Boeing 767-322
Service difficulty reports · 11,760
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 = '767322' 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 = '767322' 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 CALA2026021813870Idg · faultedRIGHT GENERATOR DRIVE DISC CAUTION LIGHT. PERFORMED QRH, CREW ASSISTED TO PERFORM IDLE ENGINE RUN TO CONFIRM RT IDG DISCONNECTED. APPROVED MEL, RT ENG GEN DISCONNECTED AND SWITCHED OFF, DEFERRED IAW MEL 2400F. THERE IS HISTORH REF LP-7704551. R & R GCU ANSDR CALA2026021713828Oxygen Mask · splitCAPTAINS CREW OXYGEN MASK HARNESS IS SPLIT, CAUSING OXYGEN LEAKAGE WHEN THE HARNESS IS INFLATED RAISING AND UPDATING SDR ORIGINAL CAPT OXYGEN MASK SWAPPED WITH SECOND OBSERVER OXYGEN MASK IAW AMM 35-11-51-004-059 AND 35-11-51-404-060. CAPT & SECOND OBSERVER OXSDR CALA2026021313765Battery · inoperativeSEAT ROW 43-48 LT, AISLE EMERGENCY LIGHTS INOPERATIVE. USING WIRING DIAGRAM N0706-D73 REV-. CONNECTOR D1982 PINS 9+11 TO GROUND IS 1.6 OHMS- NORMAL. TRIED NEW BATTERY PACK & POWER SUPPLY UNIT, NO HELP, RETURNED ORIGINAL UNITS. CHECKED SMALL FLOOR ACCESS PSDR CALA2026021013685Light · no testEMERGENCY LIGHT FAILED TEST. LIGHT DOES NOT ILLUMINATE WITH TEST 1 SWITCH, PTT OK. RESEARCHING, NEED MORE INFO OR A PICTURE WOULD BE HELPFUL. TESTED GOOD, REFERENCE: 25-65-00/001 CONFIG 1SDR CALA2026021013648Housing · brokenEMERGENCY EXIT PATHWAY LIGHT BROKEN AT MOUTING, SEAT 40D MOUNTING. REMOVED AND REPLACED HOUSING ASSEMBLEY. LIGHT WAS NOT DISCONNECTED AND OPS TEST WAS NORMAL IAW AMM 33-51-10-962-104.SDR CALA2026021013651Lamp · inoperativeDURING TRANSIT CHECK, EMERGENCY LIGHT EXTERIOR R2 DOOR INOPERATIVE. MEL 3351B, PLACARD APPLIED. DEFERRED AS APPROVED, REPLACED THE LAMPS OF THE EXTERIOR SLIDE EMERGENCY ESCAPE LIGHT AT R2 DOOR IAW AMM 33-51-06. LIGHT OPS CHKD GOOD. MEL CLEARED, PLACARD REMSDR CALA2026020913640Sensor · faultedEICAS MSG: L AFT ENT DOOR CAME ON AT FL310 OFF AT FL390. BACK ON IN DESCNT AT FL350 REQUEST MEL. APPROVED COMPLIED WITH MEL 52130. PERFORMED DOOR WARNING SENSOR TEST IAW AMM TASK 52-71-00-735-072. CLEANED AND RETIGHTENED SENSORS AS PRECAUTIONARY. OPENED ANSDR CALA2026020513602Computer · faultedAUTO THROTTLE FAILED TO ENGAGE AFTER 2 ATTEMPTS . AUTOTHROTTLE D ISC EICAS MSG. FOLLOWING FIM 22-02 TASK 801 PERFORMED MCDP TEST 30 REF FIM 22-03 FAULT TREE 818, NO FAULTS FOUND. ADD EMP:U104370 REF L/P 7813942 RUDDER RATIO ON OVERHEAD PANEL FLASHED DURING AUSDR CALA2026020413580Skin · corrodedETOPS PREDEPARTURE SERVICE CHECK PROCEDURE, AFT WASTE SYS VACUUM BLOWER VENT PORT HAS AREA WITH SKIN BULGE AND POSSIBLE CORROSION. . CUT-OUT OF CORRODED SKIN, HFEC OF CUT-OUT , & MATERIAL VERFICATION WERE ACCOMPLISHED. IAW SRM 