Boeing 767-281
Service difficulty reports · 1,831
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 = '767281' 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 = '767281' 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 ABXA060301Fitting · crackedFITTING CRACKED ON STA 168 CANTED BULKHEAD AT FORWARD NOSE LANDING GEAR ATTACH POINT LEFT SIDE. REPLACED FITTING IAW B767 SRM 51-40-02.SDR ABXA060265Bulkhead · dented2 DENTS/GOUGES IN AFT PRESSURE BULKHEAD, AFT SIDE, BETWEEN RS7 AND 8, AND BETWEEN TS6 AND INNER RING. REPAIRED DAMAGE AREA IAW SRM 53-80-08.SDR ABXA060231Rod · damagedAIRCRAFT HAS ROUGH VIBRATION SHAKES LEFT TO RIGHT. INSPECTED LEFT AND RIGHT WING FLAPS AND FAIRINGS, AILERONS, SLATS, ELEVATORS. PERFORMED VISUAL INSPECTION OF NR 1 ENGINE AND CHIP DETECTOR, NO FINDINGS. INSPECTED NR 2 ENGINE, CHIP DETECTOR (MASTER) AND COWSDR ABXA060259Window Frame · crackedRT UPPER CABIN WINDOW CRACKED. FIRST WINDOW FORWARD OF THE EMERGENCY EXIT DOOR. REPLACED CABIN WINDOW IAW AMM 56.SDR ABXA060224Slide · looseL-2 DOOR SLIDE ASSY WAS LOOSE FROM PACKBOARD. DEFERRED DI 51091. REMOVED SLIDE ASSY FROM PACKBOARD AND INSTALLED BALLAST ASSY PER MM PROCEDURE REF 52-11-4-2. DEFERRED L2 DOOR SLIDE ASSY PER MEL 52-11-4-2D, CAT B, CODE 8. PLACARD INSTALLED ON GREEN ARMING LSDR ABXA060223Beam · crackedNOSE WHEEL VERTICAL BEAM AT STA287 RBL25 HAS A .5 INCH CRACK AT WL173. FOUND CRACK WHILE COMPLETING NEA5313001-001, WO 600251505 NR104. REPAIRED IAW B767 SM 51-70-12.SDR ABXA060202Frame · crackedWHILE ACCOMPLISHING A REPETITIVE EDDY CURRENT INSPECTION TO THE RIGHT OUTER CHORD AT BULKHEAD STA. 1809, SEVERAL CRACKS WERE CONFIRMED. REPAIRED RIGHT OUTER CHORD PER J.C.'S 53800002-001, 002, 003, AND W/O# 600251128.SDR ABXA060197Structure · missingDURING MAINTENANCE POST FLIGHT INSPECTION, FOUND THE LEFT WING LEADING EDGE OUTBOARD THERMAL ANTI-ICE DUCT SEAL DOOR MISSING. REPLACED ANTI-ICE DUCT SEAL DOOR IAW B767 MM 57-41-58-04. OPS CHECKED NORMAL.SDR ABXA060198Skin · cracked5/16 INCH CRACK IN PRESSURIZED SKIN AT STA. 441, LONGERON S32L. CRACK EXTENDED OUT OF RIVET HEAD. FURTHER INVESTIGATION REVEALED LONGERON S32L CRACKED BEHIND SKIN CRACK FROM RIVET TO RIVET. TRANSFERRED TO DAMAGE WO 600252246. OPEN: TEMP REPAIRED IAW REA B653-5SDR ABXA060228Strap · corrodedUPPER SPAR CAP STRAP AT RT WING STA 792 HAD INTERGRANULAR CORROSION. REPAIRED AREA IAW REA B657-54341.SDR ABXA060227Shear Tie · corrodedFRAME CORRODED AT STA 1219 BETWEEN S38-47R. REMOVED AND REPLACED SHEAR TIE IAW B767 SRM 51-40-02.SDR ABXA060196Wire · chafedCIRCUIT BREAKER P15 ON P11 PANEL FOR AUTO 1 CABIN ALTITUDE CONTROL TRIPPED, WOULD NOT RESET. FOUND BURNED WIRING ADJACENT TO OUT FLOW VALVE A/C MOTOR. REMOVED, REPAIRED AND/OR REPLACED DEFECTIVE WIRING AS NECESSARY PER ABX 767 WDM 21-31-31, 21-31-21, 21-31-1SDR ABXA060242Bulkhead · dentedDENT IN AFT PRESSURE BULKHEAD (NEA53800006-787AX1) WAS OUT OF LIMITS IAW B767 SRM 53-80-08. REPAIRED DENT IN AFT PRESSURE BULKHEAD IAW B767 SRM 53-80-08. WORK ACCOMPLISHED ON JC 2024 T-3. CUT OUT 1 INCH PO 408452415. 