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 UALA2010031900924Indicator · faultyFLAP IND SHOWS 1-2 WIDTH NEEDLE SPLIT AFTER SELECTING FLAPS 5. NO ASSOC ROLL NOTED. REPLACED FLAP INDICATOR. OPS CHECKS OKAY.SDR UALA2010031500874Adjuster · stiffCAPTAIN'S RUDDER PEDAL ADJUSTMENT VERY STIFF. DISCONNECTED CAPT RUDDER PEDAL ADJ CABLE AND RUDDER PEDAL CAPT TO FO PEDAL ROD. CABLE STILL IN POSITION TO AID IN REF FOR INSTALLATION. REINSTALLED ROD AND REPLACED CABLE.SDR UALA2010031500865Light · obstructedAFT EEL LIGHT FWD OF DOOR 2R IS COVERED WITH CARPET, LIGHT OBSTRUCTED. CUT CARPET AS TO UNCOVER EEL LIGHT.SDR UALA2010031500864Light · improper partSEAT MOUNTED EEL AT OVERWING EXIT ON SEAT 21HJ IS INCORRECT TYPE. REPLACED WITH CORRECT LIGHT, OP NORMAL.SDR UALA2010031500863Light · missingSEAT MOUNTED EEL AT SEAT 12HJ IS MISSING. REPLACED LIGHT ASSY.SDR UALA2010031500872Valve · malfunctionedAPU BLEED DOES NOT INCRS FOR ENG START. MAX BLEED PRESS 15 PSI. ENG MAX MOTOR 20PCT N2. WITH PACKS OFF, MOTORED ENG, REACHED 22 PERCENT N2, 20 PSI DUCT PRESSURE REACHED. REPLACED APU FLOW SENSING MODULE, NO HELP. REPLACED SURGE VALVE DUCT PRESS 32 PSI UNLSDR UALA2010031500857Isolation Valve · faultyGOT EICAS L ENG HPSOV WITH LEFT BLEED LIGHT. ON DESCENT, GOT EICAS L ENG HPSOV WITH LEFT BLEED LIGHT <1 MIN LATER WENT OUT. DURING PNEUMATIC HEALTH CHECK FOUND LEFT AND RIGHT BLEED SYSTEM ISOLATION CHECK VALVES BAD. VALVES WERE REPLACED AND ENGINES RAN, BLESDR AALA20100313FRA01Cover · brokenEMERGENCY LIGHT ON FLOOR ACROSS FROM 43C SEAT COVER BROKEN. REPLACED LIGHT ASSEMBLY.SDR UALA2010031500846Cdu · inoperativeCAPT'S CDU BLANK, RTFL. REPLACED LEFT CDU, OPS CHECK OKAY. CDU INOPERATIVE. REPLACED LEFT CDU, OPS CHECK OKAY.SDR UALA2010031500851Overheat Loop · out of positionREPEAT GRIPE BODY DUCT OVERHEAT LIGHT ON MOMENTARILY AFTER SECOND ENG START. RAN ENGINES 1 AND 2 GOT DUCT OVERHEAT GOT LIGHT AGAIN. REPLACED CARD M691, NO HELP. RE-INSTALLED ORIGINAL CARD. FOUND DETECTION LOOP TS226 LAYING ON APU BLEED DUCT JUST FWD OF APUSDR UALA2010031500871Actuator · malfunctionedENGINES STARTED NORMALLY IN DEN HOWEVER APU DUCT PRESSURE WAS 18 PSI. ACTUATOR FOUND FAULTY. REPLACED APU INLET GUIDE ACTUATOR. OPS NORMAL.SDR UALA2010031500855Detection Sys · out of positionADP INOPERATIVE PERFORMANCE PENALTIES WILL BE APPLIED BECAUSE BODY LOOP DETECTION SYSTEM IS DEFERRED. FOUND DETECTION LOOP TS226 LAYING ON APU BLEED DUCT JUST FWD OF APU BLEED VALVE. REPOSITIONED LOOP. RAN ENG. DUCT LEAK LIGHT REMAINS EXTINGUISHED.SDR UALA2010031500849Structure · corrodedMAIN DECK STA 1518 LBL 28 FLOOR STRUCTURE IS CORRODED. