N258PS

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 = 'N258PS' AND registry_match = 'registration'
  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 VNAA2019061511101Warning Light · false indicationWHILE CRUISING AT FL270, RECEIVED GEN 2 OFF CAUTION LIGHT. THE CREW RAN THE QRH AND LIGHT REMAINED. PER QRH, CREW SWITCHED GEN 2 OFF AND STARTED THE APU. SHORTLY THEREAFTER CREW RECEIVED APU OIL TEMP CAUTION. RAN QRH, REQUIRED TO LAND NEAREST SUITABLE. EMJun 15, 2019 · N258PS · Cndair CL6002B19 · AC Generator-AlternatorSDR VNAA2019032499909Angle · crackedFS409+128 VERT POST @ BLO HAS A CRACK INDICATION NOTED ON BOTH LT & RT SIDES IN THE AFT RADIUS @ WL69 (MARKED ON A/C) BOTH FAILED NDT INSP. CORRECTIVE ACTION: DRILLED UP NEW SERVICEABLE ANGLES P/N 601R32208-131/132 IAW SRM 51-40-11 TR51-42.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2019032499908Beam · crackedUPON REMOVAL OF AFT CARGO FLOOR LANDING PLATE FOUND TRAVERSE BEAM AT FS 589, OUTBOARD OF LBL 27, CRACKED IN RADIUS. CORRECTIVE ACTION: COMPLIED WITH REO 601R-53-61-6908 REV.-- DATED 2019-03-15.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA2019032499907Seat Track · corrodedSEAT TRACK SEGMENT BETWEEN FS 364 TO FS 349 AT RBL9 IS CORRODED. CORRECTIVE ACTION: REPLACED SEAT TRACK WITH FABRICATED TRACK PN: N126-2075 IAW REO 601R-53-00-485.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019032499906Seat Track · corrodedSEAT TRACK SEGMENT BETWEEN FS 364 TO FS 349 AT LBL9 IS CORRODED. CORRECTIVE ACTION: REPLACED SEAT TRACK WITH FABRICATED TRACK PN: N126-2075 IAW REO 601R-53-00-485.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019032499905Doubler · corrodedGALLEY FLOOR MOUNT FITTING IS CORRODED AT RBL 5 AT FS 316. CORRECTIVE ACTION: REPLACED GALLEY FLOOR SUPPORT DOUBLER PN: 601R387781-1 IAW SRM 51-42-06, 51-42-13.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2019032499904Seat Track · corrodedLBL 9 SEAT RAIL IS GOUGED/CORRODED IN MULTIPLE LOCATIONS FROM FS 409 TO FS 409 +112. CORRECTIVE ACTION: REPLACED SEAT TRACK WITH FABRICATED TRACK PN: N126-2075 IAW REO 601R-53-00-485.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019032499903Seat Track · corrodedRT FLOOR SEAT RAIL IS CORRODED/GOUGED BETWEEN FS 409 TO FS 409+112. CORRECTIVE ACTION: REPLACED SEAT TRACK WITH FABRICATED TRACK PN: N126-2075 IAW REO 601R-53-00-485.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019032499902Angle · crackedRT MLG WHEEL WELL HYDRAULIC FUSE MOUNTING ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED MOUNTING ANGLE IAW SRM 51-42-06.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2019032499901Angle · crackedLT MLG WHEEL WELL HYDRAULIC FUSE MOUNTING ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED MOUNTING ANGLE IAW SRM 51-42-06.Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2017052500011Motor · inoperativePASSENGER DOOR ASSIST MOTOR INOPERATIVE; REMOVED AND REPLACED PASSENGER DOOR ASSIST MOTOR.May 25, 2017 · N258PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2017052300010Anchor Fitting · crackedPASSENGER DOOR CABLE SWIVEL RUBBING AGAINST THE HANDRAIL SUPPORT BRACKETS; REMOVED AND REPLACED PASSENGER DOOR’S FORWARD ANCHOR FITTING.May 23, 2017 · N258PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2017032400016Bulkhead · corrodedMAINTENANCE PERFORMED A MAJOR REPAIR TO THE REAR PRESSURE BULKHEAD WEB AT FS 621.00 WL 73.00 LBL 9.50.Mar 24, 2017 · N258PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017031300006Cup · corrodedFORWARD AND AFT PASSENGER HANDRAIL CUPS