Boeing 767-322
Service difficulty reports · 11,764
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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 CALA2023100602953Control Module · faultySTAB TRIM LIGHT ON. CREW REPORTED SHORTLY AFTER TAKE OFF FROM GSO, ( AT AROUND 3000 FT) THE AMBER STAB TRIM LIGHT ON THE OVERHEAD PANEL ILLUMINATED AS DID THE AMBER STAB TRIM EICAS LIGHT. AFTER CONTINUING TO FLY FOR ROUGHLY AN HOUR, IT WAS DECIDED TO RETURN TOSDR CALA2023101103031Buss · inoperativeBOTH UTILITY BUSSES INOP. RESET CIRCUIT BRAKES P11T4 AND P11T31(UTL BUS L&R), SYSTEM OPERATES NORMAL.REF SSM 24-51-02.SDR CALA2023100402944Cylinder · unknownREF AMM 25-65-01-024 PARAG E (3): IF THE OFF WING ESC SYS OPERATED WITH THE REGULATOR SAFETY PIN INSTALLED, YOU MUST REPLACE THE INFLATION CABLE AND THE INFLATION CYLINDER. LEFT OFFWING ESCAPE SLIDE CYLINDER AND AND CABLE REPLACED AS PER AMM TASK 25-65-02-201 SDR CALA2023100402938Unknown · unknownDURING OFF WING ESCAPE SLIDE INSPECPTION LEFT HAND WING SLIDE DOOR ACTATED OPEN. SLIDE AND BOTTLE NOT ACTIVATED. OFF-WING ESCAPE SYSTEM SPOLIER OVERRIDE ACTUATOR REPLACED IN UPDATE DUE TO PART HAVING ASSIGNED SERIAL NUMBER ACCORDANCE WITH AMM-25-65-20. SQUIB TSDR CALA2023101103030Nozzle · leakingOBSERVED SMOKE/STEAM COMING ACROSS CAPTAINS WINDOWS. 4 SEPERATE OCCURANCES. WX CLEAR. PERFORMED VISUAL CHECK OF TAT PROBE AS WELL AS FUNCTIONAL CHECK OF TAT PROBE HEAT REF AMM 30-33-00-715-010. TEST PASSED, NO DEFECTS NOTED. PERFORMED RAIN REPELLENT OPS CHECK SDR CALA2023100902995Insulation · missing**POTENTIAL CHRONIC LVL 0 **DUE TO FLIGHT ATTENDENTS OBERSERVATI ON THAT THE L AFT LAV GETS VERY HOT WHEN THE APU IS RUNNING, PLE ASE INSPECT AFT LAV FOR POSSIBLY APU AIR LEAK WHEN RUNNING. REPA IR ALL FAULTS FOUND. ORDLM MARTINEZ 09/28/2023 CARRIED BY ELB RESDR CALA2023092702890Proximity Switch · damagedLE SLAT ASYM CAUTION UPON FLAP RETRACTION BETWEEN 1 AND UP FLAP NEEDLES BOUNCED DURING PILOT DEBRIEF THE CAPTAIN INDICATED THAT THE FLAPS/SLATS NEVER DID GET TO 0 POSITION DETENT. FSEU BITE SHOWED 1 FAULT. LE OUTBD ASYM WITH MESSAGE 27-80121 MESSAGE WAS ACTUALSDR CALA2023092502872Door · delaminatedRIGHT AFT FUSELAGE EXTERNAL INSPECTION {B767-06-3-0217} - RT MLG DOOR I/B AFT CORNER DAMAGED/DELAMINATED. SEE PHOTO. INSPECTIONS EACH CYCLE AND ACCOMPLISH PART 3 PERMANENT REPAIR DOOR. CUTS RIGGING DOWN SIGNIFICANTLY. JUST A SUGGESTION. WITHIN 5 CALENDAR DASDR CALA2023092502867Floor Support · corrodedCORROSION LOCATED ON PANEL SUPPORT RAIL JUST INSIDE SERVICE DOOR L2 REFERENCE AMES NR 163376-0200-0262SDR CALA2023092202849Fuel Cap · missingFUEL RECEPTACLE CAP LEFT MISSING. MEL 2821J REQUESTED. FUEL RECEPTACLE CAP LEFT PLACED