Boeing 757-222

Service difficulty reports · 15,539

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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.

SDR 2001UALA00277Floorbeam · damagedCABIN FLOORBEAM WEB STA 324 RBL 44 HAS OVERSIZED HOLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUB AND T-CAP REPAIR PER SRM.Mar 19, 2001 · N506UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2001UALA00273Skin · dentedFUSELAGE SKIN DENTED AT STA 1600 BETWEEN STR 19LT AND 20LT. MAJOR REPAIR ACCOMPLISHED.REPAIRED SKIN PER SRM.Mar 19, 2001 · N501UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2001UALA00269Frame · gougedGOUGE IN FRAME AT STA 1500 STR 26L. 35 PERCENT MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME AT STA 1500 STR 26L PER SRM.Mar 17, 2001 · N506UA · Boeing 757222 · Fuselage Main, FrameSDR 2001UALA00519Floorbeam · crackedMID CABIN FLOORBEAM WEB STA 700 LBL 25 CRACKED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLERS ON FLOORBEAM PER SRM.Mar 15, 2001 · N509UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2001UALA00517Stringer · tool damageAFT PIT RT SIDE STR 27 STA 1590 HAS TOOL DAMAGE. MAJOR REPAIR ACCOMPLISHED.INSTALLED STRINGER SPLICE PER SRM.Mar 15, 2001 · N509UA · Boeing 757222 · Fuselage Main, Longeron/StringerSDR 2001UALA00260Chip Detector · leakingSTATUS MESSAGE, APU LOW OIL QTY DISPLAYED. APU SHUTDOWN. LEFT GENERATOR DEFERRED. SUPPLEMENTAL DATA UPDATE FOUND COMPRESSOR BEARING CHIP DETECTOR BODY LEAKING. REPLACED CHIP DETECTOR ASSEMBLY, SERVICED AND LEAK TESTED OK.Mar 15, 2001 · N541UA · Boeing 757222 · APU Oil SystemSDR 2001UALA00515Frame · dentedAFT PIT LT FRAME STA 1400 STR 28L TOP OF FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE PER MM.Mar 13, 2001 · N509UA · Boeing 757222 · Fuselage Main, FrameSDR 2001UALA00248Skin · damagedFUSELAGE REPAIR DOUBLER AT STA 1300 STR 24L DOES NOT MEET MINIMUM FASTENER SPACING. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED SKIN PER SRM.Mar 12, 2001 · N507UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2001UALA00247Stringer · tool damageMAJOR REPAIR. STR 24L STA 1296 - 1304 HAS TOOLING DAMAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SRM.Mar 12, 2001 · N507UA · Boeing 757222 · Fuselage Main, Longeron/StringerSDR 2001UALA00232Skin · damagedMAJOR REPAIR. DAMAGE TO FUSELAGE SKIN AND STRINGER AT CREASE BEAM STA 600 - 630 ON LEFT SIDE AT FLOOR LINE. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FUSELAGE SKIN AND STRINGER PER SRM.Mar 12, 2001 · N507UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2001UALA00219Skin · crackedNR 2 ENGINE PYLON IB SKIN CRACKED AT FWD LIGHTING HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED SKIN PER MAINTENANCE MANUAL.Mar 11, 2001 · N542UA · Boeing 757222 · Nacelle/Pylon, Plate/SkinSDR 2001UALA00217Bulkhead · crackedMAJOR REPAIR. NR 1 PYLON INNER WEB CASTING AT NAC STA 191.86 IS CRACKED AND DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED BULKHEAD.Mar 9, 2001 · N507UA · Boeing 757222 · Nacelle/Pylon, Bulkhead/FirewallSDR 2001UALA00218Connector · broken120 KTS STBY BUS OFF LIGHT ILLUMINATED. SELECTED STBY POWER SELECTOR TO BATTERY, OFF LIGHT WENT OUT AND DISCHARGE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE REPLACED BROKEN CONNECTOR AT DC STANDBY BUSS OFF CIRCUIT BREAKER 6A3. (BOEING SPEC BACC45FT18-8P7)Mar 8, 2001 · N593UA · Boeing 757222 · DC Power Distribution SystemSDR 2001UALA00201Transmitter · failedFLAP CONFIGURATION WARNING ON TAKEOFF. REJECTED TAKEOFF AT 95 KTS, FLAPS AT 15. *S/D* FAILED RIGHT TRAILING EDGE FLAP TRANSMITTER. REPLACED SAME AND OPS CHECKED NORMAL.Mar 7, 2001 · N510UA · Boeing 757222 · Trailing Flap Position Indicating SystemSDR 2001UALA00211Floorbeam · corrodedMAJOR REPAIR. FWD GALLEY TIE DOWN SUPPORT BEAM STA 324 TO 345 RBL 2 HAS EXCESSIVE MATERIAL LOSS, MEASURES .018 LOSS ON .110 ORIGINAL THICKNESS. