N945AS

Service difficulty reports not matched to an aircraft · 34

They name N945AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N945AS' AND registry_match IS NULL
  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 WX0600001Unknown · unknownPIA - LAS - CREW REPORTED ON TAKEOFF ROLL AT 100 KNOTS, THE PACKS SHUT DOWN AND THE RIGHT EPR GAUGE WENT TO 1.0. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE RAN AIRCRAFT AT TAKEOFF POWER. EPR SYSTEM OPERATIONALLY CHECKED NORMJan 2, 2006 · N945AS · Doug MD83 · Engine Indicating SystemSDR ASMF200508006Computer · failedAIRCRAFT RETURNED OF FLIGHT, BOTH DFGC OUT OF SERVICE. THE DFGC RTC BITE WERE PERFORMED IAW MM 22-01-05, TESTED CORRECT. THE OVERWEIGHT LANDING CHECK WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. DURING OVERNIGHT CHECK, BOTH DFGC TESTS WERE PERFORMED IAW MM 22-0Aug 15, 2005 · N945AS · Doug MD83 · Autopilot SystemSDR ASMF200506002Anti-Ice Valve · failedAIRCRAFT RETURNED TO PLATFORM, LT STARTER VALVE DID NOT OPEN AND ANTI-ICE BREAKER OF NOSE COWLING POPPED OUT. THE REPORT WAS DEFERRED BY MEL 80-2 AND THE ANTI ICE VALVE WAS REPLACED IAW MM 30-20-01, TESTED CORRECT. DEFERRED REPORT WAS CLOSED.Jun 2, 2005 · N945AS · Doug MD83 · Air Intake Anti/De-Ice SystemSDR ASMF200505024Shutoff Valve · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE, DURING LEFT ENGINE STARTED, THE START VALVE OPEN LIGHT DID NOT TURN OFF. THE CIRCUIT BREAKERS WERE RESEATED, CROSS FEED AND CONNECTORS WERE CHECKED AND FAILURE CONTINUED. THE REPORT WAS DEFERRED IAW MEL 80-1. May 22, 2005 · N945AS · Doug MD83 · Engine Start Valves/ControlsSDR ASMF200503024Apu · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER PUSH BACK, THE RIGHT ENGINE HAD A HOT STARTING PROMOTED BY LOW PRESS FORM THE APU. ENGINES WERE STARTED WITH A GPU AND APU WAS DEFERRED IAW MEL 49-1-2. DURING OVERNIGHT SERVICE, APU WAS TESTED IN BOTH MODMar 31, 2005 · N945AS · Doug MD83 · APU Bleed Air SystemSDR ASMF200410012Shutoff Valve · failedAIRCRAFT RETURNED TO PLATFORM, RT ENGINE SHUTOFF VALVE DID NOT OPEN. SHUTOFF VALVE WAS REPLACED IAW MM 80-10-02, TESTS WERE CORRECT.Oct 17, 2004 · N945AS · Doug MD83 · Engine CrankingSDR ASMF200408002Pump · failedDURING APPROACH, RT HYDRAULIC SYSTEM PRESSURE WAS LESSENED AND ABNORMAL PROCEDURE WAS PERFORMED. AIRCRAFT LANDED WITH LANDING GEAR DOORS DOWN. SYSTEM WAS CHECKED AND NO FAILURE WAS DETECTED, IT WAS PURGED AND 2 QUARTS WERE ADDED, QUANTITY AND PRESSURE TRANSMITAug 2, 2004 · N945AS · Doug MD83 · Hydraulic Handpump, MainSDR ASMF200407011Transceiver · damagedCAPTAIN REPORTED LIGHTING STRIKE AND RADAR DISPLAY FAILED. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00, ALL CORRECT, BUT RADAR ANTENNA WAS INOPERATIVE. ANTENNA AND RADAR TRANSCEIVER WERE REPLACED IAW MM 31-41-01 AND 34-41-02, TESTS CORRECT.Jul 7, 2004 · N945AS · Doug MD83 · Weather Radar SystemSDR ASMF200407004Solenoid Valve · failedAIRCRAFT RETURNED TO PLATFORM, DIFFERENCE BETWEEN ENGINES PARAMETERS. LT FCU SOLENOID WAS REPLACED IAW MM 73-20-05 AND TEST IAW MM 73-20-01, ALL CORRECT. DURING ENGINE NR 1 START FAIL CONTINUED, AIR/GROUND SENSOR R2-308 WAS REPLACED, TEST CORRECT. FLIGHT WAS CJul 3, 2004 · N945AS · Doug MD83 · Fuel Controlling SystemSDR ASMF200406021Pin · installedAIRCRAFT RETURNED OF FLIGHT, MAIN LANDING GEAR UNLOCK INDICATION AND STRONG VIBRATION. DURING MAINTENANCE REVISION, RT AND LT LOCK PINS WERE DETECTED INSTALLED IN MAIN LANDING GEAR. LOCK PINS WERE REMOVED AND MAIN LANDING GEAR AND OVERWEIGHT INSPECTION WERE PJun 21, 2004 · N945AS · Doug MD83 · Landing Gear Retraction/Extension SystemSDR ASMF200406018Pump · failedAIRCRAFT RETURNED TO PLATFORM, LT ENGINE LOW POWER. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE FUEL PUMP AND FUEL CONTROL UNIT WERE REPLACED IAW MM 73-12-01 AND 73-20-01, RESPECTIVELY, TEST WAS PERFORMED IAW MPCM 71-00-01, ALL CORRECT.Jun 18, 2004 · N945AS · Doug MD83 · Engine Fuel PumpSDR ASMF200405013Pitot Tube · fodAIRCRAFT RETURNED OF FLIGHT, FLIGHT INSTRUMENTS WITH DAMAGE. DURING MAINTENANCE REVISION A FOD WAS DETECTED ON RIGHT PITOT TUBE AS CONSEQUENCE OF BIRD STRIKE. PITOT TUBE WAS CLEANED AND BRAKES WERE COOLED IAW MM 31-00-01.May 8, 2004 · N945AS · Doug MD83 · Instrument PanelSDR ASMF200403016Fcu · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE DID NOT ACCELERATE. PARAMETERS WERE CHECKED AND WERE NORMAL IAW MM 71-00-01. ENGINE WAS SHUTOFF AND PURGE VALVES WERE CHECKED IAW MM 75-31-01. RIGHT FUEL CONTROL UNIT WAS REPLACED IAW MM 73-20-0Mar 25, 2004 · N945AS · Doug MD83 · Fuel Controlling SystemSDR ASMF200403010Strainer · cloggedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF L OIL STRAINER CLOGGING LIGHT TURNED ON AFTER ENGINE START. MAIN OIL FILTER AND SWITCH OIL FILTER WERE REPLACED, IN ACCORDANCE WITH MM 79-20-00 AND 79-30-00, ALL CORRECT.Mar 17, 2004 · N945AS · Doug MD83 · Engine Oil Distribution (Airframe Furnished)SDR MEX2003573Throttle · lack of lubeAIRCRAFT RETURNED TO PLATFORM, DUE TO SLOW ACCELERATION IN THE RIGHT ENGINE. THE WATER SUMP WAS DRAINED AND THE THROTTLE CHAMBER WAS LUBRICATED IAW MM 73-20-03. AT OVERNIGHT SERVICE IN MEX, PERFORMED A TRIM TO BOTH ENGINES AND AN ACCELERTION TEST IAW MM 71-0Dec 30, 2003 · N945AS · Doug MD83 · Power LeverSDR MEX2003506Actuator · failedAIRCRAFT RETURNED TO PLATFORM DURING TAXING, WHEN SLATS WERE EXTENDED AUTO SLAT FAIL LIGHT TURNED ON. SYSTEM WAS CHECKED WITH OTHER COMPUTERS, CONFIRMING