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 97UAL900137Slide · porousSLIDE REMOVED FROM AIRCRAFT FOR TIME CONTROLLED OVERHAUL. UNIT FAILED AIR RETENTION DUE TO POROSITY ON THE UPPER AND LOWER TUBE. SCRAPPED INFLATABLE UNIT, REPLACED WITH NEW.SDR 97UAL900136Girt · wornSLIDE REMOVED FROM AIRCRAFT FOR A TIME CONTROLLED OVERHAUL. DURING CHECK, CHAFE DAMAGE WAS NOTED IN THE SLIDE GIRT AND INFLATABLE. DAMAGE APPEARS TO BE CAUSED BY THE BACKBOARD RELEASE LATCHES. *S/D* NOTIFIED LOCAL BOEING FIELD REPRESENTATIVE. REPAIRED CHASDR 97UAL900112Actuator · defectiveLANDED IN SFO UNDER AMBER ALERT DUE TO A LEADING EDGE FLAP INDICATION PROBLEM. DISCOVERED FAULTY LEADING EDGE SLAT ACTUATOR. REPLACED ACTUATOR. OPERATION CHECKS NORMAL.SDR 97UAL900113Module · failedLANDING GEAR NOT DOWN LIGHT ILLUMINATED ABOVE 800 FEET. ACCOMPLISHED GEAR NOT DOWN EICAS MESSAGE FAILER ISOLATION PROCEDURE. REPLACED LANDING GEAR WARNING CONFIGURATION MODULE.SDR 97UAL900111Idg · failedABORTED TAKEOFF AT 60 KNOTS DUE TO RIGHT GENERATOR FAILURE. IDG (INTEGRATED DRIVE GENERATOR) FAILED. REPLACED IDG. LEAK AND OPERATIONAL CHECK WAS GOOD.SDR 97UAL900104Wire · severedEMERGENCY EXIT LIGHTING AT THE MID LAV AREA INOP. REPAIRED SEVERED PIGTAIL ON EMERGENCY EXIT LIGHT, OPERATION CHECKS NORMAL.SDR 97UAL900097Bulb · failedEMERGENCY EXIT SLIDE LIGHT INOP AT DOOR 2R. RELAMPED EMERGENCY EXIT SLIDE LIGHT AT DOOR 2R, OPERATION CHECKS NORMAL.SDR 97UAL900098Stator Vane · failedAT FLIGHT LEVEL 370 EXPERIENCED MULTIPLE COMPRESSOR STALLS. FLIGHT DIVERTED TO ORD. *S/D* 15TH STAGE STATOR VANE SEGMENT FAILED. REPLACED 15TH STAGE VANE AT SHOP VISIT.SDR 97UAL900080Pressure Syst · malfunctionedFLIGHT CREW ABORTED TAKEOFF AT 95 KNOTS DUE TO LOUD BANG SIMILAR TO DEPRESSURIZATION. *S/D* INSPECTED THE FORWARD BAGGAGE COMPARTMENT, NOSE GEAR SECTION, EQUIPMENT AND ELECTRICAL COMPARTMENT FOR DISCREPANCIES, NO FAULTS FOUND. THERE HAVE BEEN NO RELATED DISSDR 97UAL900050Air Distr · odorHOT ELECTRICAL SMELL AFT CABIN AREA AND COCKPIT. FLIGHT DIVERTED TO DEN.SDR 97UAL900013Light · inoperativeEMERGENCY EXIT LIGHTING AT DOOR 2L INOP. REPLACED EMERGENCY EXIT LIGHT AT DOOR 2L, OPERATION CHECKS NORMAL.SDR 97UAL900036Raft · deployedLIFERAFT IN AFT CABIN INFLATED WHILE AIRCRAFT CLOSED AND LOCKED FOR OVERNIGHT. INVESTIGATION REVEALED THAT AN INCORRECT O-RING WAS USED IN THE INFLATION CYLINDER REGULATOR. ALL CARLTON REGULATORS WERE RECALLED AND CHECKED. RAFT REPLACED. OPERATION CHECKS NSDR 97UAL900021Fan · failedSTRONG ELECTRIC SMELL DETECTED IN CABIN, ACCOMPANIED WITH EICAS