N950AM
Service difficulty reports · 42
Newest first, from July 9, 2004, when the mark’s previous registration was cancelled.
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 = 'N950AM' AND difficulty_date > DATE '2004-07-09' 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 = 'N950AM' AND difficulty_date > DATE '2004-07-09' 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 ASMF202508040001Shutoff Valve · faultyDUCT PRESSURE INDICATION LOW DURING TAKEOFF, CLIMB AND CRUISE, ENGINE IS THE BLEED SOURCE. FRM 361 040 00SDR 2025FA0000340Valve · malfunctionedDUCT L INDICATION PRESSURE IS LOWSDR M17F202401170001Duct · damagedWHEN READY FOR PUSHBACK DURING BEFORE START CHECKLIST A VEHICLE CRASH THE AIRCRAFT FROM THE RIGHT SIDE OF THE AIRPLANE GOING THRU THE LEFT SIDE STOPPING THE MOVEMENT ON THE LEFT ENGINE, CAUSING SEVERE DAMAGE TO THE ENGINE AND FUSELAGE.SDR 2022FA0000253Pneumatic System · secondary damageBLEED TRIP OFF EN ESTATUS DURANTE DESPEGUE (REGRESO DE VUELO) / LEED TRIP OFF IN STATUS DURING TAKEOFF (FLIGHT RETURN) SDR ASMF202101011Skin · corrodedREVISION, DETECTING A BULGE OF 2.00" LENGTH, 0.875" WIDTH AND 0.1875" DEPTH AND A DENT OF 1.3125" LENGTH, 1.0625" WIDTH AND 0.021" DEPTH WITH THREE FASTENERS DAMAGES IN FUSELAGE SKIN RIGHT COUNTER FRAME APU ACCESS DOOR. APU COWL DOOR WAS REMOVED, IAW AMM 52-4SDR ASMF202011009Acoustic Panel · dentedDURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL DENTS ON LEFT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 0.281" WIDTH AND 0.013" DEPTH, TWO DENTS OF 0.500" WIDTH AND 0.006" DEPTH, A DENT OF 0SDR ASMF2020090710Proximity Sensor · malfunctionedCAPTAIN REPORTED THAT DURING APPROACH FLAP POSITION INDICATOR HAS NEEDLE SPLIT, AFTER 2 MINUTES IT TURNED TO A TRAILING EDGE FLAP LEVER DISAGREE CONDITION. MAINTENANCE PERSONNEL PERFORMED THE BITE TO FSEU IAW FIM 27-51 TASK 801 PROCEDURE, DETECTING FAILURE COSDR ASMF2020090709Flap System · malfunctionedCAPTAIN REPORTED THAT DURING APPROACH THE FLAPS WERE NOT OPERATING CORRECTLY, REMAINING IN FLAPS 10 WHEN THE LEVER WAS PUT ON FLAPS 15. MAINTENANCE PERSONNEL PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 803 PROCEDURE, SHOWING FAILURE CODES 27-81224, 27-81203, 27SDR ASMF2020090703Module · failedCAPTAIN REPORTED THAT DURING LANDING AUTO BRAKE DISARM LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED REVISION TO SYSTEM, DETECTING LEFT ANTI-SKID VALVE WITH FAILURE. THE S2 AND S3 SWITCH PACK M1766 AND M 1767 WERE CHECKED, IAW FIM 32-42 TASK 828 PROCEDURESDR ASMF2019042317Bolt · looseDURING TRANSIT CHECK, IT WERE DETECTED SUPPORT BOLT OF LH AND RH INBOARD FLAP AFT LOOSED. AIRCRAFT WAS SENT TO THE HANGAR TO REVISION; THEY WERE ISSUED WO´S 5273684 AND 5273713 TO PERFORM TASKS; MAINTENANCE PERSONNEL PREFORMED REPLACEMENT OF BEARINGS I.A.W. AMSDR ASMF2019042301Warning Message · false activationAIRCRAFT RETURN TO PLATFORM DUE TO DURING TAKEOFF, IT WAS ACTIVE “TAKE OFF CONFIGURATION ALARM”; FLIGHT CREW ACCOMPLISHED THE QRH 15.2 