Boeing 767-306
Service difficulty reports · 2,510
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 = '767306' 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 = '767306' 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 ABXA20241218263Warning Message · illuminatedWHILE TAXIING R REV ISLN VAL MSG AFTER ENG START,AC RETURNED TOGATE (BTB) AND MTX GROUNDED AC , MTX DEFERRED RH T/R FOR DEPARTURE IAW MEL ABX-78-31-1, AND RETURNED AC TO SERVICE . AND AC DEPARTEDSDR ABXA20241207245Control Panel · failedDURIING CRUISE BOTH FD BARS FAILED LATERAL GUIDANCE FD BAR APPEARED, BUT DID NOT GIVE PROPER GUIDANCE FROM MCP. AIRCRAFT DIVERTED TO SFO. MAINTENANCE GROUNDEDTHE AIRCRAFT. MAINTENANCE RPLEACED MODE CONTROL PANEL PER 767 AMM 22-11-02,, MCDP TEST 04 PASSED, AIRCSDR ABXA20241206243Start Valve · faultedDURING TAXI OUT RH ENGINE START VALVE WOULD NOT OPEN FOR ENGINE START . AC RETURNED TO GATE (BTB)AND MTX GROUNDED AC AND DEFERRED THE START VALVE FOR DEPARTURE IAW MEL ABX-80-00-2-1 . RETURNED AC TO SERVICE AND AC DEPARTED .SDR UIEA2024111301084Warning Message · false indicationON APPROACH CENTER PRIMARY HYD PUMP #1 EICAS MSG(<P>PERFORMED TROUBLESHOOTING AND OPS CHECKS IAW FIM 29-11 FAULT TREE 810. OPS CHECK GOOD, NO C/B'S POPPED, COULD NOT DUPLICATE. NO FURTHER MX REQUIRED.</P>)SDR ABXA20241023201Target · missingAC DURING APPROACH DURING LANDING CHECKLIST EICAS "MSG LE SLAT ASYM " CREW CALLED FOR A GO-AROUND AND MISSED APPROACH, AFTER GO AROUND RECEIVED " STICK SHAKER " ADJUSTED SPEED AND FLAP SETTING FOR LANDING . CAPTAIN DECLARED EMERGENCY AND LANDED . MTX GROUNDSDR UIEA2024101801054Skin · dentedINBOARD TRAILING EDGE FLAP RH WING , UPPER SIDE INNER CORNER WITH DENTS(<P> RH WING INBOARD AFT FLAP DENT 1 WAS EVALUATED AND FOUN WITHIN ALLOWABLE LIMITS IAW SRM 57-53-01-1A-1 TABLE I NOTE C DETAIL IV DOT 89020 WAS INSTALLED AS PER ATLAS AIR GMM 3.19.1.</P> /SDR UIEA2024102101057Heater · inoperativeRIGHT SIDE WINDOW HEAT INOP FLIGHT DECK WINDOW HEAT SYSTEM, #2 SIDE WINDOWS(<P>RIGHT SIDE WINDOW HEAT INOP FLIGHT DECK WINDOW HEAT SYSTEM, #2 SIDE WINDOWS WAS REPLACED, ADJUSTED AND OPERATIONAL CHECK WAS PERFORMED IAW AMM 56-11-02-004-001 REV. 143 DATE: 22 AUGSDR UIEA2024102101058Fitting · crackedLH WING, INTERNAL FIXED LEADING EDGE, NEAR LES 281.82 WITH CRACK IN TORQUE TUBE GUIDE(<P>TORQUE TUBE GUIDE FITTING ASSY WAS REPLACED IAW SRM 51-10-02-0G-0, NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024102101059Skin · crackedRH OUTBOARD ELEVATOR, LEADING EDGE AREA, BETWEEN ELEV STA188.221 AND ELEV STA 261.665 WITH CRACK(<P>RH OUTBOARD ELEVATOR WAS EVALUATED AND REPAIRED IAW SRM 55-20- 02-2R-1 FIG. 201 AND SRM 51-70-04-0G-0 PAR. 5A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024102101060Light · no discrepancyEXTERIOR EMERGENCY LIGHTS INOP(<P>EXTERIOR EMERGENCY LIGHTS OPERATIONAL TEST WAS PERFORMED, TEST SATISFACTORY IAW AMM 33-51-00-715-001 REV 143 DATE 22-AUG-2024 </P>)SDR UIEA2024102101061Fire Seal · degradedENGINE 2, LH THRUST REVERSER, IDG OIL SERVICE ACCESS DOOR, INNER AREA, DEGRADED FIRE SEAL.