N803ML, cancelled Aug 12, 2010
Service difficulty reports · 58
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 = 'N803ML' AND deregistration_id = 'N803ML-2010-08-12' 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.
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 = 'N803ML' AND deregistration_id = 'N803ML-2010-08-12' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASMF 20090303Wire · damagedAIRCRAFT RETURNED TO DEPARTURE DUE TO PRESSURIZATION SYSTEM FAIL DURING THE INITIAL CLIMB, CABIN ALTITUDE AND FLOW LIGHTS CAME ON. MX REPLACED BOTH WIRING SECOND SEGMENT SWITCHES IAW AMM 21-31-09, THE PRESSURE CONTROLLER WAS REPLACED IAW AMM 21-32-03, THE WIRSDR MAS2008F00065Prbc · malfunctionedACFT REJECTED TAKE OFF AT 70 KNOTS DUE TO RT ENGINE DID NOT ACCELERATE. MX PERSONNEL REPLACED PRBC`S IAW MM 75-31-01 AND FCU IAW 73-20-01. ADDITIONALLY THE PS3 WAS VERIFIED AND CLEANED, THE BLEED VALVES WERE LUBRICATED IAW 75-31-05 AND TRIM BOTH ENGINES WAS SDR MAS2008F00063Engine · malfunctionedACFT REJECTED TAKE OFF 70 KNOT DUE TO RT ENGINE DID NOT ACCELERATE (EPR 1.14). MX PERSONNEL CHECKED THE RT ENGINE IAW MM 72-00-00 PAGE 501, ALL CORRECT. ADDITIONALLY, A HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-57-00, NO DAMAGES WERE FOUND. DURINGSDR ASMF200801002Blades · damagedDURING OVERNIGHT CHECK, 10 FAN BLADES OF THE RT ENG WERE DETECTED WITH DENTS AND LOSS OF MATERIAL DUE TO AN FOD. MAINTENANCE PERFORMED A BOROSCOPIC INSP IAW MM 72-00-00 AND NO ADDITIONAL DAMAGES WERE FOUND; THE 10 DAMAGED BLADES WERE REPAIRED IAW MM 72-33-21,SDR ASMF200709003Powerplant · overspeedCAPTAIN REPORTED WINDSHEAR DURING APPROACH AND ATS DISCONNECTED, SPEED DECREASED, SO AUTOTHOTTLES WERE SET TO THE MAXIMUM POWER. AT PLATFORM, MAINTENANCE PERSONNEL DOWNLOAD THE ENGINES INFORMATION FROM THE MINIQAR DETECTING THAT THE RT ENGINE HAD VALUES OF N1SDR ASMF200706006Turbine Blades · crackedDURING LT ENGINE BOROSCOPIC INSPECTION WAS DETECTED A FIRST STAGE TURBINE BLADE WITH A CRACK OF 0.500 INCH IN TIP. ENGINE WAS REPLACED IAW MM 71-00-02 AND OPERATIONALLY TESTED IAW MM 71-00-01, ALL CORRECT.SDR ASMF200703008Engine · overspeedAIRCRAFT REJECTED TAKEOFF AT 77 KNOTS DUE TO LT ENGINE REACHED ONLY 1.6 EPR WITH N1 104 PERCENT. AIRCRAFT WAS SENT TO THE HANGAR AND ENGINE WAS REMOVED AND SENT TO THE SHOP. THE NRC A0111096 WAS ISSUED TO CHECK ENGINE PT2 AND PT7 LINES AND MANIFOLD BY LEAKS ISDR ASMF200703007Unknown · unknownAIRCRAFT REJECTED TAKEOFF AT 75 KNOTS DUE TO LT ENGINE REACHED ONLY 1.6 EPR WHILE RT ENGINE REACHED 2.04 EPR WITH N1 100 PERCENT, SO AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL CHECKED ENGINE INLET/OUTLET, CONTROLS, PT2 AND PT7 LINES AND MANIFOLSDR