Boeing 767-338
Service difficulty reports · 1,326
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 = '767338' 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 = '767338' 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 ABXA20261017471Autothrottle Sys · faultedAUTOTHROTTLES DISCONECTED @ CRUISE WITH NO INDICATION WHICH LEAD TO STALL RECOVERY 210 KNOTS BEGAN RECOVERY AND ESTIMATE 90 SECONDS RECOVERY FROM 330 TO 280 CREW DECLARED EMERGENCY AND RETURNED TO MIA (ATB) A/C LANDED AND MTX GROUNDED A/C PERFORMED STALL (AFTESDR ABXA20261015468Fire Detector · illuminatedSECTION A AT ZONE 8 ON CARGO FIRE DETECTION LIGHT BAR IS ILLUMINATED AMBER. MX DEFERRED ZONE 8 AIR DETECTOR OF MAIN CARGO DECK PER MEL 26-16-2-2. PLACARDS INSTALLED. A/C RETURNED TO SERVICE.SDR IXXA20261005091Light · inoperativeSUPERNUMERARY EMERGENCY LIGHTS INOPERATIVE. PLACED ON DEFERRAL 77612 MINIMUM EQUIPMENT LIST ATI-33-51-01-01 CATEGORY D. DUE 02 FEBRUARY 2027.SDR ABXA20261004456Oxygen Mask · no testDURING SCHEDULED MTC, CAPT. OXYGEN MASK DOES NOT TEST PROPERLY.MTX REMOVED AND REPLACED CAPT OXYGEN MASK STOWAGE BOX IAW AMM 35-11-51. OPS CHK AND LEAK CHK GOOD.A/C RETURNED TO SERVICE .SDR IXXA2026100302Keelbeam · crackedLH KEEL BEAM WEB CRACKEDSDR IXXA2026100301Keelbeam · crackedKEEL BEAM WEB CRACKEDSDR ABXA20260930442Bleed Valve · defectiveDURING TAXI, R BLD ISLN VAL EICAS MESSAGE. R ISLN VAL DISCRETE LIGHT. CREW RETURNED TO THE GATE (BTB). MTX TROUBLE SHOT AND REMOVED AND REPLACED RH BLEED ISOLATION VALVE IAW B767 AMM 36-11-04. LEAKS AND OPS CHECK GOOD. AIRCRAFT REMAINS NO ETOPS. RETURNED A/C TSDR ABXA20260917427Battery · defectiveDURING INSP/MTC, 2 EACH EMERGENCY LIGHTS INOP, SUPERNUMERY AREA. REPLACED BATTERY PACK AT POSITION M736 PER B767 AMM 33-51-07. SYSTEM CHECKS NORMAL. A/C RETURNED TO SERVICE.SDR ABXA20260916412Smoke Goggles · deterioratedDURING INSP/MTC, FOUND FO SMOKE GOGGLES DETERIORATED. REMOVED F.O. SMOKE GOGGLES. REPLACED WITH SERV. GOGGLES IAW AMM 25-64-00. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.SDR IXXA202609140205Light · illuminatedEMERGENCY LIGHTS UNARM LIGHT ILLUMINATED.SDR ABXA20260913409Latch · failedSHORTLY AFTER APPROACHING 80KTS ON THE RUNWAY IN KLAS, THE FIRST OFFICERS WINDOW POPPED OPEN AND THE CAPTAIN ABORTED THE TAKEOFF (ATO). CREW RESECURED THE FIRST OFFICER'S WINDOW AND LINED BACK UP FOR TAKEOFF. A/C DID NOT RETURN TO THE GATE AND MAINTENANCE WAS SDR ABXA20260913404Controller · defectiveWHILE CRUISING AT FL370 BETWEEN THE CALIFORNIA AND NEVADA BORDER, THE FO AND CAPT HEARD A BEEPING NOISE COMING FROM THE MAIN DECK CARGO AREA. ABOUT 30 SECONDS AFTER THAT THEY RECEIVED A MASTER WARNING EICAS CABIN ALTITUDE. AT THAT TIME THEY BOTH DONNED OXYGEN SDR IXXA20260913080Warning Light · illuminatedEMERGENCY LIGHTS UNARM LIGHT ILLUMINATED.SDR ABXA20260912402Overheat Sys · false activationFIRE/OVHT SYS ON FINAL APPROACH. AC LANDED AND MTX GROUNDED A/C. PERFORMED OPERATIONAL CHECK I.A.W A.M.M B767 26-11-00. ALL FOUND NORMAL. UNABLE TO DUPLICATE FAULT, NO STATUS MESSAGE. AIRCRAFT REMAINS NO ETOPS AND RETURNED A/C TO SERVICE.SDR 2026FA0000687Skin · damagedAT ITS ARRIVAL IN