(<P>SEAL WAS REPAIRED IAW AMM 78-31-00-308-072-H00 REV 143 22-AUG-2024. NO FURTHER DEFECTS NOTED</P>)SDR ABXA20241018200Controller · faultedDURING TAXI #2 ENG START SELECTOR, SELECTED TO " GROUND" "VALVE" LIGHT DID NOT APPEAR ON THE SINGLE + BOTH POSITION. AC RETURNED TO THE GATE AND WAS GROUNDED BY MTX. MTX THEN DEFERRED THE RH ENGINE START CONTROL IAW MEL ABX-80-00-2-1 RETURNED AC TO SERVICE ,ANSDR ABXA20241012188 RPcb · faultedAT GATE: MAIN CARGO DECK FIRE INDICATED FOR 10 SECONDS. EICAS, DISCRETE LIGHTS, AURAL WARNING , CREW PERFORMED QRH AND PULLED EVERYONE FROM AC AND CALLED ARFF THEY CLEARED FOR REENTRY AND WAS SUSPECTED FALSE WARNING .AFTER LOADING RESUMED A SECOND FULL FIRE WASDR ABXA20241012188Pcb · failedAT GATE: MAIN CARGO DECK FIRE INDICATED FOR 10 SECONDS. EICAS, DISCRETE LIGHTS, AURAL WARNING , CREW PERFORMED QRH AND PULLED EVERYONE FROM AC AND CALLED ARFF THEY CLEARED FOR REENTRY AND WAS SUSPECTED FALSE WARNING .AFTER LOADING RESUMED A SECOND FULL FIRE WASDR ABXA20241011186Tat Probe · failedCREW REPORTED EICAS MSG "TAT PROBE" INFO: NO A/T, NO L NAV, NO V NAV DURING CLIMB STAGE AND PERFORMED AN AIR TURNBACK. MTC GROUNDED THE AIRCRAFT , REMOVED AND REPLACED TAT PROBE IAW B767 AMM 34-12-02 OPS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.SDR ABXA20241004184Iru · faultedDURING TAXI OUT EICAS MESSAGE R IRS FAULT AND DESCRETE CAME ON AC RETURNED TO THE GATE AND MTX GROUNDED AC .MTX DEFERRED THE R IRU IAW MEL ABX-34-21-1-1-2A. AND RETURNED AC TO SERVICE AND AC DEPARTED .SDR ABXA20240930180Pin · out of positionSTAB TRIM EICAS MESSAGE AND DESCRETE LIGHT AFTER ENGINE START WHILE TAXI OUT ,AC RETURNED TO GATE AND MTX GROUNDED AC. MTX FOUND PINS 2&3 SWAPPED ON PRESSURE SWITCH 527. CONNECTED PINS. REF BOEING SWM 20-61. STAB TRIM FUNCTIONS & INDICATIONS CORRECT REF B7676SDR ABXA20240917176Hydraulic Line · leakingDURING CRUISE, STARTED TO LOOSE CENTER HYD QTY , PILOT DECLARED EMERGENCY AND DIVERTED TO NEAREST AIRPORT( KMSY ) AND LANDED SAFELY. AC WAS .MTX GROUNDED AC AND BEGAN LOOKING FOR HYD LEAK PERFOMED TAIL SKID SYSTEM TEST PER AMM 32-71-00, DURING TEST AND GEAR HSDR UIEA2024080400788Line · leakingCREW O2 PRESSURE 10PSI. FND 1ST OBS O2 BOX SUPPLY LINE LEAK. REPLACED LINE IAW AMM 35-00-00 & LEAK CHK OK. R/R CREW O2 BOTTLES IAW AMM 12-15-08 & LEAK CHECK GOOD. PART VERIFIED PER IPC 35-11-00 ITEM 1.SDR ABXA202408064149Warning Message · false indicationDURING TAXI STAB TRIM EICAS MESSAGE APPEARED IN ONT. A/C RETURNED TO THE GATE AND MTX GROUNDED A/C, AND