N818EX, cancelled Mar 24, 2005

Service difficulty reports · 30

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 = 'N818EX' AND deregistration_id = 'N818EX-2005-03-24'
  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 PCAA0403178Battery Pack · failedMAINTENANCE CREATED DISCREPANCY DUE TO THE LEFT HAND AFT EGRESS EMERGENCY LIGHT NOT TESTING. IT WAS FOUND THAT THE ASSOCIATED BATTERY PACK WAS FAULTY. PACK WAS REPLACED AND SYSTEM OPERATIONAL CHECK GOOD.Mar 5, 2004 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA0403175Brake Assy · leakingFLIGHT 4014 REPORTED AIRCRAFT VIBRATING WHEN USING RIGHT HAND BRAKE. MAINTENANCE FOUND THE INBOARD RIGHT HAND BRAKE ASSEMBLY LEAKING. THE BRAKE ASSEMBLY WAS REPLACED AND THE SYSTEM OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.Mar 4, 2004 · N818EX · Dhav DHC8102 · Landing Gear Brake SystemSDR PCAA0312149Battery Pack · faultyWHILE AIRCRAFT WAS IN MAINTENANCE IT WAS DISCOVERED DURING TEST THAT SEVERAL OVERHEAD AND OUTSIDE EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE FOUND POSITION 300 POWER SUPPLY WITH GROUND WIRE BROKEN AND ASSOCIATED BATTERY OVERHEATING. BOTH WERE REPLACED BUT PRDec 14, 2003 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA0201016Seat Track · corrodedDURING C-CHECK INSPECTION INBOARD LEFT SEAT RAIL FOUND TO HAVE EXCESSIVE CORROSION AT STATION X208. FORWARD SECTION OF SEAT RAIL WAS SPLICED AT STATION X260 IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-3074, RD8-53-1102, & RD8-53-2295. AIRCRAFT RETURDec 26, 2001 · N818EX · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR PCAA0111146Link · wornDURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK BEARING AND PIN FOUND WORN. REPLACED LOWER LINK BEARING AND PIN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Nov 6, 2001 · N818EX · Dhav DHC8102 · Nose/Tail Landing Gear Strut/AxleSDR PCAA0108097Rivet · missingBGM- DURING FLEET INSPECTION OF NACELLES FOR LOOSE AND MISSING FASTENERS FOUND 4 RIVETS MISSING FROM OUTBOARD RIGHT NACELLE AFT OF FLAP TRACK TRAILING EDGE. MAINTENANCE REPLACED RIVETS ON RIGHT OUTBOARD NACELLE AFT OF FLAP TRACK TRAILING EDGE. AIRCRAFT RETURAug 29, 2001 · N818EX · Dhav DHC8102 · Nacelle/Pylon, Main FrameSDR PCAA0108091Wire · brokenBGM-DURING ROUTINE MAINTENANCE VISIT TWO FORWARD EMERGENCY LIGHTS ON FLOOR WERE FOUND INOPERATIVE. BROKEN WIRES REPAIRED ON TWO FORWARD EMERGENCY LIGHTS. AIRCRAFT RETURNED TO SERVICE.Aug 17, 2001 · N818EX · Dhav DHC8102 · Light System WiringSDR PCAA0107070Terminal · damagedDURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHTS FOUND TO FLICKER WHEN SELECTED ON FROM THE FLIGHT ATTENDANTS PANEL. TERMINAL END REPAIRED AT FLIGHT ATTENDANTS LIGHT SWITCH. AIRCRAFT RETURNED TO SERVICE.Jul 14, 2001 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA0104026Bushing · missingLGA-FLIGHT 3704 CREW REPORTED PASSENGER DOOR WILL NOT OPEN. MAINTENANCE FOUND THREADED BUSHING MISSING ON HANDRAIL ASSEMBLY. INSTALLED INTERIM REPAIR ON DOOR. DOOR OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. CORRECT