Boeing 757-222
Service difficulty reports · 15,539
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '757222' 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 aircraft_model_key = '757222' 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 2006UALA02055Module · failedAIRCRAFT RETURNED TO BLOCKS DUE TO LE SLAT DISAGREE MSG DISPLAYED AND SLATS LOCKED OUT AT 5 UNITS. FOUND M528 MODULE FAULT, M524 HYD PRESS SW AND M525 HYD PRESS SW FAULT BALLS SET. ALL CLEARED. RESET FSEU BREAKERS FLAPS AND SLATS OPERATED NORMALLY AFTER SDR 2006UALA02054Status Message · illuminated"L ENG CONT" AND "L ENG SEC CONT" STATUS MESSAGE APPEARED ON CLIMB-OUT THROUGH APPROX 17000. REPLACED EEC AND FAULTY EEC WAS SENT TO OEM FOR ANALYSIS. THE ROOT CAUSE COULD BE THE INTERANL ELECTRONIC COMPONENT THAT MAY BE SENSITIVE TO ALTITUDE AND OR TEMPERATSDR 2006UALA02048Unknown · odorFUMES/ODOR STRONG IN COCKPIT AFTER ENGINE START WITH PACKS OFF. VERY STRONG FROM TAKEOFF PWR THROUGH CLIMB. FOUND OIL COMING OUT BETWEEN THE NR 2 COMPRESSOR AND THE NR 3 STATOR. ALSO FOUND OIL LEAKING FROM THE NR 1 STATOR AND THE FAN. REPLACED NR 1 ENGINESDR 2006UALA02029Skin · dentedHORIZONTAL SCRAPES AND DENT ACROSS BOTTOM OF FUSELAGE AT STA 585 MEASURES 18 IN BY 5 IN BY .250 IN DEEP. INCLUDES DAMAGE FROM STA 564 TO STA 616. EXTENDS 3 INCHES ABOVE RADIO ANTENNA LT AND RT SIDES. FUSELAGE SKIN AND STRINGER DAMAGE UNDER FWD CARGO PIT. NO SDR 2006UALA02002Ball Seat · unserviceableLOW BOTTLE PRESSURE. BALL SEAT WAS FOUND LEAKING. REMOVED AND REPLACED BALL SEAT.SDR 2006UALA02010Fan · odorAPU HAD SHUTDOWN, FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED, HAD A STRONG PETROLEUM BURNING ODOR PRIOR TO AUTO-SHUTDOWN AND FAULT. THE FAILURE IS ATTRIBUTED TO COOLING FAN FAILURE. THE FAILURE OF BALL BEARING CAUSED THE COOLING FAN SHAFT TO BREASDR 2006UALA01993Display · inoperativeFOUND UPPER EICAS BLANKED OUT ON TAXI. ALTN EFI NO HELP. ACCOMPLISHED BITE TEST ON LEFT AND RIGHT EICAS - CHECKED OKAY. RESTARTED NR 1 ENGINE AND PERFORMED POWER TRANSFER CHECKS - NO PROBLEMS NOTED.SDR 2006UALA01992A/C Pack · odorFWD AND AFT CABIN AIR QUALITY IS POOR. EXTREMELY FOUL ODOR FROM PACKS AFTER LIFTOFF. AS PART OF TROUBLESHOOTING, CHECKED BOTH INLETS AND HEAT EXCHANGERS, GND AIR CONNECTION AND PACK AREAS. BOTH ENG'S RAN AT POWER 1HR., BOROSCOPED NR 1 ENGINE, FOUND NO EVIDESDR 2006UALA01997Status Message · illuminatedUPON PLACING FLAPS AT 5 UNITS, STATUS MESSAGE NOSE AIR GROUND DISAGREE DISPLAYED. MAINTENANCE EICAS PAGE SHOWED "NOSE GEAR LOCKED" AND "NOSE GEAR DOWN" MESSAGES. CLEANED NOSE GEAR SENSORS. BITE TESTED