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION LBL 7 TO LBL 3. HFEC INSP VERIFIED DAMAGE REMOVED. FABRICATED & INSTALLED NEW UPPER CAP SPLICE ANGLES AND SHIMS.SDR UALA2010031200843Module · failedAPU PNEUMATICS LOW READS APPROX 19 PSI ALONG WITH FLUCTUATING PRESSURE. REPLACED FLOW SENSING MODULE. REPLACED APU SURGE CONTROL VALVE. TESTED APU. OPS CHECKS NORMALLY.SDR UALA2010031200842Circuit Card · faultyRT ENG FIRE LP 1 ON STATUS PAGE. SAMC TEXT: CYCLED B22 ON P11 AND PERFORMED FIRE TEST FAULT CLEARED. CREW PUSHED POWER UP ON NR 2 ENG AND FAULT RE-APPEARED AND WENT AWAY WHEN BACK TO IDLE. REPLACED M683 CARD LOOP 1. RAN ENG, OPS CHECKS OKAY. NO FAULTS NOSDR UALA2010031500869Control Unit · malfunctionedLEFT AFT LAV CB P11 U7 FOUND POPPED. PER FLIGHT CREW, "THAT BREAKER THAT'S OUT" IS ACTUALLY P11-U34, RIGHT AFT GALLEY. WITH D392 DISCONNECTED FROM M226 ELCU, CB DOES NOT TRIP. REPLACED ELCU M226, GALLEY POWER CHECKS NORMAL.SDR UALA2010031500854Shutoff Valve · faultyL & R DUCT PRESSURE SPLIT & ACFT ON GROUND, WITH ENG RUNNING, LT & RT ISOL VALVES CLOSED & BLEED SW ON. PRESSURE EQUAL WHEN N2 INCREASED ABOVE 82 PERCENT. NEED HIGH PRESSURE SHUTOFF VALVE ITEM NR 375. REPLACED NR 2 ENGINE HPSOV. OPS NORMAL.SDR UALA2010031500844Handset · defectiveTHE 1L HANDSET F/A CAN'T HEAR FLIGHT DECK. REPLACED HANDSET, OP CHECK GOOD.SDR UALA2010031200837Controller · faultyAPU SHUTDOWN AT GATE. REPLACED ECU PER MM. REPLACED RELAY K197. OPS CHECK OKAY.SDR UALA2010031200840Panel · bowedFOUND RT WING LWR PANEL BOWED. FOUND WIGGLE PLATES C, D, G, WITH PULLED RIVETS AS VIEWED IN IPC. WING PANELS 661GB,WS698, AFFECTED. 3 EA WAFFEL OR RIPPLE SUPPORT PANELS REMOVED FROM RT WING PANELS ARE IN SMC OFFICE. RETRIEVED SUPPORT PANELS. MFG NEW SUPPOSDR UALA2010030800778Light · brokenF-C PAX SEAT 2B FWD EMERGENCY LIGHT ASSY BROKEN. REPLACED PAX SEAT EMERGENCY LIGHT ASSY AND OPS CK'D GOOD.SDR UALA2010030800793Module · damagedON RETRACTION GEAR HANDLE WAS VERY DIFFICULT TO MOVE THROUGH TOP THIRD OF TRAVEL. REPLACED MLG CONTROL LEVER MODULE.SDR UALA2010030800806Panel · leakingFUEL LEAK UNDER RT INBD WING. 12 FOOT SEEP AT SEAM WITH WIDE AREA OF DRIPS. LOCATED LEAK EXTERNALLY AND INTERNALLY. REMOVED SEALANT EXTERNALLY, CLEANED AND RESEALED WITH A1-2 AND B1-2 AT 1400 HRS. NEEDS TO RESEAL INTERNALLY. RESEALED INTERNALLY WITH A1-2 AND SDR UALA2010030800805Anti-Ice Valve · faultyLEFT ENG ANTI ICE VALVE TAKES ABNORMALLY LONG TIME TO CLOSE. REPLACED VALVE. LEAK CHECKED OKAY. NORMAL GROUND CHECK OF BOTH ENGINE ANTI VALVES.SDR UALA2010030800786Shutoff Valve · malfunctionedDUCT PSI FROM ENGINES SPLIT DURING TAKEOFF OR CLIMB, WITH LT & RT ISOLATION VALVES CLOSED & BLEED SWITCHES ON. LEFT 52 RT 40 SFC TO 20000'. L48 R39 THRU 28000'. EVEN 40 PSI 30000'. RAN ENGINES AT POWER CHECKED SYSTEM. FOUND FAULTY PRSOV, REPLACED PER MM. ENGISDR UALA2010030500774Line · crackedFOUND