N1075T, cancelled Jul 29, 2013
Service difficulty reports · 55
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 = 'N1075T' AND deregistration_id = 'N1075T-2013-07-29' 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 = 'N1075T' AND deregistration_id = 'N1075T-2013-07-29' 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 ASMF200610003Wire · looseAIRCRAFT RETURNED TO PLATFORM, THE PITOT STALL HEAT OFF (RUDDER LIMIT) LIGHT TURNED ON, AFTER ENGINES STARTED. THE RELAY R2-100 WAS CHECKED IAW MM 30-31-01, BEING CORRECT, BUT DURING RUDDER LIMITER PITOT TUBE REMOVAL, THE ELECTRICAL LINE OF CONNECTOR P1-361 WASDR ASMF200608021Structure · delaminatedDURING TRANSIT CHECK, LT ENGINE NOSE COWLING NOISE SUPPRESSOR WAS DETECTED DELAMINATED IN AN AREA OF 17 INCHES WIDTH X 25 INCHES LENGTH BETWEEN 6 AND 7 HOURS POSITION OUT OF LIMITS IAW MM 72-00-00 PAGE 642. AIRCRAFT WAS SENT TO THE HANGAR. PENDING FINAL ACTIONSDR ASMF200608012Control Valve · leakingCAPTAIN REPORTED THAT AFTER LANDING, THE LT HYDRAULIC SYSTEM WAS LOST AND LT REVERSE REMAINED EXTENDED. AIRCRAFT WAS TOWED TO PLATFORM AND RECHARGED OF HYDRAULIC LIQUID, DETECTING A LEAK IN THE LT HYDRAULIC REVERSE VALVE CAP. THE LT HYDRAULIC REVERSE VALVE WASSDR ASMF200608009Tube · leakingAIRCRAFT PERFORMED AN UNSCHEDULED LANDING, THE LT ENGINE (OIL PRESS LOW) LIGHT TURNED ON. CAPTAIN INFORMED THAT DURING CRUISE THE (OIL PRESS LOW) LIGHT TURNED ON, PERFORMED THE EMERGENCY PROCEDURE AND LT ENGINE WAS SHUTDOWN. DURING MAINTENANCE REVIEW, THE OIL SDR ASMF200605015Pump · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT GDL DUE TO THE AFT CENTER FUEL TANK BOOST PUMP WAS OUT OF SERVICE AND BREAKER POPPED OUT, LANDING WITH 5550 POUNDS IN THE LEFT TANK AND 3100 POUNDS IN THE RIGHT TANK. PUMPS WERE DEFERRED IAW MEL 28-2 AND AIRCRAFT WSDR ASMF200605014Hydraulic Line · leakingDURING TRANSIT CHECK IT WAS DETECTED A HYDRAULIC LEAK IN ONE LINE OF THE LEFT THRUST REVERSE CONTROL VALVE. FLEXIBLE LINE WAS INSTALLED, TESTED CORRECT. DURING OVERNIGHT CHECK THE FLEXIBLE LINE WAS REPLACED IAW MM 78-31-04, TESTED CORRECT.SDR ASMF200603006Gpu · smokeAIRCRAFT ARRIVED TO MEX WITH APU AND HIGH PNEUMATIC PURGE OF LEFT AIR CONDITIONING OUT OF SERVICE AND DEFERRED, SO GPU WAS CONNECTED AND IT INDUCED SMOKE INTO THE CABIN WHEN BOTH AIR-CONDITIONING PACKAGES WERE CONNECTED. AIRCRAFT WAS SENT TO THE HANGAR TO TESSDR ASMF200601010Starter · failedDURING TAXING CAPTAIN INFORMED THAT THERE WAS NOT INDICATION OF THE LEFT ENGINE, RETURNING TO PLATFORM. DURING MAINTENANCE REVIEW, THE ENGINE STARTER AND ITS COUPLE WERE FOUND DAMAGED. BOTH ITEMS WERE REPLACED AND SYSTEM TESTED IAW M/M 80-10-01. DURING OVERSDR ASMF200512013Blade · fodDURING TRANSIT CHECK, A BLADE OF THE LT ENGINE WAS DETECTED WITH DAMAGE BY FOD. INSPECTION WAS PERFORMED, DETECTING A CRACK OF 0.125 X 0.250 