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 2004UALA00281Slide · unserviceableDOOR 1 LEFT SLIDE RAFT PRESSURE AT 2500 PSI. REPLACED 1L DOOR ESCAPE SLIDE.SDR 2004UALA00280Battery Pack · dischargedEMERGENCY EXIT LIGHTS INTERMITTENT ROWS 15-18 LEFT SIDE. REPLACED EEL BATTERY POWER SUPPLY PACK.SDR 2004UALA00264Battery Pack · inoperativeRIGHT EMERGENCY LIGHT PATH INOP FROM 15 THROUGH ROW 18. REPLACED EMERGENCY LIGHT BATTERY PACK, CHECKED OK.SDR 2004UALA00263Support · crackedRIGHT INBOARD FLAP, CENTER SUPPORT IS CRACKED ON THE LOWER INBOARD FLANGE AT THE MID FLAP ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR TO HINGE FITTING.SDR 2004UALA00262Fitting · crackedRIGHT INBOARD T/E FLAP, MAIN FLAP INBOARD T/E HINGE FITTING SUPPORT CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCMENT REPAIR ANGLE TO HINGE FITTING.SDR 2004UALA00259Stiffener · crackedSTA 246 FLOORBEAM VERTICAL STIFFENER IS CRACKED AT LBL 23. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STIFFENER.SDR 2004UALA00258Hinge · crackedLEFT WING INBOARD FLAP MAIN TO AFT FLAP HINGE IS CRACKED ON BOTH SIDES. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIRS.SDR 2005UALA00243Compressor · stalledFLIGHT ABORTED TAKEOFF DUE TO A COMPRESSOR STALL IN THE NR 1 ENGINE. ABORTED TAKEOFF AT 100 KIAS DUE TO COMPRESSOR SURGE. ENGINE REPLACED AT EZE. UA TURBINE SHOP FINDINGS: N2 WILL NOT ROTATE. ALSO, BORESCOPE INSPECTION REVEALED HEAVY HPC 5TH STAGE BLADE DSDR 2004UALA00213Warning Light · illuminatedSTABILIZER TRIM ADVISORY ILLUMINATED DURING TAKEOFF ROLL. UNABLE TO DUPLICATE DURING TROUBLE SHOOTING. ACCOMPLISHED ADDITIONAL TROUBLE SHOOTING AS A PRECAUTION. NO FAULTS FOUND. NO ADDITIONAL INCIDENTS NOTED.SDR 2004UALA00170Warning System · activatedRETURNED TO FIELD DUE TO SLAT ASYMMETRY MESSAGE. OUTBOARD SLAT NR 10 POSITION SENSOR OUT OF LIMITS. ADJUSTED SENSOR.SDR 2004UALA00152Light · inoperativeEXTERIOR EMERGENCY LIGHT INOP AT LT FUSELAGE AFT OF TRAILING EDGE. RELAMPED, CHECKED OK.SDR 2004UALA00167Wire · damagedWIRE DAMAGE AFT CARGO PIT STA 1230. THERE WAS NO CONCLUSIVE INDICATION OF WHAT INITIATED THE WIRE DAMAGE. THERE WAS NO APPARENT CHAFING. THERE WERE METAL CHIPS NOTED IN THE AREA, BUT NONE FOUND DIRECTLY ON OR BELOW THE WIRE BUNDLE. IT IS UNKNOWN, AS TO WHETHERSDR 2004UALA00133Light · inoperativeEMERGENCY EXIT LIGHT AT NR 2AB ROW INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT, OPS OK.SDR 2004UALA00131Autothrottle Sys · malfunctionedFLIGHT ABORTED TAKEOFF AT 100 KTS DUE TO AUTOTHROTTLE INDICATION. RETURNED TO BLOCKS. THRUST MANAGEMENT COMPUTER WAS REMOVED AS A PRECAUTION. UNIT CHECKED OK IN THE SHOP. MCDP FAULT DATA DID NOT RECORD ANY TMC-RELATED FAULTS DURING THE EVENT. REASON FOR TSDR 2004UALA00118Jackscrew · failedFLIGHT DIVERTED DUE TO LEFT PACK TEMPERATURE CONTROL MESSAGE AND LIGHT. THE LEFT PACK INLET ACTUATOR WAS FOUND MECHANICALLY FROZEN. THE JACK SCREW ASSEMBLY FAILED. THE ACTUATOR WAS REPLACED AND NO FURTHER PROBLEMS WERE REPORTED.SDR 2004UALA00111Light · inoperativeEXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE, 4TH LIGHT AFT OF OVERWING, LT SIDE. RELAMPED. CHECKS GOOD.SDR 2004UALA00097Module · malfunctionedRETURNED TO FIELD DUE TO RUDDER RATIO/AILERON TRIM MESSAGE. REPLACED