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 UALA2010050601522Lanyard · faultyUNABLE TO ARM DOOR 1R. RESTOWED SLIDE LANYARD.SDR UALA2010050501517Connector · looseLAST SECTION OF EMERGENCY LIGHT IN AFT CABIN DOESN'T LIGHT UP AND THE LAST 8 IN OF COVER IS MISSING. SECURED LOOSE CONNECTOR. OPS CHECK OK.SDR UALA2010050501515Connector · damagedEMERGENCY LIGHT AT THE FWD AFT LAV INOPERATIVE. SECURED LIGHT CONNECTION.SDR UALA2010050501514Wire · damagedEMERGENCY LIGHT AT THE MID LAV INOPERATIVE. MADE PERMANENT REPAIR TO LIGHT ASSY PIGTAIL.SDR UALA2010050501513Lamp · inoperativeENTRY DOOR NR 2 LT AND NR 4 RT EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED, CKS GOOD.SDR UALA2010050501509Skin · dentedFUSELAGE DENTED AFT OF DOOR 2L, AT STA 760, 9" ABOVE WL. MAJOR REPAIR ACCOMPLISHED: DENT IS 1"W BY .200" D, IS SMOOTH, NO GOUGES OR CRACKS. DENT IS NOT ON ANY FRAMES OR STRINGERS. REMOVED DAMAGE AND ACP HFEC INSP TO VERIFY CUT OUT CRACK FREE. FABRICATED DOUBSDR UALA2010050401499Power Supply · inoperativeEMERGENCY LIGHT ABOVE 21ABC INOP DURING TEST. REPLACED M735 EMERGENCY LIGHTS PWR SUPPLY, LITE OPS RETURNED TO NORMAL DURING TEST.SDR UALA2010050301492Display · faulty1 NR ENG PRIMARY CONTROL EICAS MSGS AND BLANKING EPR. REPLACED LT PDIU. REPLACED THE NR 1 ENGINE PMA AND TESTED IAW MM.SDR UALA2010050301485Duct · leakingAFT CABIN EXTREMELY HOT. TEMP SHOWS 70 DEG COCKPIT & FWD CABIN SHOW 73 DEG FOUND AT ROW 17C AND 18C AIR DUCT HAS A LARGE LEAK AND NO COOL AIR FLOWING BEYOND ROW 20. REPAIRED REF MM21-23-01, LEAK CK GOOD.SDR UALA2010050301468Actuator · faultyRUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. SAMC TEXT: AFTER CONSULTING SFOEG SUGGEST RPL RUDDER TRIM ACTUATOR. REPLACED AIL & RUDDER TRIM CONTROL MODULE, NO HELP. NEEDS FURTHER T-S. REPLACED RUDDER TRIM ACTUATOR. OP CKS GOOD. INSPECTED ACTUATOR INSTALLSDR UALA2010043001453Lamp · inoperativeDOOR NR 4 LT EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED, OPS CK GOOD.SDR UALA2010043001452Radome · damagedBIRD STRIKE ON RADOME. COMPLETED BIRD STRIKE INSP 05-51-18-201 AND CLEANED RADOME REF 12-25-00. FOUND SEGMENTED L IGHTING DIVERTER STRIP DISBONDED AT STA 166 0N UPPER RT OF RADOME MISSING PAINT ABOUT 1. NO OTHER DAMAGE FOUND REF MM 53-12 -03 P 201 PAR 2(A). SDR UALA2010042901447Line · leakingNR 1 ENG LEAKING HYD FLUID. FOUND HYD SUPPLY LINE FOR NR 1 REVERSER, MFG NEW LINE, PRESSURE TESTED LINE. INSTALLED LINE, LEAK CHECKED GOOD.SDR UALA2010042901445Compressor · stalledENG COMPRESSOR STALL IN FLIGHT. ENG POSITION UNKNOWN. ENG RECOVERED AND CONTINUED OPERATING. IMMED PRECEDING STALL, ENG POWER WAS ACCELERATING AT CRUISE OR CLIMB POWER. SELF CLEARING COMP STALL. ACP STALL CHECKS ON