Boeing 767-322
Service difficulty reports · 11,768
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 = '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.
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
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 2005UALA00441Stop Fitting · damagedAFT CARGO DOOR STOP FITTING WAS BLENDED BEYOND LIMITS.SDR 2005UALA00439Floorbeam · crackedAFT BULK PIT STA 1439 CABIN FLOORBEAM LOWER CHORD FLANGE CRACKED. THIS REPAIR REQUIRED DUE TO KNOWN PROBLEM OF BULK CARGO DOOR IMPACTING LOWER CHORD OF MAIN CABIN FLOORBEAM UPON OPENING OF DOOR. DAMAGE REPAIRED PER FAA APPROVED REPAIR.SDR 2006UALA01168Latch · failedLT O/W SLIDE COMPT DOOR DISCONNECT HOUSING HAS FAIL CHECK. REMOVE AND REPLACE REF: UALB767 MM 25-65-98.SDR 2005UALA00395Wire · brokenRAM AIR TURBINE FAILURE. DURING ROUTINE MAINTENANCE CHECK, A DISCREPANCY WAS NOTICED ON THE RAT SPEED SENSING. UPON FURTHER TROUBLESHOOTING, A WIRE INSIDE THE RAT SPEED SENSOR WAS FOUND BROKEN. AFTER REPAIR, THE RAT TEST WAS COMPLETED SUCCESSFULLY.SDR 2005UALA00392Floorbeam · puncturedE&E COMPARTMENT BS 246 FLOORBEAM WEB PUNCTURED APPROX RBL 45, WL 200. REPAIRED FLOORBEAM WEB.SDR 2006UALA01167Housing · crackedRT O/W DOOR DISCONNECT HOUSING IS CRACKED. REPLACE HOUSING IAW 767 MM-25-65-98.SDR 2006UALA01166Latch · failedLT O/W DOOR LATCHES FAIL INTEGRATOR TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW UAL B767 MM25-65-98.SDR 2005UALA00389Bulkhead · damagedNOSE WW BULKHEAD HAS DAMAGE. AUX NOSE JACK ACCIDENTALLY OVERLOADED. BOEING AOG TEAM PERFORMED PERMANENT STRUCTURE REPAIR TO STATION 287 BULKHEAD ASSY AND REPLACED DAMAGED SKIN PANEL.SDR 2006UALA01165Latch · failedLT O/W COMPT INTEGRATOR TORQUE CHECK FAILED AND LATCHES MUST BE REPLACED. REMOVE AND REPLACE LATCHES IAW UAL B767 MM-25-65-98.SDR 2006UALA01164Latch · failedLT OFFWING SLIDE LATCH CHECK FAILS TORQUE CHECK. TORQUE TO OPEN 200 IN/LBS, MAX ALLOWED 175.SDR 2005UALA00331Stiffener · crackedE+E COMPT, BS 246 FLOORBEAM VERTICAL STIFFENER FLANGE CRACKED RBL 11.53 INCHES. STIFFENERS ON THIS FLOORBEAM ARE KNOWN TO CRACK. DISCREPANCY FOUND ON ROUTINE INSPECTION. CRACKED PART WAS REPLACED WITH NEW.SDR 2005UALA00330Stiffener · crackedE & E BAY, BS 246 FLOORBEAM, STIFFENER FLANGE CRACKED AT RBL 16.38 INCHES. CRACKS ON STATION 246 FLOORBEAM STIFFENERS ARE A KNOWN PROBLEM. THIS CRACKED STIFFENER WAS REPLACED WITH NEW.SDR 2005UALA00342Fitting · crackedLEFT WING REAR SPAR, OUTBOARD FLAP OUTBOARD DEFLECTION FITTING CRACKED. THE SUBJECT FITTING CRACKED TO CYCLICAL FATIGUE LOAD DURING EXTENSION AND RETRACTION OF THE OUTBOARD FLAP. CORRECTIVE ACTION IS REPLACEMENT OF THE FITTING WITH NEW AND IMPROVED FITTING SDR 2005UALA00341Attach Angle · crackedRT WING INBOARD FLAP, INBOARD HINGE SUPPORT ATTACH ANGLE CRACKED OUTBOARD SIDE. THE SUBJECT HINGE SUPPORT FITTING CRACKED DUE TO FATIGUE LOAD. THE CRACKED AREA WAS REPAIRED PER 767-300 SRM 57-53-02.SDR 2005UALA00317Skin · puncturedFUSELAGE LEFT SIDE STA 500 PUNCTURED SKIN AT STR 24L. UNDETERMINED CAUSE OF DAMAGE. SKIN REPAIRED PER STANDARD BOEING SRM.SDR 2005UALA00299A/C Pack · malfunctionedLOSS OF BOTH