N205AM, cancelled Oct 8, 2010

Service difficulty reports · 36

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 = 'N205AM' AND deregistration_id = 'N205AM-2010-10-08'
  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 ASMF 20081202Control Valve · leakingDURING TRANSIT CHECK, A HYD LEAK ON THE RT ENG WAS DETECTED. MX TIGHTENED HYDRAULIC LINE AND REPLACED AND TESTED THE RT ENG REVERSE CONTROL VALVE IAW AMM 78-31-04, ALL CORRECT.Dec 19, 2008 · N205AM · Doug DC987 · Engine Exhaust SystemSDR 2008FA0000473Engine · vibrationCAPTAIN REPORTED STRONG VIBRATION IN RT ENGINE WITH EPR`S BETWEEN 1.7 AND 1.75. TECHS VERIFIED THE RT ENGINE CONDITION AND PERFORMED OPERATIONAL TEST IAW AMM 71-00-01 FOUND ALL CORRECT. VIBRATION WAS WITHIN LIMITS (0.4 UNITS INDICATED). (K)Jun 19, 2008 · N205AM · Doug DC987 · Engine (Turbine/Turboprop)SDR ASMF200805005Csd · damagedDURING PUSH BACK, CAPTAIN REPORTED THAT AFTER STARTED THE LEFT ENGINE, THE CSD LIGHT TURNED ON AND TEMPERATURE REACHED 150 DEGREES CELSIUS, SO ABNORMAL PROCEDURE WAS ACCOMPLISHED. MAINTENANCE PERSONNEL DETECTED THE LEFT CSD OIL LEVEL IN RED RANGE, SO THE EXCEMay 28, 2008 · N205AM · Doug DC987 · AC Generation SystemSDR ASMF200802006Socket · burnedDURING TRANSIT CHECK, A BURNED ODOR WAS DETECTED IN PASSENGERS CABIN. MAINTENANCE PERSONNEL CHECKED AFFECTED AREA AND A LAMP IN RAW 3 WAS DETECTED OVERHEATED. THE LAMP WAS REPLACED IAW MM 33-21-03 BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND DURIFeb 24, 2008 · N205AM · Doug DC987 · Passenger Compartment LightingSDR ASMF200707014Door · damagedDURING TRANSIT CHECK, AIRCRAFT WAS HIT IN THE FORWARD SERVICE DOOR BY A CATERING SERVICE TRUCK. MAINTENANCE PERSONNEL REPLACED THE DOOR IAW MM 52-41-00, PRESSURIZATION TEST WAS CORRECT.Jul 19, 2007 · N205AM · Doug DC987 · Galley DoorsSDR ASMF200611003Blade · fodDURING TRANSIT CHECK, A LEFT ENGINE BLADE WAS DETECTED DAMAGED WITH 1INCH LENGTH, 0.640 INCH WIDTH IN THE MIDSPAN AND 0.359 INCH DEPTH. THE FIRST STAGE BLADES SET WAS REPLACED IAW MM 72-33-21, PAGE 401 AND ENGINE VIBRATION CHECK WAS PERFORMED IAW MM 72-00-00, Nov 6, 2006 · N205AM · Doug DC987 · Engine (Turbine/Turboprop)SDR ASMF200610013Panel · leakingDURING TRANSIT CHECK, CAPTAIN REPORTED A FUEL LEAK ON THE RT WING. DURING MAINTENANCE CHECK, A LEAK WAS DETECTED IN THE RT WING UPPER PANEL. TWO NUTS WERE REPLACED IAW SRM 51-30-2 AND PANEL WAS SEALED AGAIN, TESTED CORRECT.Oct 30, 2006 · N205AM · Doug DC987 · Wing, Plate/SkinSDR ASMF200610010Wire · brokenAIRCRAFT RETURNED TO PLATFORM, (RUDDER TRAVEL UNRESTRICTED) LIGHT REMAINED OFF. PROXIMITY SWITCH WAS REPLACED AND TESTED, BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND WIRING WAS CHECKED, DETECTING A SENSOR LINE BROKEN. WIRING SENSOR WAS REPAIRED Oct 17, 2006 · N205AM · Doug DC987 · Flight Control System WiringSDR ASMF200609003Wire · shortedCAPTAIN REPORTED THAT DURING LANDING WERE DETECTED SPARKS AND SMOKE, FROM THE ACCESS DOOR SYSTEM BOX ELECTRICAL WIRING (SIMULTANEOUSLY, THE CABIN OF PRESSURE ALARM CAME ON IN THE PASSENGERS CABIN). DURING TRANSIT CHECK, COCKPIT SECURITY DOOR LATCH AND OXYGEN MSep 1, 2006 · N205AM · Doug DC987 · Oxygen System WiringSDR ASMF200609002Wire · damagedCAPTAIN REPORTED THAT DURING LANDING ROLL, SPARKS AND SMOKE CAME APPARENTLY FROM THE ACCESS DOOR SYSTEM BOX (SIMULTANEOUSLY THE CABIN PRESSURE LOST ALARM CAME ON IN THE PASSENGERS CABIN). DURING TRANSIT CHECK, FLIGHT COMPARTMENT DOOR SAFETY CATCH AND OXYGEN MASep 1, 2006 · N205AM · Doug DC987 · Oxygen System WiringSDR ASMF200605009Acm · failedDURING TRANSIT CHECK, LEFT AIR CONDITIONING PACK WAS DETECTED WITH HIGH TEMPERATURE, CABIN SUPPLY TEMPERATURE WAS 40 DEGREES CELSIUS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK THE LEFT TURBINE COOLING WAS REPLACED IAW MM 21-51-01, TESTED CORRMay 19, 2006 · N205AM · Doug DC987 · Cabin Cooling SystemSDR ASMF200512002Shutoff Valve · leakingAIRCRAFT RETURNED TO PLATFORM, DURING TAXING, THE RT PRESSURE AND QUANTITY HYDRAULIC SYSTEM WAS LOST. DURING MAINTENANCE REVISION, THE RUDDER SHUTOFF VALVE WAS LEAKED AND IT WAS REPLACED IAW MM 27-20-08, TESTED CORRECT.Nov 26, 2005 · N205AM · Doug DC987 · Rudder Control SystemSDR ASMF200511008Starter · failedAIRCRAFT RETURNED TO PLATFORM, RT ENGINE DID NOT START. DURING MAINTENANCE REVISION, IT WAS DETECTED THE RT ENGINE WITHOUT TURN IN N2. THE RT ENGINE STARTER WAS REPLACED IAW MM 80-10-01, TESTED CORRECT.Nov 16, 2005 · N205AM · Doug DC987 · Engine StarterSDR ASMF200506011Cylinder · leakingDURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN RIGHT NOSE WHEEL STEERING CYLINDER. AIRCRAFT WAS SENT TO THE HANGAR AND RIGHT NOSE WHEEL STEERING CYLINDER WAS REPLACED IAW MM 32-5202, TESTED CORRECT.Jun 6, 2005 · N205AM · Doug DC987 · Landing Gear Steering SystemSDR ASMF200506007Sensor · dirtyAIRCRAFT RETURNED TO PLATFORM, DURING TAXING AND FLIGHT CONTROL TESTS THE RUDDER TRAVEL UNRESTRICTED LIGHT TURNED OFF. THE D1-33 AND D1-34 TARGET SENSORS WERE CLEANED AND ADJUSTED IAW MM 27-20-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE TARGET SENSORS OFJun 4, 2005 · N205AM · Doug DC987 · Rudder Control SystemSDR ASMF200504007Csd · failedAIRCRAFT ARRIVED WITH DEFERRED REPORT OF RIGHT CSD OIL PRESSURE LOW LIGHT TURNED ON AND BEFORE TO ENGINES STARTED, THE APU OIL TEMPERATURE HIGH LIGHT TURNED ON. ABNORMAL PROCEDURE WAS PERFORMED AND LIGHT CONTINUED ON. AIRCRAFT WAS SENT TO THE HANGAR AND DURINGApr 8, 2005 · N205AM · Doug DC987 · Alternator-Generator DriveSDR ASMF200501004Skin · damagedDURING TRANSIT CHECK WERE DETECTED FUEL PANEL AND SLAT NR 2 DAMAGED. INSPECTION WAS PERFORMED AND DAMAGES WERE DETECTED OUT OF LIMITS, THEREFORE AIRCRAFT WAS SENT TO THE HANGAR. SLAT NR 2 AND FUEL PANEL WERE REPLACED IAW MM 27-80-01 AND 57-30-03, RESPECTIVELJan 7, 2005 · N205AM · Doug DC987 · Leading Edge DevicesSDR ASMF200412013Fuel Control · failedCAPTAIN REPORTED LEFT ENGINE WITH N2 47 PERCENT IN IDLE POSITION. DURING MAINTENANCE REVISION WAS DETECTED LEFT ENGINE WITH N2 52 PERCENT, EPR 1.03; ENGINE STABILIZED AT N2 50 PERCENT, EPR 1.03. WHEN LEFT AIR CONDITIONING SWITCH WAS OPERATED N2 48 PERCENT, EPDec 28, 2004 · N205AM · Doug DC987 · Fuel Controlling SystemSDR ASMF200412001Coupler · brokenDURING ENGINES START, LEFT ENGINE WAS