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 2006UALA02354Light · shortedAFT GALLEY CROSS AISLE EEL LIGHT INOPERATIVE. AFT GALLEY CROSS AISLE EEL STRIP SECTION INOP (SHORTED INTERNALLY) IS A SMALL SECTION 15" LONG & IS ADJACENT TO AN EXISTING LONG ONE THAT IS OPERATIVE. SHORTED EEL WAS AFFECTING EEL SECTIONS 35AB THRU 41AB.REPLACESDR 2006UALA02322Cabin Pressure · warning lightRETURNED TO THE FIELD IN BOS DUE TO A PRESSURIZATION PROBLEM. CABIN ALT AUTO 1-2 FAILED. CREW VERBAL, MANUAL FAILED AT 22000FT AT DECENT MANUAL MODE STARTED TO WORK. CHECKED BOTH PACK FLOW CONTROL VALVES FOR DAMAGED THROAT PRESSURE SENSING PROBES. CHECKESDR 2006UALA02290Light · inoperativeSEAT 16H EEL LIGHT INOPERATIVE. REPLACED SEAT 16H EEL LIGHTBAR PER MM 33-51-10 AND OPS CHECK GOOD.SDR 2006UALA02266Bracket · crackedBS 246 PULLEY BRACKET SUPPORT AT LBL 2, (INBD PULLEY, OUTBD SUPPORT) CRACKED AT LOWER RIVET. REPLACED SUPPORT ANGLE 141T5282-5.SDR 2006UALA02264Unknown · odorELECT ODOR IN COCKPIT, SOURCE UNKNOWN. ACCOMPLISHED CHECK OF ENTIRE COCKPIT. INSPECTED BEHIND THE P-6 PANEL, OPEN UP ALL OVERHEAD CB PANELS RANDOMLY PULLED SEVERAL INSTRUMENTS ON CAPTAINS AND FO'S PANELS AND CENTER CONSOLE. ALSO INSPECTED FWD E&E COMPARTMENT OSDR 2006UALA02246Floorbeam · crackedBS 246 FLOORBEAM STIFFENER CRACKED AT LBL 23. REPLACED STIFFENER. CRACKING RESULT OF PRESSURIZATION CYCLES & CABIN SERVICE EQUIPMENT LOADS.SDR 2006UALA02241Slat System · malfunctionedRETURN TO FIELD DUE TO LEADING EDGE SLAT PROBLEM.SDR 2006UALA02235Light · inoperativeFOUR SEGMENTS OF FLOOR MOUNTED EMERGENCY STRIP LIGHTS ARE INOPERATIVE. THE FOUR SEGMENTS ARE LOCATED NEXT TO SEAT 10F, NEXT TO THE LAVATORY BETWEEN SEATS 10F AND 15F, NEXT TO THE LAVATORY BETWEEN SEATS 14B AND 15B, AND THE FIRST STRIP LIGHT AFT OF DOOR 1R.SDR 2006UALA02234Connector · disconnectedEMERGENCY EEL LIGHT STRIP INOP AT RT MID LAV.SDR 2006UALA02227Aspirator · unserviceableBAD ASPIRATOR. CAUSE UNKNOWN. REPLACED ASPIRATOR. THIS WAS BETWEEN SENSING TUBE AND JET PLATE ASSEMBLY.SDR 2006UALA02218Light · inoperativeSEATS 5AB, 5EF, AND 7EF EEL LIGHT BARS WILL NOT ILLUMINATE.SDR 2006UALA02217Wire · brokenTHE AFT LONG EEL LIGHT BAR IS INOPERATIVE.SDR 2006UALA02216Connector · damagedEEL LIGHT STRIP IN FRONT OF THE AFT RIGHT HAND LAV IS INOPERATIVE.SDR 2006UALA02203Aspirator · leakingSLIDE ASPIRATOR LEAKING.SDR 2006UALA02200Aspirator · unserviceableDAMAGED SLIDE ASPIRATOR. REPLACED