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT BEAM PER SRM.Mar 7, 2001 · N507UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2001UALA00210Floor Support · corrodedMAJOR REPAIR. FWD GALLEY FLOOR SUPPORT CHANNEL STA 310 - 324, RBL 39-41 IS CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT CHANNEL.Mar 7, 2001 · N507UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2001UALA00209Floor Support · corrodedMAJOR REPAIR. FWD GALLEY FLOOR CHANNEL CORRODED STA 331 - 333 RBL 5-21. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT PER SRM.Mar 7, 2001 · N507UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2001UALA00208Frame · crackedFWD PIT FRAME IS CRACKED AT STA 540 BETWEEN STR 24L AND 25L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER SRM.Mar 7, 2001 · N507UA · Boeing 757222 · Fuselage Main, FrameSDR 2001UALA00207Floor Support · corrodedFWD CABIN FLOOR SUPPORT CHANNEL CORRODED FROM UNDER DOOR DRAIN PAN STA 324-344 RBL 58-60. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.Mar 7, 2001 · N507UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2001UALA00206Intercostal · crackedAFT CABIN CENTER LINE INTERCOSTAL CRACKED BETWEEN STA 1580 TO 1600. *S/D* MAJOR REPAIR ACCOMPLISHED. L-ANGLE REPLACED.Mar 7, 2001 · N507UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2001UALA00205Frame · corrodedRIGHT CREASE BEAM INNER CHORD STA 324 AT RBL 61 HAS EXESSIVE MATERIAL REMOVED, (25 PERCENT) .018 FRAME, .071 CHORD ANGLE. REF SRM 51-40-02. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE.Mar 6, 2001 · N507UA · Boeing 757222 · Fuselage Main, FrameSDR 2001UALA00204Intercostal · damagedCABIN FLOOR INTERCOSTAL REQUIRES REPLACEMENT STA 365 TO 377, RBL 57. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL PER SRM.Mar 6, 2001 · N507UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2001UALA00203Floor Support · corrodedMAJOR REPAIR. GALLEY FLOOR SUPPORT CORRODED WITH EXCESSIVE MATERIAL REMOVED STA 331 TO 333, RBL 25 TO 37. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.Mar 6, 2001 · N507UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2001UALA00198Skin · tornLOWER FUSELAGE SKIN TORN APPROX 10 INCHES BY 1.5 INCHES TWO FEET AFT OF E&E COMPARTMENT DOOR. STATION 510 BETWEEN S-27L AND S-28L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. ACCOMPLISHED SKIN REPAIR AND INSTALLED EXTERNAL DOUBLER REPAIR.Mar 4, 2001 · N598UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2001UALA00179Intercostal · corrodedMAJOR REPAIR. CABIN INTERCOSTAL CORROSION BS 1638 TO 1640 RBL 13. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL PER SRM.Mar 4, 2001 · N507UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2001UALA00178Floorbeam · corrodedMAJOR REPAIR. CABIN FLOORBEAM T-CAP CORROSION BS 1640 FROM LBL 9 TO RT SIDE CREASE BEAM. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP.Mar 4, 2001 · N507UA · Boeing 757222 · Fuselage Main, Floor BeamSDR 2001UALA00180Oven · contaminatedCABIN CREW REPORT FLAMES IN FORWARD GALLEY. SUPPLEMENTAL DATA UPDATE FLAMES IN GALLEY OVEN CAUSED BY PAPER STUCK IN VENT. REPLACED OVEN. NO DAMAGE TO AIRCRAFT.Mar 2, 2001 · N521UA · Boeing 757222 · Buffet/GalleysSDR 2001UALA00168Plate · corrodedAFT DECK PLATE STA. 1681 BLENDED EXCESSIVELY RBL 39, 40, 46.5-47.5, 50-52. CORROSION STILL EXISTS AROUND REVET HOLES AT RBL 47. