N215PS, cancelled Dec 9, 2025

Service difficulty reports · 67

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 = 'N215PS' AND deregistration_id = 'N215PS-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 VNAA2020022311101Inverter · failedR&R #2 EMERGENCY LIGHT INVERTER IAW CRJ 200 AMM 33-51-07-000/400-801 OPS CHECK GOOD AT THIS TIME.Feb 23, 2020 · N215PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2020021399908Intercostal · crackedLH UPPER INTERCOSTAL FROM FS 621 TO FS 625, BL 45, STR 14L, WL 97.5 IS CRACKED APPROX 0.5" LONG. R.CHEUVRONT 1/12/20 (PCC) M/A: 1. REMOVED INTERCOSTAL IAW CRJ 200 SRM 51-42-21. INSTALLED INTERCOSTAL IAW CRJ 200 SRM 51-42-21 AND 51-25-16.Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2020021399907Bulkhead Web · cracked5 EA AREAS OF CRACK INDICATIONS NOTED ON FS 621 RPB WEB IN THE HEEL LINE AREA OF VERT POST. 1ST AREA AT RBL 9 WL 127 - 132.5 50% FSH, SECOND AREA AT RBL 9 WL 110 - WL 115 60% FSH, THIRD AREA AT LBL 18 WL 127.25 - WL 135 50% FSH, 4TH LBL 18 WL 100.5 - WL 105 60Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, BulkheadSDR VNAA2020021399906Post · crackedONE CRACK ON LH WINDISHIELD SIDE POST LOWER AFT ATTACH FITTING IN RADIUS 0.150" LONG. MARKED ON A/C IN RED SHARPIE. REMOVED DAMAGED LH WINDSHIELD SIDE POST LOWER AFT ATTACH FITTING IAW CRJ 200 SRM 51-42-21. INSTALLED NEW SERVICEABLE LH WINDSHIELD SIDE POST LFeb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA2020021399905Post · crackedONE CRACK INDICATION NOTED ON LH WINDSHIELD SIDE POST AT LOWER C/B FASTENER APPROX 1.500" LONG BY 100% FSH. FAILED NDT INSP. MARKED ON A/C WIHT SHARPIE. B.FLEEMAN 01/14/20 (ROSEM) M/A: 1. REMOVED L/H SIDE POST TRAP IAW CRJ-200 AMM 56-12-01-000-801-PSA J.BARTLEFeb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA2020021399904Strap · corrodedFS 559 FLOOR SUPPORT STRAP CORRODED BETWEEN LBL 45 AND LBL 27. REMOVED SUPPORT STRAP BETWEEN LBL 45 AND LBL 27 IAW CRJ 200 SRM 51-42-06. LOCATED AND DRILLED NEW SUPPORT STRAP BETWEEN LBL 45 AND LBL 27 FS 559 IAW CRJ 200 SRM TR 51-42, 51-42-06.Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA2020021399903Strap · corrodedFS 559 FLOOR SUPPORT STREP CORRODED BETWEEN RBL 27 AND RBL 45. REMOVED FLOOR SUPPORT STRAP BETWEEN RBL 27 AND RBL 45 IAW SRM 51-42-06. LOCATED AND DRILLED NEW SUPPORT STRAP BETWEEN RBL 27 AND RBL 45 IAW CRJ 200 SRM TR 51-42. INSTALLED NEW SUPPORT STRAP BETFeb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA2020021399902Frame · corrodedDEEP CORROSION ON LH FS 513 FRAME AFT FREE FLANGE JUST ABOVE FLOOR IN 1" AREA AT CORNER OF PART. MARKED WITH TAPE. BLOCKED OUT CORROSION ON FRAME, BLEND OUT IS .075" DEEP EVALUATED DAMAGE AND FOUND TO BE OUT OF ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 FIG 10Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA2020021399901Attach Angle · crackedPAX DOOR MOTOR BOTTOM ATTACH ANGLE CRACKED. DISPLACED POWER ASSIST MOTOR FOR ACCESS. CANON PLUG WAS NOT DISCONNECTED. REINSTALLED PAX DOOR MOTOR ASSIST IAW CRJ200 AMM 52-11-08-400-802. REFER TO JOB: 27880105, OP:35 FOR COMPLETION OF INSTALL AND OPERATIONALFeb 13, 2020 · N215PS · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA2019123081103Contact · dirtyLOWER EMERGENCY EXIT LIGHT INOPERATIVE ON THE L/H SIDE BY THE EMERGENCY DOOR. REMOVED EMERGENCY LIGHT, CLEANED CONTACTS, AND REINSTALLED EMERGENCY LIGHT IAW AMM. OPS CHECKED GOOD.Dec 28, 2019 · N215PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2019120541101Warning Message · false activationFLIGHT 5663 DCA/CLE DIVERTED TO CMH DUE TO MAINTENANCE. IN FLIGHT WHILE ON DESCENT INTO CLE ANTI-ICE CAUTION MESSAGE ALERT. CREW RAN QRH AND CAUTION MESSAGE EXTINGUISHED IN FLIGHT. / CREW DECIDED TO CONTINUE DIVERSION AFTER