SLIDE. OK FOR RETURN TO SERVICE.SDR 2006UALA02181Slide · inoperativeLEFT OVERWING SLIDE SYSTEM INOPERATIVE.SDR 2006UALA02163Bearing · damagedBEARINGS DAMAGED. REPLACED SLIDE. OK FOR RETURN TO SERVICE.TOO MUCH TENSION ON TENSION ROD OF SLIDE, CAUSING BEARINGS TO DETERIORATE AND CRACK OVER TIME. REPLACED BEARINGS.SDR 2006UALA02162Hinge Fitting · crackedRT WING INBD FLAP AFT CENTER HINGE FITTING OUTBD FLANGE IS CRACKED. FABRICATED REPAIR PARTS PER SRM 57-53-02 AND INSTALLED FITTING PER SRM 51-40-4 ON NON ROUTINE W1762V. INSPECTED AND OK'ED FOR RETURN TO SERVICE.SDR 2006UALA02161Hinge Fitting · crackedLT WING INBD FLAP, AFT CENTER HINGE FITTING OUTBD FLANGE IS CRACKED. LT WING INBD FLAP, AFT CENTER HINGE FITTING OUTBD FLANGE IS CRACKED. FABRICATED FITTING REPAIR PARTS PER SRM 57-53-02 AND INSTALLED PER SRM 51-40-04 ON NON ROUTINE T2145Y. INSPECTED AND OKSDR 2006UALA02155Bottle · lowFOUND LOW BOTTLE PRESSURE. REPLACED SLIDE. AIRCRAFT RETURNED TO SERVICE.SDR 2006UALA02159Skin · crackedNR 2 ENG STRUT SIDE SKIN PANEL AT FWD TORQUE BOX ACCESS HOLE CRACKED THRU EXISTING FASTENER, AND VERIFIED AND END MARKED BY HFEC INSPECTION. REQ STRUCTURAL REPAIR MANUAL REPAIR. STOP DRILLED HOLE, NR 2 ENG PYLON OTBD WEB RPR. DRILLING OUT FASTNERS, HAVE MSDR 2006UALA02109Aspirator · leakingASPIRATOR LEAKING BETWEEN HOUSING ASSEMBLY AND NAME PLATE. REPLACED EVAC SLIDE. RETURNED TO SERVICE.SDR 2006UALA02115Warning Light · illuminatedWITH NORMAL CONFIGURATION FORWARD EQUIPMENT VALVE EICAS MESSAGE AND LIGHT. VALVE IDENTIFIED AS E&E COOLING VALVE. CONDUCTED OP CHECK OF VALVE USING A-CHECK JOB CARDS. VALVE AND SYSTEM CHECKED OK.SDR 2006UALA02112Bar · brokenLT OVER WING SLIDE TENSION BAR HOLD-DOWNS BROKEN. LT OVER WING SLIDE TENSION BAR HOLD-DOWNS BROKEN. (NYLON HOOKS) REPLACED SLIDE . RETURNED TO SERVICE.SDR 2006UALA02111Light · inoperativeMID-GALLEY CROSS AISLE EMERGENCY FLOOR LIGHT IS INOP. INSTALLED SINGLE LIGHT HARD EEL STRIP, NEEDS DUAL LIGHT HARD EEL. DUAL LIGHT INSTALLED. OP CHKS OK. RETURNED TO SERVICE.SDR 2006UALA02097Aspirator · leakingASPIRATOR LEAKING BETWEEN SENSING TUBE AND BARREL. SLIDE REPLACED. RETURNED TO SERVICE AFTER VISIT.SDR 2006UALA02098Cable · unsecureDURING ACP OF EQ5495 FOUND SLIDE BALL END CABLES UNSECURED AND IMPROPERLY PACKED. *S/D* REPLACED SLIDE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE.SDR 2006UALA02114Warning Light · illuminatedEICAS MESSAGE R GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. DISCONNECTED SUCCESSFULLY. REPLACED RIGHT ENGINE IDG, OPERATIONAL CHECK . OK FOR RETURN TO SERVICE.SDR 2006UALA02083Pump · failedFAILED HYDRAULIC PUMP. RETURNED TO THE BLOCKS. REPLACED NR 1 ENG ENGINE DRIVEN HYDRAULIC PUMP. LEAK CHECK OK, RETURN TO SERVICE.SDR 2006UALA02059Angle · crackedNR 1 PYLON MIDSPAR CLOSEOUT ANGLE CRACKED AT BOTH INBD FASTENERS. STOPPED DRILLED CRACK. INSTALLED STRAP AND FILLER REPAIR.SDR 2006UALA02026Warning Light · illuminatedRETURNED TO JFK UNDER DUE TO LEADING EDGE FLAP INDICATION. ALL CHECKS FOUND NORMAL.SDR 2006UALA02027Switch · shortedFOUND SEAT 8C PCU SHORTING AND CAUSING SMOKE, FUMES IN CABIN. FOUND FAULTY SWITCH. EVIDENCE OF FLUID SPILL. REPLACED THE BACK-CYCLER SWITCH.SDR 2006UALA02009Engine · leakingDIVERTED TO BOS DUE TO LOST OF OIL IN THE NR 2 ENGINE. FOUND STARTER TO GEARBOX MOUNTING FLANGE CRACKED AND LEAKING. STARTER HAD BEEN REPLACED PRIOR TO FLIGHT. REPLACED NR 2 ENGINE GEARBOX HOUSING ASSEMBLY.SDR 2006UALA02008Warning Light · illuminatedTAT PROBE LIGHT ILLUMINATED JUST AFTER TAKEOFF. [5-1-07] REPLACED THE TOTAL AIR TEMPERATURE SENSOR. OP CHECKS OK. CAUSE SUSPECTED TO BE INTERNAL ELECTRICAL SHORT IN SENSOR CIRCUIT.SDR 2006UALA01994Circuit Card · failedEICAS MSG 'LDG GEAR MONITOR' DISPLAYED WITH LDG GEAR UP AND LOCKED. FOUND ALL EXCEPT 4 CIRCUIT CARDS DISLODGED IN PSEU. REMOVED AND REINSTALLED ALL CIRCUIT CARDS.SDR 2006UALA01974Bushing · wornLT MLG BOGIE BEAM INBD AND OTBD PIVOT BUSHINGS WORN OUT OF LIMITS. REMOVED BUSHINGS, INSP BORE PER BAC CMM32-11-50, NO DEFECTS NOTED. INSTALLED NEW BUSHINGS. LINE HONED BUSHINGS & REASSEMBLED. ACCOMP GEAR SWING. OPS CHECKS NORMAL.SDR 2006UALA01970Rod · looseLT OVER WING SLIDE FOUND TENSION ROD LOOSE ON LT OVERWING SLIDE. NYLON-PLASTIC TENSION HOOKS BROKEN 3 IN. TEAR IN SLIDE COVER, CAUSED BY LOOSE ROD. THREE INCH TEAR IN SLIDE COVER, CAUSED BY LOOSE ROD. SLIDE REPLACED.SDR 2006UALA01951Motor · faulted"AIL LOCK" LIGHT WITH ASSOCIATED "AILERON LOCKOUT" EICAS ADVISORY LEVEL MESSAGE DISPLAYED DURING HIGH SPEED FLIGHT. CONFIRMED RT AILERON LOCKOUT ACTUATOR BAD. REPLACED PER MM27-11-44. FINAL CHECK GOOD. RETURN AC TO SERVICE. DAMAGED ACTUATOR MOTOR. SUSPECSDR 2006UALA01916Fuel Sys · malfunctionedUNWANTED FUEL TRANSFER BETWEEN MAIN FUEL TANKS. AIRPLANE SEEMS TO BE TRANSFERRING FUEL FROM R TO L MAIN TANKS: 17.0 IN LEFT; 16. ON RIGHT. TESTED PER SERVICE TIP MM2 8-11-95-0200A. CROSS