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 CALA2019093001672Circuit Breaker · not reportedLP RAISED FOR SDR REPORTING REF LP 3410519 ESFR SUBMITED. ETOPS FLT CANCELLED, AIRCRAFT SWITCHED.SDR CALA2019092801655Attach Angle · damagedSUPPORT TASK QC PICK UP SHEET - TOOLING MARKS LOCATED ON ATTACH ANGLE AT STA977 AT STRINGER 22L,WL180,ON TOP OF PRESSURE DECK CAUSED BY LEVELING COMPOUND REMOVAL.REF NR LP 9131376 CABIN STA977 S22L PRESSURE DECK LUB ATTACH ANGLE REPLACED AS PER SRM 51-10-02 ANSDR CALA2019092801654Floorbeam · corrodedB767-53-3-7154 - AFT CGO COMPT L/H TORQUE BOX PNL SUPPORT BOTTOM AREA FOUND CORROSION STA 1285 LBL9-24 FLOOR BEAM AREA.REF TO NR LP:9131604 AFT CGO LH TORQUE BOX PANEL SUPPORT STA1285 LBL40-RBL40 FLOOR BE AM REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED SDR CALA2019092801653Attach Angle · damagedSUPPORT TASK QC PICK UP SHEET - TOOLING MARKS LOCATED ON ATTACH ANGLE AT STA977 AT STR 22R,WL180,ON TOP OF PRESSURE DECK CAUSED BY LEVELING COMPOUND REMOVAL.REF NR LP 9131377 CABIN STA977 STR22R WL180 ANGLE REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED ASDR CALA2019092801648Skin · wornB767-06-3-7140 - EMP RH STAB TO BODY CUTOUT LOWER FWD SKIN DEEP CHAFED, REFER NRC 9130455 DAMAGED SKIN PANEL CUT AND REMOVED AT STA1763.5, HFEC INSP CARRY OUT PER B767 NTM PART 6 51-00-19, NO CRACK FOUND. REPAIR PARTS INSTALLED PER ECRA 5331-02461 RH STAB TO BSDR CALA2019092801645Frame · corrodedB767-53-3-7035 CABIN STA 977 L/H FRAME LWR CORNER FOUND CORRODED REFER TO NR LP:9131108 CABIN STA 977 L/H FRAME OUTER CHORD REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 JUST BETWEEN STR-8L AND STR-22AL NEW CHORD P/N:145T1062-35 GRN H19S244823SDR CALA2019092801647Skin · not reportedREFERENCE LP#3339628 S/M REPAIR OVER DOOR 1L. REPAIR WAS PREFORM ED PER SRM53-00-01 REPAIR 12. DIP IS REQUIRED FOR REINSPECT. FIR ST REINSPECT IS 6,000 F/C AFTER REPAIR & REPEAT INSP EVERY 9,000 F/C REFERENCE SRM 53-00-01 REPAIR 12 TABLE 202. DIP REQUESTED FORSDR CALA2019092701637Light · looseEXIT ROW FLOOR LIGHTING STRIPS AT SEATS 21 DEF IS LOOSE AND OUT OF TRACKS. REPLACED CROSS ISLE LIGHT STRIP AND OPS CHECKED OK REF AMM 33-51-501.. ALSO BATTERY PACK REPLACED..SDR CALA2019092301631Connector · brokenCROSS AISLE FLOOR MARKER LOOSE BETWEEN SEATROW 20DEF AND 21DEF. LIGHT TEST FAILED ON CROSS AISLE FLOOR MARKER AND 4 OVERWING EXITS LOWER EXIT SIGNS THESE EMERGENCY LIGHTS CAN ONLY BE SWITCHED ON FROM COCKPIT. NOT FROM FA PANEL TEST SWITCH. FOUND SOLDERING OF CSDR CALA2019091701551Skin · crackedB767-06-3-7140 EMP - RT STAB TO BODY CUTOUT FWD SKIN CRACKED. (REF NR LP 9130454). EMP RT STAB TO BODY CUTOUT FWD SKIN BETWEEN STA 1725 - STA 1740 AND STR 15R - STR 22R REPAIRED AS PER SRM 53-80-01 REPAIR 3 FIG 201.SDR CALA2019090901508Battery · dischargedSUPPORT TASK - GALLEY NR 6 LWR CLG EMERG LIGHT FOUND DIM - REF NR LP 9131314. EMER LT BATTERY EQ NR M734 REPLACED AND LAMP