THE FAIL IN BOTH AUTO-SLAT ACTUATORS. ACTUATORS WERE REPLACED IAW MM27-80-08, TEST CORRECT. FURTHER. WOct 28, 2003 · N945AS · Doug MD83 · Leading Edge Slat Control SystemSDR ASM2003F00004Actuator · failedAIRCRAFT RETURNED TO PLATFORM DURING TAXI, WHEN SLATS WERE EXTENDED AUTO SLAT FAIL LIGHT TURNED ON. SYSTEM WAS CHECKED WITH OTHER COMPUTERS, CONFIRMING THE FAIL IN BOTH AUTO SLAT ACTUATORS. ACTUATORS WERE REPLACED IAW MM 27-80-08 TESTS CORRECT. FURTHER, THEOct 28, 2003 · N945AS · Doug MD83 · Leading Edge Slat ActuatorSDR MEX2003505Valve · failedCAPTAIN REPORTED THAT DURING AIR FOIL ICE PROTECT WAS TURNED ON, THERE WAS A PRESSURIZATION LEAK WITH FLOW LIGHT ON AND CLIMB RATE BETWEEN 500 AND 800 FPM. TO ATTEND THE FAIL, THE TECH PERSONNEL REPLACED THE PNEUMATIC AUGMENTATION VALVE, PRESSURE REGULATOR VAOct 27, 2003 · N945AS · Doug MD83 · Ice/Rain Protection SystemSDR MEX2003194Valve · failedDURING TRANSIT CHECK, DETECTED HYDRAULIC LEAK AT RIGHT MLG, HYDRAULIC TEST WAS ACCOMPLISHED DETECTING LEAK AT SHUTOFF AND SPOILER DEPRESSURIZATION VALVE. VALVE WAS REPLACED IAW MM 29-10-26, ALL TESTS CORRECT. (M)May 28, 2003 · N945AS · Doug MD83 · Hydraulic System, MainSDR MEX2003052Switch · out of positionAIRCRAFT RETURNED TO PLATFORM DUE TO ROTATION TAIL CONE LIGHT ILLUMINATED. DURING CHECK WAS DETECTED SWITCH OUT OF ITS POSITION. MECHANISM WAS CHECKED AND TAIL CONE LIGHT TURNED OFF. TEST WAS PERFORMED IAW MM. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAMar 1, 2003 · N945AS · Doug MD83 · Central WarningSDR MEX2003035Gcu · failedFLT 198 - MLM-TIJ - AIRCRAFT RETURNED TO GATE, FAIL LIGHT AC/CROSSTIE LOCK-OUT OFF RESET PROCEDURE WS PERFORMED AND LIGHT WAS TURN OFF, BUT LIGHT L GEN OFF APPEARS. GCU WAS NOT POSSIBLE RESET AND ENGINES WERE SHUTDOWN. REPORT WAS DEFERRED UNDER MEL 24-1-1 ANFeb 13, 2003 · N945AS · Doug MD83 · AC Generation SystemSDR MEX2002258Computer · failedAIRCRAFT RETURNED TO PLATFORM AS DUE TO AUTO SLAT FAIL LIGHT ON, BOTH STALL WARNING COMPUTERS WERE FOUND WITH FAILURES, PROXIMITY SWITCH AND "C" AND "D" SENSORS WERE TESTED AND FAIL CONTINUE. EXCESSIVE GREASE WAS DETECTED IN OUTBOARD SLATS ACTUATORS. ACTUATOJul 8, 2002 · N945AS · Doug MD83 · Stall Warning SystemSDR MEX2002101Control Valve · failedFLT 583 - MEX-CUN - WHEN THE AIRCRAFT GETS PLATFORM BY ITSELF THE RIGHT GYRO WAS EXCEEDED AND THE ACTUATORS WERE STUCK. AIRCRAFT WAS SENT TO THE HANGAR AND THE STEERING CONTROL VALVE WAS CHANGED IAW MM 32-52-01. (M)Apr 7, 2002 · N945AS · Doug MD83 · Landing Gear Steering SystemSDR MEX2002044Hydraulic Line · leakingFLT 448 - BJX-LAX - DURING RAMP INSPECTION IT WAS DETECTED AN HYDRAULIC LEAK IN THE RIGHT MLG COMPARTMENT. A PRESSURE LINE OF THE BRAKE MANIFOLD AND