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED DECK PLATE.Feb 28, 2001 · N507UA · Boeing 757222 · Fuselage Main, StructureSDR 2001UALA00176Frame · dentedFWD PIT FRAME FLANGE IS DENTED STA 600 BETWEEN STR 23L ABD 24L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER SRM.Feb 28, 2001 · N507UA · Boeing 757222 · Fuselage Main, FrameSDR 2001UALA00167Intercostal · crackedSTA 1200 - 1220 BL 0 INTERCOSTAL CRACKED SEVERAL PLACES. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER ANGLE TO INTERCOSTAL.Feb 28, 2001 · N507UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR 2001UALA00150Module · failedON FINAL APPROACH FLAPS 15 USING SPEEDBRAKE AIRCRAFT EXPERIENCED SIGNIFICANT ROLL RATE TO RIGHT WHEN USING LAST 2 INCHES OF SPEEDBRAKE TRAVEL. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED SPOILER CONTROL MODULE BITE TEST. FAULT BALLS NR 1 AND NR 3 DISPLAYED. ACCOMPLIFeb 27, 2001 · N506UA · Boeing 757222 · Drag Control SystemSDR 2001UALA00133Controller · defectiveRIGHT DUCT PRESSURE FLUCTUATING BETWEEN 25 PSI AND 40 PSI. EPR FLUCTUATES BETWEEN 1.16 AND 1.28 FL410. *S/D* REPLACED THE RT PRSOV AND PRSOV CONTROLLER. PROBLEM WAS MOST LIKELY CAUSED BY THE PRSOV CONTROLLER.Feb 20, 2001 · N565UA · Boeing 757222 · Compressor Bleed GovernorSDR 2001UALA00121Wire · damagedELECTRICAL SPARKS SEEN IN REAR GALLEY. *S/D* N43 CABLE FROM CONTROLLER TO CART WAS CRUSHED AND CABLE WAS DISCONNECTED FROM CONTROLLER CAUSING SPARKS IN THE REAR GALLEY. CABLE AND PIGTAIL DISCONNECT WERE REPLACED.Feb 17, 2001 · N582UA · Boeing 757222 · Equipment/Furnishings WiringSDR 2001UALA00099Skin · dentedEXTERNAL FUSELAGE DENTED-CREASED AT FUSELAGE STATION 560 BETWEEN STRINGER 26LT AND STRINGER 26. SUPPLEMENTAL DATA UPDATE DAMAGE WAS CUTOUT IN THE LOWER SKIN MEASURING 5.5 LONGITUDINALLY BY 14.25 CIRCUMFRENTIALLY, SPANNING FROM THE S-26L LAP SEAM TO ONE FASTENEFeb 11, 2001 · N538UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR 2001UALA00088Transformer · failedSPOILER EICAS AND OVERHEAD LIGHTS ILLUMINATED. FLIGHT LEVEL 380. *S/D* FAULTY RVDT ON SPOILER PCA CAUSING EICAS MESSAGE. REPLACED ROTARY VARIABLE DIFFERENTIAL TRANSFORMER ON SPOILER PCA NR 6 AND NR 7.Feb 5, 2001 · N547UA · Boeing 757222 · Drag Control SystemSDR 2001UALA00090Guide · looseDOOR 2 LEFT IS HARD TO OPEN. *S/D* GUIDE ARM PIN WAS FOUND LOOSE DURING TROUBLESHOOTING. NEW GUIDE ARM WAS INSTALLED AND ADJUSTED.Feb 5, 2001 · N548UA · Boeing 757222 · Passenger/Crew DoorsSDR 2001UALA00067Hose · leakingLEFT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. GEAR EXTENDED PRIOR TO SYSTEM DEPLETION. FLAPS EXTENDED WITH ALTERNATE SYSTEM. *S/D* REPLACED LEFT GEAR DOWNLOCK PRESSURE LINE.Jan 31, 2001 · N534UA · Boeing 757222 · Hydraulic System, MainSDR 2001UALA00058Connector · damagedLEFT ENGINE CONTROL MESSAGE DISPLAYED 3 HOURS INTO FLIGHT. *S/D* REPLACED EEC ALTERNATOR AND CONNECTOR D4858 ON EEC. EEC ALTERNATOR STATOR WAS REPLACED PRIOR TO DEPARTURE FOR MESSAGES. THREE HOURS INTO OUTBOUND FLT MESSAGE REOCCURRED. FOUND TWO PINS PUSHEJan 27, 2001 · N545UA · Boeing 757222 · Fuel Control/Turbine EnginesSDR 2001UALA00056Actuator · failedNOSE GEAR FAILED TO EXTEND ON APPROACH. GEAR EXTENDED WITH ALTERNATE SYSTEM. *S/D* REPLACED NOSE GEAR UPLOCK ACTUATOR.Jan 25, 2001 · N567UA · Boeing 757222 · Landing Gear ActuatorSDR 