PROXIMITY SENSOR ELECTRONICS UNIT -NO PROBLEMS NOTED.SDR 2006UALA01996A/C Pack · vibrationWITH BOTH PACKS ON LOUD RUMBLE AND VIBRATION HEARD AND FELT IN FIRST CLASS. REPLACED EQUIPMENT COOLING OVERBOARD AIR SHUTOFF (MOTOR OPERATED) EXHAUST VALVE. NO RE-OCURRENCE OF THIS PROBLEM NOTED SINCE THEN.SDR 2006UALA01979Hydraulic System · lowIN CRUISE "LEFT" HYDRAULIC QTY DECREASED TO .48. FOLLOWED CHECK LIST AND TURNED OFF BOTH LEFT SYSTEM PUMPS. QTY CONTINUES TO DROP AND IS NOW AT 0.40. NEED TO TOW AIRCRAFT OFF OF RUNWAY IF PTU WILL NOT SUPPLY NOSE WHEEL STEERING. QTY NOW DOWN TO 0.27 AND DROSDR 2006UALA01978Warning Message · activatedEICAS MESSAGE 'POWER XFER UNIT' IS DISPLAYED. STATUS MSG CAME ON AT CRUISE. OPERATED PTU MANUALLY, COMPLETED VISUAL INSPECTION OF PTU CONTROL AND INDICATION WIRING IN LH & RH WW, COMPLETED TEST PROCEDURE FOR THIS MESSAGE WITH BOTH ENGINES AS PER PROCEDURE - ASDR 2006UALA01973Warning Message · illuminatedLANDED ORD UNDER AMBER ALERT DUE TO HYDRAULIC SYSTEM EICAS MESSAGE. LT HYD QTY INDICATION DROPPED TO 0.45 WITH ASSOCIATED REFILL AND LOW QTY ON EICAS. LT SYSTEM HYD PUMPS CURRENTLY TURNED "OFF" PER FLIGHT MANUAL TO CONSERVE REMAINING FLUID FOR APPROACH & LASDR 2006UALA01972Unknown · unknownDURING DESCENT INTO ORD NO RUDDER TRIM LT OR RT. REPLACED RUDDER TRIM FEEL CENTERING/TRIM ACTUATOR.SDR 2006UALA01947Valve · unknownLOW BOTTLE PRESSURE. ONE HOUR WATER BATH TEST SHOWED NO LEAKS. REPLACED BOTTLE AND VALVE WITH ANOTHER BOTTLE AND VALVE. CHANGED OUT ALL THE O-RINGS ON THE VALVE THAT CAME IN WITH THE SLIDE. NO EVIDENCE OF TORN O-RINGS. ROOT CAUSE OF FAILURE NOT ESTABLISHEDSDR 2006UALA01971Iru · failedCTR IRS FAULT LT ON TAXI . SWAPPED RIGHT AND CENTER NAV UNITS TO HELP WITH TROUBLESHOOTING. THE UNIT ON RIGHT POSITION WAS FOUND TO BE NOT WORKING, THE UNIT IN CENTER POSITION WAS WORKING. REPLACED RT IRU. ACP ALL TESTS AFTER THAT, ACFT RESORTED BACK TO CASDR 2006UALA01953Warning Horn · activatedABORTED TAKEOFF AT 110 KTS DUE A CONFIGURATION WARNING HORN. TAKEOFF WARNING AT APPROX 100KTS, RTO AT APPROX 110KTS. PER CREW, "SPOILER" MESSAGE OCCURED ALONG WITH CONFIGURATION WARNING. ADJUSTED SPOILER HANDLE POSITION SWITCH AND TAKEOFF WARNING TESTED OKAYSDR 2006UALA01952Unknown · odorINBD CREW REPORTED POOR AIR QUALITY ON TAKEOFF AND LANDING. ODOR WAS REPORTED TO BE LIKE KEROSINE. ACP ENGINE BURN OUT PROCEDURE. NO ODOR NOTICED IN CABIN AFTER COMPLETION.SDR 2006UALA01949Unknown · unknownLOSS OF CABIN PRESSURE DURING FLIGHT. CABIN PRESSURIZATION PROBLEM DURING FLT, MASKS IN CABIN DID NOT DEPLOY. PERFORMED CONTROLLER BITE TEST, RESET