GUATEMALA, DAMAGE ON THE FUSELAGE WAS DETECTED UN WALK AROUND CHECK. SKIN SEEMED TO BE SEVERLY DAMAGE. AFTER INSPECTION FOUND SEVERAL FRAMES AND STRINGERS DAMAGED, BENT OR BROKEN. ALSO THE SKINS HAS SEVERAL CRACKS. STATION 350 TO 360 STRINGERSDR ABXA20260903393Module · faultedRUDDER RATIO EICAS MSG APPEARED AFTER BLOCK OUT. CREW RETURNED TO THE GATE (BTB). MTC PERFORMED B767 FIM 27-09 FT 803 CLEARED FAULT BALLS ON RUDDER RATIO CHANGING MODULES. RAN BOTH ENGINES IAW B767AMM 71-00-00 MESSAGE DID NOT RETURN NO FURTHER ACTION REQUIREDSDR ABXA20260901377Resistor · faultedDURING TAXI EMERGENCY DOORS LIGHT ILLUMINATED. CREW RETURNED TO THE BLOCKS (BTB). REMOVED AND INSTALLED RESISTOR 59032 IAW B767-WDM 52-71-12, PERFORMED PSEU BITE TEST IAW B767 FIM 32-09 FAULT TREE803, BITE TEST GOOD. A/C REMAINS NO ETOPS AND RETURNED TO SERVISDR ABXA20260901392Skin · dentedDURING C-CHECK, INSPECTION AT FUSELAGE SKIN, LOWER SKIN PANEL, AT BS 1373, BETWEEN STR 27R AND ABOVE STR 29R WAS FOUND DENTED OUT OF SRM LIMITS 53-00-01, FIG 101, DETAIL 3 AND WHILE PERFORMING SRM 53-00-01, REPAIR 14, FOUND DOUBLER TO STOP ON AN INTERNAL DOUSDR ABXA20260901391Skin · corrodedDURING C-CHECK, CORROSION WAS OBSERVED ON THE RT WING UPPER SURFACE SKIN PANEL NR 1 AT WS 434 OVER UPPER RIB FLANGE PIN 113T1545-6, THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA IAW SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF0.112 INCHES FROM INITIAL TSDR ABXA20260901390Skin · damagedDURING AN INSPECTION, LEFT WING LOWER SKIN EXISTING BLEND REPAIRS AT WS 110, STRINGER 10 WAS FOUND. THE AFFECTED FASTENERS WERE REMOVED, AND HFEC ROTO AND SURFACE INSPECTIONS WERE ACCOMPLISHED WITH NO ADDITIONAL DAMAGE. THE BLEND AFFECTS SKIN PANEL AND SKIN PASDR ABXA20260901389Skin · corrodedDURING C-CHECK AT AMES (TPA), DURING STRUCTURAL INSPECTION OF THE RIGHT-WING TOP SKIN PANEL NO.1 UPPER SURFACE, CORROSION WAS FOUND AT WS 350 UNDER WING FIXED TRAILING EDGE PANEL 113T1609-2. CORROSION WAS REMOVED BY BLENDING AND FOUND TO BE OUT OF LIMITS PER SSDR ABXA20260901388Skin · corrodedDURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 300.105 AND RS 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-5, & ABX-REA-5513-SDR ABXA20260901387Skin · corrodedDURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 300.105 AND RS STA 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SRM. ENGINEERING CONTACTED FOR FURTHER EVALUATION ANSDR ABXA20260901386Skin · corrodedDURING C-CHECK, LT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 165" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND WITH CORROSION BETWEEN RS STA 160 AND RS STA 180, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SRSDR ABXA20260901385Skin · corrodedDURING C-CHECK, LT HORIZONTAL STAB, UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 8" FROM FUSELAGE BODY. (AROUND FASTERNERS) LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 13.986 AND RS STA 30.605, UPPER REASDR ABXA20260901384Skin · corrodedDURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 2" LONG AT 70"" O/B SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION AT RS 