N750AT, cancelled May 9, 2017
Service difficulty reports · 83
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 = 'N750AT' AND deregistration_id = 'N750AT-2017-05-09' 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 = 'N750AT' AND deregistration_id = 'N750AT-2017-05-09' 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 DL75E091663Apu · malfunctionedAFTER PUSHBACK APU FAULTED AND SHUTDOWN. RESTART OK. BIT APU ECU. CLEARED REVERSE FLOW MESSAGE PER FIM 49-11-00. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.SDR DL75A080726Skin · corrodedFUSELAGE SKIN FOUND CORRODED AT STA 440 BELOW STR 28L. DAMAGE WAS CUT OUT, AREA WAS INSPECTED AND A REPAIR DOUBLER WAS INSTALLED.SDR DALA1304076902Skin · bulgedFUSELAGE SKIN WAS FOUND TO BE BULGING OUT AFT OF THE FWD LAVATORY SERVICE PANEL AT THE BUTT JOINT AT FS 440. REPAIRED IAW ERA 468316-14.SDR DL75E090203Fseu · faultedTE FLAP DISAGREEMENT WHEN FLAPS SELECTED TO TWENTY ON FINAL APPROACH. TROUBLESHOT TRANSMISSION FOR OVERLOAD INDICATION. NO TRIPS NOTED. CHECKED TRANSMISSION FOR SERVICE CHECKED OK. FSEU HAD INTERMITTENT FAULT FLAP LD RELIEF. PERFORMED FLAP LD RELIEF PER FSDR DL75A071642Link · gougedNLG LOCK LINK GOUGED ON THE LT SIDE SURFACE. LOCALLY BLENDED SURFACE TO REMOVE GOUGE.SDR DL75A071506Carbon Seal · damagedLEFT ENGINE OIL QTY WENT TO ZERO FOLLOWED BY OIL PRESS FLUX. AS CREW WAS FOLLOWING CHECKLIST LEFT ENGINE OIL PRESSURE INDICATION STARTED FLASHING RED CREW THEN SHUT ENGINE DOWN. THIS OCCURED AT CRUISE FLT. REMOVED AND REPLACED NR 1 ENGINE PRECOOLER CARBON SSDR DL75A060896Pump · unserviceableRIGHT ENGINE FAILED IN FLIGHT POST FLT STATUS MESSAGES R ENG SEC SEL R ENG OIL PRESS R ENG LOW N1. REF ITEM 7 FOR RT ENG EEC REPLACEMENT 707812. REPLACED NR 2 FUEL PUMP PER MM 664905, NEED LEAK OPN CK. REPLACED NR 2 FUEL CONTROL PER OPN 5034 STEPS 1-3 66490SDR DL75A060750Coffeemaker · burnedELECTRICAL FUMES REAR GALLEY AREA. PULLED ALL REAR GALLEY C/B`S, FUMES LESS. SUSPECT REAR GALLEY CAPTS SIDE COFFEEMAKER. RAN BREW CYCLE ON BOTH AFT GALLEY COFFEEMAKERS, CAPTS SIDE SMELLED STRONGER. REPLACED COFFEEMAKER NR 2 AFT GALLEY. RERAN BREW CYCLES NSDR DL75A060669Terminal · corrodedFOUND DURING SVC CK L-2 DOOR EXTERIOR EMERGENCY LIGHT INOP. FOUND CORROSION CAUSING HIGH RESISTANCE TO GROUND. CLEANED RECEPTACLE AND TERMINALS. OPS CHECKED GOOD.SDR DL75A060667Extinguisher · dischargedNR 2 CARGO FIRE BOTTLE FIRED. REMOVED NR 2 FIRE BOTTLE PER MM 481754, INSTALLED NR 2 FIRE BOTTLE AND REPLACED CARGO FIRE CONTROL PANEL PER AMM. MCO A PLAC REMOVED.SDR DL75A060060Control Unit · unserviceableAIR TURNBACK DUE TO UNABLE TO MAINTAIN CABIN PRESS. REPLACED PRIMARY EQUIPMENT COOLING CONTROL CARD.SDR