Boeing 767-322

Service difficulty reports · 11,768

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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 = '767322'
  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 2006UALA01253Bushing · migratedNLG ACTUATOR SUPPORT BEAM-FWD SUPPORT LINK-LOWER FUSE PIN HAS MIGRATING BUSHINGS LT AND RT SIDES AT BULKHEAD FITTING. REPLACED 2 EA. 141T2914-1 BUSHINGS PER MM 32-21-04 AND GN-MM 1-0-1-013. NOSE GEAR EXTENSION AND RETRACTION TEST PERFORMED PER 32-34-00 AND LEJun 23, 2006 · N662UA · Boeing 767322 · Nose/Tail Landing Gear Attach SectionSDR 2006UALA01231Cone · delaminatedRETURN TO FIELD DUE TO LT ENGINE COMPRESSOR STALL. COMPRESSOR SURGE WAS CAUSED BY A DELAMINATION OF THE FAN SPINNER CONE. KEVLAR AND FIBERGLASS FROM THE SPINNER ENTERED THE CORE, AND DAMAGED NUMEROUS FAN BLADES. PWA SERVICE BULLETIN PW4ENG 72-594 INTRODUCEJun 21, 2006 · N646UA · Boeing 767322 · Turbine Engine Compressor SectionSDR 2006UALA01230Clamp · strippedRT OVERWING SLIDE CYLINDER CLAMPS ARE STRIPPED. REMOVED AND REPLACED SLIDE CYLINDER CLAMPS. OK FOR RETURN TO SERVICE. ROOT CAUSE WAS SUSPECTED TO BE OVER TORQUING OF SLIDE CYLINDER CLAMPS DUE TO IMPROPER MAINTENANCE TRAINING.Jun 21, 2006 · N662UA · Boeing 767322 · Escape SlideSDR 2006UALA01194Skin · ground damageAIRCRAFT WHILE AT GATE RECEIVED APPROX A ONE FOOT BY 2 FOOT HOLE IN THE FUSELAGE BY THE BAGGAGE CART. REPAIRED DAMAGED FRAME WEB. DYE CHECKED FAIL SAFE CHORD AND AREA AND FOUND NO CRACKS.Jun 17, 2006 · N653UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR 2006UALA01190Spring · shearedRIGHT DOWN LOCK SPRING ON NOSE LANDING GEAR SHEARED. REPLACED DEFECTIVE SPRING DUE TO WEAR WAS BEYOND LIMIT.Jun 14, 2006 · N663UA · Boeing 767322 · Landing Gear Retraction/Extension SystemSDR 2006UALA01223Bearing · unserviceableFOUND THREE (3) DAMAGED BEARINGS. EXCESSIVE TENSION ON THE TENSION ROD. REPLACED DAMAGED BEARINGS. AIRCRAFT RETURNED TO SERVICE. ROOT CAUSE WAS EXCESSIVE TENSION BUILT IN DURING SLIDE ASSEMBLY.Jun 8, 2006 · N665UA · Boeing 767322 · Escape SlideSDR 2006UALA01222Aspirator · unserviceableDAMAGED ASPIRATOR AND HOLES IN THE OPPOSITE TUBE. ASPIRATOR CAUSED HOLES IN THE TUBE. ALSO, ASPIRATOR HAD A BAD SEAL WHICH MADE IT LEAK. PATCHED THE INFLATION CHAMBER AND REPLACED THE ASPIRATOR. ROOT CAUSE WAS ASPIRATOR PACKED IN SUCH A WAY AS TO ABRADE A HJun 7, 2006 · N642UA · Boeing 767322 · Escape SlideSDR 2006UALA01113Pump · failedDIVERTED DUE TO CENTER HYDRAULIC PUMP FAILURE. NR 3 SPOILER ACTUATOR LEAKING HYDRAULIC FLUID. REPLACED NR 3 SPOILER ACTUATOR LAST CHANCE FILTER PLUG O-RING. LEAK CHECKED SPOILER ACTUATORS. LEAK CHECKED OK.Jun 7, 2006 · N665UA · Boeing 767322 · Hydraulic Pump (Electric/Engine), MainSDR 2006UALA01127Warning System · activatedAUTOSPEED BRAKE EICAS MESSAGE ON FINAL APPROACH WHEN SPEEDBRAKE IN ARMED POS AFTER 