TEST RESULT NORMAL AS PER AMM 33-51-07.SDR CALA2019090901509Battery · dischargedSUPPORT TASK - EMER LIGHT L391 AND L644 FOUND DIM - REF NR LP 9130467. EMER LIGHT BATTERY PACK M733 AND CHARGER REPLACED AND LAMP TEST RESULT NORMAL AS PER AMM 33-51-07.SDR CALA2019090201491Relay · faultyTAT OVERHEAD LIGHT ON TAT PROBE LIGHT FIM 30-33-00-815-805 FOLLOWED. CURRENT SENSING RELAY FOUND AT FAULT. RELAY REPLACED AS PER WDM 30-33-11. RELAY PN 7705402 SN 08711.SDR CALA2019082301425Warning Message · false activationHORIZONTAL STABILIZER TRIM CONTROL SYSTEM EICAS MESSAGE, UNSCHED STAB TRIM DISPLAYED, UNSCHED STAB TRIM LGT ON WITH AUTOPILOT OFF. NEITHER STAB TRIM CUTOUT SWITCH RE-ESTABLISHED CONTROLLED STAB TRIM, ONLY RECEIVED THE MESSAGE WHEN USING ALTERNATE TRIM SWITCHESSDR CALA2019081601363Skin · dentedPREVIOUS REPAIR DOUBLER ON EXTERNAL FUSELAGE SKIN APPROXIMATE BS 420 TO 440 HAS DENT ABOVE STRINGER 34L. REF. AAR N/R: 9463825. REMOVED AND FABRICATED NEW REPAIR DOUBLER AND INSTALLED ON EXTERNAL FUSELAGE SKIN APPROXIMATE BS420 TO 440 IAW B767-300 SRM 53-00-01SDR CALA2019081001346Solenoid · failedFLT DECK DOOR -LOCK FAIL - LIGHT CAME ON STEADY I N FLT. DID NOT ICE A STRA NGE ODOR. CKLIST COM SUSPECT SOLONOID HAS BEEN POWERED ALL FLIGHT, PANEL REMOVED AREA INSPECTED AND FOUND DOOR LOCKING SOLONOID EXTREMELY HOT CAUSING A SLIGHT ODOUR AUTOMATIC FLIGHT DESDR CALA2019081201350Spar · damagedLT WING L/E FRONT SPAR WEB FOUND DAMAGED AT OFSS1025 REF NRC 9131148 DVI SURROUNDING STRUCTURAL WITHIN 16'' NIL FINDINGS. HFEC INSP CARRIED OUT PER B767 NTM PART 6 51-00-19, NO CRACK FOUND AT TRIM MED EDGE. HFEC OPEN HOLE INSP CARRIED OUT AT EXISTING FASTENER SDR CALA2019080901327Skin · corrodedFUSELAGE SKIN PREVIOUS REPAIR DOUBLER SKIN FOUND SURFACE CORROSION AT STA 1197+120 BETWEEN STR 37L-38L CORROSION REMOVED PER SRM 51-10-02, ORG 0.065'' BLEND OUT AREA REMAIN 0.045'' WIDTH 2'' LENGTH 2'', CHECKED NOT WITHIN SRM53-00-01 ALLOWABLE DAMAGE 1 FIG 101SDR CALA2019080501315Lavatory · inoperativeTWO FWD LAVS AND 1 ECONOMY LAV WILL NOT FLUSH/ LAV SYS 2 CB POPPED .SDR CALA2019080401299Transceiver · inoperativeAFTER T/O, WEATHER RADAR WAS NOT PAINTING AN ACCURATE DEPICTION O F LOCAL WEATHER. REPLACED WXR TRANCEIVER REF. TO AMM 34-43-00, TESTED GOOD.SDR CALA2019080431295Stringer Splice · corrodedSTA 1219-1215 S-19R STRINGER SPLICE BRACKET FOUND CORRODED, THE STRINGER SPLICE WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.SDR CALA2019080431296Floorbeam · damagedCABIN - STA 1087 LBL 23 FLOOR BEAM FOUND FLOOR PANEL HOLE ELONGATED. (REF NR LP 9131027). CABIN STA 1087 LBL 23 FLOOR BEAM UPPER FLANGE REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201.SDR CALA2019080101290Floorbeam · damagedBS 1087, LBL 23 FOUND FLOORBEAM HOLE ELONGATED. . THE FLOORBEAM WAS REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201.SDR CALA2019080101288Stringer Splice · corrodedCABIN STA 1219-1215 S-19R STRINGER