MANIFOLD SEAL CAP WAS REPLACED IAW MM 32-42-03, IPC ITEM 102, TEST OK. 5 QUARTS OF HYDRAULIC FLUID WERE NEEDEFeb 16, 2002 · N945AS · Doug MD83 · Hydraulic System, MainSDR ASAA9780054Splice · disconnectedSEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM THE CLASS DIVIDER TO ROW WERE FOUND INOPERATIVE. REPLACED SPLICE AT THE CLASS DIVIDER AND LIGHTS OPERATED NORMALLY. (M)Mar 31, 1997 · N945AS · Doug DC983 · Emergency LightingSDR ASAA9680264Terminal · looseSEA - DURING MAINTENANCE CHECK, THE OVERHEAD TAILCONE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. SECURED LOOSE TERMINAL ON LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)Nov 28, 1996 · N945AS · Doug DC983 · Emergency LightingSDR ASAA9680215Battery Pack · dischargedPDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)Oct 2, 1996 · N945AS · Doug DC983 · Emergency LightingSDR ASAA9680134Batteries · dischargedPDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (X)Jun 9, 1996 · N945AS · Doug DC983 · Emergency LightingSDR ASAA9680061Seal · excess sealantSEA - AFTER ARRIVAL OF FLT NR 367, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. TRIMMED EXCESS SEALANT FROM UPPER DOOR SEAL AREA AND OPERATED NORMALLY. (M)Feb 25, 1996 · N945AS · Doug DC983 · Passenger/Crew DoorsSDR ASAA9580297Battery · dischargedSEA - DURING MAINTENANCE CHECK, THE AFT TWO OVERHEAD EMERGENCY EXIT LIGHTS AND ONE OF THE EMERGENCY TAIL CONE LIGHTS WERE FOUND INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERY AND LIGHTS OPERATED NORMALLY. (M)Dec 26, 1995 · N945AS · Doug DC983 · Emergency LightingSDR ASAA9580268Battery · dischargedSEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 18 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X)Nov 10, 1995 · N945AS · Doug DC983 · Emergency LightingSDR ASAA9580164Eel Assy · defectiveLAX - DURING MAINTENANCE CHECK, THE L-1 PORTABLE EMERGENCY EXIT LIGHT WAS FOUND DIM. REPLACED LIGHT ASSY AND OPERATED NORMALLY. (M)Jul 20, 1995 · N945AS · Doug DC983 · Emergency LightingSDR ASAA9580116Bayonets · out of adjustANC - PRIOR TO DEPARTURE OF FLIGHT 196, CREW REPORTED L1 DOOR JAMMED IN PARTLY OPEN POSITION WHILE ATTEMPTING TO CLOSE DOOR FOR DEPARTURE. OPENED AND INSPECTED L1 DOOR, RELEASED STUCK BAYONETS AND DOOR OPERATED NORMALLY. (M)May 19, 1995 · N945AS · Doug DC983 · Passenger/Crew DoorsSDR ASAA9580097Tether · detachedSEA - DURING LIFE RAFT DEMONSTRATION INFLATION, THE SURVIVAL EQUIPMENT PACKAGE BECAME DETACHED FROM THE RAFT WHEN THE TETHER SECURING THE EQUIPMENT PACKAGE TO THE RAFT STITCHING FAILED AT THE ATTACHMENT TO THE EQUIPMENT PACKAGE. THE RAFT WAS RETURNED TO THE MApr 20, 1995 · N945AS · Doug DC983 · Life Raft
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