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 2006UALA01272Unknown · odorTAXIED OUT ON LEFT ENGINE. STARTED 2ND ENGINE. CAPTAIN SMELLED SMOKE. RETURNED TO GATE. BOTH ENG BLEED OFF. ALSO ISOLATED PACKS AND RECIR, NO SMELL OR SMOKE NOTED. ALL LIGHTS IN CABIN ON VIDEO ON, CHECKED ALL CARGO PITS AND E&E COMPARTMENT, NO SOURCES SMOKESDR 2006UALA01225O-Ring · leakingLOW BOTTLE PRESSURE. O-RING ON FILL VALVE WAS LEAKING AND FOUND DAMAGED. REPLACED O-RING ON FILL VALVE.SDR 2006UALA01228Bellcrank · fracturedDIVERTED DUE TO LEFT ENGINE OVERHEAT IN CRUISE. THE 2.5 BLEED BELLCRANK (PN 1B7787) FRACTURE WAS THE PRIMARY CAUSE OF HIGH EGT. ECM DATA SHOWS HIGH EGT NR 1 ENG PEAKED OUT 648 DEG C.14TH STG BLEED CONVERTER VALVE STUCK OPEN. REPORTED EGT EXCEEDANCE LASTED SDR 2006UALA01227Engine · shutdownRETURN TO FIELD DUE TO ENGINE SHUTDOWN. ENG2 WAS SHUT DOWN IN FLIGHT & UNABLE TO RESTART DUE TO HIGH VIBRATION. RT ENG SURGED AT 9000FT, 250 KNOTS, ENG2 HIGH VIBES, EGT AT 699, UPON LANDING FOUND METAL IN THE TAIL PIPE. DETECTED FRACTURE OF 2ND STAGE BLADESDR 2006UALA01094Light · inoperativeEEL LIGHT STRIP OUT AT 15ABC. [06-29-07] REPLACED LIGHT STRIP.SDR 2006UALA01090Generator · crackedAPU FAULT LT ON AFTER 3 START ATTEMPTS NO START. FOUND NO OIL IN APU. FOUND CRACK ON TOP OF GEN AT 1200 POSITION APU GENERATOR SHARES THE OIL SYSTEM AND RESERVIOR WITH THE APU. THE LINE AND APU SHOP HAS HISTORY OF GENERATOR HOUSINGS CRACKING IN THE SAME FSDR 2006UALA01081Circuit Breaker · trippedDIVERTED TO ORD DUE TO 4 POPPED GALLEY CIRCUIT BREAKERS. [06-29-07] RESET CB S' AND TESTED PER MM, COULD NOT DUPLICATE. OPS CHECKS OK. NO FURTHER OCCURENCES OF PROBLEM.SDR 2006UALA01123Pin · installedSLIDE SAFETY PIN WAS PREVIOUSLY INSTALLED AND NOT REMOVED BEFORE FLT. SAFETY PIN WAS ROUTINELY INSTALLED PRIOR TO RII INSPECTION OF SLIDE RAFT FOR DOOR 1R. THE SAFETY PIN WAS NOT REMOVED AS PER UA OPERATING PROCEDURE BEFORE FLIGHT. REQUIRES FURTHER TRAININSDR 2006UALA01087Squib · no testEMERGENCY SLIDE LEFT SQUIB DOES NOT TEST.SDR 2006UALA01009Light · inoperativeTHE FOLLOWING EMERGENCY LIGHTS ARE INOP, 4 L OVER DOOR EXIT SIGN, AFT GALLEY CEILING EXIT SIGN, SLIDE LIGHT DOOR 4L, EXIT SIGN OVER DOOR 2L, EXIT MARKERS DOOR 4L, 4R, 2L, 2R, SLIDE LIGHT DOOR 2L, AISLE LIGHTS ROWS 4, 29, 32, EXIT SIGN AT ROW 9.SDR 2006UALA01025O-Ring · leakingLOW BOTTLE PRESSURE FILLER VALVE O-RING WAS LEAKING. REPLACED O-RING.SDR 2006UALA00988O-Ring · damagedFOUND LOW BOTTLE PRESSURE