Boeing 767-306
Service difficulty reports · 2,509
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 ABXA20251108293Skin · corrodedDURING C-CHECK AT AMES (TPA) CORROSION WAS OBSERVED ON THE RIGHT-WING UPPER SURFACE SKIN PANEL NUMBER 1 ON STA WS 616 , THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.133¿ INCHES FROM INITIAL THICKNESS OSDR ABXA20251108292Skin · corrodedDURING C-CHECK AT AMES (TPA) CORROSION WAS OBSERVED ON THE LEFT-WING UPPER SURFACE SKIN PANEL NUMBER 1 AT WS 434 OVER UPPER RIB FLANGE P/N 113T1545-7, THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.145¿ SDR ABXA20251003243Apu · faultedON PUSHBACK APU SHUTDOWN, ACFT RETURNED TO THE GATE (BTB) AND MTX GROUNDED ACFT . MTX PERFORMED APU START, 1ST ATTEMPT APU START CHECKS GOOD IAW AMM 49-11-00. ACFT REMAINS NO ETOPS. AND RETURNED AC TO SERVICE.SDR ABXA20250909224Hmu · inoperativeDURING DESCENT, ON THE ARRIVAL TO MIA, L & R ENG CONTROL STATUS MESSAGES. RIGHT ENGINE WOULD NOT ACCELERATE FROM IDLE. DECLARED EMERGENCY AT APPROX. 1930Z AND LANDED AT MIA. AFTER LANDING L & R ENGINE CONTROL EICAS MESSAGES APPEARED. MIA FIRE DEPARTMENT CHESDR ABXA20250907214Module · defectiveDURING TAXI OUT, STAB TRIM EICAS MSG APPEARED , AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX DEFERRED STAB TRIM FOR DEPARTURE IAW MEL ABX-27-41-2 MTX RETURNED AC TO SERVICE AND AC DEPARTED. REMOVED AND REPLACED STAB TRIM MODULE IAW AMM 27-09-00. DI 6SDR ABXA20250825198Warning Message · activatedDURING TAXI, STAB TRIM MESSAGE BEFORE TAKE-OFF. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED IAW MEL 27-41-2. MTX PROCEDURES CW. PLACARD INSTALLED. SEE LP 39094-01/2 FOR RALM DOWNGRADE. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250822197Pressure Switch · failedAFTER PUSHBACK, STAB TRIM EICAS MSG APPEARED. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE REMOVED AND REPLACED RH STCM BRAKE PRESS SWITCH IAW AMM 27-41-07 OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250819181Start Valve · failedDURING TAXI OUT, LEFT ENGINE START VALVE FAILED TO OPEN. NO ROTATION, L ENG STARTER EICAS , VALVE LIGHT. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW MEL C ABX-80-00-2-1. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250720164Wire · looseDURING CRUSE FLIGHT L STRUT DUCT LEAK MSG IN-FLIGHT. DID NOT CLEAR AFTER PACK "OFF" & BLEEDS REMOVED, AC THEN DIVERTED TO CLT.BECAUSE OF ICE CONDITIONS AT CVG. AFTER LANDING MTX GROUNDED AC AND TROUBLESHOT TIGHTNED WIRES ON L STRUT TS236. RUNG WIRES PIN 1 & PSDR 21GA20250709015Target · out of positionAFTER LIFT OFF RECEIVED LE SLAT ASSYMETRY MESSAGE. RETURNED TO THE FIELD.SDR 21GA202507083014Proximity Sensor · out of adjustON APPROACH RECEIVED FLAP