N218PS

Service difficulty reports · 121

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 = 'N218PS' 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 VNAA2019010499907Seat Track · crackedDISCREPANCY: LBL9 AND RBL9 FS 409+128 TO FS 559 FLOOR SEAT TRACK SEGMENTS ARE CORRODED. C/A: REMOVED AND REPLACED SEAT TRACK BY FABBING AND ISTALLING IAW REO 601R-53-00-485 AND AMM 53-01-11-400-802.Jan 4, 2019 · N218PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019010499906Seat Track · crackedDISCREPANCY: LBL9 AND RBL9 FS 559 TO FS 559+80 FLOOR SEAT TRACK SEGMENTS ARE CORRODED. C/A: REMOVED AND REPLACED SEAT TRACK BY FABBING AND ISTALLING IAW REO 601R-53-00-485 AND AMM 53-01-11-400-802.Jan 4, 2019 · N218PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019010499905Bulkhead · crackedFS621 RPB WEB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE "HEEL LINE" AREA OF VERTICAL POST AT LBL36 WL112.5-WL114 100%FSH. FAILED NDT UT INSP. C/A: COMPLIED WITH REO 601R-53-61-6815.Jan 4, 2019 · N218PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2019010499904Bulkhead · crackedFS621 RPB WEB HAS 7EA AREAS OF CRACK INDICATIONS NOTED IN THE "HEEL LINE" AREA OF VERTICAL POSTS. AREA NR 1 - RBL27 WL128-WL132.5 70% FSH ET, NR 2 - RBL27 WL84-WL102 70% FSH ET, NR 3 - RBL9 WL105-WL114 50% FSH ET, NR 4 - LBL9 WL106-WL107.5 50% FSH ET, NR 5 - LJan 4, 2019 · N218PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2019010499903Floorbeam · corrodedRBL 9 FLOORBEAM IS CORRODED FROM FS 559+48 TO FS 559+80. C/A: REPAIRED IAW REO 601R-53-00-27.Jan 4, 2019 · N218PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2019010499902Seat Track · corrodedLBL 9 AND RBL 9 FS 399 TO FS 409+128 FLOOR SEAT TRACK SEGMENTS ARE CORRODED. C/A: INSTALLED LBL9 & RBL9 FS399 TO FS409+128 FLOOR SEAT TRACK SEGMENTS IAW AMM 53-01-11-400-802 P/N:N126-2075.Jan 4, 2019 · N218PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019010499901Seat Track · corrodedLB 9 AND RBL 9 FS 364 TO FS 399 FLOOR SEAT TRACK SEGMENTS ARE CORRODED. C/A: INSTALLED LBL9 AND RBL FS364 TO FS399 FLOOR SEAT TRACK SEGMENTS IAW AMM 53-01-11-400-802 P/N: N126-2075Jan 4, 2019 · N218PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017090411101Warning Message · illuminatedCREW REPORTED THAT SHORTLY AFTER TAKEOFF WHEN TRANSFERRING BLEED AIR FROM THE APU TO THE ENGINE BLEEDS RECEIVING A RT AND LT PACK HIGH PRESSURE MESSAGE. THE CREW DECLARED AN EMERGENCY. RAN THE QRH AND THE MESSAGE DID NOT DISAPPEAR. TRANSFERRED THE BLEEDS BACKSep 4, 2017 · N218PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA2017021200018Pressure Blkhd · crackedPERFORMED A MAJOR REPAIR TO THE FS 621.0 REAR PRESSURE BULKHEAD WEB AT LBL 27.50 WL 112.Feb 12, 2017 · N218PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017021200017Pressure Blkhd · crackedPERFORMED A MAJOR REPAIR TO THE FS 621.0 REAR PRESSURE BULKHEAD WEB AT BL 0.00 WL 113 AND WL 135, RBL 27.5 WL 114 AND RBL 18.00 WL 112 AND WL 134.Feb 12, 2017 · N218PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017020500009Angle · corrodedPASSENGER DOOR CUTOUT LOWER SILL ANGLE HAS SURFACE CORROSION BETWEEN FS 310.00 AND FS 349.00. REMOVED AND REPLACED PASSENGER DOOR LOWER SILL ANGLE BETWEEN FS 310.00 AND FS 349.00.Feb 5, 2017 · N218PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2016071200014Position Sensor · warning messageFLAPS FAIL CAUTION MESSAGE AT ZERO DEGREES ON APPROACH. THE CREW DECLARED AN EMERGENCY, CONTINUE TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACE THE LEFT HAND BRAKE AND POSITION SENSOR UNIT, AND PERFORMED CHECKS IAW THEJul 12, 2016 · N218PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2016062600029Unknown · smokeSLIGHT BURNING ODOR APPEARS TO BE COMING FROM AIR VENTS. MAINTENANCE DEFERRED LT PACK THEN OPS CHECK LT PACK AND CLEARED THE MEL. THE ACFT WAS RELEASED FOR SERVICE.Jun 26, 2016 · N218PS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2016022000026Trim Switch · failedCREW REPORTED RECEIVING STABILIZER TRIM CAUTION MESSAGED AND A STABILIZER TRIM RUNAWAY WARNING DURING CLIMBOUT AT FL010. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE PITCH TRIM DISCONNECT SWITCH, AND PERFORMED CHFeb 20, 2016 · N218PS · Cndair CL6002B19 · Autopilot Trim IndicatorSDR VNAA2016012000022Control Unit · failedCREW REPORTED FLAPS FAIL CAUTION MESSAGE ON FLAPS EXTENSION AT 45 DEGREES. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FIM, R & R FLAP ELECTRONIC CONTROL UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jan 20, 2016 · N218PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2016011900020Sensor · failedCREW REPORTED FLAPS FAIL MESSAGE AT 4000 FT AFTER SELECTING FLAPS 8 DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RT BRAKE AND POSITION SENSOR UNIT AND PERFORMED CHECKS IAW THE AMM. ACFT RELEASED FORJan 19, 2016 · N218PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2015121800014Wire · brokenCREW REPORTED EMERGENCY EXIT SIGN BY PASSENGER DOOR INOPERATIVE. MAINTENANCE INSPECTED, REPAIRED BROKEN WIRE ON EMERGENCY LIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Dec 18, 2015 · N218PS · Cndair CL6002B19 · Light System WiringSDR VNAA2015070700003Door Sill · corrodedBS 319 - 349 SERVICE DOOR LOWER SILL ANGLE HAS CORROSION. R & R SERVICE DOOR SILL ANGLE IAW SRM.Jul 7, 2015 · N218PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2015070700002Retainer · corrodedMAIN AVIONICS BAY DOOR IS CORRODED UNDER DOOR SEAL, ENTIRE CIRCUMFERENCE HAS FILIFORM CORROSION. R & R SEAL RETAINER IAW SRM.Jul 7, 2015 · N218PS · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR VNAA2015070700001Frame · corrodedFRAME AT FS 605 HAS CORROSION BETWEEN STR 27 AND STR 26L. REMOVED CORRODED FRAME AND INSTALLED A SERVICABLE FRAME.Jul 7, 2015 · N218PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2015062900034Floor Support · corrodedRIGHT FLOOR SUPPORT BETWEEN BS 559+96 AND 621 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW REO.Jun 29, 2015 · N218PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2015062900033Frame Splice · corrodedFORWARD SIDE OF BS 621 FRAME SPLICE AT STR 27 HAS PITTING CORROSION AND PROTECTIVE COATINGS ARE DETERIORATED BETWEEN STR 25L AND STR 26R AT FS 621. REMOVED MINOR CORROSION ON FORWARD SIDE OF FS 621 FRAME SPLICE AT STRINGER 27 AND APPLIED PROTECTIVE COATING BETJun 29, 2015 · N218PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2015030800013Switch · failedCREW REPORTED RECEIVING REV ICON ON RT ENGINE IN FLIGHT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. AN INTERMITTENT RT REVERSER UNLOCKED CAUTION MESSAGE ALSO RECEIVED DURING CLIMB. CREW RETUNED TO FIELD AND LANDED WITHOUT INCIDENT. INSPECTED THRUST REVERSERMar 8, 2015 · N218PS · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2015020900006Shutoff Valve · out of positionCREW REPORTED CABIN NOT PRESSURIZING DURING CLIMBOUT. LEVELED AT 10,000 FT AND CABIN WAS AT 8,000 FT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND OVERBOARD EXHAUST SHUTOFF VALVE, SOV, IN OPEN POSITION. MAINTENANCE SELFeb 9, 2015 · N218PS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2014111700009Anti-Ice Valve · failedCREW REPORTED LT COWL ANTI-ICE MESSAGE IN FLIGHT WITH SWITCH OFF. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT COWL ANTI-ICE VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Nov 17, 2014 · N218PS · Cndair CL6002B19 · Engine Anti-Icing SystemSDR VNAA2013041700010Carbon Seal · leakingCREW REPORTED SMOKE TOILET CAUTION MESSAGE DURING CRUISE. FLIGHT ATTENDANT CONFIRMED LAVATORY SMOKE ALARM SOUNDED. SMOKE WAS VISIBLE FROM ROW SIX (6) THROUGH 11. SMOKE TOILET QRH (QUICK REFERENCE HANDBOOK) WAS PERFORMED AND SMOKE DISSIPATED SHORTLY THEREAFTEApr 17, 2013 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2013041600008Carbon Seal · leakingCREW REPORTED SMOKE TOILET CAS MESSAGE CAME ON DURING DESCENT. PASSENGER NEAR LAV REPORTED ELECTRIC BURNING SMELL. CREW RAN QRH (QUICK REFERENCE HANDBOOK) AND LANDED SAFELY. MAINTENANCE INSPECTED LAV AND CABIN AREA, GROUND RAN AIRCRAFT WITH CREW AND RAN AIR Apr 16, 2013 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2013041000005Heat Exchanger · failedCREW REPORTED RUNAWAY PACK HIGH TEMP FOLLOWED BY SMOKE TOILET CAUTION MESSAGE DURING TAXI OUT. CREW RETURNED TO GATE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT HEAT EXCHANGER AND RIGHT COALESCER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAApr 10, 2013 · N218PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA2013040800003Light · inoperativeCREW REPORTED EMERGENCY CEILING FLOODLIGHT AT ROW TWO (2) INOPERATIVE. MAINTENANCE INSPECTED, RELAMPED EMERGENCY CEILING FLOODLIGHT AT ROW TWO (2) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.Apr 8, 2013 · N218PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2013032300019Unknown · malfunctionedCREW RECEIVED SMOKE TOILET MESSAGE WITH VISIBLE SMOKE IN CABIN AT FL210 IN DESCENT. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE FOLLOWING: PSU PCB (PASSENGER SERVICE UNIT PRINTED CIRCUIT BOARD) ON ROW 11 D/F (BURNTMar 23, 2013 · N218PS · Cndair CL6002B19 · Passenger Compartment LightingSDR VNAA2013030100002Light · smokeCREW REPORTED A SMOKE TOILET MESSAGE WITH SMOKE IN CABIN. MAINTENANCE TROUBLESHOT, DETERMINED THE LIGHT UNIT CAUSED SMOKE, SECURED, AND DEFERED THE LAVATORY LIGHT UNIT. PARTS ARE ON ORDER. SUPPLEMENTAL SDR WILL BE SUBMITTED WHEN REPAIRED. AIRCRAFT WAS RELEMar 1, 2013 · N218PS · Cndair CL6002B19 · Lighting SystemSDR VNAA2013022200011Carbon Seal · damagedCREW REPORTED LEFT ENGINE OIL PRESSURE CAS MESSAGE IN FLIGHT. LEFT ENGINE AT IDLE FOR REMAINDER OF FLIGHT AND OIL PRESSURE FLUCTUATING. CREW DECLARED EMERGENCY AND LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LEFT ENGINE, REMOVED AND REPLFeb 22, 2013 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2013013000012Unknown · hazeCREW REPORTED TOILET SMOKE CAUTION MESSAGE AND HAZE IN CABIN IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LAV WASTE COMPARTMENT AND PERFORMED CHECKS ON LAV SMOKE DETECTOR, AIR CONDITIONING SYSTEM AND CABIN LIGHTS USING AIRCRAFTJan 30, 2013 · N218PS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2012120300003Carbon Seal · leakingCREW REPORTED SMOKE TOILET AMBER MESSAGE IN FLIGHT. CREW FOLLOWED QRH. MESSAGE EXTINGUISHED PRIOR TO LANDING. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT ENGINE NUMBER ONE CARBON SEAL AND PERFORMED CHECKS USING AIRCRAFDec 3, 2012 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2012090500004Carbon Seal · leakingCREW REPORTED SMOKE / TOILET CAS MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED NUMBER 1 AND NUMBER 3 CARBON SEALS FOR RIGHT ENGINE (DUE TO LEAKING) AND PERFORMED CHECKS USING AIRCRAFT AND ENSep 5, 2012 · N218PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2012090400019Motor · malfunctionedCREW REPORTED LAVATORY SMOKE DETECTOR MESSAGE WITH SMOKE VISABLE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LAVATORY WASTE MOTOR ASSEMBLY USING THE AIRCRAFT MANUALS. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT Aug 29, 2012 · N218PS · Cndair CL6002B19 · Waste Disposal SystemSDR VNAA2012040800004Probe · failedCREW REPORTED LEFT AND TOTAL FUEL QUANTITY INDICATION WENT TO AMBER DASHES IN CRUISE AND RETURNED ON APPROACH. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FUEL QUANTITY INDICATING SYSTEM, REMOVED AND REPLACED NUMBER SIX (6) LEFT PROBE Apr 8, 2012 · N218PS · Cndair CL6002B19 · Fuel Quantity SensorSDR VNAA2012021500010Cowling · damagedCREW REPORTED HEARING LOUD BANG AND AIRCRAFT YAWED TO LEFT DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND DAMAGE TO LEFT ENGINE LOWER TRANSCOWL AND DENTS IN FUSELAGE. PAINTED LT LOWER TRANSITION CFeb 12, 2012 · N218PS · Cndair CL6002B19 · Engine Cowling SystemSDR VNAA2011082400021Beam · crackedDURING SCHEDULED MAINTENANCE THE TRAVERSE BEAM AT FS 280.0 WAS FOUND CRACKED. THE TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 21, 2011 · N218PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011082400020Bulkhead · damagedDURING SCHEDULED MAINTENANCE DAMAGE WAS FOUND ON PRESSURE BULKHEAD AT FS 621.0. THE PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 21, 2011 · N218PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2011082400019Skin · dentedDURING SCHEDULED MAINTENANCE THE FORWARD FUSELAGE SKIN AT FS 250.0 WAS FOUND DENTED. THE FUSELAGE AT FS 250.0 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 21, 2011 · N218PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2011082400018Skin · dentedDURING SCHEDULED MAINTENANCE THE FORWARD FUSELAGE SKIN AT FS 589.0 WAS FOUND DENTED. THE FUSELAGE AT FS 589.0 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 21, 2011 · N218PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2011082400017Structure · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FASTENER HOLE AT FS 349. THE FASTENER HOLE WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 21, 2011 · N218PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011082400016Skin · dentedDURING SCHEDULED MAINTENANCE THE FORWARD FUSELAGE SKIN AT FS 202.75 WAS FOUND DENTED. THE FUSELAGE AT FS 202.75 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 21, 2011 · N218PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2011082400015Floorbeam · corrodedDURING SCHEDULED MAINTENANCE THE FLOORBEAM AT FS 568.0 WAS FOUND CORRODED. THE FLOORBEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 21, 2011 · N218PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2011082400014Flap · dentedDURING SCHEDULED MAINTENANCE THE LEFT INBOARD FLAP WAS FOUND DENTED. THE LEFT INBOARD FLAP WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 21, 2011 · N218PS · Cndair CL6002B19 · Trailing Edge FlapsSDR VNAA2011062400022Pressure Switch · malfunctionedCREW REPORTED RECEIVING AMBER 3A HYD CAS MESSAGE UPON LIFT-OFF BEFORE GEAR RETRACTION ON DEPARTURE FROM CLT. CREW CYCLED SWITCH, RECOVERED PRESSURE AND CAS MESSAGE WENT AWAY. AFTER CREW CYCLED GEAR UP, GOT RED NOSE GEAR DOOR CAS MESSAGE. CREW RETURNED TO CLJun 20, 2011 · N218PS · Cndair CL6002B19 · Hydraulic Pressure Relief Valve, MainSDR VNAA2011031400007Adc · malfunctionedCREW REPORTED CAPTAIN’S PRIMARY FLIGHT DISPLAY (PFD) LOST ALL AIR DATA UPON GEAR RETRACTION DURING TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NR 1 AIR DATA COMPUTER (ADC) AND PERFORMED CHMar 9, 2011 · N218PS · Cndair CL6002B19 · Air Data ComputerSDR VNAA2011030900005Display · malfunctionedCREW REPORTED MODERATE TO SEVERE TURBULENCE ON APPROACH TO HPN. DURING CLIMB TO DIVERT TO PHL, CAPTAIN’S PRIMARY FLIGHT DISPLAYS BRIEFLY WENT BLANK. CREW LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL TEST OF DISPLAY CONTROL PANEL (DCP )UMar 6, 2011 · N218PS · Cndair CL6002B19 · Central DisplaySDR VNAA2011013100012Pump · low pressureON TAKEOFF FROM HSV, CREW REPORTED LANDING GEAR DISAGREE AND NOSE DOOR OPEN MESSAGES WHEN THE LANDING GEAR HANDLE WAS SELECTED UP. CREW RETURNED TO HSV AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE 3A HYDRAULIC PJan 25, 2011 · N218PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
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