NOT STARTED, START VALVE WAS OPENED MANUALLY AND FAIL CONTINUE. AIRCRAFT RETURNED TO PLATFORM AND DURING MAINTENANCE REVISION, ENGINE START COUPLER WAS DETECTED BROKEN. ENGINE START COUPLER WAS REPLACED IAW MM 72-61-00, Dec 2, 2004 · N205AM · Doug DC987 · Engine CrankingSDR ASMF200411011Sensor · damagedA/C RETURNED, DUE TO "UNSAFE NLG" LIGHT TURNED ON & STRONG NOISE DETECTED. A/C SENT TO HANGAR & NOSE L/G DOORS INSPECT, DOORS TEST & EXTENSION/RETRACTION TEST WERE PERFORMED IAW MM 32-20-00, 32-22-01, 32-30-00, RESPECTIVELY, ALL CORRECT. DURING CLIMB IN NEXTNov 20, 2004 · N205AM · Doug DC987 · Landing Gear Position and WarningSDR ASMF200411006Control Valve · failedCAPTAIN REPORTED THAT DURING TAXING AND TAKE OFF, AIRCRAFT TURNED TO THE RT SIDE. STEERING WAS CHECKED AND WHEELS WERE TURNED .5000 INCH TO THE RT SIDE OF STEERING INDICATOR CENTER. CABLES, PULLEYS, PRESSURE TIRES AND STEERING CONTROL VALVE TRIMMING PIN, WERENov 12, 2004 · N205AM · Doug DC987 · Landing Gear Steering SystemSDR ASMF200407009Servo Valve · leakingDURING TRANSIT CHECK, HYDRAULIC LIQUID LEAK WAS DETECTED ON RT MAIN LANDING GEAR WELL, BOTH SYSTEMS WERE PRESSURIZED, BRAKES AND CONTROL SURFACES WERE ACTUATED AND LEAK WAS DETECTED ON ANTI-SKID RT DOUBLE SERVO VALVE. SERVO VALVE WAS REPLACED IAW MM 32-43-02, Jul 5, 2004 · N205AM · Doug DC987 · Hydraulic System, MainSDR ASMF200407007Extinguisher · activatedDURING TRANSIT CHECK, CAPTAIN REPORTED (EXTINGUISHER AGENT NR 1) LIGHT TURNED ON. FIRE EXTINGUISHER WAS DETECTED ACTIVATED BY HIGH TEMPERATURE IN TAIL CONE AND COMPRESSOR CLAMP WAS LOOSEN. FIRE EXTINGUISHER AND CLAMP WERE REPLACED IAW MM 26-20-00, LEAKS TEST CJul 3, 2004 · N205AM · Doug DC987 · Fire Bottle, FixedSDR ASMF200406033Wire · failedAIRCRAFT RETURNED TO PLATFORM, "LEFT AIR COND SUPPLY TEMP HI" LIGHT TURNED ON. BREAKER B1-251 WAS RESEATED, TEMPERATURE SENSOR AND THERMAL SWITCH WERE DISCONNECTED AND FAIL CONTINUE. ENGINES WERE SHUTDOWN AND LIGHT WAS DEFERRED IAW MEL 21-2. DURING OVERNIGHT SJun 29, 2004 · N205AM · Doug DC987 · Fire Protection System WiringSDR ASMF200406026Extinguisher · activatedDURING TRANSIT CHECK, FIRE EXTINGUISHER NR 2 WAS ACTIVATED WITHOUT APPARENT CAUSE. AIR CONDITIONING SYSTEM WAS CHECKED BY LEAKS AND COOLING TURBINE CLAMP AND DUCT WERE DETECTED LOOSEN. CLAMP AND DUCT WERE ADJUSTED AND FIRE EXTINGUISHER WAS REPLACED IAW MM 26-2Jun 22, 2004 · N205AM · Doug DC987 · Extinguishing SystemSDR ASMF200404020Tire · failedDURING TRANSIT CHECK CAPTAIN REPORTED THAT AIRCRAFT TURNED TO THE LT DURING TAXING AND NOSE LANDING GEAR INDICATOR PIN EXTENDED ALL THE TIME. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THE NOSE LANDING GEAR TIRES WERE REPLACED IAW MM 32-40-0Apr 27, 2004 · N205AM · Doug DC987 · TireSDR MEX2004055Switch · failedFLT 944 - MEX-CUN - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT VER AS A CONSEQUENCE DURING FLIGHT, THE RIGHT OIL STRAINER CLOGGING LIGHT TURNED ON. NO METALLIC BURRS WERE DETECTED DURING MAIN FILTER. LP5 AND LP6 OIL RESTRICTORS WERE CLEANED WITH AIR BUT FAFeb 12, 2004 · N205AM · Doug DC987 · Engine Oil System WiringSDR MEX2004003Proximity