FILLER VALVE O-RING FOUND DAMAGED AND LEAKING. REPLACED FILLER VALVE O-RING.SDR 2006UALA00960Warning System · activatedRETURNED TO FIELD DUE TO A LEFT OVERWING SLIDE EICAS MESSAGE. UPON LANDING SLIDE WAS DEPLOYED BUT DID NOT INFLATE.SDR 2006UALA00989Housing · leakingTHE GAUGE BOTTOM HOUSING WAS LEAKING.SDR 2006UALA01011Slide · unknown1R MED SLIDE RAFT PRESSURE GAUGE AT BOTTOM OF GREEN BAND AFTER 5 HOURS ON GROUND.SDR 2006UALA00949Skin · crackedFUSELAGE DENTED AND CRACKED, APPROX 3 FEET AFT OF DOOR 2L, 3 TO 6 INCHES ABOVE WATER LINE. DENT CUT OUT AND REPAIR DOUBLER INSTALLED.SDR 2006UALA00936Crease Beam · damagedLEFT CABIN CREASE BEAM OUTER CHORD BS 630 IS DAMAGED. REPAIR SPLICE AND SPLICE ANGLES INSTALLED.SDR 2006UALA00994Squib · no testFOUND EMERGENCY ESCAPE (RT) SQUIB DOES NOT TEST.SDR 2006UALA00995Lanyard · tangledNR 4 RT MED SLIDE STATIC LINE AND D-RING L ANYARD TANGLED. WRAPPED AROUND GIRT BAR.SDR 2006UALA00966Light · inoperativeEMERGENCY AISLE LIGHT INOP IN BULL NOSE AT ROW 13.SDR 2006UALA01010Light · inoperativeEEL LIGHTS ON SEATS 8, 19, AND 25 ABC OUT.SDR 2006UALA00893Warning Message · illuminatedNR 1 ENG REV UNLOCK LIGHT ON EICAS DISPLAYED ON TAKE OFF ROLL. THE INITAL PROBLEM WAS AN ACTUATOR LEAK. PDX RPL THE ACTUATOR. THE DEPLOY PROXIMITY SENSOR NEEDS TO BE REMOVED FROM THE OFF ACTUATOR AND REINSTALLED TO THE NEW ACTUATOR BECAUSE ITS HARDWIRED TO SDR 2006UALA00863Unknown · unknownSIDEWALL PANEL LOCATED AT ROW 15F IS HOT TO THE TOUCH (SCALE OF 1-10 IT'S AN 8) JUST BELOW WINDOW AROUND EMERGENCY EXIT OVER WING DOOR. SIDEWALL LOCATED AT SEAT ROW 15F FELT HOT TO THE TOUCH. EXCESSIVE HEAT WAS CAUSED BY THE OVERWING EXIT HATCH THRESHOLD HEATSDR 2006UALA00833Unknown · unknownDIVERTED DUE TO DIFFICULTY MAINTAINING CONTROL OVER THE AFT CABIN TEMP.SDR 2006UALA00827Smoke · detectedFOUND SMOKE REPORTED IN CABIN. RECIRCULATING FAN MESSAGE. WIRE BUNDLE W4104 FOR THE RT SIDE CABIN AIR RECIRCULATION FAN SHORTED ON ADJACENT SUPPORT BRACKET. THE SUBJECT WIRE HARNESS WAS REPLACED WITH HARNESS. THE RT SIDE CABIN AIR RECIRCULATION FAN WAS ALSO SDR 2006UALA00810Skin · dentedFOUND SKIN DENTED AT STATION 1715, 2 INCHES BELOW STR 18L. THE AIRCRAFT SKIN WAS DAMAGED AT STA 1715, 2 INCHES BELOW STR 18L. THE DAMAGED SKIN WAS REMOVED AND AN EXTERNAL SKIN DOUBLER WAS INSTALLED PER EVA NUMBER UA-EVA-60253A. THIS REPAIR RECIEVED SFAR APPRSDR 2006UALA00771Skin · lightning strikeFOUND LIGHTNING STRIKE STA 460 BETWEEN S6L & 7L. REMOVED