24 EA BACR15BB5 FASTENERS.SDR ABXA060240Attach Angle · crackedTWO EA NOSE RIB TO LEADING EDGE ATTACH ANGLES CRACKED AT NR 8 SLAT OUTBOARD DRIVE CUTOUT. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-02.SDR ABXA060241Spar · corrodedRIGHT WING REAR SPAR AREA HAD PANEL STRUCTURE WITH CORROSION UNDER NUT PLATES. AREA WAS PREVIOUSLY BLENDED AT WBL 280 NEAR INBOARD AILERON. REPAIRED CORRODED AREA OF SPAR IAW B767 SRM 57-51-02.SDR ABXA060186Odor · detectedSTRONG ODOR OF BURNING ELECTRICAL EQUIPMENT FOLLOWED BY INCREASING TEMPERATURE FROM UNDER CAPTAIN'S SEAT AND BACK OF LEGS AND FEET. NO EICAS MESSAGES OR OTHER INDICATIONS OF A FIRE. BOTH FIRE BOTTLES WERE DISCHARGED PRIOR TO EVACUATING AIRCRAFT. INSPECTED CSDR ABXA060255Skin · corrodedLEFT LEADING EDGE AT STA 740 WAS CORRODED IN 3 SPOTS. REMOVED AND REPLACED NOSE BEAM IAW B767 SRM 51-40-02.SDR ABXA060185Fitting · crackedDURING SCHEDULED LINE INSPECTION, FOUND THE LEFT AFT OUTER CHORD, LEFT HORIZONTAL STABILIZER, STA 1809.5, CRACKED. REPAIRED CHORD IAW B767 SB 53A0078, REV 4, FIG 3 & 4, AND ABX REA B653-5399-MR.SDR ABXA060249Attach Angle · crackedNR 2 ENGINE PYLON TRAILING EDGE FAIRING AFT OUTBOARD ATTACH ANGLE WAS CRACKED. REMOVED AND REPLACED ANGLE IAW B767 SRM 51-40-02.SDR ABXA060248Intercostal · corrodedLEFT INTERCOSTAL WAS CORRODED JUST OUTBOARD OF LEFT MAIN LANDING GEAR. REMOVED AND REPLACED LEFT INTERCOSTAL IAW B767 SRM.SDR ABXA060173Battery Pack · inoperativeL1 DOOR EMERGENCY LIGHTS INTERIOR AND EXTERIOR INOP. SWAPPED BATTERY PACKS FROM M735 & M736 POWER SUPPLIED L1 DOOR EMERGENCY EXIT LIGHTS OPC GOOD IAW ABX 767 AMM 33-51-07. REPLACED M736 POWER SUPPLY BATTERY PACK WITH NEW BATTERY PACK ACQUIRED FROM DELTA OPC SDR ABXA060247Stiffener · crackedRIGHT BUTT LINE NOSE WHEEL WELL VERTICAL STIFFENER AT STA 287 WAS CRACKED APPROX 14 INCHES DOWN FROM TOP. REPAIRED AREA IAW B767 SRM 51-70-12.SDR ABXA060246Skin · corrodedRIGHT INBOARD FLAP TRAILING EDGE PANEL BULGED AROUND NUMEROUS FASTENERS. REPLACED RIGHT INBOARD FLAP ON NR 0121 IAW B767 SRM.SDR ABXA060154Circuit Card · faultyMAIN CARGO SMOKE DETECTION SYSTEM FAILS SELF TEST. REMOVED AND REPLACED AFOLTS CARD M2026 IAW FIM 26-14-00 AND OPS CHECK GOOD IAW MM 26-14-00.SDR ABXA060153Circuit Card · malfunctionedFIRE DETECTION BELL COMES ON INTERMITTENTLY ON ITS OWN, AND THEN WOULD NOT COME ON WHEN TESTED, VERIFIED. REMOVED