HYD LEAK AT RT PYLON 1 INCH RETURN LINE FITTING AT AFT END OF LINE. FOUND SLEEVE CRACKED AT AFT FITTING. REMOVED LEAKING HYD LINE, LAYING IN PLACE, PINED RESERVOIR LOCKOUT WITH BOLT STREAMER ATTACHED. REPLACED CRACKED LINE AT RT PYLON.SDR UALA2010030800795Light · inoperativeAFT EMERGENCY LIGHT INOP AT SEAT 5HJ. NEED LIGHT ASSY. REPLACED EMERGENCY LIGHT. OPS CHECKS NORMAL.SDR UALA2010030800779Fire Loop · faultyEICAS MSG 'ENG1 FIRE LP2' DISPLAYED. (LT=1,RT=2). LOOP IS FAULTY. REPLACED UPPER AFT FIRE LOOP. TEST NORMAL. NO FAULTS.SDR UALA2010030500765Wire · damagedFOUND DAMAGED WIRES 6 INCHES UP FROM NR 1 ENGINE LWR AFT FIRE DET LOOP, ON OUTBD SIDE OF ENG. REF. WD 26-11-11. RETERMINATED WIRES AT LOOP TS662. OPS OKAY.SDR UALA2010030500767Relay · malfunctionedCENTER AIR DEMAND HYD PUMP INOP IN AUTO & ON POSITIONS. FOUND LOW APU BLEED AIR SUPPLY - DF APU BLEED AS PER MEL 3611G. ENGINE NR 1 IDLE RUN ACP AT IAD AND FOUND ADP OP CHECKS NORMAL WITH ENGINE AIR. FOUND LOW APU BLEED AIR SUPPLY - DF APU BLEED AS PER MEL 3SDR UALA2010030500762Pump · inoperativeCENTER AIR DEMAND HYD PUMP INOP IN AUTO & ON POSITIONS.SDR UALA2010030800785Valve · malfunctionedRT DUCT FLUCTUATES + OR - 20 PSI. ACCOMPLISHED HPSOV HEALTH CHECK, REPLACED PRV PER AMM AND HPC PER AMM AGAIN, NO HELP. RT PNEUMATIC PRESSURE STILL FLUCTUATES 40-20, N2 77-80%, BLEED OFF LIGHT ILLUMINATED, ONLY HAPPENS ON DECELERATION. LOCKED OUT HPSOV PER SDR UALA2010030200746Wire Harness · inoperativeEMERGENCY LIGHT ON SEAT 33A IS INOP. REPLACED SEAT WIRE HARNESS. CHECKS GOOD.SDR UALA2010030200745Battery · inoperativeEMERGENCY LIGHTS MID CROSS-AISLE AND EMERGENCY LIGHT STRIP BY MID LEFT LAV INOPERATIVE. REPLACED BATTERY. CHECKS GOOD.SDR UALA2010030500763Shutoff Valve · malfunctionedRT DUCT FLUCTUATES +/- 20 PSI DURING DESCENT. LOCKED OUT HIGH STAGE VALVE CLOSED PER MEL. ACCOMPLISHED HPSOV HEALTH CHECK, REPLACED PRIORITY VAVLE PER AMM36-11-18, HPC PER AMM AGAIN, NO HELP. RT PNEUMATIC PRESS STILL FLUCTUATES 40-20, N2 77-80%, BLEED OFF LIGSDR UALA2010030100739Bleed Valve · fluctuatesRIGHT PNEUMATIC PRESS FLUCTUATES FROM 10 TO 30 PSI WHEN POWER REDUCED FOR DESCENT. REPLACED FAULTY NR 2 ENG FAN AIR MODULATING VALVE. OP CHECK AND LEAK CHECK GOOD. BITE CHECK OF AIR SUPPLY MODULE CHECK GOOD.SDR UALA2010030200740Heater Blanket · burnedSHIELD ASSY NR 2 ENGINE BURNED AND FALLING APART. REPLACED HYD HEAT SHIELD BLANKET AND SECURED. ALL OKAY.SDR UALA2010030100736Light · brokenSEAT 27AB EMERGENCY EMERGENCY LIGHT ASSY IS BROKEN. REPLACED EMERGENCY LT ASSY. OPS CHKD, OK.SDR UALA2010030100733Controller · faultyRT DUCT PRESS 30-50 IN UNISON WITH RIGHT ENG N1 FLUCTUATION .5 PERCENT AND CABIN RATE FLUCT SNPSHT VLV LOCKED CLOSED. REPLACED NR 2 HIGH PRESSURE VALVE CONTROLLER. REOPENED