Boeing 767-323
Service difficulty reports · 8,544
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 = '767323' 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 = '767323' 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 NACA2022122400001Indicator · malfunctionedL ENGINE FUEL FLOW INDICATOR SHOWING 0.0 1 MIN AFTER ENG START. PERFORMED L ENGINE IDLE RUN AND OPS CHECKED L ENG FUEL FLOW INDICATOR, HAD INSTANT READING OF 0.6 FF PER AMM 73-31-01, OPS CHECKED GOOD.SDR NACA2022122300002Unknown · unknown#2 ENGINE BLADE #19 HAS SMALL NICK NEAR BLADE TIP. BLENDED SMALL NICK ON #2 ENGINE FAN BLADE IAW B767 CF6-80C ENGINES AMM 72-31-02 BLADE FOUND WITHIN SERVICEABLE LIMITS FOR NDT SEE LOG PAGE #B067604 (GOOD)SDR NACA2022122703002Blade · not reportedFANBLADE REPAIR, PENDING PAPERWORK.SDR NACA2022122703001Filter · faultedON CLIMBOUT, LEFT ENGINE FUEL FILTER EICAS MSG MOMENTARILY APPEARED. MSG DISAPPEARED AFTER 15 SECONDS. REPLACED LEFT ENGINE FUEL FILTER AND TESTED, NO LEAKS FOUND AMM 73-11-06 ETOPS GROUND VER COMPLIED WITHSDR 2022F00522Psu · sparksFLIGHT ATTENDANT STATED THAT SPARKS AND A BURNING ODOR HAD BEEN OBSERVED AT THE PSU AREA ABOVE SEAT 14 KJ. INSPECTED AND FOUND A 3 WIRE BUNDLE OF WHAT I ESTIMATE TO BE 22 TO 24 GAUGE WIRE. ONE WIRE IN THE BUNDLE HAD SHORTED BY CONTACT WITH A FASTENER HEAD ABOVSDR NACA2022121700002Apu · shutdownAPU AUTO SHUTDOWN. CONNECTED EXTERNAL POWER IAWM B767 AMM 24-00-00 PERFORMED APU BITE IAW AMM 49-11 FAULT TREE 960, OPS CHECK NORMAL.SDR NACA2022121700001Boot · tornAPU FORWARD LOAD CONTROL VALVE RUBBER BOOT TORN. REPLACED LOAD CONTROL VALVE FWD RUBBER BOOT IAW 49-11-01, NO LEAKS NOTED.SDR NACA2022121600001Fuel Feed · erraticLH ENGINE FUEL FLOW ERRATIC WHEN ENG ANTI-ICE TURNED ON. CLEANED AND RESECURED CONNECTORS D17066, D4210 AND D4212 PER WDM 73-31-11. ENG GROUND TEST AND OPS TEST OK AND OBSERVED ON FLIGHTS, FF LH ENG SYS OK NO ISSUES.SDR NACA2022121500001Cabin Air Sys · leakingLEFT AND RIGHT DUCT PRESSURE WAS OSCILLATING BETWEEN 25 TO 45 PSI FROM 1000 TO 10000 FEET DURING CLIMBOUT. INSPECTED AND LEAK CHECKED BOTH LEFT AND RIGHT AC SYSTEMS. FOUND AIR LEAK BETWEEN RIGHT PACK HEATER AND CONDENSER, REPLACED PACKING PER AMM 21-51-07, BOTSDR IXXA20221209149Battery · inoperativeFLASHLIGHT ON CENTER COUNSEL INOPERATIVE. SYSTEM DEFERRED 36969, MEL CAT C. REMOVED AND REPLACED CENTER CONSOLE FLASHLIGHT BATTERY IN ACCORDANCE WITH B767 MAINTENANCE MANUAL 