DEFERRED STAB TRIM MEASEAGE IAW MEL ABX-27-41-2. AND RETURNED AC TO SERVICE AND A/C DEPARTED . MTX PERFORMED STAB TRIM OPS CHECK IAW B767 AMM 27-41-00 OPSSDR UIEA2024080200766Bulb · inoperativeBACKLIGHTING FOR EMERG LIGHT PAX OXY PANEL ONLY 1/2 ILLUMINATED. REPAIRED LIGHTPLATE & REPLACED BULBS PER SWPM 20-40-00. OPS CK OK PER 33-13-01.SDR ABXA20240720141Drive Assy · malfunctionedON TAXI OUT, WX RADAR FAIL AND STAB LIGHTS AND WXR SYS STATUS MESSAGE, RETURNED TO BLOCKS. AND MTX GROUNDED A/C L/H SYSTEM TEST OK R/H SYS TEST OK. OPERATED WXR L/H SYS FAILED, R/H SYS INTERMITTENT. REMOVED CONTROL PWL CONNECTOR. NO DEFECTS NOTED. REINSTALLED SDR ABXA20240719138Module · malfunctionedAFTER TAKEOFF AT V1 THE FIRE BELL SOUNDED WITH NO OTHER INDICATION INDICATING A FIRE WAS UNABLE TO SILENCE THE BELL. A/C PRFORMED ATR AND RETURNED TO THE GATE WHERE MTX GROUNDED A/C . PERF AFOLTS TEST PER AMM 26-10-00. NO DEFECTS NOTED. PERF BACU BITE CK 2SDR UIEA2024061800527Lens · brokenCABIN CREW ENTRY, LOWER PANEL LEFT SIDE, EMERGENCY SIGN LENS, BROKEN(<P>EMERGENCY SIGN LENS FROM CABIN CREW ENTRY WAS REPLACED IAW AMM 33-51-02-412-003 REV 142 DATE 22 APR 2024</P>)SDR UIEA2024061800528Fuel Cell · leakingRH WING LOWER SURFACE, FUEL LEAK AT STRINGER 15R, BWTN WBL 97.95 AND 197.4(<P>RH WING LOWER SURFACE, FUEL LEAK AT STRINGER 15R, BWTN WBL 97.95 AND 197.4. FUEL LEAK WAS REPAIRED, IAW AMM 28-11-00-308-013 REV 142 22APR24. THE FUEL LEAK TEST SATISFACTORY.</P>)SDR UIEA2024061800529Stiffener · crackedSECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 FWD FACE OF WEB WITH CRACK ON STIFFENER LBL 36.(<P>SECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 FWD FACE OF WEB WITH CRACK ON STIFFENER LBL 36 WAS FABRICATED IAW DRAWING 141T5170 AND ORDER M6753450 ISSUED SDR UIEA2024061800530Stiffener · crackedSECTION 41 FLOOR STRUCTURE, FLOOR BEAM B. STA 246 REAR FACE OF WEB WITH CRACK ON STIFFENER LBL26.(<P><SPAN>SECTION 41 FLOOR STRUCTURE, </SPAN><SPAN>FLOOR BEAM B. STA 246 REAR FACE OF WEB </SPAN><SPAN>WITH CRACK ON STIFFENER LBL26. STIFFENER </SPAN><SPAN>WAS RESDR UIEA2024061800531Skin · corrodedLH WING, UPPER SURFACE SKIN BETWEEN WS.1046.2 AND WS.1075.2 SAFETY LINE ATTCH POINT WITH POINTS OF CORROSION.(<P>LH WING, UPPER SURFACE SKIN BETWEEN WS.1046.2 AND WS.1075.2 WAS REPAIRED IAW SRM 57-20-01-2R-7 FIG 201 SHEET 1 PAG 1-2 AND SRM 51-70-17-2R-4 REPAIRSDR UIEA2024061800532Hinge · crackedEXTERNAL FUSELAGE, CRACK ON DOOR AND HINGE OF CARGO HANDLING PANNEL(<P>EXTERNAL FUSELAGE, CRACK ON DOOR AND HINGE OF CARGO HANDLING PANNEL. BROKEN HINGE IS REMOVED AND THE HINGE IS REPLACED WITH A NEW ONE IAW SRM 51-40-02-0G-0 REV 125 15APR24, SRM 51-10-02-0G-SDR UIEA2024061800533Lanyard · missingLH WING, FIXED LEADING EDGE STRUCTURE AREA FUELING STATION (PANEL 521 QB) LANYARD OF CAP (COLOR RED) MISSING.