BOTH ENGS. CREW DEBRIEF- AT 3000FT AFTER TSDR UALA2010042901441Nose Cowl · dentedRAMP REPORTED DENT IN NR 2 ENG NOSE COWL 6 O'CLOCK POSITION. EVALUATED DENT APPROX DIMENSIONS ARE 3.5 IN L X 2 IN W .090 DEPTH BEYOND ALLOWABLE LIMITS. APPEARS TO BE PREVIOUS REPAIR. IAW UA-EVA-73731 PERFORMED EDDY CURRENT (HFEC) INSP. NO DEFECTS NOTED. NOSDR UALA2010042901440Skin · damagedLIGHTING STRIKE BLENDED AT STR 4L AND STA 648.5 DAMAGE MEASURES .375 WIDE BY 1.687 INCH LONG. SKIN THICKNESS MEASURES .050 IN UNBLENDED AREA, BLENDED AREA REMAINING THICKNESS MEASURES .033, TOTAL OF .017 MATERIAL MISSING. DAMAGE IS .250 BELOW SKIN LAP. REPAIRSDR UALA2010042901435Transceiver · failedLEFT HF DOES NOT TRANSMIT. REPLACED LEFT TRANSCEIVER AND OPS CHECKED OK.SDR UALA2010042901433Windshield · damagedL1 WINDOW HAS BURN MARK AT TOP & SAW BRIEF SPARK WHEN WINDOW HEAT TURNED OFF. NO TIME TO TROUBLESHOOT. VISIBILITY NOT AFFECTED. OK FOR SVC. REPLACED WINDSHIELD. L1 WINDOW NEEDS 1EA FASTENER INSTALLED AT WINDOW FRAME. REPLACED FASTENER. REPLACED SEALANT AS SDR UALA2010042801422Hydraulic Line · leakingDURING EXTERNAL CHECK FOUND HYD LEAK AT THE PRESSURE HYD LINE FROM THE RIGHT BRAKE STABILIZER CONTROL BMS UNIT. REPLACED RIGHT HYD HORIZONTAL STAB TRIM CONTROL LINE P/N 271N6482-1116. OPS CHECK HORIZONTAL STAB. OPS CHECK NORMAL, NO LEAKS NOTED.SDR UALA2010042801419Skin · damagedLT MAIN GEAR STRUT DOOR HAS DAMAGE ON L/E AT MID POINT WITH SKIN MISSING AND OPEN TO CORE FOAM. OPEN AREA IS 4 BY 1-2 WITH L SHAPED CRACK 2 INCH BY 1 INCH AT LWR EDGE OF DAMAGE CONT OF AMIS ITEM 4482001. ACP INTERIM REPAIR PER EVA -73721, TAPE RECHECK REQUIRSDR UALA2010042801415Light · inoperativeLEFT WHEEL WELL UNSAFE LIGHT INOPERATIVE. REPLACED LAMP, OPS GOOD.SDR UALA2010042801414Fuse · faultyAFT CARGO DOOR EXTERIOR EMERGENCY EVACUATION LIGHT INOP. REPLACED LAMP, NO HELP. REPLACED FUSE P/N FU305 IN M10699, CHECKS OKAY.SDR UALA2010042901434Motor · faultyHYD GEN MOTOR TEST FAILED. SUSPECT HYD MOTOR GCU M10622. REPLACED HYD SHUTOFF VALVE IAW MM, OPS TESTED SYS, VALVE & PUMP OPS GOOD, NO INDICATION ON HYD PAGE LOWER EICAS. STILL FAILED TEST. DURING TROUBLESHOOTING, HYD GEN ON & HYD GEN VALVE NOT SHOWN ON LOWERSDR UALA2010042801408Chiller · faultyCREW REPORTS ELECTRICAL ODOR IN CABIN AROUND ROWS 28-34. INVESTIGATE AND REPORT FINDINGS TO SAMC. CHECKED ALL CABIN, GALLEY AND LAV LIGHTS. CHECKED ALL GALLEY EQUIP AND FOUND AFT GALLEY CHILLER CAUSING ODOR. PULLED CHILLER CBS AND INOP PER MEL. INSTALLEDSDR UALA2010042801425Ballast · overheatedCREW REPORTS STRANGE NON ELECTRIC TYPE ODOR ONLY IN FWD LAV. FOUND MIRROR LIGHT IN FWD LAV INOP. FURTHER INVESTIGATION FOUND LAV MIRROR LIGHT BREAKER OUT ON P34 PANEL, VERIFIED ALL LAV