR EMERGENCY FLOODLIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Oct 28, 2014 · N257PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2014061400012Access Door · out of adjustCREW REPORTED FORWARD F/A EMERGENCY EQUIPMENT ACCESS, LATCHES AND DOOR, STICKS AND HARD TO OPEN. MAINTENANCE INSPECTED, ADJUSTED EMERGENCY EQUIPMENT ACCESS DOOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jun 14, 2014 · N257PS · Cndair CL6002B19 · Fixed Inner DoorsSDR VNAA2014052000014Cargo Track · corrodedDURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON THE CARGO TRACKS AT BS 559+80, 559.0+96 AND FS 574 - 605. THE AREA WAS INSPECTED AND CARGO FLOOR TRACKS WERE REPLACED USING AMM. ACFT WAS RELEASED FOR SERVICE.May 20, 2014 · N257PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2014052000013Floor Support · corrodedDURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND AROUND CARGO FLOOR SUPPORT FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO FLOOR SUPPORT WAS REPLACED USING AMM. ACFT WAS RELEASED FOR SERVICE.May 20, 2014 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2014012600017Cover · brokenCREW REPORTED EMERGENCY LIGHT AT ROW 1 INOPERATIVE AND COVER BROKEN. MAINTENANCE INSPECTED, R & R ROW 1 FLOOR-TRACK EMERGENCY LIGHT AND COVER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jan 26, 2014 · N257PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2013121000005Connector · damagedCREW REPORTED EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROW 5 TO ROW 9. MAINTENANCE INSPECTED, R & R J391Y CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Dec 10, 2013 · N257PS · Cndair CL6002B19 · Light System WiringSDR VNAA2013091300006Selector Valve · failedCREW REPORTED GEAR DISAGREE RED CAS MESSAGE. MAIN GEAR INDICATED DOWN AND LOCKED AND NOSE GEAR INDICATED UP. STEERING INOPERATIVE AMBER CAS MESSAGE ALSO REPORTED. CREW MANUALLY EXTENDED LANDING GEAR AND LANDED SAFELY. ACFT TOWED TO RAMP. MX TROUBLESHOT, R Sep 13, 2013 · N257PS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR VNAA2012111200005Controller · failedCREW REPORTED CAPTAIN’S FRONT WINDOW CRACKED AND ELECTRICAL ARCING NOTICED. CREW RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED CAPTAIN’S FRONT WINDOW AND LEFT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MNov 12, 2012 · N257PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR VNAA2012050700009Light · inoperativeCREW REPORTED LEFT AFT EXTERIOR DOOR EMERGENCY LIGHT OUT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT AFT EXTERIOR EMERGENCY LIGHT BULB AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.May 7, 2012 · N257PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2011071800020Bpsu · failedCREW REPORTED FLAPS FAILURE DURING APPROACH FLAPS SELECTED FROM 0-08 WHEN FAILURE OCCURED SPEED WAS 190 IAS, ALT 6000 FT. CREW ELECTED TO DIVERT TO CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CHECKS USING THE AJul 13, 2011 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2011071800016Computer · failedCREW REPORTED A FLAPS FAIL AT 10,000FT SPEED 250KNTS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS ON THE FLAP ELECTRONIC COMPUTER. AIRCRAFT WAS RELEASEJul 12, 2011 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2011071500013Bpsu · failedCREW REPORTED FLAPS FAILURE WHEN FLAPS SELECTED FROM ZERO DEGREES TO EIGHT (8) DEGREES DURING APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PJul 11, 2011 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2011070800005Control Unit · malfunctionedCREW REPORTED FLAPS FAIL AT 20 DEGREES WHEN FLAPS WERE SELECTED TO 30 DEGREES WHILE ON APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKJul 2, 2011 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2011031600011Sill · corrodedDURING SCHEDULED MAINTENANCE THE LEFT PRESSURE FLOOR SILL HAD CORROSION AROUND NUT PLATES FROM FS 449.85 TO 473.15. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.Mar 16, 2011 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011031600013Post · crackedDURING SCHEDULED MAINTENANCE THE FS 409+128 BULKHEAD VERTICAL POST WAS CRACKED. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.Mar 16, 2011 · N257PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2011061600012Beam · crackedDURING SCHEDULED MAINTENANCE, THE FS 280 TRANSVERSE BEAM WAS CRACKED. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.Mar 16, 2011 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N257PS, cancelled Dec 9, 2025