PROCEDURES; MAINTENANCE PERSONNEL PERFORMED TAKE OFF WARNING SYSTEM TEST IAW FIM 31-51 TASK 803 , NO FAILURE WAS FOUND, TEST SDR ASMF201901017Warning System · false activationAIRCRAFT RETURN TO PLATFORM DUE TO DURING TAKEOFF, IT WAS ACTIVE “TAKE OFF CONFIGURATION ALARM”; FLIGHT CREW ACCOMPLISHED THE QRH 15.2 PROCEDURES; MAINTENANCE PERSONNEL PERFORMED TAKE OFF WARNING SYSTEM TEST IAW FIM 31-51 TASK 803 , NO FAILURE WAS FOUND, TEST SDR ASMF20180515001Warning Light · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINE START THE LOW OIL PRESSURE LIGHTS ILLUMINATED. MAINTENANCE PERFORMED FIM 49-90-803, TESTED CORRECT.SDR ASMF201802002Valve · leakingDURING FUELING, A FUEL LEAK IN THE LEFT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. MAINTENANCE PERFORMED A FUEL TRANSFER TO AVOID THE SPILL IAW AMM 28-21-00 AND THE VALVE WAS REPLACED IAW AMM 28-21-32, ALL TESTED CORRECT.SDR ASMF201801009Line · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS FOUND IN THE MLG WHEEL BRAKE LINE NUMBER 3. MAINTENANCE ADJUSTED THE MLG WHEEL BRAKE LINE IAW AMM 32-41-00, AND THE MLG WHEEL NUMBERS 3 AND 4 WERE INSPECTED IAW AMM 32-45-00-700-803, TESTED CORRECT.SDR ASMF20170424002Fan · fodDURING TRANSIT CHECK, DETECTED FOREIGN OBJECT DAMAGE AT INLET CASE FAN OF THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED A REVISION TO LEFT ENGINE IAW AMM 71-00-00, DETECTING TWO DENTS OF 3/4"LENGTH, 3/8"DEPTH AND 2 1/2"LENGTH, 9/16"DEPTH IN THE ABRADABLE SHSDR ASMF20170216001Warning System · false activationAIRCRAFT REJECTED TAKE OFF AT 90 KNOTS DUE TO TAKE OFF CONFIG AND REVERSE ENG 1 INDICATION. MAINTENANCE PERSONNEL PERFORMED REVISION AND OPERATIONAL TEST IAW AMM 78-31-200, TESTED CORRECT. THE HIGH ENERGY STOP INSPECTION WAS NOT NECESSARY DUE TO THE MAXIMUM GRSDR ASMF201612017Solenoid · failedAIRCRAFT REJECTED TAKEOFF AT 45 KNOTS DUE TO RIGHT FORWARD EMERGENCY OVERWING DOOR WARNING ANNUNCIATOR ILLUMINATED. MAINTENANCE PERFORMED REVISION IAW AMM 52-20-00. THE RIGHT FORWARD EMERGENCY OVERWING WARNING DOOR SOLENOID WAS REPLACED IAW AMM 52-22-41 AND TSDR ASMF201611024Shutoff Valve · malfunctionedDURING FUELING, A FUEL SPILLAGE IN THE RIGHT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED AND MAINTENANCE CLEANED THE SELECTOR. THE SHUTOFF VALVE WAS RESEATED AND TESTED SEVERAL TIMES IAW MM 28-21-00, NO LEAKS WERE DETECTED SDR ASMF201611017Wire Harness · damagedDURING TRANSIT CHECK, THE RIGHT ENGINE FIRE HANDLE LIGHT WAS NOT ILLUMINATED DURING FIRE DETECTION TEST AND LOOP B OF RIGHT ENGINE WITH FAULT. MAINTENANCE PERSONNEL PERFORMED RIGHT ENGINE FIRE DETECTION TEST IAW AMM 26-10-00, DETECTING LINE OPEN AT MW0326 WIRSDR ASMF201608006Engine · damagedIAW REMOTE DIAGNOSTIC SYSTEM, THE RT ENGINE HAD A SHARP DECREASE IN TAKEOFF, EGT MARGIN AND CORE SPEED AS WELL AS IN INCREASE IN EGT AND FUEL FLOW. MAINTENANCE PERSONNEL PERFORMED THE RT BORESCOPE INSPECTION OF THE HIGH PRESSURE TURBINE AND COMBUSTION SECTIONSDR ASMF20160620010Engine · damagedIAW REMOTE