CONTROLLER AND CHECKED ACFT PRESSURIZATION. ALL INDICATIONS NORMAL.SDR 2006UALA01950Pump · cloggedFLIGHT DIVERTED DUE TO THE LOSS OF OIL PRESSURE IN THE NR 2 ENGINE. ENGINE SHUTDOWN BY CREW. THE FAILURE IS ATTRIBUTED TO BUILDUP OF MATERIAL (BOM) RESULTING IN LUBE AND SCAVENGE PUMP FAILURE. CLOGGING OF SCAVENGE PORT OF PUMP ASSY STOPPED THE GEAR ROTATIONSDR 2006UALA01934Skin · damagedLIGHTNING STRIKE DAMAGE ABOVE STR 6 RT AND STA 465. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA. NDT CUT- OUT AND FASTENER HOLES. INSTALLED DOUBLER.SDR 2006UALA01915Generator · failedDIVERTED TO MCI DUE TO LOSS OF SECOND ENGINE GENERATOR. TROUBLESHOOT IDG FAILURES. CHECKED BPCU FOR FAULTS AND IDG OIL SVC. BPCU BITE INDICATES LT IDG SYSTEM OK. RT IDG HAD FAULTS OF HIGH RISE TEMP, UNDER FREQ TRIP, AND PMG WIRING FAILED. RT IDG TRIPPED OFSDR 2006UALA01897Cabin Pressure · unknownRETURNED TO JFK DUE TO CABIN PRESSURIZATION PROBLEM. PER FLIGHT CREW: AIRPLANE UNABLE TO HOLD CABIN PRESSURIZATION WITH INDEPENDENTLY SELECTING EITHER LEFT PACK OR RIGHT PACK ON. CABIN PRESSURE NORMAL WITH BOTH PACKS SELECTED ON. CABIN ALT WARNING, UNABLSDR 2006UALA01884Skin · dentedRAMP REPORTED DENT IN FUSELAGE APPROXIMATELY 4FT AFT DOOR 4L. MAJOR REPAIR ACCOMPLISHED ON FUSELAGE SKIN AFT OF DOOR 4L. DENT IS 5" LONG X 1" WIDE. REPAIR DOUBLERS AND TRIPLER INSTALLED AND INSPECTED.SDR 2006UALA01883Warning Message · illuminatedDIVERTED DUE TO APU OIL SERVICE INDICATION AND INOPERATIVE LEFT ENGINE GENERATOR. R GEN DF'D INOP AND APU OIL WAS SERVICED PRIOR TO DISPATCH. APU STARTED TO HAVE HIGH OIL CONSUMPTION LATER IN FLIGHT DUE TO LEAKS. NO EXTERNAL LEAKS OR REPORTS OF OIL FROM SESDR 2006UALA01868Squib · no testRIGHT SIDE NR 2 SQUIB WOULD NOT TEST. OFFWING EVACUATION SLIDE BOTTLE PRESSURE MEASURED AT 2500 PSI. BOTTLE WAS HYDROSTATICALLY TESTED - NO FAULTS FOUND. REPLACED CYLINDER.SDR 2006UALA01872Girt Bar · contaminatedFWD GIRT AT DOOR 4R HAS COME LOOSE, RAFT IS FALLING SLIGHTLY AND CAN`T GET GIRT TO ALIGN PROPERLY TO ENGAGE. FWD GIRT AT DOOR 4R HAS COME LOOSE, SLIDE RAFT FELL OUT OF POSITION SLIGHTLY. COULD NOT GET GIRT TO ALIGN PROPERLY TO ENGAGE. FOUND GIRT BAR NOT ENGSDR 2006UALA01874Valve · leakingLOW BOTTLE PRESSURE. BALL SEAT WAS LEAKING. REPLACED BALL SEAT.SDR 2006UALA01865Lanyard · dislodgedDOOR 3R SLIDE LANYARD FALLING OUT. MORE THAN ALLOWABLE SLACK TO LANYARD WITHIN ITS POUCH COULD HAVE INADVERTENTLY ALLOWED IT GET SNAGGED BY A GALLEY SERVICING EQUIPMENT. STOWED LANYARD TO SLIDE & GIRT BAR.SDR 2006UALA01846Frame · damagedSTATION 879 J-SECTION FRAME IS DAMAGED NEAR S21R. MAJOR REPAIR