25-64-02. OPERATIONAL CHECK GOOD. DEFERRAL 36769 CLEARED.SDR NACA2022120800002Indicator · erraticLEFT ENGINE FUEL FLOW ERRATIC ON CLIMBOUT WITH ANTI-ICE ON. NORMAL WITH ANTI-ICE OFF. DEFERRED PER MEL 73-31-0102 CAT C.SDR NACA2022120800001Coupler · failedLEFT HF INOP. REMOVED AND REPLACED LH HF COUPLER PER AMM 23-11-01 OPS CHECK GOOD. RH COUPLER REPLACED FOR PRECAUTIONARY REASONS.SDR NACA2022120700001Transceiver · failedHF #1 WILL NOT TRANSMIT. DEFERRED PER MEL 23-11-01-02A. REMOVED AND REPLACED HF#1 TRANSCEIVER.SDR NACA2022120600001Shutoff Valve · failedSUPPLEMENTAL INFORMATION. REMOVED AND REPLACED RH ENG HPSOV IAW B767 AMM 36-11-07 PENDING HPSOV INSTALLATION TEST STEP H (GOOD). PART IS UNKNOWN TO TRAX.SDR NACA120600001Shutoff Valve · warning messageEICAS MSG R ENG HPSOV ON FINAL APPROACH, STATUS MESSAGE. DEFERRED PER MEL 36-11-02-02 CAT C ON 12/7/2022 @ 0100Z. COMPLIED WITH MX PROCEDURESSDR NACA2022120300001Ecu · faultedDURING PREFLIGHT CHECK APU FAILED TO START, TWO ATTEMPTS. ACCOMPLISHED FIM 49-11 FAULT TREE 958, CLEARED ECU FAULTS. APU OPS CHECKED GOOD PER AMM 49-11-00SDR NACA2022120200002Indicator · erraticL ENGINE FUEL FLOW INDICATION ERRATIC WHEN ENGINE ANTI-ICE IN USE. 4.5-6.5 FF. DEFERRED [PER MEL 73-31-01-02 CAT C @ 0600Z 12/2/22SDR NACA2022120200001Relay · trippedRIGHT AFT FUEL PUMP EICAS MSG. PERFORMED FIM 28-22 FAULT TREE 831. RE-CYCLED RH AFT FUEL BOOST PUMP RESET RELAY AND CHECK OK.SDR NACA2022112500001Fuel Sys · erraticL ENGINE FUEL FLOW ERRATIC ON CLIMB OUT WITH ENGINE ANTI-ICE SELECTED ON. FLOW FROM A STABLE 13.0 DROPS TO 6.5 AND IN-BETWEEN. CLEANED CANNON PLUG ON LH FUEL FLOW TRANSMITTER PER BOEING SWPM 20-60-01 OPS CHECK GOOD PER AMM 71-00-00 TEST 3.SDR NACA2022112400001Mec · failed#1 ENGINE FUEL LEAKS OUT OF GAUGE FROM THE DRAIN MAST. REMOVED AND REPLACED #1 ENG MEC PER AMM 73-21-01, ACCOMPLISHED INSTALLATION UNTIL AMM 73-21-6SDR IXXA20221123148Unknown · smokeDURING GROUND LOADING, CREW REPORTED SMOKE IN FLIGHT DECK. WORK IN PROGRESS.SDR IXXA20221121147Battery · inoperativeDURING SCHEDULED PRE-DEPARTURE MAINTENANCE, CONSUL EMERGENCY FLASHLIGHT BATTERY INDICATOR LED NOT FLASHING. SYSTEM DEFERRED 36304 MEL CAT C. REMOVED AND REPLACED CENTER PEDESTAL EMERGENCY FLASHLIGHT BATTERY IAW B767 AMM 25-64-02. OPERATIONAL CHECK GOOD. DEFERSDR IXXA2022111400001Frame · cracked#2 ENGINE OUTBOARD CORE COWL AFT LOWER INTERNAL CORNER ATTACH ANGLE AND TRIANGLE GUSSET MISSING RIVETS SHEARED.SDR