SPLICE BRACKET FOUND CORRODED, REFERENCE NRC 9131413. CABIN STA 1219-1225 STR 19R STRINGER SPLICE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. RII INSPECTED.SDR CALA2019080101286Drive Unit · malfunctionedWX RADAR INOP, ERRATIC IMAGES AT ALL RANGES AND TILTS CAUSING AIR RETURN. REPLACED RADAR ANTENNA DRIVE REF MM34-43-05-004-094 AND -404-100. TESTED GOOD, REF MM34-43-05-714-022. NO FAULTS NOTED IN SELF TEST OR PAINTING WITH WX OR MAP MODES. ROTABLE PARTS CHANGSDR CALA2019072801260Panel · damagedFAA ADITOR FOUND 2 REPAIR ALLUMINIUM PATCHES OF MIDDLE BALL TRAN SFER PANEL IN AFT CARGO COMPARTMENT DAMAGED. NSFER PANEL IN AFT CARGO COMPARTMENT DAMAGED. FAA AUDITOR FOUND 2 REPAIR ALLUMINIUM PATCHES OF MIDLLE BALL TRA APPROVED FOR 2 CYCLE DIP PER ECRA 5332-SDR CALA2019072801255Valve Stem · blew outMLG #6 TIRE, WHILE CHECKING TIRE PRESSURE, VALVE STEM BLEW OUT OF WHEEL HUB. TIRE NEEDS TO BE CHANGED. JACK WAS PLACED UNDER L/G BEFORE TIRE WENT FLAT. COMPLETED #6 MAIN WHEEL INSTALLATION, S/N OFF H0088. REF AMM 32-45-01-404-027.SDR CALA2019063001100Slide · deployedR2 EMERGENCY SLIDE DEPLOYED WHEN DOOR OPENED ON AIRCRAFT ARRIVAL. RENDER SAFE CHKLIST ACP.DEPLOYED SLIDE REMOVED AS PER AMM 25-66- 00.NEW SLIDE INSTALLED AS PER REF 25-61-01 AND AMM REF 25-66-01. NO DEFECTS NOTED.ALL OK.RII INSPECTION RAISED.OK FOR FURTHER FLSDR CALA2019062901073Skin · cracked12 O''CLOCK & 6 O''CLOCK CRACK FOUND AT R/W LOWER SKIN STR L-9.5 BETWEEN RIB 31 AND 30 MOST OUTBOARD OPEN FASTENER HOLE FABRICATED AND INSTALLED FRAME PLUGE REPAIR PER B767 DWG 767-9420 AND SRM 51-20-01SDR CALA2019062901072Skin · crackedPERFORMED (BHEC) INSP AT L/W REPAIR/PREVENTATIVE MOD OF I/B SEGMENT STR L-9.5, CRACKS NOTED AT 3 OPEN FASTENER HOLES MARKED IN RED. FABRICATED AND INSTALLED FREEZE PLUG REPAIRS PER DWG 767-9420 & SRM 51-20-07 BY OUTSIDE VENDOR P.O# 1622069 AT L/WING ON EXTREMESDR CALA2019061700969Door · unlatchedENTRY/SERVICE DOORSDOOR OPERATION (04=L FWD, 10=L MID, 08=L AFT, 05=R FWD, 11=R MID, 09=R AFT) PROBLEM WAS ENCOUNTERED BY THE FLIGHT CREW WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS (REF FAULT CODE DIAGRAM FOR FLIGHT CREW ACTIONS) 11 FORWARD RIGHT NEAR SEASDR CALA2019061400941Oxygen Gen · missingIDTINSPECTION REQUIRED REFERENCE WORK CARD 63-3500-1-2100 F/C FWD CENTER, LEFT CLOSET SUPPLEMENTAL OXYGEN UNIT MISSING O2 GENERATORS INSTALLED 2 EACH O2 GENERATORS AS REQUIRED REF AMM 35-35-98-000-801C1. OK FOR SERVICE.SDR CALA2019061400946Warning Light · false activationRUDDER RATIO EICAS ON TAKEOFF ROLL AFTER V1..FOLLOWED FIM, L HYD PSI NORMAL. PERFORMED RUDDER RATIO CHANGER MODULE BITE PROCEDURE. REF FIM 27-21-00-815-804 AND FIM 27-09-00-815-814. OPS CHECK NORMAL. NO FAULTS NOTED. ALSO PERFORMED GENERAL VISION INSPECTION OFSDR CALA2019061400939Skin · crackedRT SIDE FUSELAGE. AT STA 1664, STRINGER 13RT,JUST ABOUT STAB L/E, FOUND A CRACK 4 INCH LONG. COMPLIED WITH EWIS W/REF TO AMM 20-60-07-912-011 AND GMM 05-35-51. 