Boeing 767-381
Service difficulty reports · 259
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 = '767381' 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 = '767381' 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 2023FA0000828Skin · unknownR/H HORIZONTAL STABILIZER LOWER SURFACE, STAB STA 95.5 - A DENT WITH A SCRATC.SDR 2023FA0000827Unknown · unknownPYLON #1, L/H CORE COWL, AFT FRAME, BETWEEN 2 AND 3 O'CLOCK - CUT OUT WITH CRACK.SDR 2023FA0000826Unknown · unknownENGINE #2, PRIMARY EXHAUST OUTER SKIN, BETWEEN NAC STA 317 AND NAC STA 349 - GOUGE AND 2 DENTS.SDR 2023FA0000825Unknown · unknownAFT PRESSURE BULKHEAD, STA 1582+7.5" 8-9 O'CLOCK - DENTS WITH SHARP CREASE.SDR 2023FA0000824Unknown · unknownAFT PRESSURE BULKHEAD, STA 1582+7.5", 3 O'CLOCK - TORN STIFFENER AND DAMAGE WEB WITH DENTS AND CREASES.SDR 2023FA0000823Unknown · unknownSEC 41, STA 347 TO STA 390, STR 36L TO STR 37L - SEVERAL BLEND OUTS ON FUSELAGE EXTERNAL SKINSDR 2023FA0000822Unknown · unknown.ENGINE #2, INLET COWL, ACOUSTIC PANEL, PERFORMED SKIN, UNDOCUMENTED 3 EXISTING FILLING REPAIRSSDR IXXA20231204087Unknown · unknownDURING PRE-FLIGHT INSPECTIONS AND MAINTENANCE LINE TECH REPORTED AFT FLIGHTDECK EMERGENCY FLASHLIGHT INOPERATIVE. LED NOT FLASHING AND NO ILLUMINATION WHEN REMOVED FROM BRACKET. AFT FLIGHTDECK EMERGENCY FLASHLIGHT BATTERY REMOVED AND REPLACED IAW B767 AIRCRAFSDR MK1Y202312207018Unknown · unknownREPAIR - ENGINE #2 LH CORE COWL WEAR STRIP WITH CORRPSION DAMAGESDR MK1Y20231127017Unknown · unknownREPAIR - FUSELAGE SKIN, SEC 48, STA 1654.5, STR 16L-17L - EXISTING PROTRUDING HEAD RIVETSDR 2023FA0000793Unknown · unknownREPAIR - LH THRUST REVERSER SKIN AFT EDGE EXISTING TRIM OUTS BETWEEN 8/11 O'CLOCKSDR 2023FA0000792Unknown · unknownREPAIR - ENGINE #1, INLET COWL, INNER LIP SKIN, EXISTING FLUSH DOUBLER, P/N 224-2101-573HLSDR 2023FA0000791Unknown · unknownREPAIR - #1 ENGINE EXHAUST NOZZLE OUTER SLEEVE OUTER SKIN DAMAGESDR MK1Y20231127013Unknown · unknownEVALUATION - ENGINE #2 - LOWER TRUCK FAIRING, INBD SIDE - FOUND EXISTING DOUBLER REPAIR, BETWEEN NAC STA 202.5 - NAC STA 215.5 AND AT 6 O'CLOCKSDR MK1Y20231127012Unknown · unknownEVALUATION - STRUT #2 - UPPER INBD SIDE - HINGE FITTING ACCESS PANEL 425GZ - FOUND EXISTING DOUBLER REPAIRSDR MK1Y20231127010Unknown · unknownEVALUATION - PREVIOS REPAIR ON THE ENGINE #2 INLET COWL, LOWER PANEL ASSY, ANTI-ICE EXHAUST DUCT, AT 6 HRSSDR MK1Y202311270101Unknown · unknownEVALUATION - ENGINE #2 - NACELLE STRUT PANELS INBD SIDE - FOUND EXISTING DOUBLER REPAIR, PANEL 447ELX AND 446CL, STRUT #2SDR MK1Y20231127009Unknown · unknownEVALUATION - STRUT #2 - UPPER TRUCK FAIRING, INBD SIDE - FOUND EXISTING DOUBLER REPAIRSDR MK1Y20231127008Unknown · noneEVALUATION - EXISTING REPAIRS, ACCESS PANEL 437 ELX, 437ERX, 436CL, 436CR, #1 ENGINE STRUTSDR MK1Y20231127007Unknown · unknownREPAIR - ENGINE #2, OUTBD CORE COWL, EXISTING DOUBLER ON CORE COWL SKIN, P/N 224-2302-545SDR MK1Y20231127006Unknown · unknownEVALUATION - ENGINE #2 - OUTBD SIDE, THRUST REVERSE UPPER AND LOWER TRACK FAIRINGS - FOUND EXISTING DOUBLER REPAIRSDR MK1Y20231127005Unknown · unknownEVALUATION - ENGINE #1 - OUTBD SIDE, CORE COWL TITANIUM FAIRING - FOUND EXISTING DOUBLER REPAIR, BETWEEN NAC STA 293.5 - NAC STA 300.5SDR MK1Y20231127004Unknown · unknownEVALUATION - ENGINE #1 - LOWER AND UPPER TRACK FAIRING, OUTBD SIDE - TWO EXISTING DOUBLER REPAIRS, BETWEEN NAC STA 207 - NAC STA 212, AND AT 6 AND 12 O'CLOCKSDR MK1Y20231127003Unknown · unknownEVALUATION - ENGINE #2 - NACELLE STRUT PANELS OUTBD SIDE - FOUND EXISTING DOUBLER REPAIR, PANEL 447ERXSDR MK1Y20231127002Unknown · unknownREPAIR - ENGINE #2 EXHAUST NOZZLE OUTER SLEEVE OUTER SKIN DAMAGESDR MK1Y20231127001Unknown · unknownEVALUATION - ENGINE #1 - INBD SIDE, THRUST REVERSER UPPER AND LOWER TRACK FAIRINGS - FOUND EXISTING DOUBLER REPAIR.SDR IXXA20231120081Unknown · unknownFORWARD EMERGENCY FLASHLIGHT INOPERATIVE. EMERGENCY FLASHLIGHT BATTERY REMOVED AND REPLACED PER B767 AMM 25-64-02. OPERATIONAL CHECK GOOD.SDR IXXA20231027077Unknown · unknownFOLLOWING LE SLAT ASYM EICAS AND LEADING EDGE LIGHT INDICATIONS CREW ABORTED APPROACH. PRIOR TO SECOND APPROACH, KCLT AIR TRAFFIC CONTROL TOWER DECLARED EMERGENCY. LANDING WAS WITHOUT INCIDENT AND ON ARRIVAL THE AIRCRAFT WAS GROUNDED FOR MAINTENANCE. POST FLIGSDR 2023FA0000680Unknown · unknownFOUND GOUGE AND DEEP NICKDAMAGE ON ENGINE #1 INLET COWL ACOUSTIC PANEL LOWER SEGMENT.SDR 2023FA0000679Unknown · unknownFOUND EXISTING REPAIR ON ENGINE #2 TRANSLATING COWL LH SIDE LOWER AFT FAIRING (BEAVERTAIL).SDR 2023FA0000678Unknown · unknownFOUND 2 EXISTING UNDOCUMENTED DOUBLER REPAIRS ON ENGINE #1 INLET COWL ANTI ICE ACCESS PANELSDR 2023FA0000677Unknown · unknownFOUND EXISTING DOUBLER REPAIR ON ENGINE #1 PRIMARY EXHAUST SKIN AT LH SIDE.SDR IXXA20230911057Unknown · unknownDURING CLIMB THRU 27,000 LEFT ENGINE SURGE. EGT HIT 937. CREW COMPLIED WITH QRH PROCEDURES LEVELED AT 28,000 AND SURGING ABATED. AUDIBLE POPS DURING CLIMB AND DESCENT. AROUND 17,000 FT AIRFRAME VIBRATIONS WERE NOTED. BOTH CLIMB AND DESCENT IN THE 60% N2 BAND.SDR IPXA2023091401301Door · corroded*SUPPLEMENTAL SDR* FAULT: CREW ENTRY DOOR FRAME UPPER HAS CORRODED FASTENERS. DOT 140-44 CLEANED PER SOPM 20-30-03 STEP 9. CREW ENTRY DOOR, NO DAMAGE WAS FOUND, NO MATERIAL LOST, ONLY PAINT WAS REMOVED REVIEWEDSDR IPXA2023091401292Door · corrodedCREW ENTRY DOOR FRAM UPPER AT PLACARD HAS CORROSION. DOT 140-43 REMOVED CORROSION IN PLACERD IAW SRM 53-00-15-1A-1 NOMINAL THICKNESS 0.032" MATERIAL LOSS .003" REMAINING THICKNESS 0.029" FOUND TO BE IN LIMITS. T89336. TREATED AND PRIMED AREA IAW SRM 51-20-01-0SDR IPXA2023091401281Door · corroded*SUPPLEMENTAL SDR* FAULT: MCD FWD OPENING ROD INBD END CORRODED. DOT 140-42 AFTER FURTHER EVALUATION NO CORROSION NOTED. CLEANED MCD FWD OPENING ROD WITH SCOTCH BRITE AND ALCOHOL. IAW SOPM 20-30-03. TREATED AND PRIMED AFFECTED AREA ON OPENING ROD. IAW SRM 51-2SDR IPXA2023091401252Door · corrodedFWD LARGE CARGO DOOR FRAME UPPER FWD CORNER CORRODED AND AT BONDING LOCATION. DOT 140-40 REMOVED CORROSION FROM FWD LARGE CARGO DOOR FRAME NEXT TO BONDING LOCATION. USED ULTRA SONIC (T89336) AND IS WITHIN LIMITS. NOMINAL THICKNESS .071, REMAINING MATERIAL .06SDR IPXA20230911301Unknown · unknown*SDR FILED OPEN* FAULT: CREW ENTRY DOOR FRAME UPPER HAS CORRODED FASTENERS. DOT 140-44 VERIFIED AREA CLEANED AND NO DAMAGE FOUND. WORK COMPLETED.SDR IPXA20230911252Unknown · unknown*SDR FILED OPEN* FAULT: FWD LARGE CARGO DOOR FRAME UPPER FWD CORNER CORRODED AND AT BONDING LOCATION. DOT 140-40 VERIFIED C.I.C. APPLIED.