BEING WITHIN LIMITS IAW MM 72-00-00. THE LT ENGINE BLADE WAS REWORKED IAW 72-00-00 PAGE 618, TESTED CORRECT.SDR ASMF200507020Strut · underservicedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF STRONG NOISE IN THE NOSE LANDING GEAR. THE NOSE LANDING GEAR INSPECTION WAS PERFORMED IAW 32-20-00, ALL CORRECT. THE STRUT WAS SERVICED IAW MM 32-21-02, TESTED CORRECT.SDR ASMF200505028Actuator · failedAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF PRESSURIZATION WAS UNSTABLE DURING CLIMB. AT PLATFORM, THE VENTRAL STAIRWAY WAS ADJUSTED IAW MM 52-63-00. PRESSURIZATION CONTROLLERS BITE WERE PERFORMED, SYSTEM VALVES WERE REVISED, MANUAL SYSTEM OPERATION WAS SDR ASMF200412005Warning Light · false activationAIRCRAFT ARRIVED WITH CAPTAIN REPORT AFTER TAKEOFF THE THREE LANDING GEAR RED LIGHTS AND AUDIBLE ALARM TURNED ON. ABNORMAL PROCEDURE WAS PERFORMED AND LIGHTS AND ALARM TURNED OFF. AIRCRAFT WAS SENT TO THE HANGAR, SWITCHES S-319 AND S1-89 WERE REPLACED IAW MSDR ASMF200407020Antenna · damagedAIRCRAFT RETURNED OF FLIGHT, RADAR WAS OUT OF SERVICE WITH (TR AND FAIL ON DISPLAY) LEGENDS. TRANSCEIVER RADAR WAS CHECKED, RACK AND UNIT CONNECTORS WERE CLEANED AND ANTENNA WAS CHECKED, ALL CORRECT. TRANSCEIVER WAS REINSTALLED AND TESTED IAW MM 34-41-00, ALL SDR ASMF200406015Radar · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING, LOW FUEL AND CAPTAIN REPORTED RADAR SYSTEM FAILED. DURING MAINTENANCE REVISION, RADAR, ANTENNA, TRANSCEIVER AND RADAR DISPLAY WERE CHECKED, ALL CORRECT. RADAR TRANSCEIVER WAS REPLACED IAW MM 34-41-04, TEST CORRECT. SDR ASMF200405017Pressure Valve · failedAIRCRAFT RETURNED FLIGHT BECAUSE IN AUTOMATIC MODE THE PRESSURIZATION SYSTEM HAD OSCILLATIONS AND IN MANUAL MODE THE PRESSURE VALVE COULD NOT BE CLOSED. DURING MAINTENANCE REVISION, THE SWITCH WAS PLACED IN MANUAL POSITION AND VALVE WAS CLOSED, THE SYSTEM OPESDR MEX2004049Strut · dischargedFLT 253 - GDL-MEX - DURING TRANSIT CHECK, THE NOSE LANDING GEAR STRUT WAS FOUND COMPRESSED WITHOUT NITROGEN PRESSURE. THE NLG STRUT SEALS WERE REPLACED IAW MM 32-31-02 AND AN AJUSTMENT TO THE GROUND SENSING CONTROL MECHANISM WAS PERFORMED IAW MM 32-23-01, TESSDR MEX2003572Coupler · leakingFLT 143 - PVR-MEX - DURING TRANSIT CHECK, OBSERVED HYDRAULIC LEAKAGE COMING FROM THE MLG COMPARTMENT. THE LT HYDRAULIC SYSTEM,WITH LOW LEVEL, WAS PRESSURIZED, OBSERVING AN HYDRUALIC LEAKAGE IN A CONNECTING COUPLE OF THE POWER TRANSFER SHUTOFF VALVE. THE COUPSDR MEX2003563Display · failedFLT 563 - MEX-TAP - CAPTAIN REPORTED THE DURING FLIGHT RIGHT IVSI WAS OCCASIONALLY OUT OF SERVICE. AIRCRAFT WAS SENT TO THE HANGAR AND THE RIGHT IVSI AND BREAKER J-16 WERE REPLACED IAW MM 34-14-00 AND 20-25-00 RESPECTIVELY, ALL CORRECT. (M)SDR MEX2003448Switch · defectiveFLT 306 - ACA-MEX - AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE REVERSE