7 SECONDS. AUTOSPEED BRAKE EICAS MESSAGE ON FINAL APPROACH WHEN SPEED BRAKE IN ARMED POSITION AFTER 7 SECONDS. REPLACED K518 AIRGROUND RELAY AND ACCOMPLISHED SYSTEM CHECK. ALJun 6, 2006 · N668UA · Boeing 767322 · Drag Control SystemSDR 2006UALA01125Warning System · activatedLT ENG BLEED LIGHT & LT ENG PRV EICAS MSG DURING DESCENT. LEFT ENGINE BLEED LIGHT & LEFT ENGINE PRV EICAS MSG DURING DESCENT WITH ENGINE BLEED SWITCH ON, & ENGINE RUNNING. LEFT & RIGHT DUCT PSI ARE: LEFT 5 PSI, RIGHT 30 PSI. PERFORMED BLEED AIR BITE TEST OK.Jun 6, 2006 · N643UA · Boeing 767322 · Pneumatic Indicating SystemSDR 2006UALA01088Beam · corrodedRT MLG IB BOGIE BEAM BUSHING AT PIVOT IS WORN, ALSO RT MLG INNER CYLINDER IB CLEVIS PIVOT BUSHINGS FOUND WORN. RT MLG BOGIE PIN CORRODED. CORROSION FOUND IN BORES. FAILURE OF THE AFFECTED PARTS WAS CAUSED BY LACK OF LUBRICATION DUE TO CHIPPED CHROME PLATING PJun 1, 2006 · N670UA · Boeing 767322 · Main Landing GearSDR 2006UALA01064Landing Gear · malfunctionedDURING TAKEOFF GEAR WILL NOT RETRACT AND GEAR HANDLE WILL NOT GO PAST THE OFF POSITION. RT MLG TILT SENSOR MOUNTING BRACKET HAS MOVED WHICH LED TO FALSE INDICATION , OUT OF LIMIT INDICATION SENSOR TO TARGET MEASUREMENT, RE-POSITIONED AND RE-AJDUSTED, CHECKED,Jun 1, 2006 · N670UA · Boeing 767322 · Landing Gear Retraction/Extension SystemSDR 2006UALA01089Warning System · activatedAILERON LOCKOUT EICAS DURING DESCENT FL110 250 KIAS. CLEANED AND SECURED CANON PLUG ON RIGHT ACTUATOR. OPS OK NOW.May 31, 2006 · N652UA · Boeing 767322 · Aileron Control SystemSDR 2006UALA01058Bottle · low pressureLOW BOTTLE PRESSURE. THE FILL VALVE IS LEAKING THROUGH THE SHRADER VALVE. REPLACED FILL VALVE.May 31, 2006 · N676UA · Boeing 767322 · Escape SlideSDR 2006UALA01043Hydraulic System · malfunctionedRETURNED TO IAD DUE TO LEFT HYDRAULIC SYSTEM QUANTITY AND PRESSURE. LEFT HYD QUANTITY ZERO FOLLOWED BY L SYS PRESS LIGHT AND EICAS. HYD PUMPS SHUT OFF. FOUND RUDDER RATIO SOLENOID VALVE LEAKING. RPL SOLENOID VALVE. LEAK CHECKED OK.May 26, 2006 · N661UA · Boeing 767322 · Hydraulic System, MainSDR 2006UALA01171Latch · failedRT O/W COMP DOOR LATCH CHECK FAILED. REMOVE AND REPLACED LATCHES REF UAL B767, MM 25-68-98.May 19, 2006 · N676UA · Boeing 767322 · Escape SlideSDR 2006UALA00996Latch · failedLT OVERWING ESCAPE SLIDE COMPARTMENT DOOR LATCHES FAILED TORQUE CHECK. REPLACED LATCHES AND ACCOMP RIG CHECK. AIRCRAFT RETURNED TO SERVICESLIDE PROBLEM ROOT CAUSE WAS SUSPECTED TO BE IMPROPER TORQUE DURING INSTALLATION.May 16, 2006 · N661UA · Boeing 767322 · Escape SlideSDR 2006UALA00919Skin · crackedNR 1 STRUT SIDE SKIN PNL FWD TORQUE BOX ACCESS HOLE HAS CRACK ON THE TOP SIDE. REPAIR DOUBLER PER SRM54-53-01, REPAIR 6 WAS INSTALLED, WITH 1 EXTRA ROW OF REPAIR FASTENERS.May 9, 2006 · N653UA · Boeing 767322 · Nacelle/Pylon, Plate/SkinSDR 2006UALA00917Unknown · unknownDIVERTED