N784XA

Service difficulty reports · 28

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 = 'N784XA' AND registry_match = 'registration'
  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 ASMF2019061309Unknown · vibrationCAPTAIN REPORTED THAT DURING TAKEOFF AND CRUISE, THE LEFT ENGINE VIBRATION REACHED 4.1 UNITS. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED FIM 71-05 TASK 808 PROCEDURE, CHIP DETECTORS AND SCAVENGE SCREENS INSPECTION, BY MISSING OR UNBOUNMay 4, 2019 · N784XA · Boeing 737752 · Engine (Turbine/Turboprop)SDR ASMF201901016Door Seal · out of positionAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, A STRONG NOISE IN L1 DOOR WAS DETECTED WITH VIBRATION AND IT WAS SHOWN MESSAGE “LNAV AND VNAV” MAINTENANCE PERSONNEL PERFORM INSPECTION IAW AMM 52-11-00, DETECTING THE SEAL DISARRANGED; SO THE DOOR SEAL WAS REPLDec 28, 2018 · N784XA · Boeing 737752 · Passenger/Crew DoorsSDR ASMF20190109001Warning System · false activationAIRCRAFT REJECTED TAKEOFF AT 78 KNOTS DUE TO WINDSHIELD INDICATION ALERT. THE FLIGHT CREW PERFORMED WINDSHIELD ESCAPE MANUAL INDICATED TO 1000 AGL BY WINDSHIELD INDICATION. MAINTENANCE PERSONNEL PERFORM HIGH ENERGY STOP / HEAT DAMAGE CONDITIONAL INSPECTION IAWOct 15, 2018 · N784XA · Boeing 737752 · Windshield/Door Rain/Ice RemovalSDR ASMF20180821006Windshield · damagedDURING A TRANSIT CHECK, FOUND THE R2 WINDSHIELD WITH DAMAGE DUE TO AN OVERHEAT WINDOW SWITCH. MAINTENANCE PERFORMED FOUND THE R2 WINDSHIELD TO BE OUT OF LIMITS. THE WINDSHIELD WAS REPLACED IAW AMM 56-12-11, TESTED CORRECT.Jun 19, 2018 · N784XA · Boeing 737752 · Flight Compartment WindowsSDR ASMF20180625014Lubrication Unit · failedAIRCRAFT RETURNED, DURING CLIMB, DUE TO THE RIGHT ENGINE OIL PRESSURE DROPPED TO 1 QUART, THE THRUST LEVER WAS RETARDED TO CLOSED, THE OIL QUANTITY DROPS TO 0 QUARTS AND REACH THE RED MARK. THE FLIGHT CREW PERFORMED A RIGHT ENGINE SHUTDOWN. MAINTENANCE PERFORMay 31, 2018 · N784XA · Boeing 737752 · Turbine Engine Oil SystemSDR ASMF20180625008Skin · damagedDURING TRANSIT CHECK, A DENT WAS DETECTED ON NOSE LANDING GEAR DOORS COUNTER FRAME. . MAINTENANCE PERFORMED REVISION DETECTING A DENT AND SCRATCHES, A DENT OF 2.50" DIAMETER, 0.094" DEPTH AT FUSELAGE SKIN BS 250 RIGHT SIDE AND 12.0" ABOVE OF NOSE LANDING GEAR May 7, 2018 · N784XA · Boeing 737752 · Fuselage Main, Plate/SkinSDR ASMF20180625007Pump · leakingDURING A RIGHT ENGINE VIBRATION TEST. DETECTED A FUEL LEAK THAT WAS OUT OF LIMITS. MAINTENANCE REPLACED THE RIGHT FUEL PUMP IAW AMM 73-11-01, TESTED GOOD.May 6, 2018 · N784XA · Boeing 737752 · Engine Fuel PumpSDR ASMF201801004Line · failedCAPTAIN REPORTED THAT THE LEFT AND RIGHT POINTER DUCT PRESSURE NOT HAD THE SAME SPLIT EITHER POINTER BELOW 18 PSI DURING TAKEOFF, CLIMB AND CRUISE, DUE TO THE ENGINE IS THE BLEED SOURCE LEFT 35 PSI AND RIGHT 14-15 PSI. THE FLEX LINE BETWEEN PRSOV AND BAR WAS Nov 18, 2017 · N784XA · Boeing 737752 · Pneumatic Distribution SystemSDR ASMF201704013Slat Track · crackedCAPTAIN REPORTED LE FLAP TRANSIT LIGHT ON. MAINTENANCE PERFORMED AN INSPECTION DETECTING A CRACK OF 1 X 0.250 INCHES IN CUT OUT FIXED LE INBOARD AUX TRACK SLAT 1 STATION 453 AND A CRACK OF 1 X 3 INCHES IN CUT OUT LE INBOARD MAIN TRACK SLAT 1 STATION 409. THEREApr 22, 2017 · N784XA · Boeing 737752 · Leading Edge DevicesSDR ASMF20161216007Window · crackedAIRCRAFT RETURNED FROM FLIGHT DUE TO DURING CRUISE THE PASSENGER WINDOW 1A GOT CRACKED. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE PASSENGER WINDOW 1A IAW AMM 56-21-00, TESTED CORRECT. THE GROUND HANDLING EQUIPMENT HITS AIRPLANE OR Nov 6, 2016 · N784XA · Boeing 737752 · Passenger Compartment WindowsSDR ASMF20161216006Coupling · brokenAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE CREW OXYGEN CYLINDER WAS LEAKING WITH STRONG NOISE AND OXYGEN LOW LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED AN OXYGEN CREW INSPECTION IAW MM 35-12-85, DETECTING OXYGEN CYLINDER MANOMETER WITH 0 PSI ANNov 3, 2016 · N784XA · Boeing 737752 · Crew Oxygen SystemSDR ASMF201608007Blade · lack of lubeIAW REMOTE DIAGNOSTIC SYSTEM, WITH CONTROL NR 20160704018 ABOUT TO AN INCREASE IN TAKEOFF AND CRX FAN VIBRATIONS. MAINTENANCE PERSONNEL PERFORMED THE FAN BLADE LUBRICATE IAW AMM 72-21-02-400-801, THE WEIGHT BALANCE BOLTS WAS VERIFIED WITHOUT FOUND DIFFERENCESJul 4, 2016 · N784XA · Boeing 737752 · Turbine Engine Compressor SectionSDR ASMF2016072600009Shutoff Valve · failedAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER ENGINES START, THE PARKING BRAKE LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED FIM 32-42 TASK 811 PROCEDURE, DETECTING THE PARKING BRAKE VALVE WITH FAILURE; SO THE PARKING BRAKE WAS DEFERRED IAW MEL 32-3 CAT. C. MMay 26, 2016 · N784XA · Boeing 737752 · Landing Gear Brake SystemSDR ASMF201510013Start Valve · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE THAT DURING LT ENGINE START, THE LT START VALVE OPEN LIGHT TURNED ON. DEFERRED IAW MEL 80-3-3 CAT C. REPLACED THE STARTER VLV IAW AMM 80-11-03, TESTED CORRECT.Aug 27, 2015 · N784XA · Boeing 737752 · Engine Start Valves/ControlsSDR ASMF201507016Warning System · false activationAIRCRAFT RETURNED TO PLATFORM, DURING RT ENG START, THE RT ENG CONTROL LIGHT TURNED ON. PERFORMED BITE TO LT EEC IAW FIM 73-06 TASK 801 PROCEDURE, SHOWING FAILURE CODE 73-31442, THE FIM 31-62 TASK 801 PROCEDURE & FIM 73-24 TASK 815 PROCEDURE, NO CONFIRMING THJun 26, 2015 · N784XA · Boeing 737752 · Fuel Controlling SystemSDR ASMF201507011Sensor · out of alignmentAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THE AUTO SLATS FAIL LIGHT TURNED ON. PERFORMED FIM 27-32 TASKS 801 & 809 PROCEDURES, SHOWING FAILURE CODE 27-31004 & DETECTING THE ANGLE OF ATTACK SENSOR OUT OF ALIGNMENT. THE ANGLE OF ATTACK SENSOR WAS ALIGNMEJun 12, 2015 · N784XA · Boeing 737752 · Stall Warning SystemSDR ASMF201501004Unknown · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO, AFTER RT ENG START THE LT ENG WAS 44% AT N2 & EGT INDICATOR FLASHING. CHECKED THE PRSOV IAW FIM 36-10 TASK 803 PROCEDURE, NO CONFIRMING FAILURE.Oct 5, 2014 · N784XA · Boeing 737752 · Pneumatic Distribution SystemSDR ASMF201409006Window · crackedCAPTAIN REPORTED LT WINDOW NR 1 CRACKED. ACFT WAS SENT TO THE HANGAR, REPLACED THE LT WINDOW NR 1 IAW AMM 56-11-31, TESTED CORRECT.Aug 11, 2014 · N784XA · Boeing 737752 · Flight Compartment WindowsSDR ASMF201406002Bonding Jumper · defectiveAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, BOTH FAIL FLAGS NAV CONTROL DISPLAYS WERE SHOWN. PERFORMED RESET TO RUPTURES P18-1 