UNLOCKED LIGHT TURNED ON. REVERSE MECHANISM AND ACTUATOR WERE LUBRICATED AND REVERSE WAS OPERATED THREE TIMES NON REPRODUCING THE FAIL. FURTHER, AIRCRAFT RETURN TO PLATFSDR MEX2003277Sensor · malfunctionedAIRCRAFT AIR TURN BACK, DURING FLIGHT THE LIGHT FWD STAIRWAY DOOR COME ON. THE FWD STAIRWAY DOOR SENSOR WAS CHECKED IAW 52-61-00, AND BITE WAS PERFORMED TO PRESSURIZATION CONTROLLERS IAW 21-32-03, ALL TESTS CORRECT.SDR MEX20030321Thrust Reverser · malfunctionedFLT 605 - DFW-MEX - AIRCRAFT RETURN TO PLATFORM, DURING TAXI THE RIGHT ENGINE REVERSE UNLOCKED INDICATOR LIGH TON. DURING REVISION THE LIGHT WAS OFF AND REVERSE WAS OPERATED THREE TIMES, ALL CORRECT. THE REVERSE WAS DEFERRED UNDER MEL 78-1. AT MEX, SWITCH RSDR MEX2003249Turbine · failedAIRCRAFT ARRIVED WITH CAPTAIN REPORT 'DEFICIENT AIR CONDITIONING'. DURING REVISION THE LEFT TURBINE COOLING WAS DAMAGED. REPORT WAS DEFERRED IAW MEL 21-1, LEFT AIR CONDITION OUT SERVICE. DURING OVERNIGHT SERVICE THE LEFT TURBINE COOLING WAS REPLACED IAW MM SDR MEX2003231Nose Cowl · dentedDURING TRANSIT CHECK WAS DETECTED NOSE COWLING ENGINE RIGHT WITH DENT OUT OF LIMITS OF APPROXIMATELY 2.0 OF DIAMETER. DURING OVERNIGHT SERVICE NOSE COWLING WAS REPLACED IAW MM, ALL CORRECT.SDR MEX2003226Indicator · failedMEX-SLC - FLT 486 - AIRCRAFT PERFORMED UNSCHEDULED LANDING, DURING CRUISE EFIS NR 2 FAILED AFFECTING VOR NR 2 AND ADI NR 1 AND DURING APPROACH BOTH TEMP OIL INDICATION CAME ON. BREAKER AHSRS 2 WAS RESET, EDP WAS TESTED AND ADDITIONALLY TEMP OIL SENSOR WERE CLSDR MEX2003225Thermocouple · damagedFLT 101 - HMO-CUL - AIRCRAFT RETURNED TO GATE DUE TO ENGINE NR 1 DID NOT HAVE EGT INDICATION. DURING REVISION FOUR, THERMOCOUPLE PROBES WERE DAMAGED. DURING OVERNIGHT SERVICE SUCH THERMOCOUPLE PROBES WERE REPLACED AND TESTED IAW MM 77-21-00, ALL CORRECT. (MSDR MEX2003185Generator · failedAIRCRAFT ARRIVED WITH REPORT RIGHT GENERATOR OUT OF SERVICE, GENERATOR WAS REPLACED AND AFTER ENGINES STARTING CAPTAIN INFORMS THAT SAME CONDITION CONTINOUS. AIRCRAFT ARRIVED BY ITS OWN IMPULSE TO THE POSITION S-7, ENGINES WERE SHUTDOWN AND WIRING WERE VERIFISDR MEX2003170Filter · failedAIRCRAFT RETURN TO PLATFORM DUE TO LOW ACCELERATION ON ENGINE NR 1. SERVICE ON ACCELERATION CAMERA WAS ACCOMPLISHED IAW MM 73-20-01. DURING OVERNIGHT SERVICE THE FUEL PUMP FILTER PS3 WAS REPLACED AND TEST WAS ACCOMPLISHED IAW MM 71-00-00, ALL CORRECT.SDR MEX2003207Relief Valve · failedFLT 926 - MEX-CUU - AIRCRAFT AIR TURNBACK AS A CONSEQUENCE OF DURING CRUISE AT 35,000 FEET, STRONG NOISE WAS HEARD, THE FLOW LIGHT CAME ON. PRESSURIZATION VALVE WAS CLOSED AND CABIN ALTITUDE WAS 7,600 FEET. PRESSURIZATION TEST WAS ACCOMPLISHED, NO LEAKS WERESDR MEX2003073Blade · damagedDURING TRANSIT CHECK, FOD ON LT ENGINE WAS DETECTED. DURING INSPECTION, DETECTED A BLADE WITH DAMAGE. FAN BLADE FROM