ACCOMPLISHED AT STA 879 FRAME S-21R. NEW FRAME INSTALLED. THIS IS A 12 MONTH CF ITEM PENDING DTA FROM BOEING.SDR 2006UALA01826Computer · unknownMADE AN UNPLANNED STOP AT DEN DUE TO AUTOPILOT PROBLEM. CREW COMMENTS: UNABLE TO ENGAGE AUTOPILOT L-C-R, L AND C AUTOPILOTS CMD SW GIVES HORN AND LT WARN, R CDM SW NOTHING. THE DISCREPANCY IS ATTRIBUTED TO A MALFUNCTIONING FLIGHT CONTROL COMPUTER. REPLACED SDR 2006UALA01810Frame · damagedFRAME AT STA 880 STR 21R HAS HEAT DAMAGE. MAJOR REPAIR ACCOMPLISHED. CONDUCTIVITY CHECK FOUND HEAT DAMAGE APPROX 3 INCH FROM EITHER SIDE OF BURNT THRU AND THE FRAME SUPPORT BRACKET ALSO HAS HEAT DAMAGE AT THAT LOCATION. UPON FURTHER INSPECTION FOUND STRINGESDR 2006UALA02273Structure · crackedMAIN ENTRY DOOR 2R IS CRACKED AT THE FWD 3RD FROM TOP STOP CUTOUT. REPLACED WITH A NEW MAIN ENTRY CABIN DOOR. REMOVED DOOR SENT TO SHOP FOR EVALUATION. ROOT CAUSE OF CRACK IS STILL UNDER INVESTIGATION.SDR 2006UALA01817Bottle · lowLOW BOTTLE PRESSURE REMOVED VALVE FOR OVERHAUL, REPLACED WITH OVERHAULED VALVE. SUSPECT VALVE DID NOT SHOW ANY LEAKAGE AFTER 2 HOUR LEAK TEST. REPLACED WITH ANOTHER BOTTLE AND A VALVE. RESULTS INCONCLUSIVE.SDR 2006UALA01788Unknown · odorSMELL OF BURNING IN COCKPIT TURNED OFF LEFT PACK AND SMELL SUBSIDED THEN RETURNED. INSP OF E&E BAY FWD AND AFT CARGO PITS; ALSO OPENED AND INSP LT PAC BAY; HOWEVER, NO SMELL OR DEFECTS NOTED. SUSPECT FRICTION IN BELT LOADER PRODUCED SMOKE.SDR 2006UALA01787Pump · failedDIVERTED DUE TO LOSS OF LEFT ENGINE ELECTRICAL AND HYDRAULIC PUMP. L HYD ENG DRIVEN PUMP EICAS MSG OFF. REPLACED LEFT HYDRAULIC ENGINE DRIVEN PUMP.SDR 2006UALA01786Unknown · odorSLIGHT BURNING ODOR IN AREA AROUND ROWS 15&16. VISUALLY INSPECTED AREA, UNABLE TO LOCATE SOURCE OF ODOR IN CABIN. MIGHT INVOLVE OVERHEAD TV MONITOR. NO DEFECTS NOTED.SDR 2006UALA01769Wire Harness · misinstalledDURING REMOVAL OF RT RECIRC FAN FOUND RECIRC FAN CONNECTOR WIRES BURNED. UPON FURTHER INSPECTION FOUND STRINGER BURNED. INCORRECT INSTALLATION OF WIRE HARNESS ALLOWING RUBBING OF WIRES AGAINST THE STRUCTURE, THIS CAUSED SHORT CIRCUIT OF AT LEAST ONE OF THE SDR 2006UALA01770Compressor · stalledAFTER FCU CHANGE NR 1 ENG HAD COMPRESSOR STALL ON DECEL AT APPROX 1.12 EPR, THEN 3 MORE STALLS AT IDLE THEN AUTO SHUTDOWN. NR 1 ENG RESTART FAILED, ENG HUNG STARTED AT 40% N2 WITH N1 ROTATION, EGT AT 225 DEG, FUEL FLOW NORMAL AT .6, DUCT PRESS WAS 30 PSI. FOSDR 2006UALA01758Radar · inoperativeMADE STOP IN ORD AND CANCELLED DUE TO AN INOP WEATHER RADAR. FOUND EXCESSIVE MOISTURE FROM UPPER SEAL. CONNECTOR D167 AND D165 AT ANT DRIVE UNIT FOUND