(<P>THE LANYARD OF FUEL CAP ADAPTER WAS REPLACED IAW AMM 28-11-04-404-019 REV: 142 DATE: 22-APR-24</P>)SDR UIEA2024061800534Door · puncturedLH WING, FIXED LEADING EDGE STRUCTURE AREA INNER SIDE FUELING STATION DOOR WITH ONE PUNCTURED.(<P>LH WING, FIXED LEADING EDGE STRUCTURE AREA INNER SIDE FUELING STATION DOOR WAS REPAIRED IAW SRM 57-41-01-2R-1 FIG 201 SHEET 3 PAG 2-4 & SRM 51-70-17-0G-0 PAR 4B FSDR UIEA2024061800537Floor Panel · crackedZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.(<P>ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.WAS PERFORMED REPAIRED IAW SRM 53-00-53-SDR UIEA2024061800539Access Panel · damagedLEFT WING, REAR SPAR, PANEL ACCESS 551UB, ABOVE MAIN LANDING GEAR RETRACT ACTUATOR, CLAMP OVER HYDRAULIC LINE DAMAGED(<P>LEFT WING, REAR SPAR, PANEL ACCESS 551UB, ABOVE MAIN LANDING GEAR RETRACT ACTUATOR, OVER HYDRAULIC LINE CLAMP WAS REPLACED IAW AMM 20-10-11SDR UIEA2024061800540Panel · unknownUPPER HALF FUSELAGE, MAIN DECK CARGO, CEILING PANELS FROM B.STA 800 TO B.STA 1400, SMOKE DETECTION SYSTEM, CEILING PANELS, OBSTRUCTED SEVERAL INTAKE ORIFICES, EVALUATION(<P>UPPER HALF FUSELAGE, MAIN DECK CARGO, CEILING PANELS FROM B.STA 800 TO B.STA 1400, SMOKSDR UIEA2024061800541Skin · crackedRH WING, SLAT 10, CRACK ON UPPER AND LOWER SKIN OSS 723.94(<P>RH WING, SLAT 10, CRACK ON UPPER AND LOWER SKIN OSS 723.94. THE TEAR ON THE SKIN OF THE SLAT #10 WAS REPAIRED IAW 53-43-01-2R-2 REV 125 15APR24, AMM 30-11-06-404-009 REV 142 22APE24, AMM 27-81-02-42SDR UIEA2024061800542Floor Panel · damagedZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE.(<P>ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE WAS REPAIRED IAW SRM 53-00SDR UIEA2024061800543Floor Panel · damagedZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124AXF, MISSING MATERIAL AFT RIGHT CORNER, CRACK ON RIGHT LATERAL EDGE (NEAR LOCK) AND MISSING MATERIAL FWD RIGHT CORNER(<P><SPAN>ZONE 100, LOWER HALF FUSELAGE, </SPAN><SPAN>FORWARD CARGO COMSDR UIEA2024061800544Door · leakingEXTERNAL FUSELAGE, LEAK ON LH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF EXTERNAL FUSELAGE, LH </SPAN><SPAN>EMERGENCY EXIT DOOR WAS REPLACED IAW </SPAN><SPAN>AMM 52-09-06-404-003 REV 142, APR 22, 2024. </SPAN><SPAN>CHECK FOR LEAKS WAS PERFORMED, NO FOUND </SPAN><SPSDR UIEA2024061900553Door · leakingEXTERNAL FUSELAGE, LEAK ON LH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF EXTERNAL FUSELAGE, LH </SPAN><SPAN>EMERGENCY EXIT DOOR WAS REPLACED IAW </SPAN><SPAN>AMM 52-09-06-404-003 REV 142, APR 22, 2024. </SPAN><SPAN>CHECK FOR LEAKS WAS PERFORMED, NO FOUND </SPAN><SPSDR UIEA2024061800545Seal · leakingEXTERNAL FUSELAGE, LEAK ON RH EMERGENCY EXIT DOOR.