DIAGNOSTIC SYSTEM, THE LT ENGINE HAD A SHARP DECREASE OF EGT HOT DAY MARGIN, AS WELL AS AN INCREASE OF EGT AND FUEL CONSUMPTION. MAINTENANCE PERSONNEL PERFORMED THE LT ENGINE BORESCOPE INSPECTION OF THE HIGH PRESSURE TURBINE AND COMBUSTION SECTION SDR ASMF201605003Warning Light · false activationAIRCRAFT REJECTED TAKEOFF DUE TO FWD OVERWING DOOR LIGHT TURNED ON BEFORE RESIZING 80% OF N1. DEFERRED THE FWD OVERWING DOOR LIGHT IAW MEL 52-3 2 CAT C. HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-51-07, NO DAMAGES WERE FOUND. THE FIM 52-20 TASK 801SDR ASMF201601002Fuel Heater · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE LT ENG. PERFORMED REVISION, DETECTING THE FUEL SERVO HEATER & HPTCC VLV LEAKING, SO THE LT FUEL SERVO HEATER & HPTCC VLV WERE REPLACED IAW AMM 73-11-07 & AMM 75-21-01, TESTED CORRECT.SDR ASMF201511011Transmitter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG OIL FILTER BY PASS LIGHT TURNED ON. PERFORMED REVISION TO CHIP DETECTOR IAW AMM 79-00-00, NO METAL PARTICLES WERE FOUND. PERFORMED FIM 79-05 TASK 817 PROCEDURE, DETECTING THE SCAVENGE OIL FILTER SDR ASMF201510009Sensor · failedDURING APPROACH, FLAPS DID NOT EXTEND. ACFT WAS SENT TO THE HANGAR & MX PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 801 PROCEDURE, SHOWING FAILURE CODE 27-53252 FLAP 3 SKEW, SO THE SENSOR T527 OF FLAP 3 WAS REPLACED IAW FIM 27-59 TASK 803 PROCEDURE, TESTED CORRSDR ASMF201510008Fan · lack of lubeDURING CLIMB, THE RT ENG VIBRATION REACHED 2.5 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED REVISION TO CHIP DETECTOR IAW AMM 79-00-00, NO METAL PARTICLES WERE FOUND. A BORESCOPE INSPECTION TO LPT STAGES 1 - 3 IAW AMM 72-00-00, NO DAMAGES WERE FOUND. LSDR ASMF201509004Warning System · false activationCAPTAIN REPORTED THAT DURING CLIMB, THE LT ENG VIBRATION REACHED 4.2 UNITS. PERFORMED FIM 77-31 TASK 801 & FIM 78-01 TASK PROCEDURES, NO DAMAGES WERE FOUND, TESTED CORRECT. AS PRECAUTIONARY ACTION, REPLACED THE VIBRATION MONITOR IAW AMM 77-31-01. TRIM BALANSDR ASMF201507009Wire Harness · damagedAIRCRAFT RETURNED TO PLATFORM, AFTER LT ENG START, THE BLEED DUCT PRESS INDICATOR SHOWED 5 PSI & IT WAS STABILIZED AT 10 PSI. PERFORMED REVISION, DETECTING THE ELEC HARNESS NR MW0311 DAMAGED. THE LT ELEC HARNESS NR MW0311, BLEED AIR REGULATOR & TUBE WERE REPSDR ASMF201506009Window · crackedAIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF THE LT WINDOW NR 2 CRACKED. REPLACED THE LT WINDOW NR 2 & WINDOW HEAT CONTROLLER MODULE IAW AMM 56-12-11 & AMM 30-41-11, TESTED CORRECT.SDR ASMF201503022Hmu · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DIFFERENCE OF ONE INCH BETWEEN THRUST LEVERS AT IDLE & THE RT ENG WITH OSCILLATIONS. PERFORMED BITE TO RT EEC IAW FIM 73-00 TASK 801 PROCEDURE, NO FAILURE DETECTED. BOTH ENGS WERE STARTED DETECTING THE LT ENG WAS 67.9% ATSDR ASMF201501024Radome · dentedDURING TRANSIT CHECK, IT WAS DETECTED A DENT IN RADOME BETWEEN 4:00 AND 5:00 HRS POSITION OF 4.0 INCHES IN LENGTH & 3.0 