CONTAMINATED WITH WATER DUE TO EXCESSIVE LEAKAGE OF RADOME SEAL. CLN'D CONNECTORS D167 AND D165. RPL'D SDR 2006UALA01746Unknown · unknownLEFT MAIN TANK TRANSFERRED INTO CENTER TANK. CREW REPORTED 400 LBS OF FUEL TRANSFER IN 3 HOURS OF FLIGHT. WHILE TROUBLESHOOTING, PRESSURIZED MANIFOLD - NO TRANSFER NOTED. PREVIOUSLY, TROUBLESHOT RH CTR TANK BOOST PUMP PRIMER CK VLV AND FEED CK VLV DUE TO APSDR 2006UALA01745Warning Message · illuminatedL/E SLAT DISAGREE WITH FLAP HANDLE AT 5 UNITS. MSG. CLEARED AT ENG SHUTDOWN , RAN FLAPS UP WITH HYDRAULICS, CHECKED CSEU NO FAULTS INDICATED, RAN FLAPS UP AND DOWN WITH HYDRAULICS NO FAULTS OR MESSAGE. TEN DAYS LATER, EICAS MESSAGE 'LE SLAT DISAGREE' DISPSDR 2006UALA01744Valve · failedBRAKE & ANTI-SKID MESSAGES ON TAXI. THE DISCREPANCY WAS DIAGNOSED AS A FAILED TWO PORT MOTOR OPERATED HYDRAULIC VALVE ASSY. REPLACED PARK VALVE, AND THE MESSAGE CLEARED.SDR 2006UALA01736Unknown · unknownLT MAIN TANK TRANSFERRED INTO CENTER TANK. FLT CREW BURNED CENTER TANK DOWN TO 800...ONE HR LATER IN CRUISE CENTER TANK SHOWS 1500# INDICATING FUEL TRANSFER. ACCOMPLISHED SUCCESSFUL TEST 4 OF THE FUEL SCAVENGE SYSTEM. CAUSE OF DISCREPANCY WAS NOT ESTABLISHESDR 2006UALA01737Plunger · bindingK LAV OXYGEN MASK DOOR FAILED DROP CHECK, DOOR DID NOT OPEN. THE PROBLEM WAS ATTRIBUTED TO A PLUNGER THAT WAS BINDING. REPLACED PLUNGER.SDR 2006UALA01721Battery Pack · inoperativeTHE FOLLOWING EMERGENCY LIGHTS ARE INOP: SLIDE LIGHT 4L, EXIT SIGN OVER DOOR 4L, EXIT MARKERS DOORS 4L & 4R. AFT GALLEY OVERHEAD EXIT SIGN, AISLE LIGHTS AT ROWS 29 & 32. THE CAUSE OF EMERGENCY LIGHT INOP CONDITION IS ATTRIBUTED TO A FAILED BATTERY CHARGER. SDR 2006UALA02272Door Frame · crackedMAIN ENTRY DOOR 2R FRAME IS CRACKED AT UPPER HINGE CUTOUT. REPLACED WITH A NEW MAIN ENTRY CABIN DOOR. REMOVED DOOR SENT TO SHOP FOR EVALUATION. ROOT CAUSE OF CRACK IS STILL UNDER INVESTIGATION.SDR 2006UALA01693O-Ring · unserviceableLOW BOTTLE PRESSURE. THE FAILURE IS ATTRIBUTED TO A DAMAGED FILL VALVE O-RING. THE O-RING WAS FOUND PINCHED AND HAD A NOTCH OUT OF IT. REPLACED O-RING.SDR 2006UALA01656Light · inoperativeTHE FOLLOWING EMERGENCY LIGHTS ARE INOP: SLIDE LIGHT 2L, EXIT SIGN OVER DOOR 2L, EXIT MARKERS DOORS 2L AND 2 R, EXIT SIGN ROW 8, AISLE LIGHT ROW 3.SDR 2006UALA01627Skin · dentedFOUND 2 DENTS ABOVE STRINGER 16L MEASURING .375 WITH .05 DEPTH. CUT OUT DAMAGED AREA IN A RECT. SHAPE PARLLEL TO STR WITH A 0.50 CORNER RAD. RETURNED ALL INDENTED AND PROJECTING SKIN TO CONTOUR. REMOVED ALL BURRS, NICKS, SCRATCHES. FABRICATED A DOUBLER R
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