MIRROR LIGHTS INOP. CHECKED FWD LAV, NO ODOR PRESENT. ALL AFFECTED LIGHSDR UALA2010042701403Panel · corrodedCORROSION ACB BULK CARGO AREA AT LAV SERVICE PANEL PAN AROUND DUCT UNDER TANK. REPLACED LAV SERVICE PANEL. ACFT PRIMARY STRUCTURE IS OK. WORK WAS ACP ON PEMCO NR 2012N00376 AND INSP BY QC 802.SDR UALA2010042701395Wire · damagedE+E BAY UNDER FLOOR AFT OF P-31 AND P-32 PANELS, WIRES HAVE SIGNS OF ARCING. ACP SMC003 CUT OUT ARCH DAMAGE AND SPLICED WIRE TOGETHER WITH COLD SHRINK SLEEVE.SDR UALA2010042601387Generator · faultyAPU GEN UNABLE TO CONNECT AT ENGINE SHUTDOWN. REPLACED APU GENERATOR AND FEEDER HARNESS ASSY. APU GENERATOR POWER FEEDER CABLES BURNED AND MELTED AT APU GENERATOR TERMINAL BLOCK. REPLACED FEEDER CABLE ASSY. OPS CHECKS GOOD ALL GEN OUTPUTS NORMAL AT RUN.SDR UALA2010042601375Elevator · damagedLT ELEVATOR DAMAGE AT TRAILING EDGE. LT ELEVATOR REMOVED. COMPLETED ELEVATOR INSTALLATION. INSTALLED STATIC WICKS ON NEW LEFT ELEVATOR.SDR UALA2010042601370Landing Gear · malfunctionedCREW REPORTED NOSE GEAR DID NOT EXTEND WITH ALTERNATE EXTEND SWITCH ON (3) ATTEMPTS. PERFORMED LANDING ALT EXTENSION CHECK WITH ACFT ON JACK, TESTED ALT GEAR EXTENSION 3 TIMES, OPS CHECK IS GOOD, ACFT WILL BE ON TEST FLT AND WILL BE VERIFIED BY EG CREW. WORK SDR UALA2010042601392Blade · damagedRIGHT ENG HAS ONE DAMAGED FAN BLADE. REPAIRED NR 2 ENG FAN BLADE IAW MM. EDDY CURRENT INSP ACP'D. NO DEFECTS FOUND. RPR WITHIN LIMITS FOR CONTINUING SERVICE.SDR UALA2010042601386Gcu · faultyGENERATOR CONTROL UNIT REQUIRES REPLACEMENT. REPLACED GENERATOR CONTROL UNIT.SDR UALA2010042601373Computer · faultyHIGH ELEVATOR FORCES. REMOVED FAULTY FEEL COMPUTER. FOUND TWO AIR LINES LOOSE ON THE OFF UNIT. REPLACED ELEVATOR FEEL COMPUTER. ACCOMPLISHED A VALIDATION TEST FLIGHT TO DETERMINE THAT INFLT ELEVATOR FORCES ARE NORMAL. TEST FLIGHT WAS SUCCESSFUL.SDR UALA2010042601388Bearing · wornDOOR 3R CANNOT CLOSE, UPPER AFT GUIDE FITTING IS DAMAGED, UPPER AFT GUIDE ROLLER HITS FITTING ON SIDE AND ROLLER IS DAMAGED. FOUND GUIDE ARM BRG WORN. REPLACED GUIDE ARM AND UPPER AFT LATCH BRG. BLENDED DMG ON GUIDE FITTING. RIGGED DOOR IAW AMM. DOOR OPERATSDR UALA2010042101331Reservoir · dischargedDOOR 2R EMERGENCY POWER RESERVOIR REQUIRES REPLACEMENT DUE TO SLIDE DEPLOYMENT. REPLACED RESERVOIR.SDR UALA2010042201349Valve · faultyLT THRUST REVERSER WOULD NOT DEPLOY. REPLACED NR1 THRUST REV DIRECTIONAL CONTROL VALVE. OPS CHECK GOOD.SDR UALA2010042201339Bottle · lowCREW O2 LOW. 1340, BEFORE SERVICING. SERVICED TO NORMAL.SDR UALA2010042201337Attach Fitting · unknownDOOR 4 LT & RT DOOR STOP TEE CLIP. ACP COA NR 506902 ON TASK CARD NR 5C0690201.SDR UALA2010042101336Cover · crackedCREW REPORTED OF FWD LT