BUSHING INSTALLED LATER THAT DAY.Apr 5, 2001 · N818EX · Dhav DHC8102 · Passenger/Crew DoorsSDR PCAA0008054Structure · crackedMDT - DURING A FLEET INSPECTION THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME 4, STRINGER 4 ON THE LEFT SIDE. REPAIRS WERE MADE IAW RD8-55-199 AND THE AIRCRAFT WAS RETURNED TO SERVICE.Aug 9, 2000 · N818EX · Dhav DHC8102 · Fuselage Main, StructureSDR PCAA00087054Structure · crackedMDT - DURING A FLEET INSPECTION THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME 4, STRINGER 4, LEFT SIDE. REPAIRS WERE DONE IAW RD8-55-199 AND THE AIRCRAFT WAS RETURNED TO SERVICE.Aug 9, 2000 · N818EX · Dhav DHC8102 · Fuselage Main, StructureSDR PCAA9800790Oil Cooler · failedNR 2 OIL TEMP PEAKED AT 120 DURING CLIMB. GOT AS LOW AS 114 DURING DESCENT. PRECAUTIONARY LANDING MADE AT BDL. LIMITATION EXCEEDED BY 7 MINS AT 115 DEGREES WHILE COMING IN ON APPROACH. REMOVED AND REPLACED OIL COOLER ASSEMBLY. GROUND RAN ENGINE, TEMPERATUOct 18, 1998 · N818EX · Dhav DHC8102 · Engine Oil CoolerSDR PCAA9800753Bulb · failedONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)Mar 15, 1998 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA9800741Light · failedCOCKPIT PORTABLE EMERGENCY LIGHT CAME ON TWICE AND REMAINED ON. CABIN EMERGENCY LIGHTS ARE OFF. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)Mar 4, 1998 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA9800714Bulb · failedFORWARD CABIN EMERGENCY EXIT SIGN HAS ONE INOPERATIVE BULB. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)Feb 8, 1998 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA9700673Engine · failedISP - DURING CLIMB-OUT FROM ISP, TEH NR 1 ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 40 PSI THEN RETURNED TO 60 PSI, ASSOCIATED WITH THE NR 1 ENGINE OIL PRESSURE WARNING LIGHT. A/C RETURNED TO FIELD. MAINTENANCE INSPECTED IAW PWC MANUAL AND FOUND NO DEFECTDec 28, 1997 · N818EX · Dhav DHC8102 · Engine (Turbine/Turboprop)SDR PCAA9700664Oil Press Sw · failedDURING TAKEOFF FROM HTS, THE NR 1 ENGINE OIL PRESSURE LIGHT CAME ON, OIL PRESSURE GAUGE INDICATED NORMAL. A/C ABORTED TAKEOFF. MAINTENANCE T/S SYSTEM AND REPLACED THE NR 1 ENGINE OIL PRESSURE SWITCH, RAN A/C AT POWER, OPERATION CHECK, LEAK CHECK GOOD. PERFODec 21, 1997 · N818EX · Dhav DHC8102 · Engine Oil PressureSDR PCAA9700625Light · brokenLEFT AFT EMERGENCY EXIT, SIDEWALL LIGHT IS BROKE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. A/C RETURNED TO SERVICE. (M)Nov 29, 1997 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA9700610Oil System · req'd serviceUPON TAKEOFF FROM ROC, THE NR 1 ENGINE OIL PRESSURE DROPPED 25 PSI. THE CREW SECURED THE ENGINE IAW PROCEDURES AND RETURNED TO FIELD. MAINTENANCE INSPECTED THE NR 1 ENGINE IAW PWC MM 05-50. NO DEBRIS OR DEFECTS NOTED. SERVICED THE ENGINE WITH 3 QUARTS OF ONov 12, 1997 · N818EX · Dhav DHC8102 · Turbine Engine Oil SystemSDR PCAA9700594Valve · failedAFTER TAKEOFF FROM SYR, NR 1 ENGINE OIL TEMP WENT TO 120 DEGREES 10 MINUTES INTO FLIGHT AND REMAINED STEADY UNTIL