ENGINE NR 1 WAS BLENDED IAW MM, ALL CORRECT.SDR MEX2003061Display · failedFLT 169 - CUL-MEX - AIRTURN BACK, DURING CLIMB IN THE FMA, AP TRIM THE NO AUTO LAND MESSAGE WAS SHOWN. THERE WAS A DIFFERENCE BETWEEN RMI'S OF 170 DEGREES. THE FD DISAPPEAR WITHOUT OBEY AUTO THROT AT SELECTED VELOCITIES. TESTS WERE PERFORMED IN STP AND SYSTSDR MEX2003041Accelerometer · inoperativeAIRCRAFT RETURNED FROM FLIGHT, AFTER TAKEOFF FLIGHT GUIDANCE COMPUTER WENT OFF. ON BOTH COMPUTERS THERE WERE NO AUTO PILOT AND ATS, PITOT HEAT OFF LIGHT TURN ON AND YAW DAMPER FAILURE LIGHT TURN ON. RESPECT TO PITOT STALL HEATER OFF LIGHT ON, IT WAS DETERMINSDR MEX2002140Csd · failedFLT 307 - MEX-ACA - TECHNICAL PERSONNEL AT GATE REPORT THAT THE ENGINE NR 1 CSD HAD DAMAGE OUT OF LIMITS AND THE MASTER CAUTION LIGHT WAS ON AS A CONSEQUENCE OF OIL LOW PRESSURE. AIRCRAFT WAS SENT TO THE HANGAR AND THE CSD AND THE RADIATOR OIL WERE CHANGED IASDR ASM2002F00003Bypass Valve · malfunctionedAIRCRAFT RETURNED FROM FLIGHT AS A CONSEQUENCE OF LANDING GEAR DOOR NOT RETRACTING. DURNING CHECK, THE LANDING GEAR BYPASS VALVE WAS OPEN AND NOT SECURED. VALVE WAS REPOSITIONED.SDR MEX2002353Display · failedFLT 353 - MEX-ZIH - AIRCRAFT RETURNED DUE TO PFD AND ND NAVIGATIONAL SYSTEM FAILURE, FIRST OFFICER RDMI FLAGS, AUTOMATIC PILOT, THROTTLES AND DIRECTOR BARS OUT OF SERVICE AND FMA WITHOUT INFORMATION. TECH PERSONNEL RECEIPT THE EQUIPMENT OPERATING IN NORMAL WASDR MEX2002317Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO LEFT ENGINE DID NOT ACCELERATE. PARAMETERS WERE ON RIGHT ENGINE 56.5 AND ON LEFT ENGINE 51.0 ENGINE 51.0. ENGINES WERE ADJUSTED ON IDLE, TESTS OK. DURING OVERNIGHT, SERVICE WAS PERFORMED A TRIM TO BOTH ENGINES IAW MM, TESDR GRAA9663Light · inoperativeLINE MAINTENANCE AT IFP, DISCOVERED THAT THE EMERGENCY FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED OPERATIONAL CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR GRAA9627Batteries · dischargedLINE MAINTENANCE AT RNO, DISCOVERED THAT BOTH OVERWING EXITS OVERHEAD EMERGENCY LIGHTS FAILED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. MAINTENANCE PERFORMED AN OPEATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. THE EMERGENCY LIGHT SYSTEM OPSDR GRAA9625Oil Filter · dirtyAT RNO, ON ENGINE START HAD THE RIGHT 'ENGINE OIL CLOGGING' LIGHT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE MAIN ENGINE OIL FILTER. MAINTENANCE PERFORMED AN OPERATIONAL AND LEAK CHECK OF NR 2 ENGINE. NR 2 ENGINE OPERATIONALLY CHECKED NORMSDR GRAA9624Lens · missingLINE MAINTENANCE AT ENV, DISCOVERED THAT THE EMERGENCY FLOOR TRACK LENS WAS MISSING AT ROW 18. MX REPLACED THE LENS ON THE EMERGENCY FLOOR TRACK AT ROW 18. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR LIGHT SYSTEM. THE SYSTEM OPERATIONASDR GRAA9623Power Supply · inoperativeLINE MAINTENANCE AT RNO, DISCOVERED THE FORWARD EMERGENCY FLOOR LIGHT LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT POWER SUPPLY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. THE EMERGENCY FLOOR LIGHT SYSTESDR GRAA9621Power Supply · inoperativeRNO - LINE MAINTENANCE DISCOVERED THE FLOOR PROXIMITY, EMERGENCY LIGHTS AT ROW 2 AND ROW 3 FAILED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. SYSTEM OPERATIONASDR GRAA96Press Controller · failedRNO - ON CLIMB-OUT, AIRCRAFT HAD THE AUTOPRESSURIZATION SYSTEM FAIL. AIRCRAFT RETURNED TO RNO WITHOUT FURTHER OCCURRENCE. MAINTENANCE DEFERRED THE AUTOPRESSURIZATION SYSTEM IAW MEL: 21-24. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR GRAA9616Battery Pack · dischargedLINE MAINTENANCE AT RNO, DISCOVERED THAT THE LEFT ACCESSORY COMPARTMENT EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY PACK. MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE SYSTEM. THE EMERGENCY SDR GRAA9607Connector · failedLINE MAINTENANCE AT ENV, DISCOVERED THAT THE FORWARD FLIGHT ATTENDANT ENTRY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG. OPERATIONALLY CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR GRAA9603Strut · req'd servUPON TAKEOFF AT FAR, NLG WOULD NOT RETRACT. AIRCRAFT RETURNED TO FAR WITHOUT FURTHER INCIDENT. MX WAS NOTIFIED AND A FERRY PERMIT WAS GENERATED. THE AIRCRAFT DEPARTED TO MKE WITH THE GEAR DOWN AND PINNED. MX DISCOVERED THAT THE NLG TORQUE LINK SCISSORS WERSDR GRAA9554Eel Lens · missingMAINTENANCE AT IFP, CLEARED A DMI THAT PERTAINED TO THE FORWARD EMERGENCY TRACK LIGHTING. MAINTENANCE REPLACED THE FLOOR TRACK LAMP PIGTAIL, AND LENS. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVSDR GRAA9553Battery Pack · dischargedAT IFP, FORWARD EMERGENCY CABIN OVERHEAD LIGHTS ILLUMINATE WHEN ELECTRICAL POWER IS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN OVERHEAD EMERGENCY LIGHTS BATTERY PACK. OPERATIONALLY CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT WAS RETURNEDSDR 95ZZZM745Eel Lamp · failedMAINTENANCE AT IFP, CLEARED A DMI THAT PERTAINED TO THE FORWARD EMERGENCY TRACK LIGHTING. MAINTENANCE REPLACED THE FLOOR TRACK LAMP PIGTAIL, AND LENS. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVSDR GRAA9552Battery Pack · dischargedAT IFP, FORWARD EMERGENCY CABIN LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE DISCOVERED THAT THE FORWARD EMERGENCY BATTERY PACK HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY BATTERY PACK. THE SYSTEM WAS OPERATIONALLY CHECKED, ASDR GRAA9545Controller · malfunctionedIFP - DURING CLIMB-OUT, THE AIRCRAFT FAILED TO PRESSURIZE. THE AIRCRAFT RETURNED TO IFP, WITHOUT FURTHER INCIDENT. MAINTENANCE RERACKED THE STANDBY PRESSURE CONTROLLER, AND RESEATED THE STATIC LINES. MAINTENANCE PERFORMED A GROUND MAINTENANCE TEST IAW MD-80
Back to N1075T, cancelled Jul 29, 2013