MESSAGE EQUIPMENT OVERHEAT. SELECTED ALTERNATE EQUIPMENT COOLING FAN, SMELL DISSIPATED AND WARNING LIGHT WENT OUT. EQUIPMENT COOLING FAN FAILED. REPLACED EQUIPMENT COOLING EXHAUST FAN.SDR 97UAL900046Valve Assy · malfunctionedCYLINDER VALVE ASSEMBLY ON SLIDE REMOVED FOR TIME, FAILED TO OPEN DURING FLAT FIRE INFLATION TEST IN SHOP. REPLACED VALVE ASSEMBLY.SDR 96UAL901000Battery · dischargedCEILING EMERGENCY EGRESS LIGHTING AT OVERWING POSITION INOP. REPLACED BATTERY PACK, OPERATION CHECKS NORMAL.SDR 96UAL900999Bulb · failedRIGHT EXTERIOR OVERWING EMERGENCY EGRESS LIGHT INOP. RELAMPED RIGHT OVERWING EMERGENCY EGRESS LIGHT, OPERATION CHECKS NORMAL.SDR 96UAL900967Bulb · failedLEFT OVERHEAD OVERWING SLIDE EMERGENCY LIGHT INOP. RELAMPED LEFT OVERWING SLIDE EMERGENCY LIGHT, OPERATION CHECKS NORMAL.SDR 96UAL900962Yaw Damper · malfunctionedTUNING NR 1 HF CAUSES RIGHT YAW DAMPER INOP, ACCOMPANIED WITH EICAS MESSAGE.SDR 96UAL900949Idg · failedRIGHT GENERATOR DRIVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD. *S/D* RIGHT INTEGRATED DRIVE GENERATOR WAS REMOVED AND SENT TO SHOP. INTEGRATED DRIVE GENERATOR HAD BROKEN PISTON SLIPPERS. NEW INTEGRATED DRIVE INSTALLED, OPERATION CHECKS NORMAL.SDR 96UAL900931Air Distr · odorODOR NOTICED MAIN CABIN DURING POWER CHANGES. MOST NOTICEABLE DURING TRANSITION FROM CRUISE TO IDLE.SDR 96UAL900925Radio Syst · malfunctionedFLIGHT OFFICER'S RADIO SYSTEM BLOCKING ALL TRANSMISSIONS AND RECEPTIONS WHEN ACTIVATED.SDR 96UAL900922Wire · looseREPEATED ELECTRICAL POWER AND SUPPLY PROBLEMS WITH THIS AIRCRAFT REVEALED A LOOSE GALLEY GROUND WIRE CONNECTION. FURTHER INVESTIGATION FOUND INDICATIONS OF ARCING AND FIRE/SMOKE DAMAGE. *S/D* DISCOVERED WIRE W3666000410 WAS NOT CONNECTED SECURELY TO AIRCRASDR 96UAL900912Gear Handle · dirtyNOSE GEAR HAD TO BE EXTENDED BY ALTERNATE SYSTEM, HAD A RED GEAR LIGHT AND NO ALTERNATE NOSE GEAR OPEN LIGHT. GPWS SYSTEM GAVE AN AURAL GEAR WARNING, CYCLED GEAR. *S/D* DETERMINED THAT GEAR HANDLE WAS NOT MOVING INTO FORWARD DETENT WHEN PUT IN DOWN POSITIONSDR 96UAL900871Inflation Tube · chafedDURING TIME CONTROLLED OVERHAUL, SLIDE UNIT INFLATABLE SHOWS CHAFE DAMAGE CAUSED BY THE PRESSURE RELIEF VALVE SCREWS. HOLES ARE WORN THROUGH THE CHAFE COVER (2) AND THROUGH THE TOP INFLATION TUBE (5 HOLES). EACH HOLE IS .25 INCH IN DIAMETER. PATCH PER MANUSDR 96UAL900867Light · failedEMERGENCY EGRESS LIGHTING IN FRONT OF AFT LAV INOP. REPLACED EMERGENCY EGRESS LIGHT ASSEMBLY, OPERATION CHECKS NORMAL.SDR 96UAL900861Battery · dischargedEMERGENCY EGRESS LIGHTING INOP ROWS 