Sensor · malfunctionedFLT 6428 - MEX-LAS - CAPTAIN REPORTED THAT DURING FLIGHT CONTROL TEST WITH THE RT RUDDER THE BLUE LIGHT OF 'RUDDER TRAVEL UNRESTRICTED' REMAINED ON. AT HANGAR, THE RUDDER PROXIMITY SENSORS WERE VERIFIED AND IT WAS DETECTED A TROUBLE IN ONE SENSOR TARGET. THEJan 1, 2004 · N205AM · Doug DC987 · Rudder Control SystemSDR MEX2003574Wire Harness · damagedFLT 605 - DFW-MEX - AIRCRAFT RETURNED TO PLATFORM, DURING THE TAXI THE LIGHT OF 'RUDDER TRAVEL UNRESTRICTED' DID NOT COME ON. THE SYSTEM WAS REVISED AND THE WIRE BUNDLE OF THE PROXIMITY SENSOR D1-33 WAS FOUND WITH DAMAGES. THE WIRE BUNDLE WAS REPAIRED IAW MMDec 30, 2003 · N205AM · Doug DC987 · Flight Control System WiringSDR MEX203546Tire · debondedAFTER LANDING WAS LISTED AN STRONG NOISE IN THE MAIN LANDING GEAR. DURING REVISION OF THE MENTIONED AREA WERE FOUND SEVERAL DAMAGES IN THE NEARBY AREA OF THE LEFT MLG CAUSED BY A TREAD SEPARATION. AC WAS CARRIED TO THE HANGAR TO REPAIR THE FOLLOWING AFFECTEDDec 4, 2003 · N205AM · Doug DC987 · TireSDR MEX2003287Tube · cloggedFLT 440 - GDL-MTY - AIRCRAFT RETURN TO PLATFORM, DURING TAXIING THE CLOGGING LIGHT OIL ENGINE NR 2 ON. THE RESTRICTORS LP5 AND LP6 WERE CLEANED, BOTH ENDS LP5 AND LP6 TUBES WERE SERVICED WITH AIR PRESSURE TO REMOVE ANY CONTAMINATION AND THE DIFFERENTIAL PRESSJul 13, 2003 · N205AM · Doug DC987 · Engine Oil Distribution (Airframe Furnished)SDR MEX2003171Csd · failedDURING TAXING, THE CSD TEMPERATURE INDICATES 380 DEGREES ON ENGINE NR 2. THE CSD, AC GENERATOR AND CSD EXCHANGER WERE REPLACED IAW MM 24-10-01. MM 24-10-01 AND MM 24-10-03, RESPECTIVELY, TEST CORRECT.May 11, 2003 · N205AM · Doug DC987 · Alternator-Generator DriveSDR MEX2003020Proximity Switch · failedFLT 486 - MEX-SLC - AIRCRAFT RETURNED, WHEN SLAT RETRACTED, THE LIGHTS SLAT DISAGREE CAME ON AND 280 KTS THE OVERSPEED ALARM WAS ACTIVATED. SPEED WAS REDUCED BELOW 280 AND AFTER 3 MINUTES LIGHT WENT OFF. IAW THE INSTRUCTIONS OF SHIFT FOREMAN AIRCRAFT RETURNEJan 2, 2003 · N205AM · Doug DC987 · Leading Edge Slat Control SystemSDR MEX2002144Hose · leakingFLT 602 - MEX-DFW - AIRCRAFT RETURN TO FLIGHT DUE TO PRESSURIZATION FAILURE FLOW LIGHT ON WITH A 7.5 OF CABIN DIFFERENTIAL PRESSURE AT 10000 FT. HOSE RUBBER LEFT COOLER TURBINE WERE CHANGED IAW MM 21-20-00, TESTS OK. (M)Aug 5, 2002 · N205AM · Doug DC987 · Cabin Pressure Control SystemSDR ASM2002F00006Indicator · inaccurateAIRCRAFT RETURN TO FLIGHT AS A CONSEQUENCE OF 60 DEGREE DIFFERENCE ON LEFT HEADING OR AUXILIARY AHRS, DIFFERENCE COULD NOT BE CORRECTED. AHRS ELECTRICAL CONNECTOR WAS CLEANED AND AHRS NR 1 WAS INTERCHANGED WITH AHRS NR 3, TESTS PERFORMED IAW MM.May 20, 2002 · N205AM · Doug DC987 · Attitude and Direction Data SystemSDR MEX2002084Relay · failedFLT 608 - MEX-DFW - AIRCRAFT RETURNED TO SOUTH POSITION AS CONSEQUENCES OF OVERHEATING OF THE RAT PROBE AND A FAIL FLAG WAS APPEARED. DURING THE CHECKING SYSTEM IT WAS FOUND ALSO THAT THE TAKEOFF ALARM DID NOT WORK. IT WAS DETECTED A TROUBLE WITH THE RELAY RMar 25, 2002 · N205AM · Doug DC987 · Outside Air Temperature Indicator/Sensor
Back to N205AM, cancelled Oct 8, 2010