PAX WINDOW FRAME FELL OFF. FOUND COVER OVER LT OVERWING EXIT DOOR HANDLE SECURED ONLY BY LANYARD. COVER FOUND CRACKED NOT ALLOWING COVER TO SNAP SECURELY IN PLACE. PERFORMED INTERIM REPAIR OF CRACK ON INSIDE OF COVER WITH TAPE, COVER SDR UALA2010042001316Door · bindingDOOR 2L WILL NOT OPEN FROM OUTSIDE WITHOUT ASSISTANCE. YOU CAN BOUNCE THE DOOR HARD TO GET IT TO BREAKOVER AND OPEN OR PUSH FROM INSIDE. ALSO HAS A POPPING SOUND. IT STICKS IN THE HALFWAY OPEN POSITION. DOOR 2R REMOVED FOR REPAIRS. WORKING HINGE REPLACEMENT OSDR UALA2010042001314Actuator · faultyCABIN PRESSURIZATION OUTFLOW VALVE WILL NOT CLOSE IN MANUAL MODE. REPLACED FAULTY OUTFLOW VALVE ACTUATOR, OPS CK NORMAL.SDR UALA2010042001311Stator · faultyRT ENGINE PRI CONT STATUS MSG. AUTO THRT DISCONNECTED SEVERAL TIMES AS REPR BLANKED. READ EPCS MESSAGES AND FOLLOW FIM 73-21-00 FIG 114. COPY FAXED TO OPS. EPCS MSGS ARE P PDIU EEC, S PDIU EEC AND S 274-18.CHECKED ENG NR 2 CLEARED MSGS, REPLACED PMA. REPLACESDR UALA2010042001315Structure · unknownDOOR 4 LT & RT DOOR STOP TEE CLIP. ACP COA 506902 ON TASK CARD 5C0690201 BY INSP Q816. NO CRACKS FOUND.SDR UALA2010042001307Lens · dislodgedEXIT SIGN OVER 2L FELL OFF. LENS FOUND UNSECURE. REPLACED EXIT SIGN LENS. OK FOR SERVICE.SDR UALA2010042001306Skin · dentedRT HORIZONTAL STAB LOWER SKIN DENTED. DENT ON LOWER SKIN 41.5" OTBD OF FUSELAGE AND 12" AFT OF L/E. DENTS ARE BETWEEN AUX SPAR AND FRONT SPAR. MOST FWD DENT MEASURES 1.5" LONG BY 1.125 IN WIDTH. AFT DENT 1.250 LONG BY 1" WIDE. DENTS HAVE APROX. .250" SEPARATIOSDR UALA2010041901302Actuator · failedRUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. CREW COMMENTS: INTERMITTENTLY INOPERATIVE. REPLACED RUDDER TRIM ACTUATOR. ACCOMPLISHED TRIM TEST, ALL OPERATIONS AND INDICATIONS NORMAL. DURING RUDDER TRIM INDICATION TEST NOTICED RUDDER TRIM INDICATOR IN THE PESDR UALA2010041901291Line · leakingCTR HYD QTY LIGHT AND EICAS ILLUMINATED. CTR HYD FLUID IS LOW. FLUID LEAKING FROM PINHOLE LEAK ON ONE OF THE SUPPLY LINES ON THE ELEVATOR CONTROL VALVES ON THE ELEVATOR TORQUE BOX. LEAK WILL FUMIGATE TAIL AREA WITH JUST PRESSURE ON CTR HYD SYS. WITH NO MOVSDR UALA2010041901288Valve · shortedLANDING GEAR ALTERNATE EXTENSION MOTOR CONTINUED TO RUN. PULLED C-B TWICE AND RESET BOTH TIMES MOTOR RAN AGAIN. PULLED AND LT PUMP BREAKER OUT. REPLACED RT GEAR DOOR ACTUATOR UNLOCK SOLENOID SHORTED. ALL OPS NORMAL.SDR UALA2010041901287Battery Pack · inoperativeLT EXTERIOR EMERGENCY EVACUATION LIGHT AFT OF WING INOPERATIVE. REPLACED BATTERY M735 AND CKD OK.SDR UALA2010041901285Lamp · inoperativeRIGHT MLG WHEEL WELL UNSAFE LIGHT INOPERATIVE. REPLACED LAMP, OPS GOOD.
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