FEED VALVE CHECKED GOOD NO TRANSFER NOTED. TESTED SYSTEM 03OCT2006 & FSDR 2006UALA01870Wire · damagedEICAS MESSAGE NORM ANTISKID & ALTN ANTI-SKID DISPLAYED. TAKEOFF FOLLOWED BY STATUS MESSAGE :ANTISKID CNTRL SHOWS XDUCR 7 FAULT, REPLACED TRANSDUCER 7. PROBLEM CONTINUED. FOUND WIRE TO PIN 1 IN TRANSDUCER CONNECTOR, D2024, BROKEN IN BACKSHELL CLAMP. REPLACED SDR 2006UALA01869Computer · failedL EICAS COMPUTER STATUS MSG DISPLAYED. REPLACED LEFT EICAS COMPUTER. A11 FLASH BAD. REPLACED A11U4 AND U10. OPS CHECK NORMAL.SDR 2006UALA01871Slide · no testLEFT OVERWING SLIDE WILL NOT TEST. BATTERY INOPERATIVE. REPLACED LEFT OVERWING SLIDE BATTERY.SDR 2006UALA01867Compressor · stalledNR 2 ENG COMPRESSOR STALL IN FLIGHT. ENG RECOVERED AND CONTINUED OPERATING. RECOVERED AND CONTINUED OPERATING. PRIOR TO STALL, ENG POWER WAS DECELERATING. ACCOMPLISHED BOROSCOPE OF NR 2 ENGINE, REPLACED ELECTRONIC ENGINE CONTROL, REPLACED IPCV VALVE, HPSOV,SDR 2006UALA01866Wire · damagedRIGHT WING T/E, WS 410, RIGHT MAIN FUEL QUANTITY WIRE BUNDLE FOR CONNECTOR, AFT SHELL CORRODED. FURTHER INSPECTION FOUND THE CORROSION WAS LIMITED TO THE CN1156 -4 CONNECTOR, HOWEVER, WHILE REMOVING THE CONNECTOR BACK SHELL, THE BACKSHELL BROKE APART INTO SESDR 2006UALA01864Latch · wornLT OVERWING SLIDE INTEGRATOR TORQUE CHECK FAILED. SLIDE DOOR LATCHES SHOW DEEP WEAR GROOVES ON LATCH SLIDERS PREVENTING PROPER LATCH MOVEMENT. REPLACED 4 LEFT OVERWING SLIDE DOOR LATCHES.SDR 2006UALA01801Generator · unknownRETURNED TO IAD DUE TO NR 2 GENERATOR PROBLEM. FOUND OVERFILL PRESSURE FITTING LEAKING OIL. REPLACED FITTING AND SERVICED TO FULL.SDR 2006UALA01798Floorbeam · crackedFOUND STA 246 FLOORBEAM ATTACH ANGLE AT RBL 11 IS CRACKED. REPLACED SUPPORT ANGLE 141T5146-5 PER SRM 51-40-2.SDR 2006UALA01863Switch · faultyRT WING SLIDE DOOR SENSOR S219 IS OUT OF LIMITS. REPLACED THE S219 PROXIMITY SENSOR.SDR 2006UALA01751Support Beam · crackedLT MLG TRUNNION WING DOOR ATTACH SUPPORT BEAM CRACKED. STRUT ASSY FOUND GOUGED & CRACKED. ACCOMPLISHED MAJOR REPAIR PER REO G1 1788. HFEC INSP FOR HIDDEN CRACKING AFTER REPAIR PER NDT 51-00-00-19, PT 6. OK FOR SERVICE.SDR 2006UALA01722Stiffener · crackedCRACKED VERTICAL STIFFENER ON FLOORBEAM BS 246, LBL 40, AFT SIDE. FABRICATED STIFFENER 141T5171-64 PER BACO DWG 141T5171 AND REPLACED PER SRM 53-10-51 AND 51-40-2. SUSPECT FORWARD GALLEY SERVICE EQUIPMENT LOADS.
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