NACA2022110900001Unknown · malfunctionedFWD CABIN TEMP CONTROL INOP. PERFORMED FWD CABIN TEMPERATURE CONTROLLER BITE TEST PROCEDURE PER FIM 21-61 FAULT TREE 803, OPS CHECK NORMAL NO FAULT NOTED AT TIME.SDR IXXA2022110901Panel · delaminatedVERT. STAB LH PANEL DELAMINATEDSDR NACA2022110700001Unknown · leakingDURING SHUTDOWN NR 1 ENGINE THERE WAS A STATIC FUEL LEAK. AFTER SHUTDOWN #1 ENGINE STATIC LEAK HAS STOPPED. THERE IS NO FUEL LEAK, IT IS WITHIN LIMITS REF AMM 73-21-00-602SDR NACA2022110500001Connector · failedAS PER CUSTOMER REQUEST, RIGHT ENGINE EGT INDICATION (ECM ALERT). FOUND CONNECTOR D10990 IN BAD CONDITION AND CHANNEL B WIRE BARE, FOUND LOWER THERMOCOUPLE DAMAGE AND 3 PROBES QUIT READING. REPLACED CONNECTOR D10990, THERMOCOUPLE 3,4,5 AND REPLACED RIGHT ENGINSDR IXXA20221109145Door · openCABIN ALTITUDE EICAS WARNING (CABIN WOULD NOT HOLD PRESSURIZATION). CABIN AUTO INOPERATIVE EICAS CAUTION MESSAGE WITH INTERMITTENT MASTER AURAL WITH NO ASSOCIATED DISCRETE LIGHT EICAS ALERT. AIR TURN BACK TO DEPARTURE STATION. EMERGENCY DECLARATION WITH NO ASDR IXXA2022110402Stabilizer · delaminatedVERTICAL L/E PANEL DIRECTLY BELOW 322BL R/H SIDE IS DELAMINATED IN 4 AREAS ON INTERNAL SKIN FOUND DURING CURSORY INSPECTION.SDR IXXA2022110401Bracket · crackedRH #7 SLAT TORQUE SHAFT SUPPORT CRACKEDSDR NACA2022102800001Bleed Valve · faultedON PUSHBACK OUT OF MDSD WE TRIED TO START THE RIGHT ENGINE BUT WE COULD ONLY GENERATE 11.6 N2, DUCT PRESSURE WAS 20PSI. MI DUE TO ABOVE @MDSD 1826Z. DEFERRED APU BLEED VALVE ON 10/28 @ 1845Z CAT C, MX PROCEDURES COMPLIED WITH. REMOVED AND REPLACED APU SURGE SDR NACA2022102700002Pump · faultedLEFT FORWARD PUMP FUEL PRESSURE LIGHT INOP IN FLIGHT. PERFORMED OPS ON LH FWD BOOST PUMP LOW PRESSURE LIGHT PER AMM 28-22-00. OPS CHECK LH FWD BOOST PUMP LO PRESSURE LIGHT NORMAL. INFO: LH FWD BOOST PUMP LOW PRESSURE LIGHT WOULDNOT COME ON IF APU OPERATING IN SDR NACA2022102700001Terminal · damagedR HPSOV DEFERRED ON LOGPAGE B063815 ITEM P1 AS REFERENCE MEL 36-11-02-02 CAT C. REPAIRED TERMINAL CONNECTION ON RIGHT ENGINE HPSOV PER WFM36-11-62 AND OPS CHECK GOOD PER AMM 36-11-00SDR IXXA2022110301Frame · crackedL/H FRAME STA 883.5 THE LOWER END OF FRAME COMMON TO STUB BEAM IS CRACKEDSDR IXXA202210254141Battery · inoperativeDURING PRE-DEPARTURE CHECK FOUND CENTER CONSOLE FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IN ACCORDANCE WITH MAINTENANCE MANUAL 25-64-02. OPERATIONAL