ON MAL 2821J.DDP C/W. FUEL RECEPTACLE CAP LEFT MISSING. DEFERRED REF MEL 2821J FUEL CAP LANYARD ATTACHING BRACKET BROKEN. AIRPLANE ARRIVED WITH TWO RECTABLE CAPS. THIS CLEARSDR CALA2023092002824Controller · faultyIMMEDIATELY AFTER APU SHUTDOWN FLT ATTENDANTS REPORTED HOT AFT L LAV +SMELLED SMOKE IN LAV SMOKE/ODOR IN THE PLANE QUESTIONAIRE FILLED OUT BY FLT CREW PERFORMED INITIAL INSPECTION AS PER REF AMM 05-51-56. NO DEFECTS NOTED. A/C OK TO CONTINUE ADD EMP:U375129,USDR CALA2023092202860Computer · failedAUTO THROTTLE WOULD NOT ENGAGE ON TAKEOFF ROLL. PICTURE FROM INSTALLED TMS ADDED. PERFORMED FIM 22-02 TASK 801. PERFORMED TMS SYSTEM TEST, TMS OPS TEST AND MCDP GROUND TEST 52 AS PER AMM 22-32-00. TMS COMPUTER FAILED. THRUST MANAGEMENT COMPUTER REPLACED PER ASDR CALA2023091802806Fuel Cap · missingLEFT FUEL RECEPTACLE CAP MISSING. MEL 2821J APPROVAL REQUIRED LEFT FUEL RECEPTACLE CAP PLACED ON MEL. 2821J DDP C/W. APPROVED MEL 2821J. REPLACED REFUELING CAP REF AMM28-00-00.REMOVED MELSDR CALA2023091502791Fan · inoperativeAFT FA AND IN ROWS 22 + 35 SMELLED ELEC BURNING SMELL FOR 10 SEC S. NO FURTHER SMELL AFTER THAT SPOKE TO CREW. FLIGHT ATTENDANT REPORTED THAT THE BURNING SMELL FORM ATTACH TO LOG PAGE. CAME FROM A PAX FINDINGS. AT THE MOMENT OF OCCURANCE AFT FLIGHT ATTENDANTSDR CALA2023091502799Latch · unknownROW 36 CENTER OVERHEAD PANEL FELL DOWN FOUND PSU LATCH OPEN, ARMED LATCH AND CLOSED PSU PER AMM 25-23-01.SDR CALA2023091402780Skin · crackedB767-54-3-7005 #1 PYLON STRUT EXTERNAL SKIN IS CRACKED AT AFT UPPER CORNER OF PANEL 416BR CUTOUT.SDR CALA2023091502800Fuel Cap · missingFUEL CAP LEFT MISSING AT WING FUEL STATION. REPLACED FUEL CAP REF IPC 28-21-01-01.SDR CALA2023091302775Transceiver · unknownWXR SYS EICAS S THE WXR DISPLAY IS NOT PRESENT WHEN WXR IS SELECTED ON THE EFIS CONTROL PANEL. T/S C/O FOR WXR SYS EICAS MESSAGE AS PER FIM 34-43 TREE 817. WXR ARE NORMAL. OK TO CONTINUE. PARTS USED: 19-3440-9-0001,QTY BITE TEST C/O ALL OPS NORMAL. AS PRECAUTSDR CALA2023083002660Slat System · warning messageLE SLAT DISAGREE AT FLAP 25. GO AROUND. QRH. FLAPS 20 LAND. LAND AT 147 KIAS. AB 3. BETWEEN POSITIONS 1 AND 5 LE SLAT DISAGREE FOR FRACTION OF A SECOND BEFORE DISAPPEARING. NO DISAGREE FROM POSITION 5 ALL THE WAY TO 30. NO DISAGREE FROM 30 BACK TO UP. CYCLED FSDR CALA2023090502716Engine · damagedUPON REACHING TO EPR LOUD BANG WITH SWERVE RIGHT . REJECTED T/O . NO FIRE. R REV ISLN VAL EICAS ENG2 SN. 724371 (TSI= 16306) SURGED AT T/OFF POWER, CHEK INLET, LOST N1, OIL PRESSURE IN RED 60 TO 70PSI PER FLIGHT CREW EXHAUST, TAIL PIPE FOR METAL, CHECK ALL CHISDR CALA2023090502715Isolation Valve · unknownREJECTED TAKEOFF AROUND 60 KNOTS DUE TO R