ASMF200703006Seal · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN AN UPPER PANEL OF THE LT WING. MAINTENANCE PERSONNEL RELOCATED THE SEAL AND APPLIED SEALANT IAW SRM 51-20-04 AND 51-22-2A, LEAK WAS CORRECTED. AS A PRECAUTIONARY ACTION, DURING OVERNIGHT CHECK THE SEAL WAS REPSDR ASMF200702006Unknown · unknownCAPTAIN REPORTED THAT A GEN LOW AND TAIL COMP TEMP HIGH LIGHTS TURNED ON. DURING MAINTENANCE CHECK, THE TAIL CONE COMPARTMENT WAS DETECTED WITH HIGH TEMPERATURE AND THE FIRE EXTINGUISHER CONTAINER ACTIVATED. AIRCRAFT WAS SENT TO THE HANGAR AND RT FIRE EXTINGUISDR ASMF200611002Csd · failedAIRCRAFT RETURNED DUE TO HIGH TEMPERATURE IN THE LT CSD AND APU DID NOT START AT 34,000 FEET. DURING OVERNIGHT CHECK, LT CSD AND HEAT EXCHANGER WERE REPLACED IAW MM 24-10-01 AND 24-10-03, AS WELL AS TRIM AND TEST WERE PERFORMED TO THE APU IAW MM 49-00-00, ALL SDR ASMF200608014Skin · damagedDURING TRANSIT CHECK, AIRCRAFT HAD A STRIKE ON THE FORWARD SERVICE DOOR BY A CATERING SERVICE TRUCK, PRODUCING A DAMAGE OF 4 X 3 INCHES LENGTH AND 0.085 INCHES DEPTH, BETWEEN LONGERONS 20 AND 21 AND STATIONS 168 THROUGH 180. THE DAMAGED AREA WAS INSPECTED BEINSDR ASMF200608015Connector · contaminatedAIRCRAFT RETURNED, (FIRE DETECTOR LOOP A), (APU FIRE) AND (LT CSD HIGH TEMPERATURE) LIGHTS TURNED ON, AUDIBLE ALARM WAS ACTIVATED, LT GENERATOR WAS INOPERATIVE AND CAPTAIN ACTIVATED FIRE EXTINGUISHER BOTTLES. AIRCRAFT WAS SENT TO THE HANGAR AND FIRE DETECTIONSDR ASMF200608006Coupling · damagedAIRCRAFT RETURNED TO PLATFORM, LT ENGINE DID NOT HAVE TURN IN N1, NEITHER PNEUMATIC SUPPLY AND THE STARTER VALVE LIGHT OPERATING CORRECT. DURING MAINTENANCE REVIEW, THE ENGINE STARTER COUPLE WAS FOUND DAMAGED. THE COUPLE WAS REPLACED IAW MM 80-00-00, TESTED COSDR ASMF200608005Coupling · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO THE LT ENGINE DID NOT HAVE TURN IN N2. DURING MAINTENANCE REVIEW, THE ENGINE STARTER COUPLE WAS FOUND DAMAGED. THE COUPLE WAS REPLACED IAW MM 80-00-00, TESTED CORRECT.SDR ASMF200605011Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LEFT ENGINE START THE TEMPERATURE REACHED 510 DEGREES CELSIUS. DURING MAINTENANCE REVISION, FUEL WAS IN ENGINE CHAMBER NR 1. OVER TEMPERATURE INSPECTION WAS PERFORMED IAW MM 72-00-00, AND ENGINE STARTESDR ASMF200605002Warning System · malfunctionedAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF -L & R LANDING GEAR- LIGHTS REMAINED ON WITH MAIN LANDING GEAR LEVER IN UP POSITION. PROXIMITY SWITCH COMPUTER AND D1-25 AND D1-26 SENSORS WERE TESTED AND CHECKED IAW MM 32-60-04 AND MM 32-31-04, RESPECTIVELY, BSDR ASMF200604002Circuit Breaker · failedAIRCRAFT AIR TURNED BACK AS A CONSEQUENCE OF LOST OF INDICATION OF THE