INCHES WIDE. EVALUATED THE DAMAGE & FOUND OUT OF LIMITS IAW SRM 53-52-00. ACFT WAS SENT TO THE HANGAR & ISSUED THE NON-ROUTINE CARDS A0223SDR ASMF201501014Warning System · false activationDURING TRANSIT CHECK, THE ANTI-SKID LIGHT TURNED ON WAS DETECTED ON CABIN CREW. PERFORMED FIM 32-42 TASK 829 PROCEDURE, CONFIRMING THE FAILURE, SO THE ANTI-SKID SYS WAS DEFERRED IAW MEL 32-2-2 CAT C. ACFT PERFORMED AN UNSCHEDULED LANDING DUE TO RAIN IN THE DSDR ASMF201402010Warning System · false activationAIRCRAFT REJECTED TAKE OFF AT 40 KNOTS, DUE TO RT FWD OVERWING LIGHT TURNED ON. PERFORMED A REVISION AT THE FWD OVERWING DOOR IAW AMM 52-20-00, DETECTING THE FWD OVERWING DOOR WAS LOCKED CORRECTLY. FWD OVERWING DOOR DEFERRED IAW MEL 52-3-2 CAT C. THE HIGH SDR ASMF201312012Warning System · false activationAIRCRAFT REJECTED TAKE OFF AT 80 KNOTS DUE TO RIGHT FWD OVERWING LIGHT TURNED ON. PERFORMED THE QRH 1.14 PROCEDURE, NO CONFIRMING THE FAILURE & INITIATING AGAIN SEQUENCE OF TAKEOFF. AT MEX, AS PRECAUTIONARY ACTION, PERFORMED BITE TO OVERWING EXIT DOOR FLIGHSDR ASMF201308007Unknown · odorACFT RETURNED TO PLATFORM AFTER ENGINES START. A RUBBER BURNING ODOR WITH NO EVIDENCE TO SMOKE. MX PERSONNEL PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56 AND FIM 21-00 TASK 806 PROCEDURE, NO ODOR OR SMOKE EVIDENCES WERE FOUND. THSDR ASMF201303020Pump · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED. MAINTENANCE PERSONNEL DETECTED THE FUEL PUMP SEAL DAMAGED ON RT ENGINE, FUEL PUMP WAS REPLACED IAW AMM 73-11-01 AND TESTED IAW AMM 71-00-00, ALL CORRECT.SDR ASMF201303006Connector · out of positionCAPTAIN REPORTED THAT DURING CLIMB AN ELECTRICAL CABLE BURNED ODOR WITH NO EVIDENCE OF SMOKE, DISAPPEARING DURING CLIMB. MX PERSONNEL PERFORMED FIM 21-00, TASK 806 PROCEDURE AND SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56, DETECTING A FORWASDR ASMF201211011Case · damagedDURING TRANSIT CHECK, IT WAS DETECTED SCRATCH ON RT ENGINE FAN INLET CASE. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED AN ENGINE REVISION IAW MM 72-24-01, DETECTING SCRATCH AND GROOVE ON RT ENGINE FAN INLET CASE OUT OF LIMITS; SO THE RT ENGINE WAS SDR ASMF201211009Blade · dentedCAPTAIN REPORTED THAT DURING TAKEOFF AT ROTATION SPEED A BIRD STRIKE ON RT ENGINE; FLIGHT CREW CONTINUED TO DESTINATION DUE TO RT ENGINE PARAMETERS WERE NORMAL AND VIBRATION REACHED 2.9 OF N2. . MX PERSONNEL PERFORMED A BIRD STRIKE CONDITIONAL INSPECTION IAW MSDR ASMF201210006Windshield · leakingCAPTAIN REPORTED THAT DURING CLIMB AT 3.8 PSI’S OF DIFFERENTIAL PRESSURE, A STRONG NOISE IN CREW CABIN WAS HEARD. FLIGHT CREW ACCOMPLISHED THE QRH 2.1 PROCEDURE, NO CONFIRMED FAILURE, CONTINUED TO DESTINATION. MX PERSONNEL REPLACED THE LT WINDSHIELD NR 2 IAWSDR ASMF201207002Line · leakingDURING PUSH BACK, DETECTED A HYD LEAK IN THE RT MLG. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED FLEXIBLE BRAKE LINE NR 4 IAW MM 32-41-00, TESTED CORRECT.
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