N505MD, cancelled Sep 25, 2013

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 = 'N505MD' AND deregistration_id = 'N505MD-2013-09-25'
  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 ASMF200505009Computer · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING TO AUTO SLAT FAIL AND AUTO SLAT DISAGREE LIGHTS COME ON. SYSTEM WAS RESET AND TESTED BUT FAILURE CONTINUED. STALL WARNING COMPUTER BITE WAS PERFORMED AND DETECTING FAILURE IN THE NUMBER 1. THE May 6, 2005 · N505MD · Doug DC982 · Airspeed/Mach IndicatorSDR ASMF200505001Cooler · failedDURING TRANSIT CHECK, IT WAS DETECTED OIL LEAK IN THE LEFT ENGINE FUEL-OIL COOLER AND THE OIL TANK OVERFILLED WITH FUEL SMELT. FUEL-OIL COOLER OF THE LEFT ENGINE WAS REPLACED IAW MM 79-20-01 AND ENGINE LUBRICATING OIL PROCEDURE WAS PERFORMED IAW MM 72-00-00, May 2, 2005 · N505MD · Doug DC982 · Engine Oil Storage (Airframe Furnished)SDR ASMF200504014Line · damagedCAPTAIN REPORTED THAT DURING FLIGHT LOT HYDRAULIC LIQUID IN THE LEFT SYSTEM WITH HYDRAULIC PRESSURE CORRECT. DURING REVISION WAS DETECTED THE HYDRAULIC TANK LEFT SYSTEM EMPTY, IT WAS RECHARGED. THE LEFT SYSTEM WAS PRESSURIZED AND BRAKE RETURN LINE HAD A LEAKApr 16, 2005 · N505MD · Doug DC982 · BrakeSDR ASMF200409007Link · jammedCAPTAIN REPORTED THAT AFTER TAKEOFF, NOSE LANDING GEAR NOT RETRACTED, LIGHT ON, ABNORMAL PROCEDURE PERFORMED. AIRCRAFT SENT TO THE HANGAR AND NOSE LANDING GEAR OPERATIONAL TEST WAS PERFORMED. NOSE LANDING GEAR LINK WAS JAMMED DURING RETRACTION, THEREFORE NOSSep 19, 2004 · N505MD · Doug DC982 · Landing Gear Retraction/Extension SystemSDR ASMF200408013Compensator · failedCAPTAIN REPORTED DIFFERENCE BETWEEN LT AND RT FUEL INDICATORS. DURING COMPENSATORS TEST WAS DETECTED THAT THE RIGHT TANK HAD 2500 LBS, LT TANK HAD 2600 LBS AND CENTRAL TANK HAD 3000 LBS. FUEL WAS TRANSFERRED FORM PRINCIPAL TANKS TO CENTRAL TANK AND BOTH TANKS Aug 14, 2004 · N505MD · Doug DC982 · Fuel Quantity SensorSDR ASMF200408011Regulator · openCAPTAIN REPORTED THAT AT FL 330 FLOWS LIGHT TURNED ON DUE TO PRESSURIZATION FAILURE PERFORMING AN ABNORMAL AND EMERGENCY PROCEDURE. ANTI-ICE WAS APPLIED TO ENGINES AND WINGS BUT LIGHT CONTINUE AND CABIN ALTITUDE LIGHT TURNED ON, PRESSURIZATION WAS CONTROLLED Aug 12, 2004 · N505MD · Doug DC982 · Pressure Regulator/Outflow ValveSDR ASMF200407030Slide · dislodgedDURING TRANSIT CHECK, CAPTAIN REPORTED THAT FOOD SERVICES COMPANY PERSONNEL FELL DOWN THROUGH LT SERVICE DOOR SLIDE. LT SERVICE DOOR SLIDE WAS REINSTALLED IAW MM 25-62-01. DURING OVERNIGHT SERVICE, LT SERVICE DOOR SLIDE INSTALLATION WAS CHECKED IAW MM 25-62-Jul 25, 2004 · N505MD · Doug DC982 · Escape SlideSDR ASMF200407002Actuator · damagedDURING OVERNIGHT SERVICE, GROUND SPOILER WAS DETECTED OUT OF SERVICE, AUTO SPOILER ACTUATOR WAS REPLACED AND SPOILER TRIMMING WAS PERFORMED AND TESTED AND FAILURE CONTINUE. OPERATIONAL TEST WAS PERFORMED AND BARS WERE ADJUSTED AND BUSHING AND ACTUATOR WERE REJul 1, 2004 · N505MD · Doug DC982 · Drag Control SystemSDR ASMF200406031Lever · defectiveCAPTAIN REPORTED, SPEED BRAKES AND GROUND SPOILERS SYSTEM OUT OF SERVICE DURING FLIGHT. SYSTEM WAS CHECKED AND LEVER WAS DETECTED VERY HARD AND OCCASIONALLY JAMMED. SPOILER MECHANISM WAS CHECKED AND SPOILER ACTUATOR CONNECTOR WAS DISCONNECTED. CONNECTOR WAS REJun 27, 2004 · N505MD · Doug DC982 · Drag Control SystemSDR ASMF200406012Door · unlockedAIRCRAFT RETURNED, ELECTRIC/ELECTRONIC DOOR LIGHT TURNED ON. DURING MAINTENANCE REVISION WAS DETECTED THAT ELECTRIC/ELECTRONIC DOOR WAS NOT LOCKED. DOOR WAS CORRECTLY CLOSED AND LOCKED, ALL CORRECT.Jun 13, 2004 · N505MD · Doug DC982 · Electrical/Electronic Compartment DoorsSDR ASMF200406006Computer · failedAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF FAIL IN LT FLIGHT GUIDANCE SYSTEM INDICATION. SYSTEM WAS REACTIVATED AND ELECTRICAL BUSS TURNED OFF, AUTO TEST IN BOTH SYSTEMS WAS PERFORMED, ALL CORRECT. DURING OVERNIGHT SERVICE, FLIGHT GUIDANCE COMPUTER WAS RJun 7, 2004 · N505MD · Doug DC982 · Autopilot SystemSDR ASMF200405018Buss · looseAIRCRAFT RETURNED TO PLATFORM BECAUSE BUSS WERE LOOSEN. GCU´S WERE CHECKED, ALL CORRECT. FLIGHT DIRECTOR BUSS WAS CHECKED AND IT WAS DETECTED WITH FAIL. DFGC NR 1 WAS RESEATED AND BOTH DFGC´S WERE TESTED IAW MM 22-00-00, CORRECTING THE FAIL.May 15, 2004 · N505MD · Doug DC982 · Navigation System WiringSDR ASMF200403019Skin · dentedCAPTAIN REQUESTED A CHECK FOR DENTS IN RIGHT SIDE OF FUSELAGE NEAR TO THE STATIC PORTS. AIRCRAFT WAS CHECKED BY DENTS IAW SRM 53-04 AND DENTS WERE WITHIN LIMITS.Mar 30, 2004 · N505MD · Doug DC982 · Fuselage Main, Plate/SkinSDR MEX2004066Pump · failedFLT 351 - MEX-ZIH - AIRCRAFT RETURNED TO PLATFORM, DUE TO LOSS OF HYDRAULIC PRESSURE. CAPTAIN REPORTED THAT THE LEFT HYDRAULIC SYSTEM WITH 1100 PSI ON HIGH, LOW AND SHUTOFF POSITION. THE LEFT HYDRAULIC PUMP WAS REPLACED IAW MM 29-00-00, TEST CORRECT. (M)Feb 17, 2004 · N505MD · Doug DC982 · Hydraulic Pump (Electric/Engine), MainSDR MEX2004060Hydraulic System · leakingDURING TRANSIT CHECK, THE LEFT HYDRAULIC SYSTEM WAS EMPTY. DURING REVISION AT THE TAIL AREA IN THE VENTRAL STAIR WAS DETECTED A HYDRAULIC LIQUID LEAK. THE AREA WAS CLEANED AND LEAK WAS REPAIRED. (M)Feb 15, 2004 · N505MD · Doug DC982 · Hydraulic System, MainSDR MEX2004057Sensor · failedFLT 256 - MEX-HMO - DURNIG APPROACH THE RED MAIN LANDING GEAR LIGHT TURNED ON. DURING REVISION IN HANGAR THE MLG SENSOR WAS CALIBRATED IAW MM 32-60-05 AND CHAFING BETWEEN HYDRAULIC LINE AND BRAKE CONNECTOR WAS CORRECTED IAW MM 32-11-02. (M)Feb 14, 2004 · N505MD · Doug DC982 · Landing Gear Position and WarningSDR MEX2003549Adapter · leakingTHE DISPENSER FUEL NOZZLE WAS REMOVED INADEQUATELY AFTER THE FUEL REFILLING SERVICE, THE ADAPTER CHECK VALVE SEAL WAS REMOVED AND A LITTLE FUEL LEAKAGE APPEARED. SUCH SEAL WAS REINSTALLED AND NO LEAKAGES APPEARED AGAIN. THE FUEL FILL ADAPTER WAS REPLACED ANDDec 11, 2003 · N505MD · Doug DC982 · Aircraft Fuel Distribution SystemSDR MEX2003537Sensor · dirtyFLIGHT RETURNED DUE TO THE 'E/E DOOR OPEN' LIGHT TURNED ON AFTER 15 MINUTES. DURING REVISION AT MLM STATION THE DOOR WAS FOUND CLOSED. THE MECHANISM, DOOR AND THE SENSOR WERE CLEANED, TESTS WERE PERFORMED IAW MM 52-30, ALL CORRECT. (M)Nov 27, 2003 · N505MD · Doug DC982 · Door Warning SystemSDR MEX2003442Cooling Turbine · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING, AT FL290 LIGHT FLOW CAME ON AND THE CABIN PRESSURE STARTED TO CLIMB OF 1500 FT/MIN, UNABLE TO CONTROL IT IN MANUAL AND AT 9500 FEET CABIN LIGHT CAME ON AND EMERGENCY DESCENT WAS DONE, PROCEEDING TO LANDING AT DCO. ATSep 22, 2003 · N505MD · Doug DC982 · Cabin Cooling SystemSDR MEX2003367Skin · damagedDURING OVERNIGHT CHECK WAS DETECTED LIGHTNING IMPACT AT FUSELAGE LEFT SIDE. LIGHTNING INSPECTION WAS DETECTING DAMAGES AT STATION Y332 AND LONGERON 15 WITH EIGHT RIVETS DAMAGED. THE FOLLOWING PARTS WERE REPLACED IAW. 2 FASTENERS AT FORWARD ENTRANCE LT DOOR Aug 14, 2003 · N505MD · Doug DC982 · Fuselage Main, Plate/SkinSDR MEX2003270Control Unit · failedDURING PREFLIGHT TRANSIT CHECK WAS DETECTED THE ENGINE FIRE ALARM SYSTEM DID NOT CANCEL AURAL WARNING. DURING REVISION RIGHT ENGINE LOOP B, BREAKER B-1 AND AMPLIFIER A2-6 WERE WITH DAMAGES. THE DUAL CONTROL UNIT WAS REPLACED IAW MM, ALL TESTS CORRECT.Jul 7, 2003 · N505MD · Doug DC982 · Fire DetectionSDR MEX2003190Valve · malfunctionedHMO - FLT 104 - GDL - DURING DESCENT, INDICATION STARTED TO CLIMB AND LOW FLOW LIGHT TURNED ON WITH PRESURIZATION VALVE CLOSED, ENGINE ACCELERATED TO 1.5 EPR AND A/C INDICATED PRESSURE OF 12 PSI. SYSTEM WAS CHECKED FOR LEAKAGES AND BOTH CONTROLLERS PRESSURE TRMay 23, 2003 · N505MD · Doug DC982 · Air Distribution SystemSDR MEX2003060Fuel Control · failedFLT 189 - TIJ-MEX - AIRCRAFT RETURNED TO PLATFORM, OSCILLATION IN ENGINE PARAMETERS. OIL FILTER, OIL MAIN FILTER AND CHIP DETECTOR