DL75A040945Control Cable · wornHMV-3 VISIT IN DFW. CABLE WORN, AILERON CABLE WORN AT LEFT WING OVERRIDE QUADRANT. CABLE FOUND TO BE IN POSITION A1B-4 AND PN BACC2C4AD06518FG. REPLACED CABLE PER OPN 2000 AND INSTALLED RECOMMENDED OPTIONAL CABLE PN BACC2C4CD06518FG ON RC 1388-1392 WITH RIISDR DL75A040662Skin · crackedFUSELAGE, SKIN L1 DOOR CUTOUT, UPPER FWD CORNER REPAIR OF CRACK FATIGUE CRACK FOUND DURING INSPECTION OF THE L1 DOOR CUTOUT. ERA WAS GENERATED INSTALLING A REPAIR DOUBLER, TRIPLER AND QUADRUPLER TO REPAIR THE DAMAGE. ERA 097855-14AD REVISION ORIGINALSDR DL75A040287Tire · separatedNR 4 AND NR 8 MAIN TIRES BLOWN/DEFLATED CONFIRMED BY GROUND PERSONNEL ON TAKEOFF AT LGA. NR 8 TIRE LOST CAP, NR 4 TIRE FLAT. REPLACED ALL 4 WHEEL ASSYS ON RIGHT TRUCK. ALSO REPLACED NR 8 BRAKE LINE AND NR 4 AND 8 BRAKE ASSYS DAMAGED BY TIRE CAP. REPLACED SDR DL75A020074Connector · not seatedLEFT HYD ELECT PUMP EICAS MSG CAME ON AND PRESS LIGHT IN THE LEFT HYD PUMP SWITCH ILLUMINATED. FOUND PUMP OPN NORMAL. RESEATED PRESSURE SWITCH PLUG. PUMP, LIGHT, AND MSG ALL CHECK OK. REPLACED OVERHEAD HYD CONTROL PANEL AND LEFT SYS HYD ELECT PUMP LOW PRESSDR DL75A011665Fseu · malfunctionedIN CRUISE RECEIVED EICAS MSG LEADING EDGE SLAT ASYMMETRY WITH LEADING EDGE INDICATOR LIGHT. FLAPS INDICATED BETWEEN UP AND 1 POSITION. HANDLE WAS IN UP OR 0 POSITION. VISUAL CHECK CONFIRMED LEADING EDGE SLATS IN UP POSITION. CYCLED FLAPS AND SLATS AFTER CLSDR DL75A011670Floorbeam · corrodedTHE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND CORRODED IN SEVERAL AREAS. THE ENTIRE CAP WAS CUT OFF TO REMOVE ALL CORROSION. A NEW CAP WAS FABRICATED AND INSTALLED IN PLACE OF THE REMOVED CAP PER ER/A 381633-14, REV A.SDR DL75A011657Door Frame · corrodedTHE FWD FRAME OF THE C2 DOOR OPENING AT FS 1380 WAS FOUND WITH CORROSION ON THE OUTER FRAME CAP NEAR STRINGER 27R. THE CHORD WAS CUT JUST ABOVE THE DAMAGE AND THE LOWER SECTION REMOVED. A NEW SECTION OF CHORD WAS FABRICATED AND SPLICED IN WITH REPAIR ANGLES.SDR DL75A011648Skin · dentedFUSELAGE / SKIN / FS 690 / STRG. 24R-25R : SKIN CUTOUT REPAIR AN EXISTING SKIN REPAIR DOUBLER WAS DAMAGED AND REMOVED. THE UNDERLYING SKIN WAS CLEANED UP WITH A 8" X 4" CUTOUT. THE CUTOUT WAS REPAISDR DL75A011649Door Frame · corrodedTHE LOWER SILL BEAM OF THE C2 DOOR OPENING WAS BADLY CORRODED AND REQUIRED REPLACEMENT. TO REMOVE AND INSTALL A NEW SECTION, THE OUTER CHORD OF THE FS 1440 OPENING FRAME WAS CUT AT STRINGER 26R AND THE WEB CUT AT STRINGER 23R. THE LOWER SECTIONS WERE REMOVEDSDR DL75A011563Skin · dentedFUSELAGE / SKIN / FS 278 / WL 208 : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 278 AT WL 208. THE DENT WAS REMOVED WITH A 5" X 