N806AM

Service difficulty reports not matched to an aircraft · 25

They name N806AM, 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 = 'N806AM' 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 ASMF200604009Slide · unwanted deployAT PLATFORM, GROUND PERSONNEL DEPLOYED THE R1 DOOR RAFT-SLIDE. DURING REVIEW, IT WAS DETECTED THE BAR IN ARMED POSITION. THE RAFT-SLIDE AND POWER RESERVOIR WERE REPLACED IAW MM 25-66-01 AND 52-11-33, TESTED CORRECT.Apr 16, 2006 · N806AM · Boeing 7572Q8 · Escape SlideSDR ASMF200601008Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF OIL LOW PRESSURE AND HIGH EGT INDICATIONS DURING THE LEFT ENGINE STARTING. AT PLATFORM, THE TECHNICAL PERSONNEL PERFORMED AN ENGINE STARTING TEST IAW MM 71-00-04, ALL CORRECT. DURING OVERNIGHT SERVICE, THE LEFTJan 14, 2006 · N806AM · Boeing 7572Q8 · Engine Oil QuantitySDR ASMF200512004Engine · flamed outAC PERFORMED AN UNSCHEDULED LANDING, FWD AND AFT FUEL PUMP LIGHTS TURNED ON AND RT ENGINE FLAMED OUT ON FLIGHT AND DURING LANDING THE TIRES POSITION 4 AND 8 WAS FLATTED. THE TIRES POSITION 3, 4, 7 AND 8 WERE REPLACED IAW MM 32-45-01 PAGE 401. DURING MAINTENANCNov 28, 2005 · N806AM · Boeing 7572Q8 · Engine (Turbine/Turboprop)SDR ASMF200512003Engine · noneAIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE LT ENGINE WAS SHUTOFF WITH 420 OF EGT. DURING MAINTENANCE REVISION, THE LT ENGINE PARAMETERS WAS VERIFIED FINDING WITHIN LIMITS IAW MM 71-00-00. THE LT ENGINE WAS STARTED AND THE OPERATIONAL TEST WAS PERFORMED INov 28, 2005 · N806AM · Boeing 7572Q8 · Engine (Turbine/Turboprop)SDR ASMF200511003Pressure Switch · failedAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF EICAS MESSAGE -L ENG FUEL FILT- WAS SHOWN. THE FUEL PUMP FILTER AND DEFERENTIAL PRESSURE SWITCH WERE REPLACED IAW MM 73-11-02 AND MM 73-34-014 RESPECTIVELY, TESTED CORRECT.Nov 4, 2005 · N806AM · Boeing 7572Q8 · Engine Fuel/Oil CoolerSDR ASMF200509006Eec · failedCAPTAIN REPORTED RT ENGINE EGT INDICATION WITH OSCILLATIONS OF 100 GRADES IN EICAS. THE RT EEC EBG AND THERMOCOUPLE HARNESS JUNCTION BOX WERE REPLACED IAW MM 73-21-04 AND 77-51-12, RT ENGINE WAS TESTED IAW MM 71-00-01, ALL CORRECT.Sep 13, 2005 · N806AM · Boeing 7572Q8 · Fuel Controlling SystemSDR ASMF200507013Window · openAIRCRAFT REJECTED TAKEOFF AT 90 KTS AS A CONSEQUENCE OF LT WINDSHIELD OPENED WITHOUT APPARENT REASON. WINDSHIELD ADJUSTMENT CHECKED IAW MM56-11-01, TESTED CORRECT. REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-51-14, ALL CORRECT.Jul 17, 2005 · N806AM · Boeing 7572Q8 · Flight Compartment WindowsSDR ASMF200503020Inlet Guide Vane · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CAPTAIN REPORTED APU PNEUMATIC PRESSURE DOWN TO 8 PSI WHEN LEFT ENGINE STARTED INSULATION VALVE WAS OPENED. ENGINES WERE STARTED WITH A GPU AND REPORT WAS DEFERRED IAW MEL 49-11-01. DURING OVERNIGHT SERVICE, Mar 27, 2005 · N806AM · Boeing 7572Q8 · Engine Air Intake SystemSDR ASMF200503014Control