WERE VERIFIED. N2 WAS ADJUSTED AT LOW LEVEL REMAIN AT 52 PERCENT AND THE REST OF PARAMETERS WERE OK. AN ENGINE VISUAL INSPECTIMar 4, 2003 · N505MD · Doug DC982 · Fuel Control/Turbine EnginesSDR MEX2003049Recorder · inoperativeAIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN DISCONTINUE ENGINE NR 1 STARTING, FOR FIRE DURING STARTING OF ENGINE NR 2, WITH INDICATION AT CABIN. ENGINES WERE INSPECTED AND TESTED IAW MM, ALL CORRECT. IAW MAINTENANCE CONVENIENCE FLIGHT DATA RECORDER WAS REPLFeb 28, 2003 · N505MD · Doug DC982 · Data Recorders (Flight/Maintenance)SDR MEX2002359Pressure Switch · failedFLT 210 - MEX-CUU - AIRCRAFT ABORTED TAKEOFF DUE TO BOTH AIR CONDITIONING PACKAGES SHUTOFF AND FLOW LIGHT TURN ON AT 132 KTS. AIRCRAFT WAS SENT TO THE HANGAR AND BOTH PACKAGES WERE TESTED AT TAKEOFF POWER (2.02), ALL CORRECT. SECOND SEGMENT SWITCHES WERE CHECNov 12, 2002 · N505MD · Doug DC982 · Cabin Cooling SystemSDR MEX2002248Line · damagedON DEPARTURE, CAPTAIN REPORTED THE PRESENCE OF SMOKE IN THE PASSENGER CABIN. THE HYDRAULIC SYSTEM WAS VERIFIED TO BE LEAKING AND THE APU WAS SHUTDOWN DUE TO HYDRAULIC FLUID IN IT, AND THE A/C PACK WAS CONTAMINATED. HYDRAULIC LINE OF THE RT REVERSE FILTER WAJul 30, 2002 · N505MD · Doug DC982 · Hydraulic System, MainSDR MEX2002218Valve · failedFLT 132 - MEX-BJX - WHEN THE ANTI-ICE SYSTEM IS ON, THE LIGHT CABIN FLOW WAS TURNED ON. AT RON MEX 14/15, IT WAS PERFORMED THE ANTI-ICE TEST IN MODE 1 AND 2. THE LEFT AUGMENTATION VALVE WAS REPLACED, TESTS OK IAW MM 21-31-021. (M)Jul 14, 2002 · N505MD · Doug DC982 · Ice DetectionSDR MEX2002168Control Valve · failedFLT 315 - MEX-ACA - CAPTAIN REPORT THAT DURING DESCENT WITH INDICATIONS OF 22 AND 19 IN BOTH AIR CONDITIONING PACKAGES AND WITH ALL VALVES CLOSED THE FLOW LIGHT TURNS ON. AIRCRAFT WAS SENT TO THE HANGAR. AFTER CHECK, THE RIGHT FLOW CONTROL VALVE, THE RIGHT AMay 21, 2002 · N505MD · Doug DC982 · Cabin Cooling SystemSDR ASM2002F00000Computer · failedAIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF LOW ACCELERATION IN ENGINE NUMBER TWO AND THE THROAT EPR NR 2 WAS OUT OF SERVICE. THE EPR TX ASSY NUMBER TWO WAS REPLACED IAW MM.May 18, 2002 · N505MD · Doug DC982 · Engine Pressure Ratio (EPR)SDR MEX2002263Wire · brokenDURING TAXI CAPTAIN INFORMED THAT THE LIGHT OF RUDDER TRAVEL UNRESTRICTED DID NOT TURN ON. PROXIMITY SWITCH WAS VERIFIED AND FOUND A FAILURE IN THE CARD 706. PROXIMITY SWITCH WAS REPLACED BUT FAILURE DID NOT CORRECT. PROXIMITY SENSORS WERE VERIFIED AND SOMEDec 8, 2001 · N505MD · Doug DC982 · Flight Control System Wiring
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