53-60-01-2R-3. VERIFIED HFEC OF SDR CALA2026020413545Idg · faultedAFTER TAKEOFF LOST L GEN. CREW FOLLOWED FM AND DISCONNECTED IDG .BPCU READ OUT DISPLAYED L IDG HIGH DELTA TEMP. NR 1 ENG C DUCTS OPENED TO INSPECT IDG FOUND NO LEAKS OR EXTERNAL DEFECTS, FOUND DURING IDG SERVICING 1,5 QT OF OIL ON OVERFLOW CAME OUT. NO OTHER SDR CALA2026020513597Light · inoperativeLEFT, AFT EMERGENCY LIGHT IS INOPERATIVE. R & R AFT EMERGENCY LIGHT IAW AMM 33-51-06-902-082, OPS CHECKED GOODSDR CALA2026020213494Idg · faultedLEFT GEN DRIVE EICAS CAME BACK ON & STAYED ON, LT GEN DRIVE DISCONNECT PUSHED IAW QRH FOR MAINTENANCE ACTION. REMOVED NR 1 ENG IDG IAW AMM 24-11-01. ACP IDT INSPECTION OF FEEDER CABLES INSTALLATION, IAW GMM 09-10-05. UNIONS FROM OLD IDG NEED TO BE TRANSFERRSDR CALA2026020213493Shutoff Valve · faultedRIGHT ENG BLEED & RT PACK OFF CAUTION LIGHTS ILLUMINATED AFTER TAKEOFF. UPON ARRIVAL OF AIR RETURN, ACCOMPLISHED AIR SUPPLY BITE MODULE TEST IAW FIM 36-20 FT 804 & RT PRSOV FAULT LIGHT ILLUMINATED. REMOVAL OF RT PRSOV ACCOMPLISHED ON LP 7776435, OPS TESTED SDR CALA2026020213477Drain · faultedCLEANUP WAS PERFORMED IN THE FWD E&E FROM BS 143.4 - 204.5. PLACED ON DIP PER ECRA 2011-01000 GALLEY SPILL SECTION 2.B. STARTED IN DEPTH CLEAN UP REF ECRA 2011-01000. REMOVED MAIN EQPT CTR FLOOR PANEL REF AIPC 53-01-51-01B ITEM 35. FOUND JUNKS OF ICE ON INSULASDR CALA2026012813420Wire · detachedWHILE T/S MEL 7400Q. FOUND WIRE BUNDLE BURNT ON EMERGENCY LIGHTS PANEL. MEL 7400Q RELATED TO LP 7743774, NR 2 ENG IGNITION ISSUES. REMOVED EMERGENCY LIGHTS CONTROL PANEL IAW 33-51-08 FOR AVIONICS SUPPORT. RETERMINATED PIN THREE WIRE 1003 OF CONNECTOR D838J (SDR CALA2026012913421Blades · shingledRIGHT N1 VIBRATION OF 5.0 OR HIGHER WITH NOTICABLE VIBRATION. DEBRIEFED CREW. STATED N1 VIBE WAS AT 5.0 THROUGHOUT CRUISE. VIBE DECREASED WHEN POWER ADDED TO ABOUT 3.0 & INCREASED BACK TO AROUND 5.0 WHEN POWER REMOVED. CREW STATED VIBRATION NOTICEBLE PHYSICALSDR CALA2026012613311Lamp · inoperativeLEFT EXTERIOR AFT DOOR INDICATION LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP ON THE LT AFT ENTRY DOOR EXTERIOR EMERGENCY INDICATION LIGHT IAW AMM 33-51-06-902-082. OPS CHECKED GOOD.SDR CALA2026012613280Arming Lever · no discrepancyUNABLE TO ARM L2 DOOR. EXERCISED DOOR ARMING MECHANISM L2 DOOR, ARMED SLIDE 2L, OPS OK, REF AMM 52-00-00SDR CALA2026012613275Regulator · no discrepancyDISARM THE OFF-WING ESCAPE SYSTEM-INSTALLED THE SAFETY PIN INTO THE SAFETY HOLE OF THE LEFT INFLATION CYLINDER REGULATOR FOR MX.PER AMM 25-65-00. REMOVED AND STOWED SAFETY PIN FROM LEFT INFALTION CYLINDER REGULATOR IAW 25-65-01 VERIFIED REMOVAL AND STOWAGE OF SDR CALA2026012613272Regulator · no discrepancyDISARM THE