2001UALA00057Relay · failedVARIOUS EICAS MESSAGES, FLAP ISOLATION STATUS, RUDDER RATIO, MACH SPEED TRIM, STAB TRIM, ANTISKID AUTOBRAKE. *S/D* FAILURE OF TWO RELAYS, (LISTED BELOW), CAUSED THE EICAS MESSAGES TO APPEAR. VERIFICATION FLIGHT CONFIRMED ALL SYSTEMS NORMAL AFTER REPLACEMENTJan 25, 2001 · N590UA · Boeing 757222 · Trailing Edge Flap Control SystemSDR 2001UALA00048Duct · failedAT 12,00FT IN CRUISE RIGHT PACK STOPPED OPERATING. *S/D* REMOVED AND INSTALLED RT EXTRACTOR DUCT AND LEAK CHECKED. FAILED WELD JOINT ON DEFECTIVE DUCT.Jan 22, 2001 · N549UA · Boeing 757222 · Air Distribution SystemSDR 2001UALA00040Window · leakingLOUD SQUEAL FROM WINDOW 2 LEFT. *S/D* PRESSURE SEAL WAS REPLACED PER MM 56-11-53 AND WINDOW ADJUSTED PER MM 56-11-02 WHEREIN, VERTICAL UP AND FORWARD CLEARANCES WERE FOUND WITHIN LIMITS. SUBSEQUENT PRESSURIZATION TO A DIFFERENTIAL PRESSURE OF 8.0 PSI, REJan 20, 2001 · N583UA · Boeing 757222 · Flight Compartment WindowsSDR 2001UALA00119Windshield · crackedRIGHT WINDSHIELD OUTER PANE CRACKED. RIGHT WINDOW HEAT EICAS MESSAGE. *S/D* WINDOW FINDINGS: 1) SLIGHT MOISTURE INGRESSION ON UPPER BUS BAR BY SENSOR WIRES. 2) BUS BARS IN GOOD CONDITION, SLIGHT DISCOLORATION. 3) HUMP SEAL REPAIR HISTORY, MINIMAL EROSION, BJan 16, 2001 · N573UA · Boeing 757222 · Flight Compartment WindowsSDR 2001UALA00032Tire · separatedNUMBER 2 REAR LT MLG TIRE TREAD SEPARATED AND WAS INGESTED INTO THE NUMBER 1 ENGINE ON TAKEOFF. *S/D* SUBSEQUENT INVESTIGATION REVEALED THAT THE NR 2 FWD TIRE ENCOUNTERED FOD ON THE RUNWAY AND THREW IT BACK TO THE NR 2 REAR TIRE. THE NR 2 REAR TIRE SUBSEQUEJan 16, 2001 · N561UA · Boeing 757222 · TireSDR 2000UALA00797Service difficultyDOOR 1L OPENED WITH SLIDE ARMED, DOOR STOPPED LESS THAN HALF WAY OPEN. CHAINS ON BOTTOM OF SLIDE RESTRAINED DOOR FROM OPENING FURTHER.Dec 19, 2000 · N538UA · Boeing 757222 · Escape SlideSDR 2000UALA00794Lever · failedAFTER TAKEOFF UNABLE TO RETRACT GEAR. *S/D* REPLACED LANDING GEAR CONTROL LEVER MODULE.Dec 15, 2000 · N511UA · Boeing 757222 · Landing Gear SelectorSDR 2000UALA00793Idg · failedLEFT GENERATOR FAILED 10 MINUTES AFTER DEPARTURE. *S/D* REPLACED IDG. SHOP FINDINGS, THE ROTOR FAILED TEST. UPON FURTHER TESTING AN OPEN CIRCUIT WAS FOUND IN THE EXCITER ROTOR. ALSO, THE UNIT WAS FOUND TO BE LEAKING AT THE TERMINALS. THE TERMINAL SEALS WDec 15, 2000 · N551UA · Boeing 757222 · Alternator-Generator DriveSDR 2000UALA00789Fitting · misinstalledUPON GEAR EXTENSION, NOSE GEAR DOWNLOCK GREEN LIGHT NOT ILLUMINATED. EICAS MESSAGE, GEAR DISAGREE STATUS, NOSE GEAR DISAGREE GEAR MONITOR. *S/D* REMOVED 1/8 DIAMETER PRESS FIT ZERK FITTING. FITTING WAS FOUND AT THE LOCK LINK OVERCENTER JOINT WHICH PREVENTEDec 12, 2000 · N511UA · Boeing 757222 · Landing Gear Retraction/Extension SystemSDR 2000UALA00777Fan · failed'EQUIPMENT OVERHEAT' EICAS MESSAGE FOLLOWED BY ADI BACKGROUND TURNING BLACK. SUPPLEMENTAL DATA UPDATE THE AIRCRAFT EXPERIENCED A LEFT RECIRCULATION FAN FAILURE. AFTER BEING DEFERRED, THE EQUIPMENT COOLING CIRCUIT BREAKERS WERE NOT RESET. THIS CAUSED THE EQUDec 6, 2000 · N566UA · Boeing 757222 · Air Distribution FanSDR 2000UALA00776Control Unit · contaminatedALTERNATE EXTEND MOTOR CIRCUIT BREAKER POPS WHEN GEAR DOOR OPEN SWITCH ACTUATED. *S/D* FOUND INTERNAL MECHANISM OF POWER PACK CORRODED AND FULL OF WATER AND SKYDROL. REPLACED ALTERNATE EXTENSION POWER PACK.Dec 4, 2000 · N505UA · Boeing 757222 · Landing Gear Retraction/Extension System
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