(<P><SPAN>SEAL OF RH EMERGENCY EXIT DOOR </SPAN><SPAN>WAS REPLACED IAW AMM 52-09-06-404--</SPAN><SPAN>003 REV 142, APR 22, 2024; CHECK FOR LEAKS </SPAN><SPAN>WAS PERFORMED, NO LEAKS FOUND</SPAN></P>)SDR UIEA2024061800546Frame · crackedCRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE.(<P>CRACK INDICATION FOR PLUG PREVIOUSLY INSTALLED AT FRAME, STA 456 AND STGR 26L, SEE PICTURE. WAS REPAIRED IAW TRE6753695 ISSUED DATE JUN 08/2024, FVCI CONTROL# 24088-SDR UIEA2024061900551Support Angle · corrodedAFT FUSELAGE SECTION 48, CORROSION ON INTERNAL SKIN, BSTA 1725.5, BETWEEN STRINGERS 7 RH AND 6 RH, BELOW APU INTAKE DOOR(<P>AFT FUSELAGE SECTION 48, BSTA 1725.5, BETWEEN STRINGERS 7 RH AND 6 RH, BELOW APU INTAKE DOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02SDR UIEA2024061900554Stringer · damagedSECTION 43, HIDDEN DAMAGE (NICK) IN STGR 26LH STA 456(<P>SECTION 43, HIDDEN DAMAGE (NICK) IN STGR 26LH STA 456. THE STRINGER SEGMEMT WAS REPLACED PER SRM 51-10-02-0G-0 PAR 9 REV 125 15APR24 AND SRM 51-40-02-0G-0 REV 125 15APR24.</P>)SDR UIEA2024051400390Connector · faultedREJECTED TAKEOFF DUE TO NO AUTO THROTTLE AFT ENGAGING, EPR, AND V SPEEDS. DELETE TMC ANNC LIGHT(<P>REMOVED AND REPLACED CONNECTOR D4224P REF WDM 73-21-11. OPS CHECK GOOD AT THIS TIME.</P>)SDR UIEA2024051000374Warning Message · false activationREJECTED T/O IN MIA, LOW SPEED, DUE TO T/O CONFIG WARNING FOR STAB TRIM. STAB TRIM WAS SET PROPERLY AND SUBSEQUENT T/O WAS SUCCESSFUL.(<P>NOTED BY MX AS PRECAUTIONARY. PERFORMED TAKE OFF CONFIGURATION WARNING TEST PER AMM 31-51-00. OPS CHECK GOOD.</P>)SDR UIEA2024050100328Servo · faultedAIRCRAFT DID NOT ACCELERATE THROUGH 10000 FT IN VNAV (ATB)(<P>PERFORMED MCDP TEST 30 & 40, FAULTING NO INFC. FCC C ELEV SRVO CMD REF AMM 22-00-02. REF LOGPAGE 1742397 ITEMS M7 & M8 FOR CTR AUTOPILOT ELEVATOR SERVO REPLACEMENT. REMOVED AND REPLACED FCC CENTER ESDR UIEA2024031300145Oxygen Mask · faultedAT DEPARTURE CREW NOTIFIED FO'S MIC STUCK ON.(<P>R/R FO'S O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD, LEAK CHECK GOOD.</P>)SDR UIEA2024031400146Oxygen Mask · inoperativeO2 MASK INOP SUPERNUMERARY, TRANSFERRED TO MDDR 204626 PER MEL 35-11-03-02A. O2 MASK FAILED TO TEST. FOUND STOWED INCORRECTLY. RESTOWED O2 MASK AT SUPERNUMARY SEAT CLOSEST TO LAV IAW AMM 35-11-51. OPS TEST GOOD IAW AMM 35-11-00. THIS CLEARS MDDR 204626, PLACASDR UIEA2024030600143Button · stuckOBSERVER INTERCOM WILL NOT TRANSMIT USING HEADSET MIC.(<P>FOUND RESET TEST BUTTON STUCK ON OXYGEN MASK BOX. REMOVED AND REPLACED OBSERVER OXYGEN MASK BOX IAW AMM 35-11-51. PERFORMED HEADSET MIC OPS CHECK IAW AMM 23-51-00, OPS CHECK GOOD. NO DEFECTS NOTED AT THSDR UIEA2024022600129Elt · damagedPORTABLE ELT BY L1 DOOR CORD RIPPED..(<P>REMOVED AND REPLACED L1 DOOR PORTABLE ELT IAW AMM 25-63-03. NO FURTHER DEFECTS NOTED</P>)
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