ISLN VALVE DISPLAYING UNABLE TO DUPLICATE THE CONDITION, HIGH POWER ENGINE RUN WAS PERFORMED BY U101442 NO DEFECTS NOTED DURING THE RUN NO EICAS OR LIGHTS ON ISLN VALVES , AIRCRAFT GOOD FOR SERVICESDR CALA2023082802651Control Panel · unknownO2 MASK IN ROWS 22 32 42 DEPLOYED PERFOMED VISUAL INSPECTION AND IT WAS FOUND OXYGEN MASK NOT DEPLOYED JUST FELL DOWN IN CENTER ROW 22 (D/F),32 (D/E/F) 42(D/E/F).REPOSITIONED THE OXYGEN MASKS AND PSU PANEL PIN REF.AMM 35-21-13 AIPC 25-23-01 GOOD TO SERVICE.SDR CALA2023082802643Exciter · inoperativeENG. 2 DID NOT LIGHT OFF WITH IGNITER 1.. OK IN BOTH IGNITERS. THIS ITEM IS RELATED TO LP 5547676 TO BE CLEARED AN REFER TO RIGHT ENGINE IGNITER NO. 1 PLACED ON MEL 7400E DDP C/W. THIS LP AND MEL 7400E REQUIRED. CONFERRED WITH DISPATCH AND VERIFIED THIS IS NOSDR CALA2023082502628Actuator · failedOXYGEN MASKS 45D E F FELL IN FLIGHT. STOWED LOOSLY FAULT CONFIRMED THE OXIYGEN MASKS COMPARTIMENT AT POSITION 45DEF OXYGEN MASK COMPARTMENT LATCH DOES NOT RESET. NEED PSU OPENING INVOLUNTARY. APPLIED MEL 3521C REPLACEMENT. PART NO SPA GIG. NOC DESK: 767 NAMESDR CALA2023081802566Spring · missingPDA 1. AIRCRAFT WALK AROUND INSPECTION {B767-51-3-6003} - WALKROUND CHECK FOUND R/H LANDING GEAR JURY STRUT SPRING MISSING. INSTALLED 2X R/H LANDING GEAR JURY STRUT SPRINGS. IAW AMM 32-32-05/401.SDR CALA2023081402505Access Door · missingDURING ETOPS PDSC, FOUND #2 ENGINE RT SIDE STRUT ACCESS DOOR 446BR MISSING. LOCATION PIC ADDED. CDL 54D REQUESTED. DEFERRED IAW CDL 54D. MISSING INSTALLED NEW #2 ENGINE RT SIDE STRUT ACCESS DOOR PANEL 446BR PER AMM 20-11-00 AND AIPC 54-53-01-17 ITEM 647.SDR CALA2023081802573Door · damagedBLOCKER DOOR HONEYCOMB MISSING. REPORTING PARTS DEPARTING AIRCRAFT ON FLT #2206 APPROXIMATELLY 12X12 HONEYCOMB BLOCKER DOOR WAS R & R ON CDL NO DAMAGE FOUND C DUCT OR ENGINE. BLOCKER DOOR. NR 1 ENGINE INBOARD THRUST REVERSER C SECTION 1 EACH BLOCKER DOOR DASDR CALA2023081402510Unknown · unknownHARD LANDING ON NOSE GEAR. SPOKE TO CAPTAIN KELLY ON THE PHONE. HE CONVEYED THAT THE LANDING ON THE MAIN LANDING GEAR WAS VERY SMOOTH AND ROUTINE. THE NO SE GEAR TOUCHED DOWN NORMALLY, HOWEVER THE SPEED BRAKES WERE ON MEL AND DID NOT AUTO DEPLOY. A GUST OF WINSDR CALA2023081102472Fitting · shearedNOSE GEAR TOW FITTING SHEARED DURING TOWING PLEASE PERFORM CONDITIONAL INSPECTION AMM 05-51-29 AND UPDATE THIS ITEM WITH FINDINGS. NOSEWHEELS REPLACED PRECAUTIONARY IAW AMM 32-45-02/401. CONDITIONAL INSPECTION OF NOSE GEAR CARRIED OUT IAW AMM 05-51-29. PHASE 1SDR CALA2023080902471Slide · unwanted deployWHILE PERFORMING FCD #2565-01155 ACCIDENTAL DEPLOYMENT OF THE LH OVERWING ESCAPE SLIDE DOOR WITH THE SAFETY PIN INSTALLED. NEED TO REPLACE INFLATION CABLE & INFLATION CYLINDER AS PER SLIDE REMOVAL AMM 25-65-01-024-001-001 STEP #3. VERIFIED INSTALLATION OF INFLSDR CALA2023080702431Relay · damagedELETRICAL BURNING ODOR FROM FWD GALLEY/FWD PORTION OF FIRST CLASS 10 MINUTES INTO FLIGHT. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-56-940-801-C1. FOUND SIDEWALL LIGHT BALLAST AT SEAT 1A TO BE SOURCE OF ELEC ODOR. NEEDS BALLAST 76-3321-3-0013. R+R BALLASTSDR CALA2023080402423Panel · missingPDA 1 PDA PANEL 652 MISSING FROM ACFT, ALONG WITH SECTIONS OF PANELS AND FARINGS SURROUNDING GEAR STRUCTURE. ADDING IMAGES ADDITIONAL IMAGESDR CALA2023080402429Trunnion · brokenGEAR DISAGREE AFTER TAKE OFF. FOUND R/H FORWARD TRUNNION BROKEN, REQUIRING GEAR REPLACEMENT DUE TO DAMAGE. GEAR REPLACED ON TASK CARD 63-3211-1-9002.SDR CALA2023080202397Ceiling Panel · detached31AB CEILING FELL OFF PANEL FOUND CEILING PANEL 33AB LOOSE, REPOSITIONED CEILING PANEL REF AMM 25-22-01. ADD EMP:U395709.SDR CALA2023073102381Charger · malfunctionedB767-33-3-7000 - LHS OVERHEAD EXIT SIGNS AND EMER AISLE LT ON SEAT 16A-33A DIM TRANSFER REF HXWO 1996055 AND ORIGINATED BY EMP V920570 EMER POWER SUPPLY (M737) REPLACED AND TEST NORMAL AS PER AMM33-51-07 ATTACHED FORM 44-0008 ITEM 1 TO 2.SDR CALA2023072802368Control Valve · faultedCENTER PEDESTAL EXTRMLY HOT TO TOUCH. GLARESHIELD TOO HOT TO TOUCH. HOT AIR COMING FR OM UNDER GLARESHIELD. UNABLE TO COOL FLIGHT DECK OBSTRUCTIONS AND OPS NORMAL. REF AMM 21-58-00Z PERFORMED FIM 21-58 FAULT 912, WITH NO INDICATION OF EQUIP COOLING ADVISORY MSSDR CALA2023072802347Heat Shield · damagedNR 2 ENG OIL TANK HEAT SHIELD DAMAGED/MISSING. PLACED #2 ENGINE OIL TANK INSULATION HEAT BLANKET ON DIP FOR 10 CYCLES. MM 79-11-00-202-0001-N01 PER AMM 79-11-00-202-001-N01 OK TO PLACE ENG 2 OIL TANK TOMC-APPROVAL FROM SC1ELBYC COMMENT HEATSHIELD ON DIP TO BE SDR CALA2023072802346Heat Shield · damagedDEBRIS FOUND WHEN OPENING #1 ENG CORE COWL. INSPECTED AND FOUND OIL TANK HEAT SHIELD DAMAGED APPROX 50%. SEE PHOTOS. REPLACED HEAT SHIELD WITHIN 10 CYCLES. MM 79-11-00--202-001-N01. DIP APPROVED FOR ENG 1 OIL TANK HEAT SHEILD DETERIORATED MORE TOMC-APPROVAL FSDR CALA2023072602340Fastener · missingPDA 3 #1 ENG O/B CORE COWL TRAILING EDGE MISSING 2 EACH FASTENERS. REMOVED AND REPLACED FASTENERS REF SRM 51-40-02SDR CALA2023072602338Screw · missingPDA 3 UPPER PYLON PANEL ON #1 ENG O/B HAS 1 EACH MISSING SCREW. REPLACED 1 EACH SCREW ON #1 ENG O/B PYLON.SDR CALA2023072402314Shutoff Valve · crackedEVIDENCE OF HYD LEAK COMING FROM TAIL SKID AREA. BOTTOM OF TAIL WET WITH HYD FLUID. SEE PHOTO. INSPECTED AND FOUND V103 C EMPENNAGE SHUTOFF VALVE HOUSING CRACKED. SEE PHOTOS. REMOVED AND REPLACED