ASSYMETRY MESSAGE WHEN FLAP SET TO 5 DEGREES. DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. CLEANED AND SET CLEARANCES ON LEADINF ESGE SLAT SENSORS.SDR ABXA20250531110Door · tornWHILE TAXING INTO THE GATE, GROUND FOUND THE LH PACK BAY DOOR RIPPED OFF THE A/C. AIRCRAFT IS CURRENTLY IN WORK AT CVG. STILL UNDER INVESTIGATION. AN AMENDED SDR REPORT WILL BE FILED ONCE COMPLETED. AMENDED: REMOVED AND REPLACED LH PACK BAY DOOR REF SRM 51-SDR ABXA20250515097Bleed Valve · defectiveON TAXI OUT, R ENG BLEED EICAS MSG ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE REPLACED RT ENGINE PRSOV IAW AMM 36-11-09, RAN RT ENGINE AS PER AMM 71-00-00 AND ABX B767-10A. OPS CK NORMAL PER B AMM 36-11-09. AIRCRAFT REMAINS NO ETOPS. AIRCRSDR ABXA20250514095Warning Message · illuminatedAUTOPILOT EICAS MESSAGE ON BLOCK OUT. AIRCRAFT RETURNED TO BLOCKS. (BTB). MAINTENANCE DEFERRED RALM STATUS TO CAT 1 MBCB C-CK, PLACARD INSTALLED. PERFORMED MCDP TEST 30/40 IAW B767 AMM 22-00-02. NO FAULTS NOTED AT THIS TIME. PLACARD REMOVED. DI CLEARED. NOSDR ABXA20250421083Bleed Valve · warning messageON TAXI OUT, APU BLEED VALVE EICAS MSG ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED APU IAW MEL ABX-49-11-1A. PLACARD INSTALLED. MX PROCEDURES C/W. NO ETOPS. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250218046Warning Message · illuminatedCARGO DOOR INDICATION, PRESSURIZATION NORMAL, LIGHT WENT OUT AFTER FLIGHT DESCENDED BELOW FL240. FLIGHT DIVERT TO KATL WHILE AT FL180,A/C LANDED SAFELY AND MTX GROUNDED A/C THEN DEFERRED MAIN CARGO DOOR INDICATION IAW MEL ABX-52-71-1-2 AND RETURNED AC TO SERVISDR ABXA20250218045Autothrottle Sys · faultedLOW SPEED ABORT DUE TO AUTOTHROTTLES NOT ENGAGING AT 50 KTS AFTER A/C ABORTED T/O , THEY RETURNED TO THE GATE AND MTX GROUNDED A/C AND DEFERRED THE AUTO- THROTTLE IAW MEL ABX-22-30-1. AND RETURNED A/C TO SERVICE .SDR ABXA20250213036Psu · faultedDURING TAXI THE WARN ELEX STATUS MSGAPPEARED AND WON'T CLEAR, A/C RETURNED TO THE GATE AND MTX GROUNDED A/C AFETER TROUBLE SHOOTING WARN FLEX MSG IAW B767 FIM 31-51 FT 806 FOUND WARN FLEX PSU B FAULTING REMOVED AND REPLACED WARN FLEX PSU B IAW B767 AMM 31-5SDR ABXA20250127023Generator · malfunctionedDURING TAXI AFTER STARTING LH ENG,GOT LEFT ENG. CONTROL AND LEFT GEN DRIVE DISSCONNECT LIGHT, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C ,MTX DEFERRED LH GEN IAW MEL ABX-24-00-1-1 .AND RETURNED A/C TO SERVICE.SDR UIEA2025011300052Skin · dentedRH WING, SLAT #11 DENT ON UPPER SKIN.(<P>RH WING, SLAT 11 WAS REPAIRED IAW SRM 57-43-02-2R-1 REP 1 PAGE 2-3 FIG 201 AND SRM 51-70-1 OOR REP 4 PAGE 1-7 FIG 201 (SHEET 2) REV 127. 15-DEC-24. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011300053Line · leakingENG 2 NACELLE STRUT LINE WITH LEAK.