ENGINE WAS BROUGHT BACK TO FLIGHT IDLE. A/C DIVERTED INTO BGM, AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT AND FOUND THE NR 1 ENGINE OIL COOLER Oct 31, 1997 · N818EX · Dhav DHC8102 · Engine Oil Temperature RegulatorSDR PCAA9700593Door · malfunctionedNR 1 ENGINE OIL TEMP WENT TO 120 DEGREES ON TAKEOFF AND REMAINED STEADY. AIRCRAFT RETURNED TO FIELD SYR AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED THE NR 1 ENGINE OIL COOLER DOOR PER CDL. OIL TEMPERATURE REMAINED WITHIN LIMITS AND A/C WAS DISPATCHED UOct 31, 1997 · N818EX · Dhav DHC8102 · Engine Oil Distribution (Airframe Furnished)SDR PCAA9700560Light · inoperativeCOCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)Oct 2, 1997 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA9700511Light · inoperativeCOCKPIT PORTABLE EMERGENCY LIGHT DIM. REMOVED AND REPLACED COCKPIT PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)Aug 9, 1997 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA9700442Battery · looseSEVERAL LAMPS INOPERATIVE IN EMERGENCY FLOOR PATH LIGHTING. FOUND NR 3 BATTERY LOOSE IN CASE. RESECURED BATTERY. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)Jul 7, 1997 · N818EX · Dhav DHC8102 · Emergency LightingSDR PCAA9705001Frame · crackedDURING ROUTINE MAINTENANCE, AFT FUSELAGE NR 4 FRAME FOUND CRACKED AT NR 4 STRINGER. REPAIRED FRAME IAW DHC RD 8-55-199.May 22, 1997 · N818EX · Dhav DHC8102 · Fuselage Main, FrameSDR PCAA9700363Oil System · malfunctionOIL SYSTEM MALFUNCTIONApr 9, 1997 · N818EX · Dhav DHC8102 · Turbine Engine Oil SystemSDR PCAA9700351Hyd Hose Assy · failedAFTER TAKEOFF FROM BWI, NR 2 ENGINE LOST HYDRAULIC CONTENTS. A/C RETURNED TO FIELD. MAINTENANCE INSPECTED AND FOUND A HYDRAULIC HOSE TO THE NOSE GEAR ACTUATOR LEAKING. REMOVED AND REPLACED HOSE ASSEMBLY, ENGINE DRIVEN HYDRAULIC PUMP AND CASE DRAIN FILTER IAFeb 21, 1997 · N818EX · Dhav DHC8102 · Hydraulic System, MainSDR PCAA9600319Windshield · shatteredEN ROUTE FROM LGA TO MHT, CAPTAIN'S WINDSHIELD SHATTERED DURING CRUISE FLIGHT. A/C DIVERTED TO BDL. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD, REPLACED HEAT CONTROLLER AS PRECAUTIONARY MEASURE. WORK PERFORMED IAW DHC MM. A/C RETURNED TO SERVICE. (X)Nov 5, 1996 · N818EX · Dhav DHC8102 · Flight Compartment WindowsSDR PCAA9600304Selector Valve · leakingFLT 3701 - DURING CRUISE NR 2 HYDRAULIC QTY INDICATED ZERO. HYDRAULIC PRESSURE WAS NORMAL. DURING APPROACH GEAR HAD TO BE MANUALLY EXTENDED. INSPECTED AND FOUND LANDING GEAR CONTROL SOLENOID VALVE LEAKING DUE TO TORN PACKING. REPLACED UPPER PACKING. BLED Sep 9, 1996 · N818EX · Dhav DHC8102 · Landing Gear SelectorSDR PCAA9500250Windshield · crackedFIRST OFFICERS WINDSHIELD HAS LARGE CRACK IN IT. AIRCRAFT RETURNED TO FIELD IN BWI. FERRIED TO MDT FOR REPAIR. REMOVED AND REPLACED FLIGHT OFFICERS WINDSHIELD AND HEAT CONTROLLER AS A PRECAUTIONARY MEASURE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SNov 21, 1995 · N818EX · Dhav DHC8102 · Flight Compartment Windows
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