TO YYZ WITH ELECTRICAL PROBLEMS. RT GEN TRIPPED OFF ON TAKEOFF DRIVE LIGHT & EICAS ILLUM, DISCONNECTED IDG. OIL WAS FOULD LOW, SERVICED WITH 4 QUARTS OF OIL, NO EXTERNAL LEAKS EVIDENT. RAN ENGINE WITH IDG ON LINE FOR 20 MINS ALL OPS NORMAL. RE-INMay 7, 2006 · N655UA · Boeing 767322 · Electrical Power SystemSDR 2006UALA00912Odor · detectedDIVERTED TO YBG DUE TO ELECTRICAL ODOR AND FUMES IN FLIGHT DECK. CHK'D FOR BURNED WIRING AND PROBLEMS WITHIN E&E COMPARTMENT. NO EICAS MESSAGE NOTED BY FLIGHT CREW. CLEANED DIRTY OVENS AT FWD GALLEY. CHECKED WIRING AND COMPONENTS IN AREA AND FOUND NO DISCRMay 7, 2006 · N649UA · Boeing 767322 · Air Distribution SystemSDR 2006UALA00913Wire · damagedRETURNED TO HNL DUE TO NR 2 ENGINE PNEUMATIC BLEED PROBLEM. THE PRV (MR36213 - 483) & PRV CONTROLLER (MR36140 - 111) WERE REMOVED 1ST. HOWEVER, THERE WAS STILL NO PRESSURE IN THE SYSTEM AFTER REPLACING THE PRV AND CONTROLLER. NEXT, THE RH PRSOV (MR36159 - 23)May 6, 2006 · N671UA · Boeing 767322 · Turbine Engine System WiringSDR 2006UALA00856Light · faultyEEL ROW 10-17 AIRCRAFT RIGHT ON WHEN EMERGENCY LIGHTS SWITCH ARMED IN COCKPIT, CHRONIC.Apr 30, 2006 · N674UA · Boeing 767322 · Emergency LightingSDR 2006UALA00835Display · unknownDIVERTED TO LHR DUE TO LEFT CENTRAL DISPLAY UNIT PROBLEM. LEFT CDU FAILED. REPLACED LEFT CDU. OPS CHECK NORMAL.Apr 29, 2006 · N651UA · Boeing 767322 · Indicating/Recording SystemSDR 2006UALA00857Wire · burnedAFT CARGO BAY FWD OF PDU CONTROL PANEL, (FWD-DOWN) WIRING BURNED. SPLICED WIRES W710-301B, 3 01R, 301Y, W710-306B, 306R, 306Y WITH NEW WIRING PER BSWPM 20-30 -12. REPAIRED ALL WIRING. A/C RETURNED TO SERVICE. SUSPECT WIRING DAMAGED BY CARGO LOADING ACTIONS.Apr 28, 2006 · N654UA · Boeing 767322 · Electrical Power System WiringSDR 2006UALA00807Wire · inoperativeEEL STRIP INOP AT 1H, 22A AND FROM 14HJ TO MID GALLEY RIGHT LAV. REPLACED EEL STRIP AT SEAT 1H. REPLACED FEEDER CABLE TO EEL STRIP AT SEAT 22A. REATTACHED FEEDER CABLE CONNECTOR AT SEAT 14HJ TO MID-GALLEY-RIGHT LAV EEL STRIP. ALL EEL LIGHTS, OP CHECK OK.Apr 23, 2006 · N665UA · Boeing 767322 · Emergency LightingSDR 2006UALA00808Rod · brokenFOUND LEFT OVERWING SLIDE TENSION ROD BROKE. REPLACED SLIDE. AIRCRAFT RETURNED TO SERVICE. ROOT CAUSE WAS TENSION ROD BEARINGS BROKEN. SUSPECT OVER TIGHTENING DURING INSTALLATION.Apr 22, 2006 · N654UA · Boeing 767322 · Escape SlideSDR 2006UALA00718Warning Light · illuminatedLANDED AT ORD UNDER AMBER ALERT DUE TO ILLUMINATED FLAP DISAGREE LIGHT.Apr 17, 2006 · N644UA · Boeing 767322 · Trailing Edge Flap Control SystemSDR 2006UALA00713Aspirator · malfunctionedBOTH ASPIRATORS STAYED OPEN DURING SLIDE DEPLOYMENT.Apr 17, 2006 · N649UA · Boeing 767322 · Escape SlideSDR 2006UALA00711Slide · departedLEFT WING SLIDE APPEARS TO HAVE DEPARTED THE AIRCRAFT ON CLIMBOUT.Apr 16, 2006 · N655UA · Boeing 767322 · Escape SlideSDR 