FASTENER, HFC FOUND NO CRACKS, INSTALLED SOLID FASTENER.SDR 2006UALA00770Skin · lightning strikeFOUND LIGHTNING STRIKE STATION 443 STRINGER 7L. REMOVED FASTENER, HFC FOUND NO CRACK AND INSTALLED SOLID FASTENER.SDR 2006UALA00806Actuator · malfunctionedELEV ASYM EICAS MESSAGE IS DISPLAYED. THE FAILED ELEVATOR ASYMMETRY LIMITER ACTUATOR WAS DETECTED BY THE STABILIZER TRIM/ELEVATOR ASYMMETRY MODULE (SAM). A DISCREPANCY IN THE ACTUATOR FAULT LOGIC CAUSES THE ELEV ASYM STATUS /MAINTENANCE MESSAGES TO DISPLAY. SDR 2006UALA00805Generator · failedAPU ELECTRICAL INOP. AIRCRAFT LOG INDICATED THAT THE APU GENERATOR HAD A BPCU GENERATOR TRIP MESSAGE DUE TO A DIODE FAILURE. THE APU GENERATOR WAS REMOVED AND REPLACED, OPS CHECK OK. SHOP FINDINGS INDICATED THAT THE UNIT HAS BEEN OPERATING FOR TEN YEAR AND SDR 2006UALA00809Charger · failedFOUND EMERGENCY HATCH HANDLE LIGHT AFT LAMP INOP AT SEAT 15F & 16F.SDR 2006UALA00828Slide · leakingTHE SLIDE IS LEAKING IN BETWEEN THE GIRT ON THE SEAM. THE FAILURE IS ATTRIBUTED TO WEAR DAMAGE ON LOWER TUBE SEAM OF THE INFLATABLE AT THE GIRT ATTACHMENT.SDR 2006UALA00773Smoke · detectedDIVERTED UNDER AMBER ALERT DUE TO SMOKE IN THE CABIN.SDR 2006UALA00731Apu · failedRETURNED TO DEN DUE TO INOPERATIVE GEN & LOSS OF APU EN ROUTE. APU NO START DUE TO LOW OIL PRESSURE. APU GENERATOR HOUSING CRACKED AT 12:00 POSITION. APU SHARES OIL SYS WITH GEN. LOSS OF OIL FROM CRACKED GEN HOUSING CAUSED INSUFFICIENT OIL LEVEL IN APU RESDR 2006UALA00699Skin · damagedFOUND DAMAGED SKIN AT FASTENER, LOCATION IS APPROX 9 INCHES ABOVE FWD END OF RAIN GUTTER ABOVE DOOR 2L. DAMAGE CUT OUT AND REPAIRED PER EVA UA-EVA-60232, 8100-9 PROVIDED BY BOEING, 12 MONTH DTA INFORMATION TO FOLLOW.SDR 2006UALA00661Skin · puncturedLEFT AFT FUSELAGE HAS PUNCTURE IN UNPRESSURIZED SKIN JUST BELOW SKIN LAP AND JUST FWD OF STAB COMPT ACCESS DOOR. DAMAGE WAS CUT OUT AND DOUBLER INSTALLED PER EVA 60177. A 8100-9 RECEIVED FROM BOEING. DTA INFORMATION TO FOLLOW FROM BOEING.SDR 2006UALA00582Light · inoperativeAFT CABIN EEL LIGHTS INOP FROM ROWS 23-31.SDR 2006UALA00572Skin · dentedLEFT SIDE OF FUSELAGE FWD OF NR 2 MAIN ENTRY DOOR HAS A PUNCTURE & DENT.SDR 2006UALA00564Skin · damagedTHREE AREAS OF DAMAGE FOUND FROM STATIONS 600 TO 620 ON LEFT SIDE BETWEEN STRINGERS 15L AND 20L. CAUSE OF DAMAGE - AIRCRAFT IMPACTED BY JETWAY AT DOOR 2L. SKIN AND FRAME DAMAGE WERE CUT OUT AND DOUBLERS INSTALLED PER EVA-60167 AND EVA-60176.SDR 2006UALA00542Warning