(<P>ENG 2 NACELLE STRUT LINE WITH LEAK, TORQUE WAS APPLIED 127 LB-IN SN:1017801833</P> / <P>DATE: 11-APR-25 IAW AMM: 71-00-02-404-049-H03 REV.144 DATE: 22-DEC-2024. LEAK CHECK WAS GOOD.</P>)SDR UIEA2025011600068Strip · corrodedENG 1, RH CORE COWL, UPPER STRIP WITH CORROSION. L: 2.500 IN, W: 1.000 IN.(<P>THE CORROSION METAL STRIP WAS REMOVED, THE NEW METAL STRIP WAS DRILLED AND WAS INSTALLED CORRECTLY. SRM 51-40-02-0G-0 REV 127 15DEC24 AND SRM 51-10-02-0G-0 PAR 9. LEVEL 1. NO FURTHERSDR UIEA2025011600070Orifice · obstructedAFT AND BULK CARGO COMPATMENT CARGO SMOKE DET AIR SAMPLING ORIFICES BLOCKED AND DIRTY.(<P>SMOKE DET AIR SAMPLING ORIFICES WERE CLEANED IAW 26-05-03-202-001 REV 143 22AUG24. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011600071Pca · leakingRIGHT WING INBOARD AILERON, PCA´S WITH LEAK EVIDENCE.(<P>RIGHT WING INBOARD AILERON, PCA´S LH, AND RH WERE REPLACED I.A.W AMM 27-11-48-022-003. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011600072Orifice · obstructedFWD CARGO COMPARTMENT CARGO SMOKE DET AIR SAMPLING INTAKE ORIFICES BLOCKED AND DIRTY.(<P>FWD CARGO COMPARTMENT CARGO SMOKE DET AIR SAMPLING INTAKE ORIFICES WERE CLEANED IAW AMM 26-05-03-202-001 REV 143. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011600073Access Panel · looseENG 1, INNER ACCESS PANEL 432 FL, PIPE "FIRE PROTECTION" WITH NUT LOOSE.(<P>ENG 1, INNER ACCESS PANEL 432 FL, PIPE "FIRE PROTECTION" NUT WAS TORQUED AND VERIFIED IAW AMM 20-11-00-910-801. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011600074Access Panel · misinstalledACCESS PANEL OF MAIN DECK CARGO SMOKE DETECTOR WAS <SPAN STYLE="FONT-SIZE: 13.3333PX;">INSTALLED WRONG. </SPAN><SPAN STYLE="FONT-SIZE: 13.3333PX;"> </SPAN>(CCD ZONE 121)(<P>CARGO SMOKE DETECTOR ACCESS PANEL WAS INSTALLED CORRECTLY IAW AMM 23-16-01-400-801-061 SDR UIEA2025011600075Fuel Cell · leakingFUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-6 AND WBL 97.5 APROX.(<P>FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-6 AND WBL 97.5 APROX. THE AREA WAS VENTILATED, THE REMAINING FUEL WAS CLEANED, THE SEALANT IS REMOVEDSDR UIEA2025011600076Fuel Cell · leakingFUEL LEAK EVIDENCE, LH WING LOWER SIDE AT BODY SPLICE AND STRINGER 10 AND 15.(<P>THE AREA WAS VENTILATED, THE REMAINING FUEL WAS CLEANED, THE SEALANT WAS REMOVED, THE AREA WAS CLEANED CORRECTLY, CLASS "A" AND CLASS "B" SEALANT WAS APPLIED CORRECTLY, THE FUEL LSDR UIEA2025011600077Structure · noneCONTAMINATED EWIS WITH CIC OF NOSE LANDING GEAR WHEEL WELL.<BR>(<P>NOSE LANDING GEAR WHEEL WELL EWIS WAS CLEANED IAW SWPM 20-10-04 REV 87. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011600078Skin · delaminatedLH WING, L/E OUTBD FLAP, FROM INBD EDGE TO 58 INCHES TO OUTSIDE WITH DELAMINATION.