PACKS CAUSED RESULTANT PRESSURIZATION PROBLEM. ALTHOUGH RT PACK WAS DEFERRED IN STANDBY MODE PER MEL AT THE TIME OF THE EVENT, THERE IS NO RECORD OF ANY DEFECT OR MAINTENANCE ACTIVITY AGAINST THE LT PACK, PRIOR TO OR AFTER THE EVENT. RT PACK COMSDR 2006UALA01163Latch · failedRT O/W DOOR LATCH INTEGRATOR FAILS TORQUE CHECK. REPLACE LATCHES IAW 767, MM-25-65-98.SDR 2006UALA01162Rod · chafedLT OVERWING SLIDE CENTER LATCH ROD ASSEMBLY CHAFFED. REPLACE ROD IAW 767, MM-25-65-98.SDR 2006UALA01161Latch · failedLT OVERWING SLIDE NR 3 DOOR LATCH FAILED INSP CHECK. REPLACE LATCH IAW 767 25-65-98.SDR 2005UALA00282Aspirator · leakingTHE ASPIRATOR LEAKING BY BARREL. REPLACED ASPIRATOR.SDR 2006UALA01159Latch · wornRT O/W DOOR LATCHES (NR 3 AND NR 4) FAIL EDGE MARGIN CHECK. REPLACE LATCHES IAW MM 25-65-98.SDR 2005UALA00207Compressor · stalledNR 1 ENGINE COMPRESSOR STALL AND AUTO SHUTDOWN. ABORTED TAKEOFF AT 50 KIAS DUE TO COMPRESSOR SURGE. CAPT REPORTED STRONG X-WIND AT 20 GUSTING 33. FOUND METAL IN THE TAILPIPE. ENGINE REPLACED AT IAD. ENGINE RETURNED TO LESSOR ON 06/08/05 WITHOUT BEING DISASDR 2005UALA00174Skin · dentedBULK CARGO DOOR OUTER SKIN IS DENTED, AFT END MID SECTION. REPAIRED DOOR SKIN WITH DOUBLER AND FILLERS PER SRM 52-30-01.SDR 2005UALA00199Control Panel · failedNR 2 CARGO FIRE SQUIB DOES NOT TEST. FOUND 757 TYPE APU/CARGO FIRE CONTROL PANEL INSTALLED. WITH THAT PANEL INSTALLED, THE NO. 2 CARGO SQUIB TEST LAMP WILL NOT LIGHT DUE TO DIFFERENT INTERNAL CIRCUITRY IN THE PANEL, PANEL WAS REPLACED WITH 767-322 TYPE APUSDR 2005UALA00157Stiffener · crackedFLOORBEAM AT STA 246 HAS A CRACKED VERTICAL STIFFENER ON FWD FACE OF BEAM AT APPROX LBL 26. REPLACED CRACKED STIFFENER.SDR 2005UALA00156Stiffener · crackedFLOORBEAM AT STA 246 HAS A CRACKED VERTICAL STIFFENER ON FWD FACE OF FLOORBEAM AT APPROX RBL 26.39. CRACKED STIFFENER WAS REPLACED.SDR 2005UALA00155Rib · crackedRT WING L-E CAVITY AT FSS 512, UPPER RIB LOWER CHORD PREVIOUS REPAIR CRACKED AT AFT END-OUTBD OF NR 8 SLAT OUTBD ACTUATOR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. RIB REPAIRED WITH ANGLE DOUBLER.SDR 2005UALA00118Bracket · brokenTORQUE BAR SUPPORT BRACKETS BROKEN. INSTALLED NEW SUPPORT BRACKETS.SDR 2005UALA00100Aspirator · leakingLEAKING ASPIRATOR. REPLACED ASPIRATOR.SDR 2005UALA00096Blade · fracturedNR 1 ENGINE SURGED, FLAMED OUT AND SEIZED. ENGINE WAS REMOVED FROM SERVICE AND DISASSEMBLED. ROOT CAUSE OF THE FAILURE WAS DETERMINED TO BE A FRACTURE OF THE 5TH STAGE HPC BLADE IN THE ROOT.SDR 2005UALA00132Connector · mispinnedFUEL JETTISON SYSTEM FAILED. THE JETTISON SYSTEM FAULT LIGHT ILLUMINATED AND THE LH JET PUMP EICAS MESSAGE APPEARED WHEN THE LH JETTISON PUMP FAILED TO GENERATE SUFFICIENT PRESSURE TO SET THE PRESSURE SWITCH. THIS WAS A RESULT OF THE PUMPS SHIP SIDE ELECTRICASDR 2006UALA01156Latch · failedLT O/W HATCH FAILS INTEGRATOR TORQUE CHECK. REPLACED LATCHES.SDR 2005UALA00065Hydraulic System · failedRETURNED TO LAX DUE TO RIGHT HYDRAULIC SYSTEM FAILURE. LOSS OF FLUID DUE TO FAILED O-RING ON CASE DRAIN MODULE DIFFERENTIAL PRESSURE INDICATOR BOSS. REPLACED O-RING AND RESERVICED HYDRAULIC SYSTEM.SDR 