4" CUTOUT. THE CUTOUT WAS REPAIRED WITH ANSDR DL75A011001Bulkhead · gougedFUSELAGE / SKIN & BULKHEAD / FS 1700-1780 / STRG. 26L-26R : GROUND DAMAGE REPAIR THE FUSELAGE SKIN FWD AND AFT OF THE FS 1720 BULKHEAD WAS GOUGED AND PUNCTURED FROM A TAIL STRIKE DURING LANDING. THEBULKHEAD WEB WAS SLISDR DL75A010409Wire · brokenEMERGENCY LIGHT INOP AT SEAT ROW 33DEF. REPAIRED BROKEN WIRE AT SEAT ROW 33DEF, EMERGENCY LIGHT OPS CK. GOODSDR DL75A992796Pwr Supply · inoperativeFWD CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.SDR DL75A991983Compressor · stalledCHS OPS CALLED TO REPORT A/C RTB DUE TO COMPRESSOR STALL AND NR 2 ENG FIRE REPORTED BY THE TOWER. PER FLT CREW, ON TAXI-OUT EXPERIENCED STALL AND TOWER REPORTED FIRE FROM THE BACK OF NR 2 ENGINE. NO EPCS MESSAGES, NO OVERTEMPS. CREW PUSHED THROTTLE UP A FEWSDR DL75A991651Slide · deployedR-1 DOOR SLIDE DEPLOYED AT GATE BY PERSONNEL.SDR DL75A981332Slide · out of positionAFTER T/O, R AFT ENTRY DOOR LIGHT CAME ON. F/A TRIED TO GET HANDLE TO LOCK DOWN, NO LUCK. RETURNED TO ATL. FOUND 3R DOOR SLIDE SHIFTED OFF FWD SUPPORT. REPOSITIONED SLIDE, DOOR CLOSES NORM.SDR DL75A980474Switch · intermittentINFLIGHT, FLIGHT ATTENDANT AND PASSENGER REPORTED FUMES WHICH SMELLED LIKE SMOLDERING RUBBER IN THE AREA OF THE LAST THREE ROWS IN PASSENGER CABIN. STRONGER ON CO-PILOTS SIDE. FUMES WERE INTERMITTENT. MAINTENANCE CHECKED AREA, NO VISIBLE SIGNS OF FUMES. NOSDR DL75A970218Wire · shortedON SHORT FINAL, AN APPARENT STATIC DISCHARGE OCCURED BY THE L-1 DOOR. A SHOWER OF SPARKS CAME FROM THE WALK-AROUND O2 BOTTLE MOUNTED ON THE BULKHEAD. F/A-S ON JUMPSEAT WITNESSED LARGE DISPLAY OF SPARKS AS WELL AS PASSENGERS FIVE ROWS BACK. FOUND TERMINAL SPSDR DL75A962620Battery Pack · dischargedFIRST CLASS TRACK LIGHTING INOP. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHK NML.SDR 96ZZZM885Charger Assy · inoperativeIND - EMERGENCY LIGHT IN BULLNOSE ABOVE 25ABC INOP. EMERGENCY LIGHT IN BULL NOSE ABOVE 27DEF INOP. REMOVED AND REPLACED BATTERY CHARGER AT FUSELAGE STATION 1243 LEFT, LIGHT OPS NORMAL.SDR 96ZZZM84Bleed Linkage · wornIND - LEFT ENGINE POWER FLUCTUATES AT 9 CONSTANT POWER SETTINGS. FL 27,000, OAT -29, MACH .80, N1 77.8 TO 78.3, EPR 1.03 TO 1.04 EGT 415 TO 418. PERFORMED FIM PROCEDURES PER FIM 73-21-00 FIG 107. FOUND 2.5 BLEED LINKAGE WORN TO .125 INCH ITEM PLACED ON MCI SDR 95ZZZW325Egt Sys · malfunctionATL - FLT 400 - RT ENG EGT INCREASED TO 649 DEGREES CELSIUS FOR 2 SECONDS, ON TAKEOFF FROM HOWARD AFB, PANAMA. NO SURGE ASSOCIATED. NO OTHER PARAMETERS EXCEEDED, OAT PLUS 35. INSPECTED ENGINE PER MM 72-00-00 P615, NO DAMAGE NOTED. EICAS RT ENG 649 DEGREES
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