BY OPBLM FOR FAILED ENG RUN. DURING ENGINE START HPSOV EICAS MESSAGE APPEARED. AT IDLESDR UALA2010030100734Control Rod · bindingCAPT FELT BINDING ON AILERON ON APPROACH AFTER LANDING ON GROUND. FLT CONTROL BINDING AILERON DISCONNECTED AND CONNECTED CONTROL RODS. OPS CHECKS NORMAL. NO BINDING FOUND IN SYS. RII INSPECTION METHOD NR 1 OF REMOVED AILERON CONTROL RODS AS CALLED OUT IN FIM.SDR UALA2010022600711Wire · shortedTAKEOFF CONFIGURATION WARNING. ACP PROX SENSOR WIRING RESISTANCE CHECK FOR S266,S267,S268. FOUND S267 R & B WIRES SHORTED TO GROUND WITH 27MEG OHM. ALL OTHER PROX SWITCHES TEST OK. REPLACED S267, STILL NEEDS CHK GAPS WITH TRUCK TILTED. MEASURED GAPS USINGSDR UALA2010022500705Gcu · faultyACFT WON'T SWITCH TO APU GENERATOR POWER. NO TIME TS, TRIED RESETS NO HELP. REPLACED APU GCU. RAN APU AND POWER TRANSFERRED NORMALLY. APU GENERATOR VOLTS AND FREQ NORMAL AND ONLINE.SDR UALA2010022500703Torque Tube · stiffON TAXIOUT DURING FLT CONTROL CHECK, THE ELEVATORS PRODUCED A RATCHETING FEELING FROM FULL FWD TO FULL AFT. BOTH CAPT AND F/O'S CONTROL COLUMNS FELT THE RATCHETING. ALL HYD SYS NORMAL AND A-P ARE DISENGAGED. FOUND ELEVATOR TORQUE TUBE AND BELL CRANK PUSH PULSDR UALA2010022600713Processor · malfunctionedFUEL CONFIG LIGHT CAME ON WITH 1100 LBS DIFFERENCE IN MAINS AND 35.7IN CTR AND STAYED ON. ACCOMPLISHED TEST IAW SERVICE TIP. REPLACED FQIS PROCESSOR. OPS CHECK NORMALSDR UALA2010022500699Tire · damagedIAW DISPATCH, CREW FELT NOSE GEAR POSSIBLY STRUCK SOMETHING OR BLEW A NOSE TIRE ON TAKEOFF ROLL. GEAR RETRACTED NORMALLY. INSPECTED ACFT IAW MOP. FOUND NO DAMAGE TO AIRFRAME ON FLAP SURFACES, MLG WHEEL WELL AREAS AND ENGINE INTAKE AND ENGINE COWL AREAS, WINGSDR UALA2010022400692Emitter · fluctuatesRIGHT MAIN FUEL QTY INDICATOR FLUCTUATING +0 TO -1000 LBS OF LT MAIN FUEL QTY INDICATOR. CREW STATES AS MAIN FUEL BURNED DOWN FLUCTUATION HAS DECREASED BUT IS STILL PRESENT. RT TANK READ 3 INCH DIFFERENT ON DRIP READING WITH 7K IN EACH TANK, AFTER FUELING TASDR UALA2010022400691Indicator · faultyO-H FUEL PANEL-FUEL TEMP INOPERATIVE. REPLACED OVERHEAD FUEL QUANTITY PANEL. ACCOMPLISHED FUEL QUANTITY BITE CHECK.SDR UALA2010022400680Lamp · brokenFWD EMERGENCY LIGHT ON SEAT WAS BROKEN OFF. REPLACED SEAT 6H EMERGENCY LIGHT LAMP ASSY, OP CHECKS GOOD.SDR UALA2010022300674Controller · faultyON ENGINE SHUTDOWN GOT BLEED LT AND HPSOV MSG FOR RT ENGINE. REPLACED NR 2 ENG HIGH PRESSURE CONTROLLER. NEEDS RUN TO CONFIRM FIX. REPLACED M860 CARD FILE. REACTIVATED HPSOV AND TESTED OK ON ENG RUN.SDR UALA2010022300668Pump · leakingADP HAS A 24 DROPS PER MINUTE HYD LEAK WITH THE PUMP NOT OPERATING OUT OF THE WEEP HOLE PLUG ON THE INBOARD SIDE OF THE GEARBOX. REPLACED ADP. OPS NORMAL.
Back to Boeing 767-322