2006UALA00698Skin · crackedAFT LT FUSELAGE SKIN DENTED & CRACKED AT STA 1197 + 84 AND STRINGER S-19L.Apr 16, 2006 · N655UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR 2006UALA00710Wire · inoperativeEEL LIGHT INOP LEFT SIDE ZONE-A AND ZONE-A GALLEY. REPLACED ENTIRE EEL FEEDER CABLE INCLUDING LIGHT STRIPS, OPS CKApr 15, 2006 · Boeing 767322 · Light System WiringSDR 2006UALA00709Battery · dischargedEMERGENCY EEL LIGHT AFT OF SEAT 1A, AT SEAT 14A AND FROM 19A TO 15A INOP. REPLACED EEL POWER SUPPLY. OP CHECKS OK.Apr 14, 2006 · N660UA · Boeing 767322 · Emergency LightingSDR 2006UALA00707Compressor · stalledABORTED TAKEOFF AT 100 KNOTS DUE TO COMPRESSOR STALL OF NR 1 ENGINE.Apr 14, 2006 · N660UA · Boeing 767322 · Engine (Turbine/Turboprop)SDR 2006UALA00712Wire Harness · burnedFWD CARGO PIT LOADING SYSTEM IS POPPING SEVERAL C/B'S. FOUND WIRE HARNESS BURNED AT CLAMP BELOW FLOOR IN FWD PIT STA 650. FWD CARGO PIT LOADING SYS. IS INOP. FOUND WIRE HARNESS BURNT AT CLAMP BELOW FLOOR IN FWD PIT STA.650,JUST RH OF CENTERLINE. PERFORMED Apr 12, 2006 · N642UA · Boeing 767322 · Equipment/Furnishings WiringSDR 2006UALA00708Trigger · brokenLEFT OVERWING SLIDE PACK TRIGGER BROKEN. REPLACED SLIDE. AIRCRAFT RELEASED TO SERVICE. ROOT CAUSE WAS SLIDE PACK TRIGGER BROKEN DURING INSTALLATION.Apr 4, 2006 · N649UA · Boeing 767322 · Escape SlideSDR 2006UALA00637Hinge Fitting · crackedRIGHT INBOARD AFT FLAP, CENTER HINGE FITTING CRACKED ON OUTBOARD SIDE IN COVE AREA. *S/D* THE RIGHT INBOARD AFT FLAP, CENTER HINGE FITTING, WAS FOUND CRACKED ON THE OUTBOARD SIDE IN THE COVE AREA. REPAIRED FITTING PER 767 SRM 57-53-02.Apr 3, 2006 · N649UA · Boeing 767322 · Trailing Edge FlapsSDR 2006UALA01187Latch · wornNR 1 AND NR 2 LATCHES EDGE MARGIN BEYOND LIMITS. REMOVED AND REPLACED LATCHES.Mar 30, 2006 · N649UA · Boeing 767322 · Emergency EquipmentSDR 2006UALA00603Light · inoperativeFOUND A-ZONE AND MOST AFT LEFT EEL FLOOR LIGHTS OUT.Mar 27, 2006 · N648UA · Boeing 767322 · Emergency LightingSDR 2006UALA01160Block · out of positionLT OVERWING STOP BLOCK IS RUBBING AGAINST RELEASE TRIGGER. REPLACE LOCATOR PIN IAW 767 SRM 51-40-02.Mar 25, 2006 · N651UA · Boeing 767322 · Emergency EquipmentSDR 2006UALA00593Pin · crackedRT MAIN LANDING GEAR BOOGIE PIN SHOWS CRACK. INITIAL ULTRASONIC TEST INDICATED CRACKING. THEREFORE, THE PART WAS REPLACED WITH A NEW -5. SUBSEQUENT TESTING REVEALED THAT THE PART WAS NOT CRACKED.Mar 24, 2006 · N648UA · Boeing 767322 · Main Landing GearSDR 2006UALA00592Support · looseRT OVERWING SLIDE LACING ATTACH NYLON FINGERS, 8 BROKEN, SUPPORTING TUBE LOOSE, LAYING ON SLIDE COMPARTMENT LWR SURFACE. ROOT CAUSE APPEARS TO BE OVER TIGHTENING DURING SLIDE OVERHAUL.Mar 24, 2006 · N648UA · Boeing 767322 · Escape SlideSDR 2006UALA00591Warning Light · illuminatedON APPROACH, WHEN FLAPS WERE SELECTED TO 1, HAD EICAS MSG TE FLAPS DISAGREE