16 TO 23. REPLACED BATTERY PACK, OPERATION CHECKS NORMAL.SDR 96UAL900854Bulb · failedEXTERIOR EMERGENCY EGRESS LIGHT AT DOOR 2L INOPERATIVE. RELAMPED EXTERIOR EMERGENCY EGRESS LIGHT AT DOOR 2L. OPERATION CHECKS NORMAL.SDR 96UAL900840Interlock Act · failedLEFT HAND THROTTLE HAS MECHANICAL STOP SHORT OF FULL MOVEMENT. *S/D* REDUCED THROTTLE MOVEMENT DUE TO THRUST REVERSER INTERLOCK ACTUATOR LOCKED IN EXTENDED POSITION DUE TO OPEN CIRCUIT BREAKER. RESET CIRCUIT BREAKER, OPERATION CHECKS NORMAL.SDR 96UAL900837Hpc Rotor · fractureNR 2 ENGINE REMOVED FOR HPT T1 BLADE DISTRESS, DISCOVERED DURING BORESCOPE INSPECTION. DISASSEMBLY OF THE ENGINE REVEALED FOD DAMAGE THROUGHOUT ALL STAGES OF THE COMPRESSOR 6TH THROUGH 17. *S/D* C6 BLADES OLD STYLE RECEIVED FOD, DEBRIS FROM C6 BLADES CAUSEDSDR 96UAL900836Slide Regulator · corrodedDURING OVERHAUL OF SLIDE, INFLATION REGULATOR FAILED. REGULATOR AND ASPIRATORS SHOWED SIGNS OF HEAVY CORROSION. DISASSEMBLY OF REGULATOR REVEALED FOD WAS PREVENTING NORMAL OPERATION OF THE REGULATOR.SDR 96UAL900813Bulb · failedEMERGENCY EXIT LIGHT INOP ROW 33 ABC. RELAMPED EMERGENCY EXIT LIGHT. OPERATION CHECKS NORMAL.SDR 96UAL900784Bulb · failedDOOR 4R EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT, OPERATION CHECKS NORMAL.SDR 96UAL900781Inverter · failedEMERGENCY EGRESS LIGHTING ROWS 23 THROUGH 28 INOP. REPLACED INVERTER FOR EMERGENCY EGRESS LIGHTING, OPERATION CHECKS NORMAL.SDR 96UAL900780Bulb · failedEMERGENCY LIGHT AT DOOR 2R INOP. REPLACED BULB, OPERATION CHECKS NORMAL.SDR 96UAL900775Fuel Pump · failedON APPROACH, LEFT ENGINE FLAMED OUT. ENGINE SHUTDOWN. *S/D* IMPROPER LAPPING OF BEARINGS BY THE OEM CAUSED THE FUEL GEAR STAGE BEARINGS TO BIND WITH THE HOUSING. UAL OVERHAULED AND REPLACED BEARINGS ON FUEL PUMPS PRODUCED DURING THE SAME TIME PERIOD, OPERSDR 96UAL900769Side Panel · corrodedDISCOVERED CORRODED AFT CARGO FLOOR SIDE PANEL MEMBER, JUST INBOARD FO CARGO DOOR SILL, SRM 53-60-53 PG 8 NR 4. REMOVED CORROSION AND REPAIRED PER SRM GUIDELINES, OPERATION CHECKS NORMAL.SDR 96UAL900768Excape Slide · deployedPER CREW, DOOR 4R SLIDE DEPLOYED. AIRCRAFT FERRIED TO LAX. REPLACED SLIDE AND DOOR EMERGENCY BOTTLE, OPERATION CHECKS NORMAL.SDR 96UAL900766Fuel Cap · failedDURING FLIGHT, LEFT OVERWING FUEL CAP DEVELOPED A LEAK. AIRCRAFT DIVERTED TO DEN. REPLACED FUEL CAP, OPERATION CHECKS NORMAL.SDR 96UAL900764Regulator · failedSLIDE REMOVED FOR TIME CONTROLLED OVERHAUL. DURING FLAT FIRE, BOTTLE VALVE FAILED TO FULLY OPEN DUE TO DAMAGED ROTATION SHAFT AND PIN. OVERHAULED VALVE, REPLACED