RIGHT OIL PRESS, OIL TEMP, FUEL TEMP, HYD QTY, HYD PRESS AND FLAPS. THE CIRCUIT BREAKERS ASSOCIATED WITH THE FAILURE WERE CHECKED, FOUND THEM IN CLOSE POSITION. THE CIRCUIT BREAKER T-34 OSDR ASMF20060309Fcu · leakingA FUEL LEAK WAS DETECTED DURING APU STARTING. APU WAS DEFERRED IAW MM 49-1 AND AFT ACCESSORIES AREA WAS CHECKED, BEING CORRECT. DURING OVERNIGHT CHECK, THE FUEL CONTROL UNIT AND THE AIR CONDITIONING WATER SEPARATORS WERE REPLACED IAW MM 49-30-01 AND 21-20-02,SDR ASMF200512010Warning Horn · activatedDURING GROUND TESTS, THE CAUTION LONG TRIM STABILIZER WAS OUT OF RANGE ACTIVATING THE TAKEOFF ALARM. AIRCRAFT WAS SENT TO THE HANGAR AND THE TRIM STABILIZER WAS TESTED IAW MM 27-40-12 AND DURING OVERNIGHT CHECK, THE TAKEOFF ALARM SYSTEM WAS VERIFIED IAW MM 27SDR ASMF200511005Coupler · failedDURING RIGHT ENGINE STARTING, THE RIGHT ENGINE DID NOT HAVE TURN IN N1 AND N2 AND START VALVE LIGHT TURNED ON. THE ADAPTER SHAFT STARTER WAS REPLACED IAW MM 80-10-01 PAGE 204, TESTED CORRECT. DURING OVERNIGHT CHECK, OPERATIONAL TEST WAS PERFORMED IAW MM 71-0SDR ASMF200508008Engine · making metalAIRCRAFT RETURNED TO PLATFORM, DURING RT ENGINE START, THE RT START VALVE OPEN LIGHT FLASHED AT 40 PERCENT RPM, N2 DECREASED TO 35 PERCENT AND RETURNED TO 50-56 PERCENT, 20 SECONDS AFTER THAT ENGINE STOPPED. AIRCRAFT WAS SENT TO THE HANGAR AND DURING MAINTENANSDR ASMF200508007Augment Valve · out of adjustAIRCRAFT RETURNED TO PLATFORM, DURING THE LT ENGINE START, THE FIRE EXTINGUISHER AGENT 2 LOW LIGHT TURNED ON. THE FIRE EXTINGUISHER POSITION 2 WAS REPLACED IAW MM 26-20-01; LT AUGMENTING VALVE WAS ADJUSTED IAW MM 36-10-01; THE CLAMS OF AUGMENTING VALVE AND REGSDR ASMF200507007Proximity Switch · out of adjustAIRCRAFT RETURNED TO PLATFORM, PASSENGER DOOR LIGHT COME ON. PASSENGER DOOR TEST WAS PERFORMED WITH A COMPLETE OPEN/CLOSE CYCLE IAW MM, BEING CORRECT. DURING OVERNIGHT SERVICE, THE GAP BETWEEN PRINTED CIRCUIT AND PROXIMITY SWITCH OF PASSENGER DOOR WAS VERIFIESDR ASMF200504024Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CAPTAIN REPORTED DID NOT HAVE ACCELERATION IN RIGHT ENGINE. DURING CHECK BOTH ENGINES WERE DETECTED STABILIZED AT 52 PERCENT OF N2, TESTS WERE CORRECT. AIRCRAFT WAS SENT TO THE HANGAR AND TRIM TO BOTH ENGINESSDR ASMF200504021Cadc · failedTECHNICAL PERSONNEL INFORMED THAT DURING TRANSIT CHECK AIR SPEED FLAG WAS SHOWN IN LEFT AIR SPEED INDICATOR AND ALTIMETER. TESTS WERE PERFORMED AND FAIL CONTINUED. CADC NR 1 WAS REPLACED IAW MM 34-16-01, TESTED CORRECT.SDR ASMF200504020Cadc · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF ADC NR 1 FAILURE, AUTO SLATS FAIL LIGHT TURNED ON AND RIGHT EFIS LOST INFORMATION. TESTS WERE PERFORMED CONFIRMING