DISPLAYED AND TRAILING EDGE LIGHT ILLUMINATED. REPLACED FLAP/STAB POSITION MODULE (FSPM), MR27011, P/N 285T0099-17, MOD A.Mar 24, 2006 · N665UA · Boeing 767322 · Trailing Edge Flap Control SystemSDR 2006UALA00590Pin · crackedDURING ULTRASONIC INSPECTION OF LT MLG BOGIE PIN, CRACK INDICATION WAS FOUND. INITIAL ULTRASONIC TEST INDICATED CRACKING. THEREFORE, THE PART WAS REPLACED WITH A NEW -5. SUBSEQUENT TESTING REVEALED THAT THE PART WAS NOT CRACKED.Mar 24, 2006 · N648UA · Boeing 767322 · Main Landing GearSDR 2006UALA00571Generator · unknownRETURNED TO IAD DUE TO NR 2 GENERATOR PROBLEM. AFTER EVENT, INITIAL IDG SERVICE AND ENGINE RUN PRODUCED NO FAULTS OR LEAKAGE, AND MONITORING AC REVEALED NO DUPLICATE EVENTS. INDICATION OF LOW OIL PRESSURE FROM INTERNAL CHARGE PRESSURE SWITCH CLOSURE MOST LIKEMar 22, 2006 · N655UA · Boeing 767322 · Electrical Power SystemSDR 2006UALA00604Toilet · malfunctionedRETURNED TO IAD DUE TO A WATER LEAK IN THE MAIN CABIN. TOILET OVERFLOWED AND WATER KEPT RUNNING UNTIL CREW CLOSED LAV WATER VALVE.Mar 17, 2006 · N659UA · Boeing 767322 · LavatoriesSDR 2006UALA00468Attach Fitting · misdrilledRIGHT WING INBOARD AILERON, INBOARD SECTION LEADING EDGE ATTACH FITTING MISDRILLED. S/D* THE SUBJECT FITTING WAS MISDRILLED DURING INSTALLATION. REPAIRED PER TIMCO REO-G11452.Mar 12, 2006 · N641UA · Boeing 767322 · AileronsSDR 2006UALA00471Fitting · crackedNR 2 PYLON MIDSPAR FITTING LOWER TANG AT INBOARD CLOSEOUT ANGLE HAS 2 EACH CRACKS COMING OUT OF THE INBOARD BOLT HOLE. 2 CRACKS EMANATING FROM INBD BOLT HOLE OF CLOSEOUT ANGLE INSTALLED OVER NR 2 PYLON MIDSPAR FITTING LOWER TANG WAS FOUND. THE CLOSEOUT ANGLE Mar 12, 2006 · N641UA · Boeing 767322 · Nacelle/Pylon, Main FrameSDR 2006UALA00470Stiffener · gougedLT WING STIFFENER GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. THE LEFT WING STIFFENER, P/N 112T1237-1, WAS FOUND GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. NO DAMAGE WAS REPORTED ON THE ADJACENT STRUCTURES. THEREFORE, THE GOUGED WAS LIKELY CAUSED BY FOD. REPLMar 12, 2006 · N641UA · Boeing 767322 · Wing Miscellaneous StructureSDR 2006UALA00469Angle · crackedCLOSEOUT ANGLE BELOW MID SPAR FITTINGS OF NR 2 PYLON HAS CRACKS FROM INBOARD AND OUTBOARD ENDS. INBD AND OUTBD ENDS ON CLOSEOUT ANGLE BELOW MID SPAR FITTINGS OF NR 2 PYLON WERE FOUND CRACKED. THE CLOSEOUT ANGLE WAS REPLACED USING 767-300 SRM 51-40-02.Mar 12, 2006 · N641UA · Boeing 767322 · Nacelle/Pylon Miscellaneous StructureSDR 2006UALA00452Failsafe · corrodedCORROSION ON STA 1562 FAIL-SAFE, P/N 146T1223-30, BETWEEN STR 39L & 39R. REPAIRED BL 0 AREA CORROSION AT STA 1562 FAILSAFE CHORD WITH A REPAIR ANGLE AND FILLER PER TIMCO REO(EVA) G11428 AND UA EVA 60127. REPAIR IS FAA APPROVED AND PERMANENT.Mar 9, 2006 · N641UA · Boeing 767322 · Fuselage Main, Structure
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