275.605, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLSDR ABXA20260901383Skin · corrodedDURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 2" LONG AT 47" FROM OTBD SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 290 & RS 310, UPPER REAR SPAR AREA STRG-1) COSDR ABXA20260901382Skin · corrodedDURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APPROX 3" LONG AT 22" FROM OTBD SIDE & 2.5" FWD OF REAR SPAR. (AROUND FASTERNERS). CORROSION BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-10 AND ABX-REA-5513-66201SDR ABXA20260901381Skin · corrodedDURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 4" LONG AT 161" FROM FUSELAGE BODY. (AROUND FASTERNERS) CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-7, & ABX-REA-5513-66193-00.SDR ABXA20260901380Skin · corrodedDURING C-CHECK, R/H HORIZONTAL STAB UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 5" LONG AT 95" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND CORROSION BTWN RS STA 104.105, UPPER REAR SPAR AREA AND STRG 1. CORROSION WAS BLENDED IAW SRM. ENGINEERING SDR ABXA20260901379Skin · dentedDURING C-CHECK & INSPECTION, FUSELAGE SKIN, LOWER SKIN PANEL AT BS 1373, BTWN STR 27R & ABOVE STR 29R WAS FOUND WITH A DENT OUT OF SRM LIMITS 53-00-01, FIG 101, DETAIL 3, & WHILE PERFORMING SRM 53-00-01, REPAIR 14, FOUND DOUBLER TO STOP ON AN INTERNAL DOUBLERSDR ABXA20260822372Actuator · malfunctionedLEFT ENG SPAR VALVE LIGHT ILLUMINATED AFTER FUEL ADDED, START NOT SUSTAINED. ACFT RETURNED TO THE GATE (BTB). MTC REMOVED LT ENG SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. INSTALLED NEW LT ENG FUEL SPAR ACTUATOR IAW AMM 28-22-11. ALL CHECKS IN LIMITS OPS TEST GOSDR ABXA20260821370Pitot Tube · defectiveDURING TAXI OUT CAPT. PITOT LIGHT ON OVERHEAD PANEL ILLUMINATED. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX REMOVED AND REPLACED CAPTAINS (LEFT UPPER) PITOT-STATIC PROBE PER B767 AMM 34-11-01. LEAK CHECK GOOD PER B767 AMM 34-11-00. AIRCRAFT REMASDR ABXA20260812359Throttle · stiffSTIFF RESISTANCE FELT ON THROTTLE LEVERS. SLOW ACCELERATION AND RESPONSE DURING TAXI. A/C RETURNED TO THE GATE (BTB). MTX ACCOMPLISHED ACCELERATION AND DECELERATION TEST IAW B767 AMM 71-00-00. BOTH ENGINES WITHIN LIMITS. CYCLED THROTTLES MULTIPLE TIMES, NO RESSDR ABXA20260811358Control Box · dislodgedAT FL340, LT ENGINE N1 DROP DOWN TO IDLE, NO INDICATION OF OTHER ABNORMAL. CREW DECLARED AN EMERGENCY AND DIVERTED BACK TO CVG. AFTER TROUBLESHOOTING MTX FOUND L ENGINE PUSH-PULL CABLE CONTROL BOX DISLODGED FROM MEC AT THE HOUSING BODY. GAINED ACCESS TO, THEN SDR ABXA20260806350Bleed Valve · defectiveL ISLN VALVE LIGHT ON START, L N2 INADEQUATE FOR ENGINE START. A/C RETURNED TO THE GATE (BTB). MTC REMOVED AND REPLACED LEFT ISLN VALVE OPS CHECKS NORMAL IAW B767 AMM 36-11-04. AIRCRAFT REMAINS ETOPS 180. A/C RETURNED TO SERVICE.SDR IXXA20260722059Elec Connector · dirtyEMERGENCY LIGHTS NOT ARMING. CLEANED EMERGENCY LIGHT PANEL ELECTRICAL CONNECTOR IAW SOPM 20-60-01. OPS CHECKED GOOD.SDR ABXA20260720326Warning Message · illuminatedDURING TAXI AFTER START R ENG BLEED LIGHT DID NOT EXTINGUISH NO DUCT PRESSURE INDICATED. EICAS MESSAGES "R ENG BLLED" AND "R PACK OFF"A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C MTX PERFORMED GROUND TEST NR 3. IAW AMM 71-00-00 OPS TEST GOOD BOTH PACKS SDR ABXA20260716323Controller · faultedDUIRNG TAXI OUT AFTER ENG START WE GOT AFT CABIN TEMP, FWD CABIN TEMP , FLT DECK TEMP INOP. CAME ON AND A/C RETURNED TO THE GATE (BTB). MTX GROUNDED ACFT, AND RESET ZONE TEMP CONTROLLER IAW AMM 21-51-13 OPS CK GOOD ACFT REMAINS NO ETOPS. AND RETURNED ACFT TOSDR ABXA20260705303Bleed Air Sys · no discrepancyLEFT PACK OFF AND L ENG BLEED OFF AFTER PUSHBACK AND AFTER START CHECKLIST. L DUCT PRESSURE DROPPED TO ZERO. R DUCT PRESSURE NORMAL AC RETURNED TO THE GATE (BTB) MTX GROUNDED A/C ,MTX PERFORMED LH ENGINE RUN REF AMM 71-00-00, NO FAULTS NOTED AT THIS TIME RETURSDR ABXA20260625285Test Switch · stickingDURING INSP/MTC, FIRE/OVERHEAT TEST FOUND SYS FAIL/RESET SWITCH STICKY. REMOVED AND REPLACED FIRE/OVHT TEST PANEL ASSY PER B767 AMM 26-11-01. OPS CHECK SATISFACTORY. ACFT REMAINS ETOPS 180. ACFT RETURNED TO SERVICE.SDR IXXA20260622053Terminal · faultedDURING PRE-FLIGHT CREW REPORTED RIGHT CHART LIGHT SHOCKED PILOT WHEN TOUCHED. REMOVED AND REPLACED RIGHT CHART LIGHT IN ACCORDANCE WITH B767 AMM 33-14-00. OPERATIONAL CHECK GOOD.SDR ABXA20260619268Warning Message · illuminatedDURING TAXI, AFTER BLOCK OUT, L AFT FUEL PUMP EICAS MESSAGE APPEARED ACCOMPLISHED QRH. RETURNED TO GATE (BTB). DEFERRED L AFT FUEL PUMP IAW MEL 28-22-1. PLACARDS INSTALLED. ACFT DOWNGRADED TO ETOPS 120. ACFT RETURNED TO SERVICE.SDR ABXA20260617266Start Valve · faultedDURING ENGINE START, LT ENGINE START VALVE INOPERATIVE. ACFT RETURNED TO THE GATE (BTB). DEFERRED LT START VALVE IAW MEL 80-00-2-1. MX ACTIONS ACCOMPLISHED PLACARDS INSTALLED A/C REMAINS ETOPS 180. REMOVED AND REPLACED L ENG STARTER VALVE IAW B767 AMM 80-11-02SDR ABXA20260617264Radar · faultedDURING TAXI, CREW RECEIVED NO LAND 3 AND C RAD ALT INDICATION. RETURNED TO THE GATE (BTB). MTC DEFERRED RAD ALT PER MEL 34-33-1-2A-1 MX PROCEDURES APPLIED. PLACARD INSTALLED ACFT DOWNGRADED TO CAT II. ACFT RETURNED TO SERVICE.SDR IXXA20260612050Guard · detachedEMERGENCY LIGHT SWITCH GUARD SPRING RELEASED/DETACHED. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GUARD IN ACCORDANCE WITH B767 AMM 20-11-00. OPERATIONAL CHECK IN ACCORDANCE WITH B767 AMM 33-51-08 NOTED NO FAULTS.SDR IXXA20260609002Web · crackedNUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL SUPPORT WEB IS CRACKED REFERENCE AMES WO N503AZ-28 NR 193266-0400-0075SDR IXXA20260609001Channel · crackedNUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL O/B WEB STIFFENER IS CRACKED IN LOWER RADIUS REFERENCE AMES WO N503AZ-28 NR 193266-0400-0076SDR IXXA20260606001Strut · crackedLEFT WING L/E UPPER SUPPORT STRUCTURE HAS CRACKAT LOCK FASTENER AFT END, VERIFIED BY EDDY CURRENT AROUND LES 506SDR ABXA20260604242Detection Sys · faultedAFTER FIRE TEST ALL -B- MAIN DECK CARGO LIGHTS ILLUMINATED WHITE. NO EICAS INDICTATIONS MTX ,MTX GROUNDED ACFT AND PERFORMED AFLOTS TEST IAW B767 26-10-00. FAULTS CLEARED NO FURTHER DEFECTS NOTED.AC RETURNED TO SERVICE
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