(<P>LH WING, L/E OUTBD FLAP, FROM INBD EDGE TO 58 INCHES WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 10 AND SRM 51-70-17-17-0G-0 PAR.4.A REV 127. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011700080Acoustic Panel · corrodedENGINE 2, AIR INLET COWL, ACOUSTICAL PANEL AT 7 TO 8 O'CLOCK POSITION WITH EVIDENCE OF CORROSION.(<P>ENGINE 2, AIR INLET COWL, ACOUSTICAL PANEL AT 7 TO 8 O'CLOCK POSITION WITH EVIDENCE OF LEVEL 2 CORROSION WAS REPLACED IAW AMM 71-11-01-404-005-H00 REV 144. NO SDR UIEA2025011700081Lens · brokenBROKEN EMERGENCY LIGHT ON FWD LH PASSENGER DOOR.(<P>LINING INSTL- FWD ENTRY DOOR, FWD SIDE DOORWAY LENS (EXIT) WAS INSTALLED IAW AMM 33-51-01-400-801-001. OPS CHK OK</P>)SDR UIEA2025011700082Structure · noneMISSING CIC ON SEVERAL AREAS OF NOSE LANDING GEAR WHEEL WELL.(<P>MISSING CIC ON SEVERAL AREAS OF NOSE LANDING GEAR WHEEL WELL. DAMAGED CIC WAS REMOVED AND AREA CLEANED FOR APPLICATION, CIC IS APPLIED CORRECTLY. AMM 51-24-09-377-008 REV 143 AND AMM 51-24-09-917SDR UIEA2025011700083Fuel Tank · leakingFUEL LEAK ON RIGHT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-15 AND WBL 97.5 APROX.(<P>THE SEALANT IS REMOVED, THE AREA IS CLEANED CORRECTLY, CLASS "A" AND CLASS "B" SEALANT IS APPLIED CORRECTLY AND THE FUEL LEAK TEST PERFORMED WAS SATISFACTORY. AMM 28-SDR UIEA2025011700084Retainer · corrodedMAIN LANDING GEAR DOOR RH, TRACK OF SEAL BULB AFT, WITH EVIDENCE WITH CORROSION.(<P>MAIN LANDING GEAR DOOR RH, TR ACK OF SEAL BULB AFT, WITH EVIDENCE WITH CORROSION, WAS REPLACED IAW SRM 51-10-02-0G-0 REV 127. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011800086Support Angle · crackedBROKEN ENG 2, ACCESS PANEL 447DB, ANGLE SUPPORT WITH CRACK.(<P>THE BROKEN SUPPORT ANGLE WAS REMOVED, THE AREA WAS CLEANED, THE NEW SUPPORT ANGLE WAS DRILLED AND INSTALLED CORRECTLY. THE SUPPORT ANGLE WAS REPLACED WITH A NEW ONE. DWG 313T3360 SRM 51-40-02-OG-O SDR UIEA2025012000090Pca · leakingLH WING INBOARD AILERON INBOARD PCA WITH EVIDENCE HYDRAULIC LEAK.(<P>INBOARD PCA WAS REPLACED I.A.W. AMM 27- 11-48-422-040, REV. 144, DATE: DEC. 22, 2024. TORQUE APPLIED: ROD END: 1200 IN- LB, S/N: 0808504320. INBOARD AILERON ADJUSTMENT AND OPERATIONAL TEST WESDR UIEA2025012000091Skin · crackedFORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE 2 ON SKIN, POSITION 11 O´CLOCK AND 5 O'CLOCK, SEE N.D.T. INSPECTION REPORT.(<P>TWO CRACK INDICATIONS AT HOLE 2 ON SKIN, POSITION 11 O´CLOCK AND 5 O'CLOCK, WERE REPAIRED IAW SRM 53-SDR UIEA2025012000092Skin · crackedFUSELAGE - SECTION 41 - SERVICE DOOR CUTOUT AFT LOWER CORNER WITH A CRACK INDICATION AT HOLE 2 ON SKIN AND BEAR STRAP, POSITION 2 O´CLOCK, SEE N.D.T. INSPECTION REPORT.