Light · illuminatedDIVERTED TO PIT UNDER AMBER ALERT WITH NR 1 ENGINE SHUT DOWN DUE TO AN ENGINE OIL FILTER BYPASS EICAS MESSAGE. BUMPER BEARING FAILURE DUE POSSIBLY TO EXCESSIVE VIBRATION FROM LOWER DRIVE SHAFT. LOWER DRIVE SHAFT FAILED BALANCE CHECK PER PWA SB 72-693SDR 2006UALA00543Flap System · malfunctionedRETURN TO FIELD DUE TO A FLAP EXTENSION PROBLEM. THE TE FLAPS DISAGREE EICAS MESSAGE WAS DISPLAYED AND CAUTION LIGHT ILLUMINATED. THE TE FLAPS DISAGREE EICAS MESSAGE WAS DISPLAYED AND CAUTION LIGHT ILLUMINATED WHEN THE NR 2 FLAP/SLAT ELECTRONICS UNIT (FSEU) SDR 2006UALA00732Skin · damagedRIGHT HAND TRAILING EDGE MAIN INBD FLAP HAS PREVIOUS REPAIR COMING OFF TOP SIDE OF FLAP ACCOMPLISHED INTERIM REPAIR PER EVA UA-EVA-60124 WITH NEW PATCH RIVETED AND COVERED WITH SPEED TAPE ON TOP OF INBD MIDFLAP. MUST INSPECT EVERY 3SV. PERMANENT REPAIR MUST SDR 2006UALA00472Light · inoperativeEEL STRIP INOP AT AFT LAV.SDR 2006UALA00322Aspirator · leakingASPIRATOR FLAPPER VALVES LEAKING. ASPIRATOR WAS OBSERVED LEAKING DURING AIR RETENTION TEST. LEAK WAS DUE TO WORN ASPIRATOR FLAPPER VALVE. ASPIRATOR WAS REPLACED.SDR 2006UALA00320Warning Light · illuminatedRETURNED TO ORD DUE TO FUEL FILTER EICAS MESSAGE. REPLACED MAIN FUEL FILTER, RAN ENGINE NO FAULTS OR LEAKS, CLEARED MESSAGE. NO REPEATS SINCE EVENT. NO ADDITIONAL FINDINGS AS ENGINEERING NEVER RECEIVED THE FUEL FILTER.SDR 2006UALA00262Smoke · detectedDIVERTED DUE TO SMOKE IN THE CABIN. CHECKED RECIRC FAN, MIX MANIFOLD AND SEATS 9, 10, 11 C & D AREA FOR ANY SIGNS OF OVERHEATING OR BURNED WIRING CHECKED THESE AREAS AND ALSO APU DUCTING IN WHEEL WELL AND BEHIND SIDEWALL AND THE SEAT 9, 10 AND 11 AREA AND NO SDR 2006UALA00221Slide · leakingSLIDE FAILED AIR RETENTION TEST DUE TO LEAKING SEAM. AT COMPONENT SHOP MAINTENANCE, SLIDE FAILED AIR RETENTION CHECK DUE TO SEAM LEAK. SLIDE WAS RETURNED TO OEM FOR INFLATABLE REPLACEMENT.SDR 2006UALA02271Door Frame · crackedDOOR 2R FRAME 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 2006UALA00172Probe · brokenDIVERTED TO DEN DUE TO LEFT ENGINE PROBE HEAT INDICATION PROBLEM, NON-ICING RESTRICTION. REPLACED P2-T2 PROBE PER MM 72-21-03 AND FAULT WAS REMOVED/INDICATOR EXTINGUISHED. ENGINE RUN AFTER PT REPLACEMENT WAS CLEAR. ITEM RESURFACED ON THE 02/01/2006, AND DENSDR 2006UALA00171Fan · failedDIVERTED TO ORD DUE TO ELECTRICAL ODOR IN THE CABIN. REPLACED RIGHT RECIRC FAN. OPS CHECK OK.
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