A-3 & P6-1 A-15 IAW FIM 34-51 TASK 812, NO FAILURES WERE FOUND. THE OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO THE ACFT LAApr 8, 2014 · N784XA · Boeing 737752 · Dependent Position Determining SystemSDR ASMF201303013Aileron Sys · out of adjustCAPTAIN REPORTED THAT DURING FLIGHT AND ON GROUND, THE AILERONS WERE HARD TO MOVE. MX PERSONNEL PERFORMED AILERON ADJUSTMENT AND TEST IAW AMM 27-11-00, ALL CORRECT.Jan 27, 2013 · N784XA · Boeing 737752 · Aileron Control SystemSDR ASMF201205013Shutoff Valve · damagedDURING FUELING, A IMBALANCE BETWEEN LT AND RT FUEL TANKS WERE OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. FLIGHT CREW DECIDED TO CONTINUE TO DESTINATION. SHUTOFF VALVE WAS REPLACED IAW MM 28-21-51, TESTED CORRECT.May 27, 2012 · N784XA · Boeing 737752 · Fuel Selector/Shut-Off ValveSDR ASMF201205011Shutoff Valve · damagedDURING FUELING, A FUEL SPILLAGE IN THE LT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. MX PERSONNEL CLOSED THE VALVE MANUALLY. THE SHUTOFF VALVE WAS REPLACED IAW MM 28-21-51, TESTED CORRECT.May 27, 2012 · N784XA · Boeing 737752 · Fuel Selector/Shut-Off ValveSDR ASMF20120403001Regulator · failedACFT PERFORMED AN EMERGENCY LANDING, DURING CRUISE AL 41,000 FT, THE RT BLEED TRIP OFF LIGHT TURNED ON, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE AND DESCENDING AT 14,000 FT. MX PERSONNEL PERFORMED THE FIM 36-10 TASK 801 DEApr 3, 2012 · N784XA · Boeing 737752 · Pneumatic Distribution SystemSDR ASMF20111221007Nose Cowl · dentedDURING TRANSIT CHECK, DETECTED A BIRD IN RT ENGINE, SO BIRD STRIKE CONDITIONAL INSP WAS PERFORMED IAW MM 05-51-18, DETECTING A DENT OF 8.0" LONG, 5.0" WIDE AND 0.375" DEPTH IN THE NOSE COWLING AT 12 HRS POSITION, THIS DENT WAS FOUND OUT OF LIMITS IAW SRM 54-10Dec 21, 2011 · N784XA · Boeing 737752 · Nacelle/Pylon, Main FrameSDR ASMF201110006Bleed Valve · leakingDURING RT ENGINE START, A FUEL LEAK WAS DETECTED. MX PERSONNEL PERFORMED REVISION DETECTING THE BLEED VALVE WITH LEAK OUT OF OPERATION LIMITS IAW MM 75-20-00. REPLACED IAW MM 75-23-01 AND OPS TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT.Oct 18, 2011 · N784XA · Boeing 737752 · Compressor Bleed ValveSDR ASMF201109007Skin · damagedDURING TRANSIT CHECK, MX PERSONNEL DETECTED 1 DENT WITH NICK ON FWD CARGO DOOR SKIN AT STA 467 BETWEEN LONGERONS 19 AND 20 OF 1.562 LONG, 1" WIDE AND 0.047" DEPTH. MX PERSONNEL CONFIRMED THAT THE DENT WAS OUT OF LIMITS IAW SRM 52-30-01. ACFT WAS SENT TO THE Sep 21, 2011 · N784XA · Boeing 737752 · Cargo/Baggage DoorsSDR ASMF201007002Precooler · damagedACFT PERFORMED AN UNSCHEDULED LANDING DUE TO DURING CLIMB AT 22,000 FEET, WITH ENGINE AND WING ANTI ICE SHUTDOWN, THE RT PACK BLEED TRIP OFF LIGHT TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE. MX PERSONNEL DEFERRED THE REPJul 4, 2010 · N784XA · Boeing 737705 · Cabin Cooling SystemSDR ASMF100109001Retaining Ring · damagedACFT PERFORMED AN UNSCHEDULED LANDING, DURING CLIMB AT 18,500 FEET, THE LT ENG WAS SHUTDOWN SUDDENLY. MX PERSONNEL REVIEWED THE ENGINE AND CHIP DETECTORS AND NO DAMAGES WERE FOUND, SO BOROSCOPE INSPECTION WAS PERFORMED ON COMPRESSOR AND TURBINE, DETECTING HPTJan 9, 2010 · N784XA · Boeing 737752 · Engine (Turbine/Turboprop)
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