CHECK GOOD.SDR IXXA2022110801Skin · corrodedCORROSION ON UPPER SKIN OF HORZ STAB BOX BETWEEN RIB 1 AND 2R AT FWD AREASDR NACA2022102100001Igniter · wornLEFT ENGINE NO LIGHT OFF W ENGINE START SELECTOR IN #2 POSITION. PERFORMED QRH ABORTED ENG START CHECKLIST, MOTORED ENGINE AND RESTARTED WITH ENG SELECTOR SET TO BOTH. FOUND #2 IGNITOR PLUG WORN. REMOVED AND REPLACED #2 IGNITOR PLUG ON #1 ENGINE PER AMM 74-21-SDR IXXA2022111701Panel · crackedP33 BACK PANEL CRACKED AT LOWER LEFT TRIANGLE DOUBLERSDR NACA202210240001Warning Message · illuminatedAFT CABIN TEMP, FWD CABIN TEMP, FLT DECK TEMP EICAS MESSAGES APPEARED DURING CRUISE FLIGHT. PERFORMED BITE PER AMM 21-61-00, CLEARED FAULT, PERFORMED AC OPERATIONAL TEST PER AMM 21-00-00, NO FAULTS NOTED.SDR NACA2022101800001Hose · damagedLH ENGINE THROTTLE CABLE COOLING HOSE DAMAGED. REMOVED AND REPLACED LH ENGINE THROTTLE CABLE COOLING HOSE REF BOEING AMM 76-11-02SDR NACA20221024001Drain · leakingLEFT ENGINE LEAKING FUEL APPROX 1 DROP EVERY 2-3 SECONDS. PERFORMED TS PER AMM 71-71-00, LOCATED FUEL LEAKS FROM MEC DRIVE PAD DRAIN REF AMM 71-71-00. ALLOWABLE LEAK IS 48 DROPS PER MINUTE, FUEL LEAK FROM MEC DRIVE PAD DRAIN IS WITHIN LIMITS.SDR NACA2022101700002Duct · damaged#1 ENGINE LEFT INBOARD CORE COWL DUCT HAS INTERNAL DAMAGE AND MATING LIP WORN. REMOVED #1 ENGINE LEFT IB CORE COWL DUCT. INSTALLED #1 ENGINE LEFT IB CORE COWL DUCT IAW AMM 71-11-06SDR NACA2022101700001Precooler · damaged#1 ENGINE PRECOOLER HAS INTERNAL DAMAGE. REMOVED #1 ENG PRECOOLER IAW MM 36-11-15, INSTALLED #1 ENGINE PRECOOLER IAW AMM 36-11-15 NO LEAKS NOTED.SDR IXXA2022101801Channel · corrodedL/H HORZ STAB TIP FOUND AFT O/B "C" CHANNEL TO BE CRACKED WITH PIECES MISSING, AND AFT O/B UPPER AND LWR NUT PLATE CHANNEL CORRODED 100% MATERIAL LOSSSDR IXXA2022101601Skin · delaminated# 11 SLAT HAS DELAM ON UPPER WEDGE. TAP TEST BAD.SDR IXXA2022101403Stringer Clip · crackedSTRINGER CLIP CRACKEDSDR IXXA2022101401Floor Panel · crackedBILGE FLOOR PANEL CRACKEDSDR NACA2022101300001Probe · faultedL ENG EEC LIGHT AND A/T DISCONNECT IN FLIGHT. COMPLETED QRH AND TURNED R EEC OFF AS DIRECTED. PERFORMED EEC MONITOR UNIT BITE, FOUND T2 ENG RANGE MSG. PERFORMED FIM 71-01 FT 823, REMOVED AND REPLACED T2 TEMP PROBE PER AMM 73-21-06. EEC GROUND TEST PER AMM 73-2SDR IXXA2022101204Access Door · cracked#2 PYLON OB HYDRAULIC BAY DOORSDR IXXA2022101202Skin · delaminated#4 SLAT DELAMINATED
Back to Boeing 767-323