CAUTION MESSAGE EXTINGUISHED. C/W OPDec 4, 2019 · N215PS · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR VNAA2019042641101Computer · failedEMERGENCY DECLARED DUE TO LT AND TOTAL FUEL READOUT DASHED OUT DURING CRUISE. CAPTAIN CONTINUED FLT AND LANDED SAFELY. READOUTS REMAINED DASHED OUT FOR THE REST OF THE FLIGHT AFTER THE EMERGENCY WAS DECLARED.Apr 24, 2019 · N215PS · Cndair CL6002B19 · Fuel Quantity IndicatorSDR VNAA2017121399908Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 WL83; BL0 WL114; RBL 18 WL 113; RBL 27.5 WL 87; RBL 27.5 WL 132; BL 0 WL 132. C/A: PERFORMED 621 BLKHD REPAIR IAW REO 601R-53-61-6352 REV -- WITH REF REO 601R-53-61-1240 REV DDec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017121399907Frame · corrodedFRAME FS 605, LOWER SECTOR, 27-26L FWD FLANGE IS CORRODED. C/A: INSTALLED FRAME SECTOR @ FS 605 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017121399906Strap · corrodedRIGHT FLOORBEAM STRAP AT FS 559 BETWEEN RBL 27 AND RBL 43 IS CORRODED.C/A: INSTALLED NEW SERVICEABLE STRAP IAW CRJ 200 SRM 51-42-06 & 51-42-15.Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017121399905Strap · corrodedLEFT FLOORBEAM STRAP AT FS 559 BETWEEN LBL 27 AND LBL 43 IS CORRODED. C/A: LOCATED, DRILLED AND INSTALLED LEFT FLOOR SUPPORT STRAP AT FS 559 BETWEEN LBL 27 AND LBL 43 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017121399904Frame · crackedFUSELAGE FS 333.0 FRAME IS CRACKED BETWEEN STGR0 AND STGR 1L. C/A: REMOVED AND REPLACED CRACKED FRAME SECTOR BETWEEN STGR 0 AND STGR 1L @ FUSELAGE FS 333.0 IAW BOMBARDIER CRJ 200 SRM REF 51-42-06.Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017121399903Frame · crackedFUSELAGE FS 718 FRAME IS CRACKED AT STGR 11R. C/A: INSTALLED NEW PART F.S 718 P/N 600-36030-24 IAW CRJ200 SRM 51-42-06, 51-42-21, AND 51-41-00.Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017121399902Frame · corrodedPASSENGER DOOR INTERNAL FRAME CORRODED. LOCATED AT CENTER-LINE JUST BELOW PASSENGER DOOR HANDLE HOUSING. C/A: INSTALLED NEW FRAME IAW CRJ200 SRM 51-42-06 AND 51-42-21 AND 51-77-00.Dec 13, 2017 · N215PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2017121399901Vane Cap · chafedRH INBD FLAP VANE SKIN IS CHAFED AT TWO LOCATIONS (MIDDLE AND INBD). C/A: INSTALLED SERVICEABLE LEADING EDGE. P/N 601R14303-52S & -54S IAW CRJ 200 SRM 51-40-11, 51-42-13.Dec 13, 2017 · N215PS · Cndair CL6002B19 · Trailing Edge FlapsSDR VNAA2017072611101Carbon Seal · leakingON FLIGHT LEVEL 270, THE AIRCRAFT LOST THE RIGHT ENGINE OIL PRESSURE. THEY DECENDED TO FLIGHT LEVEL 170 WHERE THEY CONTINUED TO LOSE OIL PRESSURE, AND SHUT DOWN THE RIGHT ENGINE AND DIVERTED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENJul 26, 2017 · N215PS · Cndair CL6002B19 · Engine Oil PressureSDR VNAA2016121200023Wire Harness · faultyEMERGENCY FLOOR LIGHTS ON ROW 1 THROUGH 5 INOPERATIVE. REMOVED AND REPLACED WIRING HARNESS.Dec 12, 2016 · N215PS · Cndair CL6002B19 · Light System WiringSDR VNAA2016062800032Control Unit · faultyHORIZONTAL STABILIZER TRIM CONTOL UNIT FLAGGING MOTOR NR 1 DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE STAB TRIM MOTOR CONTROL UNIT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASE FOR SEJun 28, 2016 · N215PS · Cndair CL6002B19 · Stabilizer ActuatorSDR VNAA2016020700013Bottle · low pressureCREW REPORTED OXYGEN LOW PRESSURE CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, SERVICED CREW OXYGEN SYS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Feb 7, 2016 · N215PS · Cndair CL6002B19 · Crew Oxygen SystemSDR VNAA2015020500002Proximity Sensor · contaminatedCREW REPORTED STEERING INOPERATIVE AND WEIGHT ON WHEELS, INPUT CAUTION MESSAGES JUST AFTER ROTATION. MESSAGE CLEARED WHEN GEAR WAS SELECTED DOWN. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND NLG WOW SENSOR HAD FAULTEFeb 5, 2015 · N215PS · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA2014102800018Element · out of positionCREW REPORTED RIGHT FOURTEENTH DUCT MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RT FOURTEENTH PYLON LOOP RUBBING AIRFRAME IN 2 PLACES AND UNCLAMPED IN ONE. MAINTENANCE CLAMPED AND REPOSITIONED LOOP AOct 28, 2014 · N215PS · Cndair CL6002B19 · Overheat DetectionSDR VNAA2014102800017Reservoir · leakingCREW REPORTED LOSS OF FLUID FROM HYDRAULIC SYSTEM NR 2 WITH QUANTITY AT ZERO PERCENT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R NR 2 HYD RESERVOIR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Oct 28, 2014 · N215PS · Cndair CL6002B19 · Hydraulic Reservoir, MainSDR VNAA2014041100011Computer · faultedDURING CRUISE AT FL290 AND WITH APU OFF, CREW REPORTED YAW DAMPER NR 2 AND AUTOPILOT WENT OFF AND EFIS COMPUTER MONITOR MESSAGE AND HDG AND PIT BOXES DISPLAYED. F/O SIDE PRIMARY FLIGHT DISPLAY (PFD) FLICKERED WITH VERTICAL BARS. ATTITUDE INDICATOR CLIMBING, HApr 11, 2014 · N215PS · Cndair CL6002B19 · Attitude and Direction Data SystemSDR VNAA2014032900021Feeder Cable · damagedCREW REPORTED FLOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE PAST ROW 8. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT CABLE ASSEMBLY IN FRONT OF LAVATORY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Mar 29, 2014 · N215PS · Cndair CL6002B19 · Light System WiringSDR VNAA2014032300019Cargo Track · corrodedDURING SCHEDULED MAINTENANCE, AT THE CARGO COMPARTMENT FLOOR TRACKS AND TIE DOWNS CORROSION WAS FOUND. THE AREA WAS INSPECTED AND TRACKS AND TIEDOWNS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICEMar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2014032300018Sill · corrodedDURING SCHEDULED MAINTENANCE, AT THE CARGO DOOR LOWER SILL CORROSION WAS FOUND AROUND FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO DOOR SILL WAS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA20130323Sill · corrodedDURING SCHEDULED MAINTENANCE, AT THE CARGO DOOR LOWER SILL CORROSION WAS FOUND AROUND FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO DOOR SILL WAS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2014032300017Skin · crackedDURING SCHEDULED MAINTENANCE, SKIN AT FS 235 WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2014032300016Skin · damagedDURING SCHEDULED MAINTENANCE, AREA AFT OF NOSE LANDING GEAR DAMAGED, CAUSED BY LIGHTNING STRIKE. THE AREA WAS INSPECTED AND REPAIRED USING AMM. A PERMANENT REPAIR WAS MADE. AIRCRAFT WAS RELEASED FOR SERVICE.Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2014032300015Skin · crackedDURING SCHEDULED MAINTENANCE, THE RT FORWARD CABIN WINDOW SKIN CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2014010500003Controller · failedCREW REPORTED CAPTAIN’S WINDSHIELD CRACKED AT FL29. DESCENDED, DECLARED AN EMERGENCY AND LANDED AT NEAREST SUITABLE AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDSHIELD, R & R LT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMJan 3, 2014 · N215PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR VNAA2013090800004Relay · failedCREW REPORTED ODOR OF BURNING RUBBER NEAR EXIT ROW. LIGHTS OUT ABOVE BINS ON ROW 8 D/F. MX INSPECTED, R & R POWER RELAY AT ROW 8 D/F AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Sep 8, 2013 · N215PS · Cndair CL6002B19 · Passenger Compartment LightingSDR VNAA2013053100018Fuel Control · failedCREW REPORTED RIGHT ENGINE OVERSPEED MASTER WARNING MESSAGE BELOW 80 KNOTS ON TAKEOFF. CREW REJECTED TAKEOFF AND SAFELY RETURNED TO GATE. MAINTENANCE INSPECTED, PERFORMED POWER ASSURANCE RUN AND FOUND RIGHT ENGINE EXCEEDED MAXIMUM