BOTH STABILIZER TRIM/AILERON LOCKOUT MODULES.SDR 2004UALA00089Access Door · lightning strikeFUSELAGE EXTERIOR AT MAIN EQUIPMENT CENTER, ACCESS DOOR 119AL HAS LIGHTNING STRIKE DISCHARGE ON EXISTING DOUBLER. MAJOR REPAIR ACCOMPLISHED. DOOR REPAIRED WITH NEW DOUBLER.SDR 2004UALA00088Hinge · crackedRIGHT INBOARD FLAP CENTER HINGE, OUTBOARD FLANGE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE FITTING.SDR 2004UALA00055Skin · gougedLEFT HORIZONTAL STAB LOWER SKIN IS GOUGED AT OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2004UALA00049Battery · inoperativeEMERGENCY EXIT PATH LIGHTS ROW 15-17 BLINK ON AND OFF. REPLACED M737 BATTERY ASSEMBLY.SDR 2004UALA00417Warning System · activatedFUEL CONFIGURATION LIGHT ON 1 HOUR INTO FLIGHT. FUEL IMBALANCE.SDR 2004UALA00415Squib · blownRT OVERWING SLIDE DOOR SQUIB BLOWN. SQUIB BLOWN IN CONJUNCTION WITH INADVERTANT SLIDE DEPLOYMENT. SQUIB REPLACED.SDR 2004UALA00047Wedge · dentedT/E WEDGE DENTED ON UPPER SURFACE OF NR 4 SLAT. MAJOR REPAIR. REPLACED WITH NEW T/E WEDGE.SDR 2004UALA00419Light · malfunctionedEEL LIGHTS BLINKING FROM ROWS 20 TO 28 CHECKED SYSTEM PER WDM33-51-11 & 33-51-14, SPLICES SM42, SM41,SM5 OVER M1559 OK. SPLICES SM44, SM43 & SM45 OVER M1556 ALSO OK.SDR 2003UALA00978Wire · brokenEMERGENCY LIGHT INOP AT DR1 FWD CROSSAISLE. REPLACED BROKEN FEEDER CABLE. OPS CKD NORMAL.SDR 2003UALA00967Light · inoperativeEXTERIOR EMERGENCY LIGHT INOPERABLE AT DOOR 4L. RELAMPED, OPS CHECKED NORMAL.SDR 2003UALA00948Skin · crackedCRACK ON FWD UPPER PYLON SKIN INSIDE ACCESS PNL 432BR, NR 1 ENG. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00946Skin · dentedTWO EACH SKIN DENTS WITHIN 22 INCHES OF E&E BAY DOOR, ONE BETWEEN STATION 303 & STATION 325 (STR35L). MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 51-00-01.SDR 2003UALA00947Bolt · missingRETURN TO FIELD DUE TO GEAR DISAGREEMENT EICAS MESSAGE. DAMAGE INCURRED FROM HANGING BRAKE ROD AFTER SEPARATION FROM BRAKE. ROD BELIEVED TO HAVE DETACHED FROM TORQUE ARM DUE TO MIGRATION OF BRAKE TORQUE ARM PIN. SAFETY BOLT BELIEVED TO HAVE COME LOOSE OR POSDR 2003UALA00936Wire Harness · damagedEMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT NEAR GALLEY 402. ACCOMPLISHED WIRE BUNDLE REPAIR PER MM 33-51-10-301. DEVICE WORKS FINE.SDR 2003UALA00929Battery Pack · misinstalledRIGHT EMERGENCY ESCAPE SLIDE SQUIB WILL NOT TEST. EVENT CAUSED BY IMPROPERLY INSTALLED BATTERY PACK.SDR 2003UALA00951Line · failedC-HYDRAULIC SYSTEM QTY SLOWLY DECREASING. LEFT MAIN GEAR HYDRAULIC LINE FOUND LEAKING AT UPPER TRUNNION LOCATION. RESERVICED CENTER SYSTEM TO NORMAL. RYNGLOK REPAIR ACCOMPLISHED ON BRAKE HYDRAULIC LINE/TUBE. SPECIFIC HYDRAULIC LINE AND CAUSE OF LEAK NOT IDESDR 2003UALA00916Battery Pack · malfunctionedLT SIDE OF CABIN EEL LIGHT FLOOR PATH LIGHTING IS INOP INCLUDING OVERWING EXIT MARKERS STARTING AT COACH SEATS. REPLACED BATTERY PACK. TESTS OK.SDR 2003UALA00897Stiffener · crackedFLOORBEAM STATION 246 STIFFENER IS CRACKED AT LBL 26, FWD SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER PER SRM 51-40-2 AND BAC DWG 141T5814.SDR 2003UALA00896Skin · crackedNR 2 PYLON OUTBOARD SIDE, FWD TORQUE BOX, NACELLE STA 240 AND WL 150, EXTERIOR SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SIDE