THE FAILURES. ADC NR 1, LEFT STALL COMPUTER AND RIGHT AHRU WERE REPLACED IAW MM 34-16-01, 34-SDR ASMF200501017Valve · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES "L ENG BLEED OFF" AND "PACK BITE" WERE SHOWN. CAPTAIN REPORTED THAT PURGE VALVE OF RIGHT ENGINE DID NOT OPEN, RESTARTED RIGHT ENGINE AND THE PURGE VALVE OPENED NORMALLY. SDR ASMF200409008Pump · failedAIRCRAFT RETURNED TO PLATFORM, LT HYDRAULIC PUMP FAILED. HYDRAULIC PUMP SOLENOID WAS CHECKED AND CIRCUIT BREAKERS WERE RESEATED AND FAIL CONTINUED. LT HYDRAULIC PUMP WAS REPLACED IAW MM 29-01-02, TEST CORRECT.SDR ASMF200408008Servo Valve · leakingDURING TRANSIT CHECK, HYDRAULIC LEAKAGE WAS DETECTED IN INTERIOR DOUBLE SERVO VALVE. IT WAS REPLACED IAW MM32-43-02, TEST WERE CORRECT.SDR ASMF200407029Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM, LT ENGINE WITH LOW POWER AND IN IDLE POSITION TEMPERATURE REACHED 485 DEGREE (C) OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THRUST LEVER TRIM WAS CHECKED IAW MM 76-11-00, LT ENGINE BLEED VALVES SDR ASMF200407018Prbc · failedDURING TRANSIT CHECK WAS DETECTED HIGH TEMPERATURE ON LT ENGINE, REACHED 482 DEGREE F. ENGINE RUNNING WAS PERFORMED TO VERIFY EGT INDICATION APPLYING PNEUMATIC AND ELECTRICAL CHARGES GETTING MAXIMUM TEMPERATURE INDICATION OF 445 DEGREE F, BEING WITHIN LIMITSSDR ASMF200407001Wheel · damagedDURING TRANSIT CHECK, CAPTAIN REPORTED STRONG VIBRATION IN NOSE LANDING GEAR. BOTH NOSE LANDING GEAR WHEEL WERE REPLACED IAW MM 32-40-00, ALL CORRECT.SDR ASMF200406036Blade · damagedDURING TRANSIT CHECK, LT ENGINE BLADE WAS DETECTED WITH DAMAGE FROM FOD. BLADE WAS REPAIRED IAW MM 72-33-21, ALL CORRECT.SDR ASMF200406017Computer · failedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING AHRU NR 2 FAILED. AHRU WAS REPLACED IAW MM 34-21-10, TEST CORRECT. DURING OVERNIGHT SERVICE SYSTEM WAS CHECKED, ALL CORRECT.SDR ASMF200406014Ahrs · failedAIRCRAFT RETURNED, AHRU NR 1 FAILED. AIRCRAFT WAS DISPATCHED IAW ABNORMAL PROCEDURES MANUAL 10-4. DURING OVERNIGHT SERVICE, MAGNETIC FLOW VALVE WAS REPLACED IAW MM 34-21-06, TEST CORRECT.SDR ASMF200406013Gyro · failedCAPTAIN REPORTED THAT DURING FLIGHT UNTIL APPROACH, RDMI AND ND WITH DIFFERENCE BETWEEN 30-40 DEGREES. DURING TRANSIT CHECK AT CUU, AHRU NR 1 WAS REPLACED IAW MM 34-21-10, TEST CORRECT. AIRCRAFT WAS DISPATCHED AND RETURNED OF FLIGHT, DFGC AND AHRU NR 2 FAISDR ASMF200404013Fcu · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF HIGH TEMPERATURE AND EGT OSCILLATIONS ON ENGINE NR 2. AIRCRAFT WAS SENT TO THE HANGAR. THE LEFT FUEL CONTROL UNIT (FCU) WAS REPLACED IAW MM 73-20-01, TEST CORRECT.SDR ASMF200403009Warning Horn · activatedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF TAKEOFF ALARM ACTIVATED. TECHNICAL PERSONNEL PERFORMED TESTS TO THE PROXIMITY SWITCH STALL COMPUTER AND STATUS TEST PANEL, BEING ALL CORRECT. DURING OVERNIGHT SERVICE AT MEX WIRING WAS REPAIRED ON S30-111 LEASDR ASMF200403002Clamp · leakingDURING TRANSIT CHECK WAS DETECTED HIGH TEMPERATURE ON TAIL CONE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE AUGMENTATION VALVE AND REGULATOR PRESSURE VALVE CLAMPS WERE REPLACED IAW MM 20-10-11, GASKET AND NIPPLE OF 13A STAGE BLEED VALVE WERSDR MEX2003519Switch · malfunctionedDURING TRANSIT CHECK, HYDRAULIC LEAKAGE WAS DETECTED IN THE SWITCH S1-168, SUCH SWITCH WAS BEHEADED. THE SWITCH WAS REPLACED AND THE HYDRAULIC SYSTEM WAS TESTED IAW MM 29-30-03. DURING OVERNIGHT SERVICE, THE SYSTEM WAS CHECKED BY LEAKAGES, ALL OK.SDR MEX2003518Pump · failedAIRCRAFT RETURNED TO PLATFORM DUE TO HIGHT TEMPERATURE ON RT HYDRAULIC SYSTEM. THE RT HYDRAULIC PUMP WAS REPLACED. DURING OVERNIGHT SERVICE THE PTU AND RELIEF VALVE WERE REPLACED IAW MM 29-10-12 RESPECTIVELY.SDR MEX2003492Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM, AFTER LT ENGINE START, IT HAD HIGH TEMPERATURE INDICATIONS (447 WITHOUT BLEED AND 491 WITH BLEEDS). ENGINE WAS TESTED AND IT HAD 450 WITHOUT BLEED AND 460 WITH BLEEDS BEING WITHIN LIMITS IAW MM 72-00-00. DURING OVERNIGHT SERVICSDR MEX2003392Proximity Sensor · will not testAIRCRAFT RETURNED TO PLATFORM DURING TAXING, NOSE LANDING GEAR RED LIGHT CAME ON. THE BITE WAS PERFORMED TO PROXIMITY SWITCH, SENSOR AND CONNECTOR WERE CLEANED AND CHECKED IAW MM, ALL CORRECT.SDR MEX2003258Wire · failedDURING FUELING SERVICE, WAS DETECTED THE REFUELING CONTROL PANEL OUT OF SERVICE. DURING REVISION WAS DETECTED THE BREAKER E-5 OF PANEL P-11 DAMAGED. THE REFUELING CONTROL PANEL WAS DEFERRED IAW MEL 28-41-6. THE REFUELING CONTROL PANEL WIRING WAS REPAIRED IASDR MEX2003257Light · intermittentAIRCRAFT RETURNED TO GATE, TAIL CONE LIGHT CAME ON INTERMITTENTLY. LIGHT TEST, SAFETY MECHANISM AND SW OF TAIL CONE WERE CHECK IAW MM 52-70-11, ALL TESTS CORRECT. (M)SDR MEX2003172Lock · brokenTHE RADOME RIGHT LOCK WAS BROKEN BY F.O.D. THE RADOME LOCK WAS REPLACED IAW MM 53-51-02, TEST CORRECT.SDR MEX2003163Indicator · failedAIRCRAFT RETURN TO PLATFORM DUE TO LT ENGINE EPR INDICATION FAILURE. DURING REVISION THE INDICATION ON EDP IS LESS THAN 1, THEREFORE, THE LT ENGINE WAS SHUTDOWN. THE EPR TRANS WAS REPLACED IAW MM, TEST CORRECT.SDR MEX2003148Transmitter · failedAIRCRAFT AIR TURNBACK DUE TO RADAR FAIL. TX RADAR WAS REPLACED IAW MM, TEST CORRECT.SDR MEX2003131Pitot Tube · failedCAPTAIN REPORTED LEFT PITOT SYSTEM OUT OFF SERVICES. PITOT TUBE WAS REPLACED IAW MM, TEST CORRECT.
Back to N803ML, cancelled Aug 12, 2010