PERMITTED N2. MAINTENANCE May 31, 2013 · N215PS · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR VNAA2013031100008Controller · failedCREW REPORTED RIGHT AOA HEAT, RIGHT PITOT HEAT, RIGHT TAT PROBE HEAT AND RIGHT STATIC HEAT CAS MESSAGES AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) AIR DATA SENSOR HEAT CONTROMar 11, 2013 · N215PS · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR VNAA2013030600007Engine · malfunctionedCREW REPORTED LEFT ENGINE OIL PRESSURE CLIMBED TO APPROXIMATELY 133 PSI ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT REMar 6, 2013 · N215PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2012093000024Bulkhead · crackedDURING SCHEDULED MAINTENANCE FOUND A CRACK AT THE FS 621 BULKHEAD WEB. THE FS 621 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Sep 30, 2012 · N215PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2012093000023Bulkhead · crackedDURING SCHEDULED MAINTENANCE A CRACK AT FS 202.0 BULKHEAD WAS FOUND. THE FS 202.0 BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Sep 30, 2012 · N215PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2012081200005Control Unit · failedCREW REPORTED, STEERING INOP MESSAGE ON GEAR EXTENSION. CREW RESET NOSEWHEEL STEERING IN ACCORDANCE WITH QRH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT NOSEWHEEL STEERING SYSTEM, REMOVED AND REPLACED NWS (NOSEWHEEL STEERING) ECU (ELECTRONICAug 12, 2012 · N215PS · Cndair CL6002B19 · Landing Gear Steering SystemSDR VNAA2011110200031Skin · dentedCREW REPORTED BIRD STRIKE ON RIGHT WING LEADING EDGE ON APPROACH TO PHL. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION, APPLIED AERODYNAMIC FILLER TO DENT ON RIGHT WING MIDDLE LEADING EDGE AND PERFORMED CHEOct 30, 2011 · N215PS · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA2011100600007Skin · damagedAT GSP, CREW REPORTED BIRD STRIKE ON LEADING EDGE OF LEFT WING. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED DENT ON LEFT WING INBOARD LEADING EDGE (L/E ZONE 1) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.Oct 2, 2011 · N215PS · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA2011060300023Acm · seizedCREW REPORTED STRONG ELECTRICAL SMOKE SMELL IN CABIN AT PHL. GROUND PERSONNEL WITNESSED WHITE SMOKE IN VICINITY OF PACK EXHAUST VENTS. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT PACK ACM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAMay 28, 2011 · N215PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA2011060300022Bracket · damagedCREW REPORTED WOW INPUT MESSAGE WITH GEAR IN WELL, THEN STEERING INOP CAS MESSAGE, AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED SENSOR BRACKET, RIGGED SENSOR AND PERFORMED CHECKS USINMay 27, 2011 · N215PS · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA2011060200020Wire Harness · defectiveCREW REPORTED WOW INPUT AND STEERING INOP AMBER CAS MESSAGES AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NR 1 PROXIMITY SENSOR HARNESS ASSEMBLY AND PERFORMED CHECKS USING AIRCRAFT MAMay 27, 2011 · N215PS · Cndair CL6002B19 · Landing Gear System WiringSDR VNAA2011021400006Beam · damagedDURING SCHEDULED MAINTENANCE FS 280.0 J-CHANNEL, TRASVERSE BEAM, AND FLOOR SUPPORT CAPS WERE CRACKED AND CORRODED O/B OF RBL6 AND LBL9. REPAIRS WERE MADE USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.Feb 14, 2011 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011021400007Channel · damagedDURING SCHEDULED MAINTENANCE FS 280.0 J-CHANNEL, TRANSVERSE BEAM, AND FLOOR SUPPORT CAPS WERE CRACKED AND CORRODED O/B OF RBL 6 AND LBL 9. REPAIRS WERE MADE USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.Feb 14, 2011 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N215PS, cancelled Dec 9, 2025