Valve · failedAIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTED WITH CROSSED FEEDING, EICAS MESSAGES R HYD R SUR PRESS, R ENG REV CONE, L ENG REV CONE, L ENG FIRE LOOP 2, EPR DET LOOP 2 INCHES AND (RT ENGINE EPR OUT OF SERVICE) WERE SHOWN AND PNEUMATIC AUXILIARY POWER UNIMar 14, 2005 · N806AM · Boeing 7572Q8 · Engine (Turbine/Turboprop)SDR ASMF200501006Valve · leakingDURING FUEL SERVICE WAS DETECTED HIGH SUPPLY PRESSURE ON FUEL DISPENSER (80 PSI), PROMOTING FUEL LEAK ON RT CENTRAL TANK VALVE. AIRCRAFT WAS FUELED THROUGH LT VALVE AND RT VALVE WAS DEFERRED IAW MEL 28-21-1. DURING OVERNIGHT SERVICE RT FUEL VALVE WAS REPLACED Jan 12, 2005 · N806AM · Boeing 7572Q8 · Aircraft Fuel Distribution SystemSDR ASMF200412003Shutoff Valve · failedCAPTAIN REPORTED THAT WHEN LEFT THRUST LEVER WAS LOCATED IN IDLE POSITION THE AIR-CONDITIONING PACK WAS SHUTDOWN AND "HI STAGE" LIGHT TURNED ON. DUAL VALVE WAS REPLACED IAW MM 36-11-08, ALL CORRECT. DURING ENGINE STARTING, "HI STAGE" LIGHT DID NOT TURNED OFF,Dec 15, 2004 · N806AM · Boeing 7572Q8 · Cabin Cooling SystemSDR ASMF200410017Mechanism · out of adjustAIRCRAFT REJECTED TAKEOFF AT 80 KTS, AFT CABIN DOOR LIGHT TURNED ON. CAPTAIN REPORTED THAT DURING TAXING, LIGHT TURNED OFF AND TURNS ON AGAIN AT PLATFORM. CAPTAIN REQUESTED TO FLT ATTENDANTS TO CHECK THE DOOR, LINKING THE SLIDE BAR TURNING OFF THE LIGHT. AIROct 23, 2004 · N806AM · Boeing 7572Q8 · Passenger/Crew DoorsSDR ASMF200408009A/C Pack · inoperativeCAPTAIN REPORTED, AFTER ENGINE STARTED (LT ENGINE BLEED) LIGHT TURNED ON AND LT AIR CONDITIONING PACKAGE WAS INOPERATIVE. ENGINE WAS ACCELERATED, BLEED SWITCH WAS RESEATED AND FAIL CONTINUE. ENGINE BLEED SWITCH WAS RESEATED AGAIN AND ENGINE WAS ACCELERATED, (Aug 9, 2004 · N806AM · Boeing 7572Q8 · Cabin Cooling SystemSDR ASMF200407028Controller · failedCAPTAIN REPORTED RT AIR CONDITIONING (PACK OFF) LIGHT TURNED ON CONTINUALLY AFTER ENGINE START AND WHEN ENGINE WAS IN IDLE POSITION, PNEUMATIC BLEED OF RT ENGINE WAS SHUTDOWN. PILOT CONTROLLER OF 14TH STAGE WAS REPLACED IAW MM 36-11-19, TEST CORRECT.Jul 24, 2004 · N806AM · Boeing 7572Q8 · Cabin Pressure ControllerSDR ASMF200406028Circuit Breaker · trippedAIRCRAFT RETURNED TO PLATFORM, "CTL HYDRAULIC PUMP" LIGHT TURNED ON AND EICAS MESSAGE, ENGINES WERE SHUTDOWN. DURING MAINTENANCE CHECK, HYDRAULIC PUMP BREAKER K24 WAS ACTIVATED AND REESTABLISHED, FIM PROCEDURE 29-11-00 WAS PERFORMED, ALL CORRECT.Jun 23, 2004 · N806AM · Boeing 7572Q8 · Hydraulic Pump (Electric/Engine), MainSDR MEX2004040Line · leakingDURING PUSH BACK, FOUND HYDRAULIC LEAKAGE ON THE LT ENGINE WHEN IT WAS STARTED. AT REVISION WAS FOUND A BROKEN HYDRAULIC LINE, SUCH LINE WAS REPLACED BY AN ALTERNATE PN OF THE SAME PRESSURE CAPACITY AND SYSTEM TESTED IAW FIM.Jan 30, 2004 · N806AM · Boeing 7572Q8 · Hydraulic System, MainSDR MEX2003530Light · inoperativeAIRCRAFT RETURNED TO PLATFORM DURING TAXIING RT AFT SLIDE ARMED LIGHT DID NOT TURN ON. AT PLATFORM, TECH