C EMPENNAGE SHUTOFF VALVE REF AMM 27-23-01. OPS CHECK NORMAL.SDR CALA2023072102297Skin · damagedAC DAMAGE BELOW R1 DOOR FWD FUSELAGE. PUNCTURE HOLE. REQUIRES SHEET METAL. CUT OUT DAMAGED SKIN AND REQUIRES HFEC AROUND CUT OUT, REF SRM PERFORMED HFEC AROUND CUT-OUT, REF PART 6, NDT 51-00-01. NO 53-00-01-2R-14, STEP 4, NDT PART 6, 51-00-01. INDICATION NOTEDSDR CALA2023071702270Extinguisher · unknownRAISING SDR FOR INCORRECT FITMENT OF COMPONENT PER TASK CARD 63-2620-1-2827. SDR RAISED FOR DISCOVERY OF INCORRECT FITMENT OF COMPONENT DURING TASK CARD 63-2620-1-2827 ON 15-JUL-23. TSAP RAISED.SDR CALA2023072102305Fastener · missingPDA 3 #2 ENGINE AFT PYLON OUTSIDE STRUT FAIRING PAN ASSEMBLY MISSING ONE FASTENER. ONE MISSING FASTENER. SEE DETAIL III AND IV. CONFIRMED ONE MISSING FASTER. NO PART AVAILABLE GIGJL. AS PER SRM 51-10-05-2R-1 PARAGRAPH 4, ALL CONDITIONS ARE PERMITTED FOR DIP 5SDR CALA2023071202222Shutoff Valve · failedR ENG HPSOV EICAS ON T/O ROLL WITH ASSOC BLEED LIGHT. BLEED LIGHT DID NOT EXTINGUISH. V347 FAILED INTERNAL ELECTRICAL CHECK PER WDM 36-11-62, NEEDS NEW VALVE, REF AHM LP 5113215. REF AMM#36-11-18 REMOVED AND REPLACED HPSOV. LEAK AND OPS CHECKS GOOD WITH NO FUSDR CALA2023071202237Bolt · missingPDA 3 WING TE STRUCTRURE LEFT PANEL 552HB MISSING ONE BOLT. REF. AMM TASK 06-44-00-992-001 ZONE 550 AND 650 ACCESS DOORS AND PANELS. SEE PIC. INSTALLED BOLT IN WING TE STRUCTRURE LEFT PANEL 552HB PER SRM 51-40-02, GOOD FOR SVC,PARTS USED: 00-0593-3-0257,QTY :SDR CALA2023063002097Skin · crackedCRACK INDICATION FOUND ON FUSELAGE SKIN AT BS 1654.50 PLUS 7.5 INCHES, BELOW STR 13R. CRACK LENGTH=1.500 INCHES. REFER TO AEROMAN NON ROUTINE 2023-350701. ALUMINUM SHEET 7075-T6 0.050" PO #2012545969 THIS REPAIR IS EXTERNAL DETAILED INSPECTION AT INTERVALS 7,5SDR CALA2023062602029Pressure Switch · no testRAT DID NOT PRESSURIZE CENTER HYDRAULIC SYSTEM. RAM AIR TURB MODULE PRESSURE SWITCH REPLACED AND TEST RESULT NORMAL AS PER AMM 29-21-11 AMD 29-21-00. WORK ACCOMP BY MECH V924756 INSP BY V924743. ADD EMP:V924743SDR CALA2023062301990Skin · corrodedB767-28-3-0067, RHW FUEL TANK OVERWING FILL PORT ATTACH UPPER SKIN FOUND CORROSION REF HX NR WO.1865480, ORIG BY V897897 RHW FUEL TANK OVERWING FILL PORT UPPER SKIN PANEL CORROSION REPAIRED AS PER ECRA 5725-01126 REV.- ATTACHED MAINTENANCE WORK SHEET FORM 44.SDR CALA2023062301989Skin · crackedSUPPORT TASK - EA5315-01152 OP 002 1EA FASTENER HOLE FOUND CRACK AT 2O''CLOCK AND 8O''CLOCK (COUNT FROM INBOARD) ON FUSELAGE SKIN LAYER- TRNAFER REFER NON-ROUTINE WO.1843964 AND ORIGINATED BY V924735 RII INSPECTED OKAY BY HX 310582 ADD EMP:V896895 FUSELAGE SKI
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