2005UALA00071Battery · inoperativeSQUIB TEST 1 LEFT INOP. REPLACED BATTERY AND CHECKS OK.SDR 2006UALA01155Latch · failedLT O/W SLIDE DOOR INTEGRATOR FAILS TORQUE CHECK. REPLACED LATCHES IAW 767 MM 25-65-98.SDR 2005UALA00015Bearing · failedFLT CREW REPORTS ELECTRICAL ODOR AND LIGHT HAZE IN COCKPIT. THE FORWARD EQUIPMENT COOLING EXHAUST FAN FAILED. SHOP FINDINGS DETERMINED BEARING FAILURE TO BE THE ROOT CAUSE.SDR 2005UALA00010Skin · puncturedAIRCRAFT DAMAGE AT DOOR 4 LEFT AT APPROX STA 1582 BELOW DOOR SILL. PUNCTURE THROUGH SKIN. UNDETERMINED CAUSE OF DAMAGE TO SKIN. REPAIRED PER SRM.SDR 2004UALA01257Light · malfunctionedEMERGENCY EXIT FLOOR LIGHTS FWD CABIN COME ON, GO OFF, AND FLASH INFLIGHT FOR NO REASON. REPLACED EEL LIGHT BATTERY PACK BEHIND KICK PANEL AT SEAT GROUP 1AB.SDR 2004UALA01254Connector · failedEMERGENCY EXIT LIGHTS AT ALL SEATS AND WALL EXITS FLICKERED ON AND OFF DURING CLIMB. REPLACED 9 EA SPADE CONNECTORS AND AFT LT CONTROL SWITCH.SDR 2004UALA01210Warning System · activatedASYMMETRICAL FLAP WARNING. PERFORMED PSEU BITE TEST. FAULTED SWITCH S303. REPLACED SWITCH, SYSTEM OPS CHECKS GOOD.SDR 2004UALA01230Relay · failedLEFT SQUIB ON NR 1 ESCAPE SLIDE WILL NOT TEST. REPLACED RELAYS K3, K4, K5, & K6 ON M1135 MODULE ABOVE LEFT AFT OVERWING DOOR PER WIRING DIAGRAM 25-65-11 AND PERFORMED REPETITIVE ITERATIONS OF SQUIB TEST. ALL CHECKS GOOD.SDR 2004UALA01170Autopilot Sys · malfunctionedCREW REPORTS TWO UNCOMMANDED YAW EVENTS EN ROUTE. LT AND RT YAW DAMPENER MODULES WERE CHECKED FOR RECORDED FLT FAULTS AND NONE WERE FOUND. MCDP CHECKS 1, 9, 40, AND 69, RELATING TO THE AUTOPILOT DIRECTIONAL SERVOS, WERE PERFORMED AND ALL CHECKED OK. CENTERSDR 2004UALA01163Stiffener · crackedSTATION 246 FLOORBEAM AT APPROX LBL 11, STIFFENER IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER.SDR 2004UALA01162Stiffener · crackedSTATION 246 FLOORBEAM AT APPROX LBL 2, STIFFENER IS CRACKED. REPLACED STIFFENER.SDR 2004UALA01151Wire Harness · sparksWIRE BUNDLES UNDERNEATH PIT FLOOR FROM PDY 6R AREA TO PDU 6L AREA SPARKING AND POPPING CB'S. REPAIRED BY SPLICING IN NEW WIRING PER BOEING STANDARD PRACTICES.SDR 2004UALA01131Battery Pack · inoperativeBUSINESS CLASS EMERGENCY LIGHTS ON AFTER TAXI OUT. REPLACED EMERG LT POWER SUPPLY CHARGER ASSY, POWER SUPPLY BATTERY AND EEL BATTERY POWER PACK AT SEAT 1A. ALSO REPLACED EEL BATTERY POWER PACK AT SEAT 8A.SDR 2004UALA01129Warning Light · illuminatedRETURNED TO ORD DUE TO LEADING EDGE SLAT INDICATION. REPLACED THE S282, AND S297 SWITCHES. SYSTEM OPS CHECKS GOOD.SDR 2004UALA01130Squib · will not testCREW REPORTS BOTH EMERGENCY EXIT SQUIBS WON'T TEST. REPLACED DIODES K839 AND K838, BATTERY PACKS P/N 2013-1, AND CHARGERS P/N 2012-1.SDR 2004UALA01046Transceiver · inoperativeRETURNED DUE TO AN INOPERATIVE WEATHER RADAR. REPLACED BOTH THE WX RADAR R-T UNIT, AND THE WX RADAR SCANNER. THERE HAVE BEEN NO FURTHER REPORTS OF WX RADAR PROBLEMS TO DATE.SDR 2004UALA01034Battery · failedLEFT AND RIGHT HAND OVERWING SLIDE SQUIB FAILS TEST. REMOVED AND REPLACED LT OVERWING BATTERY IN ACCORDANCE WITH AMM.
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