ARE CORRODED. REMOVED AND REPLACED FORWARD AND AFT CUPS.Mar 13, 2017 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2016100600010Wire Harness · damagedPASSENGER DOOR, SERVICE DOOR, AND CARGO DOOR MESSAGES DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FOUND DAMAGE TO WIRES ON AFT CARGO DOOR WIRING HARNESS. MAINTENANCE REMOVED AND REPLACED AFT CARGO DOOR HARNESS AND PERFORMED CHECKSOct 6, 2016 · N258PS · Cndair CL6002B19 · Door System WiringSDR VNAA2016091900025Control Lever · faultyFLAPS FAIL AT 30 DEGREES DURING APPROACH. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLAP CONTROL LEVER AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FORSep 19, 2016 · N258PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2016090800003Selector Valve · faultyGEAR DISAGREE, ANTI-SKID, AND PARKING BREAK SHUT OFF VALVE MESSAGES AFTER TAKE OFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE. PERFORMED CHECKS IAW THE AMM. TSep 8, 2016 · N258PS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR VNAA2016030600011Selector Valve · inoperativeCREW REPORTED RECEIVING A GEAR DISAGREE MESSAGE ON DESCENT. THEY DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE MLG SELECTOR VALVE AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SMar 6, 2016 · N258PS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR VNAA2016021900023Carbon Seal · leakingCREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE NR 7 CARBON SEAL AND PERFORMED CHECKS IAW THE AFeb 19, 2016 · N258PS · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR VNAA2016021900022Carbon Seal · leakingCREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE NR 6 CARBON SEAL AND PERFORMED CHECKS IAW THE AMFeb 19, 2016 · N258PS · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR VNAA2015082300034Controller · failedCREW REPORTED CRACK IN LT WINDSHIELD IN FLIGHT AND SUBSEQUENTLY RECEIVED A LT WINDSHIELD HEAT AMBER CAUTION MESSAGE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD HEAT CONTROLLER DUE TO ARCING IN WINDSHIELD AND PAug 23, 2015 · N258PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR VNAA2015082300033Windshield · crackedCREW REPORTED CRACK IN LT WINDSHIELD IN FLIGHT AND SUBSEQUENTLY RECEIVED A LT WINDSHIELD HEAT AMBER CAUTION MESSAGE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD DUE TO ARCING IN WINDSHIELD AND PERFORMED CHECKS Aug 23, 2015 · N258PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2015080800013B-Nut · looseCREW REPORTED RT ENGINE OIL PRESSURE MESSAGE IN FLIGHT AND ELECTED TO DIVERT. PRIOR TO LANDING, OIL PRESSURE CONTINUED TO DROP, SO CREW ELECTED TO SHUTDOWN RT ENGINE. MAINTENANCE INSPECTED AND FOUND OIL LEAK DUE TO LOOSE B-NUT ON B-SUMP SCAVENGE TUBE BELOW PUAug 8, 2015 · N258PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2015080100001Wire · brokenPRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED EMERGENCY LIGHTS NOT WORKING FROM ROW 9 TO 12. MAINTENANCE TROUBLESHOT, REPAIRED CONNECTOR WIRE, REINSTALLED AFT RT FLOOR EMERGENCY LIGHT TRACK ASSY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Aug 1, 2015 · N258PS · Cndair CL6002B19 · Light System WiringSDR VNAA2015061800014Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTAL FITTING HAS INDICATION NOTED, APPROX .300" IN LENGTH, FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1230 AND REO 601R-53-61-5490.Jun 18, 2015 · N258PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA20150618Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTAL FITTING HAS INDICATION NOTED. APPROXIMATELY .300" IN LENGTH, FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1230 AND REO 601R-53-61-5490.Jun 18, 2015 · N258PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2015061800013Bulkhead · crackedFS 202.75 BULKHEAD IS CRACKED AROUND THE HOLE FOR THE PARKING BRAKE CABLE. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71 IAW REO AND SRM.Jun 18, 2015 · N258PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2015061800012Strap · corrodedTENSION STRAPS BETWEEN RBL 36 AND RBL 27 AT FS559 HAVE FILIFROM AND PITTING CORROSION. R & R TENSION STRAPS WITH NEW SERVICABLE STRAPS IAW SRM.Jun 15, 2015 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2015061800011Strap · corrodedTENSION STRAPS BETWEEN LBL 36 AND LBL 27 AT FS559 HAVE FILIFORM AND PITTING CORROSION. R & R TENSION STRAPS WITH NEW SERVICABLE STRAPS IAW SRM.Jun 15, 2015 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2015061800015Skin · crackedEXTERNAL FUSELAGE SKIN AT NLG CUTOUT AFT RT CORNER HAS CRACK APPROXIMATELY 1" LONG. REPAIRED IAW REO.Jun 13, 2015 · N258PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2015041400019Duct · unknownCREW REPORTED NO AIR FLOW FROM ANY VENTS WHEN BLEEDS WERE TRANSFERRED TO ENGINE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R PRECOOLER OUTLET DUCT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Apr 14, 2015 · N258PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA2015041400018Regulator Valve · failedCREW REPORTED NO AIR FLOW FROM ANY VENTS WHEN BLEEDS WERE TRANSFERRED TO ENGINE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT PACK VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Apr 14, 2015 · N258PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA201412290009Battery Pack · dischargedCREW REPORTED THAT THE EMERGENCY LIGHTS HAD BEEN LEFT ON ALL NIGHT. FERRIED, WHERE MAINTENANCE R & R EMERGENCY LIGHT BATTERIES AND PERFORMED CHECKS IAW MM. ACFT RELEASED FOR SERVICE.Dec 26, 2014 · N258PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2014110200001Connector · damagedCREW REPORTED CABIN FLOOR EMERGENCY LIGHTS AT ROW 8 THROUGH 12 WOULD NOT COME ON. MAINTENANCE INSPECTED EMERGENCY FLOOR PATH LIGHTING AND FOUND BROKEN WIRES AT FLOOR CONNECTION. MAINTENANCE INSTALLED NEW CONNECTORS AND PINS ON EMERGENCY LIGHT STRIP AND PERFORNov 2, 2014 · N258PS · Cndair CL6002B19 · Light System WiringSDR VNAA2013090300002Radar · failedCREW REPORTED WEATHER RADAR STOPPED WORKING AT ALTITUDE AND LOST RETURNS ON CAPTAIN’S AND F/O MFD (MULTIFUNCTION DISPLAY). CREW DIVERTED DUE TO WEATHER AND LANDED WITHOUT INCIDENT. MX INSPECTED, R & R WEATHER RADAR RECEIVER/ TRANSMITTER AND PERFORMED CHECKS Sep 3, 2013 · N258PS · Cndair CL6002B19 · Weather Radar SystemSDR VNAA2013071500013B-Nut · looseCREW REPORTED A STRONG ODOR OF JET FUEL WHILE OPERATING ON APU BLEED SYS. MX INSPECTED, TIGHTENED B-NUT ON FUEL CONTROL SUPPLY LINE AND PERFORMED CHECKS ON APU USING AMM. NO LEAKS NOTED. ACFT RELEASED FOR SERVICE.Jul 15, 2013 · N258PS · Cndair CL6002B19 · APU Oil SystemSDR VNAA2013062000010Structure · crackedDURING SCHEDULED MAINTENANCE FS 621.0 WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Jun 20, 2013 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2012060100001Pump · failedCREW REPORTED HYDRAULIC SYSTEM TWO (2) AT ZERO PSI AND ZERO PERCENT IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) EDP (ENGINE DRIVEN PUMP) AND PERFORMED CHECKS USING AIRCRAFT MAINTJun 1, 2012 · N258PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR VNAA2012052200019Wire · burnedCREW REPORTED SMELL OF SMOKE IN CABIN ON TAXI OUT. CREW RETURNED TO GATE. MAINTENANCE INSPECTED AND FOUND CAUSE OF BURNING SMELL TO BE BURNT GROUND WIRE ON BOTTOM OF COFFEEMAKER. MAINTENANCE REMOVED AND REPLACED COFFEEMAKER AND PERFORMED CHECKS USING AIRCRAMay 22, 2012 · N258PS · Cndair CL6002B19 · Equipment/Furnishings WiringSDR VNAA2012020900002Seal · damagedCREW REPORTED RUMBLING NOISE COMING FROM SERVICE DOOR IN FLIGHT. NO CHANGES IN AIRCRAFT PRESSURIZATION OBSERVED. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED SERVICE DOOR SEAL AND PERFORMED CHECKS USING AIRCRAFT MAIFeb 6, 2012 · N258PS · Cndair CL6002B19 · Service DoorsSDR VNAA2011100100004Structure · dentedDURING SCHEDULED MAINTENANCE A DENT WAS FOUND TO AIRCRAFT AT FS 682+4 JUST FORWARD OF THE RAM AIR DUCT. THE AREA WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 2, 2011 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011100100003Structure · corrodedDURING SCHEDULED MAINTENANCE CORROSION WAS FOUND AROUND DRAIN HOLES AND FASTENERS UNDER AFT BELLY FAIRING FROM FS 559 TO FS 559+112. THE AREA WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 2, 2011 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011100100002Skin · dentedDURING SCHEDULED MAINTENANCE A DENT WAS FOUND TO AIRCRAFT SKIN BETWEEN FS 654 TO 672. THE AREA WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 2, 2011 · N258PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2011100100001Floorbeam · 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.Oct 2, 2011 · N258PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2010051800005Pump · leakingCREW REPORTED A HYDRAULIC PUMP 3A AMBER MESSAGE ON APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED ELECTRIC MOTOR DRIVEN (HYDRAULIC) PUMP 3A AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCMay 12, 2010 · N258PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR VNAA2009051500004Shutoff Valve · failedCREW REPORTED A RT PACK OVERPRESSURE AFTER TAKEOFF . THE PRESSURE NEVER WENT BELOW 60 PSI AND WAS AT 94 PSI WHEN FAILED. CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE RT PRESSURE REGULATING SHUTOFF VALVE (PRSOVMay 12, 2009 · N258PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA2009050600002Rivet · damagedCREW REPORTED A LIGHTNING STRIKE IN CLT. MAINTENANCE INSPECTED AND REPLACED RIVETS, RADOME, AND DRAIN MAST. WORK WAS DONE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.May 4, 2009 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2008120400011Sensing Element · shortedON CLIMBOUT FROM PHL CREW RECEIVED AN ANTI ICE WARNING MESSAGE. AIRCRAFT RETURNED TO PHL, LANDING WITHOUT INCIDENT. MAINTENANCE FOUND SENSING ELEMENT A15WK SHORTED TO GROUND. MAINTENANCE REMOVED AND REPLACED ELEMENT AND NO OTHER DEFECTS NOTED. AIRCRAFT WASNov 30, 2008 · N258PS · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR VNAA0809007Radome · delaminatedCREW REPORTED DURING LANDING A BIRD STRIKE TO THE NOSE OF THE ACFT. MX FOUND DELAMINATION ON THE RADOME. THE RADOME WAS R&R. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.Sep 15, 2008 · N258PS · Cndair CL6002B19 · Aerodynamic FairingsSDR VNAA0802005Smoke Detector · failedCREW REPORTED A SMOKE TOILET AMBER MESSAGE ON APPROACH. CREW COULD NOT VISUALLY SEE ANY SMOKE AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND MEL'D THE LAV SMOKE DETECTION SYSTEM PER MEL 26-16-01. MAINTENANCE REMOVED AND REPLACED THE LAVATFeb 11, 2008 · N258PS · Cndair CL6002B19 · Smoke Detection
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