(<P>CRACK ON RH FUSELAGE, R1 DOOR CUTOUT, AFT LOWER CORNER ON SKIN WAS REPAIRED IAW SRM 53-SDR UIEA2025012000093Fuel Cell · leakingFUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L-15 AND WBL 97.5 APROX.(<P>FUEL LEAK ON LEFT WING LWR SIDE OF BODY SPLICE PLATE AT STRINGER L- 15 AND WBL 97.5 APROX. SEALANT WAS REMOVED AND REPLACED. CLASS "A" AND CLASS "B" SEALANT WAS INSTALSDR UIEA2025012000094Servo · leakingVERTICAL STABILIZER, REAR SPAR, YAW DAMPER SERVOS ASSY, LEAKING EVIDENCE.(<P>YAW DAMPER SERVOS LEFT AND RIGHT, WERE REPLACED, TEST WERE PERFORMED AND HYD LEAKAGE CHECK WAS PERFORMED AND TORQUE WAS APPLIED IAW AMM 22-21-02-414-016 REV 143. OPS CHECK GOOD. </P>)SDR UIEA2025012000095Pcu · leakingLH ELEVATOR, PCU'S LEAKING EVIDENCE.(<P>LH ELEVATOR, INBOARD, AND OUTBOARD PCA WERE REPLACED IAW AMM 29-31-05-424-027 REV144. TORQUE APPLIED: 200 LB-IN, 270 LB-IN S/N:040674400. ADJUSTMENT WAS PERFORMED. OPERATIONAL TEST WAS SATISFACTORY.</P>)SDR UIEA2025012100098Frame · corrodedENGINE 2 AIR INLET COWL, FAN FRAME, AROUND AT 7 TO 8 O CLOCK POSITION WITH CORROSION.(<P> ENG 2 INLET COWL WAS REPLACED IAW 71-11-01-404-005-H00 REV 144. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025012100099Skin · wornRH WING, SLAT # 7, WORN LOWER SKIN.(<P>RH WING, SLAT 7 LOWER SKIN WAS REPAIRED I.A.W SRM 57-43-02-2R-1 PG 1-3 FIG 201 AND SRM 51-70-10-2R-4 PG 1,15 FIG 202 SHEET 8 REV 127 15-DEC-24. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025012100100Frame · corrodedENG 1, FAN FRAME, BTWN 4-8 O'CLOCK SURFACE WITH SEVERAL POINTS OF CORROSION.(<P>ENG 1, FLOWPATH EXTENSION BETWEEN 4 TO 8 O'CLOCK WERE REPLACED IAW AMM 72-33-00-308-104-H00 REV 144. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025012100101Pcu · leakingRH ELEVATOR PCU'S LEAKING EVIDENCE.(<P>RH ELEVATOR, INBOARD, AND OUTBOARD PCA WERE REPLACED IAW AMM 29-31-05-424-027 REV 144. TORQUE WAS APPLIED: 200 LB-IN, 270 LB-IN S/N: 0406744400. ADJUSTMENT WAS PERFORMED. OPERATIONAL TEST WAS SATISFACTORY.</P>)SDR ABXA20241230273Warning Light · illuminatedDURING TAXI AUTOPILOT DESCRETE LIGHT STAYS ILLUMINATED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX PERFORMED FIM 22-02 F/T 801 MESSAGE CLEARED. A/C REMAINS CAT I.AND REURNED AC TO SERVICESDR ABXA20241219265Warning Light · false activationON PUSH GOT A/P EICAS & DISCREET LIGHT. TRIED RESETTING AND BOTH REMAINED.AC TRTURNED TO GATE (BTB)AND MTX GROUNDED AC T/S AS PER FIM 22-03-00 NO FAULTS NOTED PERFORMED MCDP GND TEST 30 NO FAULTS PERFORMED TEST 40 TEST NO FAULTS. PERFORMED 22-03 FT 818. 819 ASDR 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 DEPARTED
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