AND RESEATED BELL CHIME CARD (M1000) IN P51 PANEL IAW B767 AMM 26-10-00 PERFORMED BITE PROCEDURE 26-16-00-10, NO PROBLEMS AT THIS TIME. FIRE WARSDR ABXA060152Girt Bar · contaminatedENTRY DOOR SLIDE WILL NOT ARM. CLEANED METAL SHAVING FROM GIRT BAR: DOOR CLOSED AND LOCKED NORMALLY, METAL SHAVING WAS FROM "C" CONTAINER.SDR ABXA060236Fitting · crackedRIGHT WING HAD BROKEN FITTING LOCATED BETWEEN AFT MAIN LANDING GEAR TRUNNION AND FALSE SPAR OUTBOARD OF RIGHT MAIN LANDING GEAR PIVOT POINT. REMOVED AND REPLACED FITTING IAW B767 SRM 51-40-2.SDR ABXA060235Beam · crackedNR 2 PYLON OUTBOARD BEAM WAS CRACKED AT AFT LATCH PIN RECEPTACLE. REPAIRED AREA IAW REA B654-53516-MR.SDR ABXA060234Skin · damagedRIGHT OUTBOARD ELEVATOR: HOLE RUBBED IN LEADING EDGE. REPAIRED AREA IAW REA B655-53514.SDR ABXA060089Battery Pack · inoperativeEMERGENCY LIGHTS FAIL SATURDAY AM DEEP CYCLE TEST. REPLACED EMERGENCY LIGHTS MAIN BATTERY PACK IAW B767 AMM 33-51-07-2. CHECKS AND TESTS GOOD AS PER SAME.SDR ABXA060022Actuator · overheatedSMOKE IN COCKPIT AT AROUND 30,000 FT. RAM AIR DOOR ACTUATOR OVERHEATED (BEARINGS). REPLACED ACTUATOR.SDR ABXA050241Rib · corrodedLT WING LEADING EDGE RIB AT STA. WA 920 (APPROXIMATELY) HAD EXFOLIATED CORROSION AT FORWARD END AND LOWER FLANGE LOWER SURFACE. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-01.SDR ABXA050216Battery · dischargedAIRCRAFT EMERGENCY LIGHTING SYSTEM INOPERATIVE (SPARE BATTERY). REMOVED AND REPLACED EMERGENCY LIGHT SPARE BATTERY PACK. OPS CHECKED GOOD IAW B767 MM 33-56-35.SDR ABXA050210Selector Valve · bindingINBOUND TO ILN DID A GEAR RECYCLE. GEAR DISAGREE LIGHT WITH THREE GREEN. FOUND SHAFT ON MAIN LANDING SELECTOR VALVE BINDING. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE IAW B767 AMM 32-31-02-4. OPS AND LEAK CHECKED GOOD.SDR ABXA050207Battery · dischargedEMERGENCY LIGHTS INOPERATIVE. SWAPPED EMERGENCY LIGHT BATTERY WITH SPARE. OPS CHECKED GOOD IAW B767 AMM 33-00.SDR ABXA050202Fuel Control · defectiveON TAKEOFF ROLL, RIGHT ENGINE FAILED TO PRODUCE TAKEOFF POWER. WITH LEFT ENGINE ACCELERATING NORMALLY. RIGHT ENGINE STOPPED ACCELERATING AT 58 PERCENT N1. REMOVED AND REPLACED RIGHT ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-4. PERFORMED ENGINE RUN, SDR ABXA050201Module · defectiveWITH GEAR HANDLE DOWN, 3 GREEN LIGHTS. GEAR DISAGREE ILLUMINATED AND GEAR DISAGREE MESSAGE. GEAR RECYCLED. LANDING GEAR HANDLE MODULE WAS REMOVED AND REPLACED IAW BOEING MM.SDR ABXA050209Door · stiffMAIN ENTRY DOOR WOULD NOT OPEN ABOVE FLIGHT. ADJUSTED BUSTLE AS NEEDED. OPS CHECKED DOOR SIX TIMES. OPS CHECKED GOOD.SDR ABXA050185Odor · detectedFORWARD EQUIPMENT COOLING EICAS MESSAGE DISPLAYED AS WELL AS NO COOLING LIGHT. ACRID SMELL IN