<BR>WORK COMPLETED.SDR IPXA20230911292Unknown · unknown*SDR FILED OPEN* FAULT: CREW ENTRY DOOR FRAM UPPER AT PLACARD HAS CORROSION. DOT 140-43 VERIFIED APPLIED TOPCOAT WORK COMPLETED.SDR IPXA202309111281Unknown · unknown*SDR FILED OPEN* FAULT: MCD FWD OPENING ROD INBD END CORRODED. DOT 140-42 VERIFIED APPLIED TOP COAT. WORK COMPLETED.SDR IPXA2023090328518Unknown · unknownR ENG HPSOV ON EICAS AFTER STARTING THE RIGHT ENGINE AFTER PUSHBACK RESULTED IN A BTB ** OII 2 ** (LINKED TO T3F18E002BZ2A) DEFERRED IAW MEL 36-11-2-2SDR ABXA20230822177Unknown · unknownAFTER BOTH ENGINES STARTED FWD EQPT VAL EICAS MESSAGE AND VALVE DISCRETE LIGHT ON EQUIP COOLING PANEL ILLUMINATED. QRH PROCEDURE DID NOT CLEAR THE MESSAGE AND LIGHT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPAIRED BROKEN GRD WIRE GD12SDR ABXA2023040346Valve · stickingR ENGINE BLEED OFF EICAS MESSAGE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED PRSOV IAW AMM 36-11-09. INSTALLED NEW SERVICEABLE R/H PRSOV ON #2 ENGINE IAW B767 AMM 36-11-09 A/C REMAINS NO ETOPS OPS CHK GOOD. AIRCRAFT RETSDR ABXA20230331045Unknown · unknownSET PARKING BRAKE AFTER PUSH BACK BUT NO PARK BRAKE LT ILLUMINATED AND NO PARK BRAKE ON EICAS APPEARED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE CLEANED CANNON PLUG OPERATED BRAKES SEVERAL TIMES OPS CK NORMAL IAW 32-44-00. AIRCRAFT RETURSDR ABXA2023032337Unknown · unknownCAPTAIN ALTIMETER OFF FLAG APPEARED DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND RESEATED CAPT ALTIMETER CANNON PLUG OPS NORMAL OF CAPT ALTIMETER PER B767 AMM 34-13-01 NO DEFECTS AC IS RVSM COMPLIANT. AIRCRAFT RETURNSDR ABXA2023032036Unknown · unknownLEFT THRUST REV GREEN LIGHT COMES ON, HOWEVER HANDLE DID NOT GO PAST INTERLOCK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPERATIONAL TEST OF BOTH LEFT AND RIGHT REVERSER SYSTEMS. BOTH MESSAGES CLEARED . OPS CHECK GOOD. REF B767SDR ABXA2023011612Display · odorFO'S EHSI DISPLAY FAILED INFLIGHT AFTER FAILURE STRONG ODOR OF BURNT ELECTRONICS. AIRCRAFT COMPLETED FLIGHT AND LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE GROUNDED AIRCRAFT. MAINTENANCE REMOVED AND REPLACED COPILOTS EHS DISPLAY IAW B767 AMM 31-41-01 OPS CHESDR IPXA2023011289809Eec · faultedATB, EMERGENCY DECLARED, LEFT ENGINE FAILURE ON T/O. ENGINE RECOVERED. PERFORMED FIM TASK 71-01-00-810-994-H01 REV 138.00. DUE TO PIMU FAULT CODE 160-14. REPLACED EEC IAW AMM 73-21-15 PB 401 REV 138.01. FOUND OPS TEST SATIS.SDR ABXA2022128149None · noneRABBIT STRIKE ON T/O ABORTED 120KTS. AIRCRFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. INSPECTION C/O IAW AMM 05-41-01 NO DEBRIS FOUND, NO DAMAGE. SATISFACTORY. AIRCRAFT RETURNED TO SERVICE
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