PERSONNEL SWAPPED BOTH AFT SLIDE LIGHTS, AND CLEANED PROXIMITY SENSOR IAW MM 25-10-00, TESTS CORRECT.Nov 22, 2003 · N806AM · Boeing 7572Q8 · Escape SlideSDR MEX2003360Shutoff Valve · failedAIRCRAFT RETURN TO PLATFORM AFTER LEFT ENGINE WAS STARTED. THE LT FUEL SPAR VALVE LIGHT COME ON AND THE LEFT ENGINE SHUTDOWN WITH CODE 282209. DURING REVISION, WAS DETECTED FUEL SHUTOFF VALVE ACTUATOR DAMAGED, THE FUEL SHUTOFF VALVE ACTUATOR WAS REPLACED IAWAug 13, 2003 · N806AM · Boeing 7572Q8 · Engine Fuel DistributionSDR MEX2003220Bypass Valve · leakingFLT 494 - MID-MEX - AIRCRAFT RETURN TO GATE, HYDRAULIC LEAK AT LEFT COMPARTMENT RESERVOIR AND DURING ENGINES STARTING THE 'LIGHT RUDDER PCU' EICAS STATUS MESSAGE TURN ON. THE LEFT SLATS BYPASS VALVE WAS REPLACED IAW MM, TASK CARD 27-81-09-024-001 AND 27-81-09Jun 9, 2003 · N806AM · Boeing 7572Q8 · Hydraulic System, MainSDR MEX2003155Actuator · inoperativeAIRCRAFT RETURN TO PLATFORM DUE TO RUDDER PCA EICAS MESSAGE. THE RUDDER MODULE WAS VERIFIED AND THE ALARM WAS FOUND IN RIGHT RUDDER RATIO. IN HANGER THE FIM 27-21-00 PROCEDURE WAS ACCOMPLISHED. BEING ALL CORRECT.May 3, 2003 · N806AM · Boeing 7572Q8 · Rudder Control SystemSDR MEX2002367Indicator · failedAIRCRAFT RETURNED DUE TO FIRST OFFICER AIRSPEED INDICATOR OUT OF SERVICE, CAPTAIN PERFORMED ABNORMAL PROCEDURES AND FAIL CONTINUED DURING DESCENT, AIRSPEED INDICATOR STARTED FUNCTIONING AND WARNING INDICATIONS STOPPED. FIRST OFFICER AIRSPEED INDICATOR AND CADec 18, 2002 · N806AM · Boeing 7572Q8 · Airspeed/Mach IndicatorSDR MEX2002347Panel · failedCAPTAIN REPORTED THAT THE RT ENGINE BLEED VALVE SWITCH WAS OUT OF SERVICE PANEL WAS REMOVED AND SWITCH WAS UNCLOGGED AND PNEUMATIC SYSTEM WAS LET OUT OF SERVICE IAW MM. DURING TRANSIT PANEL ASSEMBLY BLEED AIR WAS REPLACED IAW MM.Nov 22, 2002 · N806AM · Boeing 7572Q8 · Engine Bleed Air SystemSDR MEX2002266Warning System · activatedAT START OF RT ENGINE, ALL THE FIRE ALARMS ACTIVATED. FUEL CONTROL WAS DISCONNECTED AND MASTER WARNING WAS ADJUSTED, CREW REQUESTED TO PERFORM A VISUAL INSPECTION TO CONFIRM FIRE PRESENCE. FIRE HANDLE WAS PULLED AND FIRE ALARM CONTINUED AFTER 30 SEC. THE FIAug 14, 2002 · N806AM · Boeing 7572Q8 · Fire DetectionSDR MEX2002123Panel · failedFLT 902 - MEX-MTY - AIRCRAFT GOT PLATFORM WITHOUT AUDIBLE FIRE ALARMS. PERFORMED A FIRE DETECTION TEST IAW FIM 26-11-00 AND WEU AUDIBLE SYSTEM TEST IAW FIM 31-51-00. M100 ELECTRONIC CARD WAS CHANGED AND TESTS WERE PERFORMED IAW MM 31-51-04. DURING OVERNIGHTApr 25, 2002 · N806AM · Boeing 7572Q8 · Fire DetectionSDR MEX2002067Panel · failedFLT 941 - MTY-MEX - CABIN CREW REPORTED OTU OF SERVICE THE LANDING ALTITUDE SELECTOR, AS CONSEQUENCE OF SPARE PARTS MISSING IN MTY, MEX SENT SUCH PARTS IN FLT 944. AT ARRIVING, THE SELECTOR PANEL WAS SWAPPED, TEST OK, IAW MM 21-31-01. AT RON MEX 13/14 TESTS Mar 3, 2002 · N806AM · Boeing 7572Q8 · Cabin Pressure Control System
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