SKIN WITH DOUBLER-TRIPLER PER SRM 54-53-01.SDR 2003UALA00895Hinge · crackedRIGHT WING INBOARD FLAP, AFT FLAP HINGE MID ATTACH FITTING, OUTBD AND INBD SIDES CRACKED AT LOWER ENDS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE PER SRM 57-53-02, FIG 201 AND REINSTALLED FITTING PER MM 27-51-06.SDR 2003UALA00894Seat Track · corrodedSEAT TRACK BETWEEN STA 764-784, LBL 62 IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF SEAT TRACK AND FABRICATED SPLICE REPAIR PER BAC DWG 145T2222-4 AND SRM 51-40-2.SDR 2003UALA00888Attach Fitting · crackedLT WING, INBOARD FLAP, AFT FLAP MID ATTACH FITTING IS CRACKED ON OUTBOARD AND INBOARD SIDES, T/E FLAP HINGE FITTING. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING PER SRM 57-53-02, FIG 201.SDR 2003UALA00882Skin · dentedBULK CARGO DOOR LOWER AFT SKIN IS DENTED AND GOUGED BS 1450. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00865Fitting · crackedLEFT WING INBD FLAP CENTER EXTERNAL HINGE FITTING CRACKED ON INBD SIDE FLANGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE FITTING PER SRM 57-53-02, FIG 201 AND INSTALLED REPAIR PER SRM 51-40-2.SDR 2003UALA00859Wire · wornEMERGENCY EXIT LIGHTS - FLOOR STRIPS ON. ALSO FLASHING ON AND OFF. FOUND SEVERAL LOCATIONS WHERE STRIP WAS TORN AND PINS PUSHED IN. REPAIRED WITH SPLICE TOOL. OPS CK NORMAL.SDR 2003UALA00853Hinge · crackedRT WING INBD FLAP CENTER HINGE EXTERNAL IS CRACKED ON BOTH SIDES, (FLANGE REAR SPAR MID FLAP). MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE FITTING PER SRM 57-53-02, FIG 201. INSTALLED FITTING PER MM 27-51-06.SDR 2003UALA00850Hinge · crackedLT WING INBOARD T/E FLAP EXTERNAL CENTER HINGE CRACKED ON INBD SIDE. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE PER SRM 57-53-02, FIG 201 AND REINSTALLED FITTING PER MM 27-51-06.SDR 2003UALA00840Hinge Fitting · crackedRIGHT WING INBOARD FLAP AT CENTER HINGE FITTING IS CRACKED BROKEN. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING PER SRM 51-40-2 AND 57-53-02, FIG 201.SDR 2003UALA00836Battery Pack · not seatedRIGHT WING OVERWING SLIDE SQUIB FAILS TO TEST. RESEATED BATTERY PACK ON RIGHT SIDE, TESTS OK.SDR 2003UALA00827Screw · looseNR 2 ENGINE FLAMEOUT. FLAME OUT WAS CAUSED BY FUEL LEAK AT THE AIR/OIL COOLER MUSCLE LINE. THE FUEL MUSCLE LINE WAS REPLACED AND THE ENGINE WAS REMOVED WITH IN 25 CYCLES DUE TO A SURGE ABOVE 1.25 EPR CAUSED BY THE FLAME OUT. THE MUSCLE LINE FAILED DUE TO VIBRSDR 2003UALA00831Compressor · leakingNR 1 ENGINE SURGE ON TAKEOFF. ENGINE SELF RECOVERED AND CONTINUED NORMAL OPERATION. ENGINE EXPERIENCED GROUP 3 SURGE ON TAKE OFF. CAUSE OF THE SURGE IS OPEN CLEARANCES IN THE REAR OF THE HPC. FINAL FIX FOR SURGE ISSUES IS THE OVERHAUL OF THE ENGINE TO A RINGSDR 2003UALA00825Relay · failedLT OVERWING EXIT FAILS SQUIB-SPOILER TEST. SQUIB FAILED TEST DUE TO INTERMITTENT RELAY K839. REPLACED RELAY AND SQUIB TESTED OK. RELAY WAS PART NUMBER 3SAH1326A2 OR BACR13CE2 .SDR 2003UALA00807Radar · inoperativeRETURNED TO FIELD DUE TO INOP WEATHER RADAR. THE WX RADAR R-T. SHOP FINDINGS FOR THE REMOVED WX RADAR R-T WERE LOW POWER OUT. THIS CONDITION WAS CORRECTED IN THE SHOP BY REALIGNING THE FREQUENCY MULTIPLIER OF THE UNIT.
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