OFF-WING ESCAPE SYSTEM. INSTALLED THE SAFETY PIN INTO THE SAFETY HOLE OF THE RT INFLATION CYLINDER REGULATOR FOR MX IAW AMM 25-65-00. REARMED THE OFF WING ESCAPE SYS & REMOVED SAFETY PIN TO RT INFLATION CYLINDER REGULATOR IAW AMM 25-65-00-442-010.SDR CALA2026012613271Light · inoperativeEMERGENCY ESCAPE PATH LIGHTS SEATS 43D AND 44D SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE SEATS 43D AND 44D ESCAPE PATH LIGHT. LIGHT ASSEMBLY REPLACED IAW TASK 33-51-10-962-104.SDR CALA2026012613249Unknown · odorAFT GALLEY FLT ATTENDANTS REPORTED AN ODOR DURING FLIGHT. DE-BRIEFED FLT CREW AFTER INBD FLT ZRH-ORD. PILOTS STATED AT NO POINT DURING THE FLT DID THEY EXPERIENCE ANY SMOKE/ODOR, NO ABNORMAL INDICATIONS IN FLT DECK. 3 FLT ATTEDANTS REPORTED TO FEEL LIGHT HEASDR CALA2026012613244Unknown · smokeNEED TO PERFORM SMOKE ODOR, CONDITIONAL INSPECTION CREW DEBRIEFING REFERENCE: TASK 05-51-56-940-801-C1 PERFORMED VISUAL INSPECTION OF OVENS AND COFFEE MAKERS FOR BURNING AND ARCING INSIDE AND BEHIND. NO EVIDENCE NOTED IN AFT GALLEY. ALSO OPS CHKD EACH OVEN BYSDR CALA2026012613238Sink · cloggedMID LAV OVER FLOW BLACK GOING DOWN ISLE. RETURNING TO EWR FOUND LAV C SINK CLOGGED. UNCLOGGED MID LAV SINK USING COMPRESSED AIR GUN. UNCLOGGED AND WATER DRAINS NORMALLY FROM THE DRAIN MAST. VERIFIED NO FURTHER LEAKS HAPPENED INSIDE FWD AND AFT CARGO COMPARTESDR CALA2026012613237Idg · inoperativeLEFT GEN DRIVE LIGHT NOT ILLUMINATED. LT ENGINE GENERATOR DRIVE LIGHT INOPERATIVE. EICAS VERIFIED TO OPERATE NORMALLY PLACED ABOVE ITEM ON DEFERRAL PER MEL 2411G INOP, COMPLIED WITH DDP. DM IAW WDM 24-11-11. RELAY (K1033),PANEL (M10063) & GCU (M146). R & R SDR CALA2026012613236Duct · collapsedON CLIMBOUT BETWEEN 5K- 9K FEET WE HEARD SVRL THUMPS WITH HIGH CABIN RATE OF CLIMB. DIFF TO ZERO. PERFORMED CABIN PRESSURE CONTROLLER BITE PROCEDURE OF BOTH CONTROLLERS IAW FIM 21-31, FAULT TREE 803. NO FAULTS FOUND FOR THE CURRENT AND PREVIOUS FLIGHTS. FURTSDR CALA2026012713340Lens · brokenLAVATORY C, LT AFT WALL MOUNTED EMERGENCY LIGHT INOPERATIVE. EMERGENCY LIGHT REPLACED IAW AMM 33-51-10-962-173, & SWPM 20-30-12.SDR CALA2026012313177Smoke Detector · false activationLAV 2R SMOKE DETECTOR WENT OFF ON APPROACH NO ONE INSIDE AND NO EVIDENCE OF SMOKE WHEN CREW REPORTED THIS TO HMC THEY ADDED THAT THERE WAS NO SMELL IN THE LAV AS WELL. REMOVED AND REPLACED SMOKE DETECTOR AT LAV M IN REF TO AMM 26-13-01-424-004. SYSTEM TEST PASSDR CALA2026012013107Light · inoperativeFOUND PATHWAY LIGHT ON SIDE OF SEAT 39D INOP. FOUND 39F LIGHT INOP AS WELL. REPLACED BOTH PATHWAY LIGHTS AT SEATS 39D AND 39F. STILL NOT WORKING. REFERENCE CMM 25-23-52. DISCONNECTED BOTH PATHWAY LIGHTS AT 39 D&F. MEASURED 6V AT BOTH CONNECTORS