SHAFT AND CONTACTED MANUFACTURER.SDR 96UAL900756Battery · dischargedEMERGENCY LIGHTS ROW 16L, 18L INOP. EMERGENCY EGRESS LIGHTING ROWS 16-23 INOP. BATTERY PACK FAILED. REPLACED BATTERY PACK. OPERATION CHECKS NORMAL.SDR 96UAL900740Lock Pin · not removedON CLIMB-OUT, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. REMOVED NOSE LANDING GEAR DOWNLOCK PIN. OPERATION CHECKS NORMAL.SDR 96UAL900710Breather Tube · brokenDURING CRUISE, NR 2 ENGINE OIL QUANTITY INDICATED ZERO. FLIGHT CREW SHUTDOWN ENGINE AND DIVERTED TO COS. *S/D* OIL LOSS DUE TO BROKEN BREATHER TUBE.SDR 96UAL900693Lock Actuator · malfunctionedNOSE LANDING GEAR DID NOT EXTEND. RECYCLED GEAR, WOULD NOT EXTEND. A SHORT TIME LATER GEAR EXTENDED. ACCOMPLISHED BOEING SERVICE BULLETIN 757-32-0113 TO CORRECT PROBLEM. OPERATION CHECKS NORMAL.SDR 96UAL900690Hf Tr Unit · damagedTUNING RIGHT HIGH FREQ SYSTEM CAUSES ERRATIC AUTOPILOT AND FALSE RIGHT AFT EMERGENCY DOOR OPEN EICAS MESSAGE. REPLACED RIGHT HIGH FREQ TRANSCEIVER, OPERATION CHECKS NORMAL.SDR 96UAL900679Fill Valve · not closedCREW REPORTED POTABLE WATER QUANTITY DROPPED TO ZERO AFTER TAKEOFF ACCOMPANIED BY AN EXTERNAL AIR NOISE NEXT TO DOOR 2R. FLIGHT DIVERTED TO PIT. INSPECTED AIRCRAFT, FOUND ALL DOORS CLOSED. INSPECTION REVEALED WATER FILL VALVE IN OPEN POSITION. CLOSED SAME.SDR 96UAL900665Compressor · stalledNUMBER ONE ENGINE HAD A COMPRESSOR STALL IN FLIGHT. ENGINE RECOVERED AND CONTINUED OPERATING. PRIOR TO STALL ENGINE WAS DECELERATING. *S/D* PERFORMED ENGINE BORESCOPE, 6TH THROUGH 9TH STAGE COMPRESSOR BLADES AND 2ND, 3RD STAGE LOW PRESSURE TURBINE, ALL CHESDR 96UAL900664Battery · dischargedEMERGENCY ESCAPE PATH LIGHTING INOPERATIVE ROW 9 THROUGH ROW 15. REPLACED BATTERY PACK. CHECKS O.K.SDR 96UAL900633Upper Tube · porousUNIT RETURNED TO SHOP FOR SECOND TIME CONTROLLED OVERHAUL. UNIT HAS POROSITY ON THE UPPER INFLATION TUBE WHERE IT MEETS THE TOP TUBE. UNIT RETURNED TO MANUFACTURER FOR REPAIR.SDR 96UAL900632Wire · wornDURING CLIMB-OUT FROM PHL, RECEIVED EICAS MESSAGE ON LEFT ENGINE PRIMARY CONTROL, ACCOMPANIED BY LENGTHY SECONDARY CONTROL MESSAGE. FLIGHT DIVERTED TO ORD. CONNECTOR W2P7 ON FUEL CONTROL HAD LOOSE BACKSHELL. WIRES WERE TWISTED IN BUNDLE INSIDE BACKSHELL. OSDR 96UAL900634Resistors · damagedAFTER LANDING EXPERIENCED HEAVY SHUDDER ENTERING TAXIWAY. AIRCRAFT TOWED TO GATE. *S/D* REPLACED ANTI-SKID UNIT. FAULTY UNIT RETURNED TO SHOP WHERE 4 RESISTORS WERE FOUND DAMAGED. RESISTORS REPLACED, OPERATION CHECKS NORMAL.
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