COCKPIT ABOUT 5 MINUTES BEFORE LIGHTS DISPLAYED. CREW REPORTED THIS HAPPENED JUST BEFORE LANDING. EQUIPMENT COOLING WAS IN OVERRIDE. DUE TO CONFIGURATION, THIS COSDR ABXA050165Slide · damagedEMERGENCY SLIDE ON MAIN PASSENGER DOOR WOULD NOT STAY IN POSITION. REMOVED AND REPLACED DOOR ESCAPE SLIDE IAW B767 AMM 25-66-01-4. PLACARD REMOVED.SDR ABXA050122Slide · deployedLIFE RAFT SLIDE DEPLOYED WITHOUT BEING ARMED. THE LOWER FORWARD ENTRY DOOR HUNG WHILE TRYING TO CLOSE IT. WHEN THE DOOR WAS RAISED FOR RE-CLOSURE, THE SLIDE DEPLOYED. INSPECTED DOOR AND GIRT BAR ATTACHMENTS. NO DEFECTS NOTED. REMOVED AND REPLACED SLIDE ASSDR ABXA050125Warning Light · intermittentEMERGENCY DOOR LIGHT FLASHED INTERMITTENTLY IN TURBULENCE. FOUND EMERGENCY DOOR LIGHT FLICKERING ON GROUND. NO EICAS MESSAGE. CODE 007 ON PSEU. RESEATED CARD 3 AND 4 IN PSEU. RETESTED PSEU IAW B767 MM 32-09-04. NO FAULTS NOTED. DOOR LIGHT EXTINGUISHED.SDR ABXA050113Light · inoperativeL1 DOOR EMERGENCY EXTERIOR LIGHT WAS INOP. RELAMPED AND SEALED LENS TO L1 DOOR EMERGENCY LIGHT. OPS CHECKED GOOD.SDR ABXA050121Drag Brace · crackedRIGHT MAIN LANDING GEAR DRAG BRACE LUG HAD CRACK INDICATION REF: EA 32110006-001. REPLACED RIGHT MAIN LANDING GEAR IAW DC-9 MM.SDR ABXA050096Connector · corrodedEMERGENCY LIGHT AT L1 POSITION (EXTERNAL) INOPERATIVE (GROUND ILLUM) L388. CLEANED CORROSION AT CONNECTOR IAW B767 MM 33-51-06. OPS CHECKED GOOD.SDR ABXA050095Battery · dischargedDURING AM CHECK, FOUND EMERGENCY LIGHT WOULD NOT STAY ON FOR MORE THAN 5 MINUTES. SWAPPED BATTERIES, NO HELP. CHECKED VOLTAGE AT CHARGER IAW AMM 33-51-07-2, CHECKED GOOD. CHARGED BATTERIES FOR MORE THAN 4 HOURS. OPS CHECKED GOOD.SDR ABXA050092Bushing · dirtyWHEN LOWERED, THE GEAR HAD 3 GREEN LIGHTS WITH A GEAR DISAGREE LIGHT. LANDED WITH GEAR DISAGREE LIGHT, STAYED ON UNTIL PARKED. SWUNG GEAR AND VERIFIED GEAR DISAGREE LIGHT REMAINED ON WITH GEAR DOWN AND LOCKED. ISOLATED PROBLEM TO DIRTY GEAR LEVER BUSHING. CLSDR ABXA050034Wedge · delaminatedWHILE PERFORMING LINE MAINTENANCE, FOUND LEFT WING NR 4 SLAT WEDGE DELAMINATED BEYOND LIMITS AT INBOARD END. REPLACED NR 4 SLAT IAW B767 MM 27-81-02-4.SDR ABXA050025Warning Light · illuminatedEICAS MESSAGE GEAR DISAGREE DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GEAR DOWN LIGHTS ILLUMINATED. INITIALLY THERE WAS NO RIGHT MAIN GREEN LIGHT DOWN. THE LIGHT CAME ON DURING RETURNING FOR APPROACH. PERFORMED BITE OF PSEU AND FOUND LANDING GEAR LEVESDR ABXA050005Fitting · crackedLEFT FORWARD OUTER CHORD FITTING CRACKED PER DETAILED VISUAL INSPECTION IAW JC NEA53800004-001 AND AD 2001-09-13. REPAIRED LEFT FORWARD OUTER CHORD FITTING IAW S/B 767-53A-0078.
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