AND MEASURED GSDR CALA2026012013109Idg · faultedLEFT DRIVE LIGHT ON AT CRUISE, DRIVE MAS DISCONNECTED WITH CHECKLIST, REMOVED AND REPLACED IDG ON ENG NR 1 IAW AMM 24-11-01-424-002.SDR CALA2026011613009Lamp · inoperativeEMERGENCY LIGHT AT BS 1197 LT, INOPERATIVE, REAR OF WING TRAILING EDGE. EMERGENCY LIGHT LAMP REPLACED IAW AMM 33-51-06-902-08, LIGHT NOW OPERATES WHEN SELECTED.SDR CALA2026012113128Engine · faultedFL320 EPR ON RT ENGINE WENT TO 0. FUEL FLOW 0. N1 & N2 AND EGT NORMAL. DESENDED FL260 REF LOGPAGES 7585195, 7585208, 7585331, 7585968 DUE TO ENG 2 EXCEEDENCES AND DAMAGE FOUND, REPLACED ENG 2 PER JOB CARD 76-0572-8-0015.SDR CALA2026011312914Lock · failedFLT DECK DOOR LOCK FAILED AFTER PUSHBACK AND WOULD NOT RESET. MEL 5251C APPLIED BY FLIGHT CREW NOC.MEL 5251C APPROVED MEL 5251C APPLIED *DM* RECOMMEND FIM 52-52 FAULT TREE 812 FOR INITIAL T/S ON INITIAL EVAL COULD NOT GET FLT DK ELECTRIC DOOR LOCK TO FAIL. OPESDR CALA2026011212882Circuit Card · faultedFWD EQUPMENT EXHAUST FAN STATUS MESSAGE WITH FWD EXH EQU IP COOL FAN BREAKER ON P6 PANEL TRIPPED. PILOT REPORTED SMOKE IN FLIGHT DECK WHEN CB TRIPPED. FOUND TO BE BINDING & REPLACED IAW AMM 21-58-06/401. ECS FAN CONTROL CARD M990 REPLACED IAW AMM 21-26-05/401SDR CALA2026010812795Lamp · inoperativeEMERGENCY LIGHTS TEST WITH TEST SWITCHES , EMERGENCY LIGHTS IN CEILING ABOVE POSITIONS 36K, 21B AND 6L DO NOT COME ON WHEN SWITCH IN TEST. IT WAS VERIFIED LAMP BURNED AND REPLACED IN REF AMM 33-51-04-002-001. IT IS OK FOR SERVICE.SDR CALA2026010712748Blade · damagedRAM AIR TURBINE BLADES DAMAGED WHEN CARRYING OUT RAT DEPLOYMENT TEST. HUB REMOVED IAW AMM 29-21-01/401. RAT HUB ASSY INSTALLED IAW AMM 29-21-01-434-078. SPEED SENSOR TEST IAW AMM 29-21-15-835-001 AND SYSTEM TEST IAW AMM 29-21-00-735-001 CARRIED OUT, NO FAULTSDR CALA2026010412640Door · missingUPON ARRIVAL, FOUND THE RIGHT WING THERMAL ANTI-ICING DUCT SEAL DOOR ASSEMBLY MISSING.SDR CALA2026010212586Seal · leakingNUMBER 1 ENG OIL QTY SLOWLY REDUCED TO 0 OVR 90 MINS ALL OTHER ENG IND. NORM AT THIS TIME. CAPT REPORTED THE OIL PRESSURE WAS 92 PSI UPON ENG SHUTDOWN AFTER LANDING CREW REPORTED ENG NR 1 OIL PRESSURE DROPPED DOWN TO 90 PSI. ACP'D ENG NR 1 INSPECT FOUND OIL COSDR CALA2025122412381Panel · missingRIGHT ENGINE PYLON PANEL MISSING, PANEL 446BL, NR 2 ENGINE INBD NACELLE STRUT ACCESS DOOR PANEL, THE PANEL WAS REMOVED DUE TO 2 MISSING FASTENERS.SDR CALA2025122912509Skin · damagedDURING WALKAROUND, OBSERVED SMALL DAMAGED ON RT LOWER FUSELAGE BETWEEN BS 1219 & 1241, S36 & 37R. REMOVED PAINT. PERFORMED HFEC AS PER NDT PART 6 51-00-19, IT WAS FOUND A CRACK IN THE AREA. MEASUREMENT: CRACK: 1,5 IN; CRACK TO BS 1219: 15 IN; CRACK TO S-38R 6,SDR CALA2025122312319Girt Bar · fodL2 DOOR WHEN ARMING, THE YELLOW FLAP THAT IS SUPPOSE TO COME OUT AND BLOCK HANDLE, STICKS FOUND DEBRIS IN GIRT BAR FLOOR BRACKETS. PERFORMED CLEANING AND LUBRICATION OF DOOR L2 GIRT BAR FLOOR LINKAGE. OPS TEST GOOD. YELLOW FLAG IS ENGAGING WITHOUT INTERFERENSDR CALA2025122112282Gauge · faultedFYI LT FUEL TANK GAUGE BLANK WITH ASSOCIATED STATUS MESSAGE FUEL QTY IND THIS ITEM IS CLEARED REF 7345418.SDR CALA2025122112274Adc · faultedIAS DISAGREE EICAS MSG. CAPT SIDE SHOWING .785 FO SIDE SHOWING. 815 AT 340 CREW VERBAL. STAND BY IND MATCHED F/O SIDE, CAPT ADC SWITCHED TO ALT AND SYS MATCHED . PERFORMED BITE TEST ON BOTH LEFT AND RIGHT ADC COMP. WITH NO FAULTS. REQ FURTHER T/S. REF FIM 34-1SDR CALA2025121912265Computer · faultedPILOTS REPORT THAT ON ENGINE DISPLAY NO COMMAND BAR NOR TAKEOFF INDICATION SHOWN, EPR & AUTOTHROTTLE WILL NOT ENGAGE. PERFORMED AUTO FLT BITE IAW FIM 22-02, TASK 801. R & R THRUST MANAGMENT COMPUTER IAW AMM 22-31-01-404-005. OPS CHECKED GOOD , PERFORMED GROSDR CALA2025121812212Light · inoperativeSEAT 23F EMERGENCY LIGHT FOUND INOPERATIVE. R & R THE SEAT MOUNTED EMERGENCY LIGHT IAW AMM 33-51-10-962-104. OPS CHECKED GOOD.SDR CALA2025121712183Skin · damagedAFTER INPECTION REQUESTED IN AVO15988 REV.A, WAS FOUND MOISTURE INGRESSION ON LT OTBD AILERON. NECESSARY REMOVE THE MOISTURE AND REPAIR. ALL STEPS OF THE ECRA: 5760-01130 WERE ACCOMPLISHED WITHOUT DEVIATION. ALL STEPS OF THE ECRA: 5760-01130 WERE ACCOMPLISHEDSDR CALA2025121612159Skin · contaminatedAFTER INPECTION REQUESTED IN AVO15988 REV.A WAS FOUND MOISTURE INGRESSION ON RH OUTBOARD AILERON. NECESSARY REMOVE THE MOISTURE AND REPAIR. ALL STEPS OF THE ECRA: 5760-01131 WERE ACCOMPLISHED WITHOUT DEVIATION. PERFORMED NDT INSPECTIONS, REMOVED THE DAMAGES ONSDR CALA2025121612141Structure · damagedLEFT WING CENTER TANK LOWER CHORD AND WEB DAMAGE LOCATED AT LBL 62.05 FROM BSS 785.9 TO BSS 955.1 BTW STRINGER L-4 TO L-6. THIS LP WAS CLASSIFIED AS RII IAW GMM 03-20-20. QC AWARE. REMOVED FASTENERS, PERFORMED TRIMMED THE DAMAGED AREA AND PERFORMED NDT INSPECTSDR CALA2025120811899Duct · crackedBELOW 50 PERCENT THRUST LT ENG ANTI ICE VALVE CAME ON A FEW TIMES THEN RESOLVED PERFORMED L ENG IDLE RUN FOUND LT ENG ANTI-ICE VALVE LIGHT INTERMITTENTLY ILLUMINATED, C/W AMM 36-11-00-715-149, ASPCU OPERATIONAL TEST. FOUND ASPCU SHOWING LT HPSOV FAULT. FOUSDR CALA2025120811863Wire Harness · damagedDAMAGE FOUND TO NR 2 ENG ON LOOM FROM PYLON DISCONNECT TO EEC CONNECTOR D11686. HARNESS DISCONNECTED FOR FURTHER TROUBLESHOOTING. FOUND BENT PIN T ON CONNECTOR D11686. FOUND DAMAGE TO EEC CONNECTOR F THAT CONNECTES TO D11686. EEC REPLACEMENT CARRIED OUT ON
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