53-80-01, REPAIR 7, PARAGRAPH 4.B. REMOVED 11 FASTENERS IN STR. 13R COMMON TO CRACKED AREA PER SRM SDR CALA2019061000923Light · brokenST 25D EXIT PATH LT HANGING BY THE WIRES REQUEST DEFERRAL FOR 25D EMERGENCY PATH LIGHT 25D EMERGENCY LT INOP DEFERRED 25D PATH LIGHT FOUND EPL ASSY BROKEN OFF AT SCREW MOUNTING LOCATIONS.... PN 1013436-001 REQUIRES REPLACE...REF... IFM 25-21-52 NEXT STATION PLSDR CALA2019060700907Access Panel · missingPDA 3 # 2 ENG PYLON OUTBOARD ACCESS PANEL 446AR MISSING ON ARRIVEL... REF TO LOG#3397137( DF PER CDL 54D)...TOM MOSDR CALA2019060700908Waste Tank · crackedREPORTS OF LAVATORY URINE ODORS WHILE AIRCRAFT IS ON THE GROUND. ODORS ARE NOTICEABLE FROM ROW 32 TO THE AFT GALLEY AREA. 1) ACCOMPLISH A GEN VIS INSP OF LAVS G, H, J, K, L AND M FOR EVIDENCE OF LEAKS. 2) REPLACE FWD AND AFT WASTE TANK AIR/LIQUID SEPARATORS SDR CALA2019060700903Lens · detachedAFT RIGHT HAND FLOOR LEVEL EMERGENCY EXIT LIGHT INOP. LENS DETACHED LIGHT INOP, EXIT CONSIDERED INOP,SDR CALA2019053100867Pump · failedAT FL360 NOTICED RIGHT ENGINE INDCATIONS WERE AT REDUCED POWER. EPR 1.03 AND FF 3.3 REF LOG PAGES 3371080 AND 3371024, RIGHT ENG FUEL PUMP, FMU AND EEC REPLACED REF APPLICABLE MM''S REFERENCED IN EACH LOG PAGE. ACP''D POWERPLANT TESTS 2, 3, 4 AND 15. ALL TESTSSDR CALA2019053100863Rotor · damagedPDA 2 ON ARRIVAL LHR, FOUND #5 BRAKE ROTER SHATTERED. BRAKE TEMP READS 3 UNITS IN THE COCKPIT WITH NO STATUS MSG. #5 BRAKE UNIT REMOVED AND REPLACED IAW AMM 32-41-08-404-017. IDT INSPECTION REQUIRED FOR BRAKE ROD INSTALLATION. PDA GROUP 2 REPORTED IAW GMM 02-3SDR CALA2019053100859Light · damagedPDA 2 FOUND RIGHT NOSE LANDING LAMP SMASHED ON ARRIVAL AT LHR, GLASS MISSING. RIGHT NOSE TAXI LIGHT RELAMPED PER AMM 33-42-01-962-021. OP TEST OK.SDR CALA2019053100858Access Door · missingPDA 2 ENG #2 PYLON ACCESS DOOR 446BL MISSING ON ARRIVAL. IPC REF 54-53-01-01, ITEM 525. NIL STOCK. COMPLIED WITH CDL REQUIREMENTS. DISPATCH DESK: 63 DATE: 29-MAY-19- APPROVED CDL 54D CDL APPROVED BY TOMC. PDA PROCEDURES ARE FOLLOWED.SDR CALA2019052000808Compressor · inoperativeNO WATER IN GALLEYS AND LAVS WHEN AIRBORNE BUT WORKS ON GROUND WHEN LANDED REMOVED AND REPLACED THE H2O SYSTEM UNDERLOADER CHECK VALVE, FOUND BAD. PRESSURIZED THE SYSTEM WITH 1 ENG IDLE, OPS CHECK GOOD. H2O AIR COMPRESSOR INOP. REMOVED AND REPLACED THE AIR COMSDR CALA2019052000804Panel · unsecureROW 27, 28 DEF SEATS O2 PANEL OPENED DURING TAKE OFF. PER CREW TOMC MO LOG#3251826 HAS BEEN CREATED BY CREW. TOMC MO FOUND PSU PANEL AT ROW 27 TO BE IN THE UNLATCHED AND DOWN POSITION. RESTOWED PSU PANEL IAW AMM 25-23-01-404-005. OPS CHECKED GOOD.SDR CALA2019051300764Power Supply · lowREF NR LP 9131288 SUPPORT TASK- MID CROSS AISLE EMERGENCY LIGHT FOUND DIM M1559 POWER SUPPLY REPLACED AND TEST NORMAL AS PER AMM 33-51-07.SDR CALA2019051300746Skin · crackedREF NR LP 9130407 SUPPORT TASK EA 5380-01178 RT FUSELAGE BS1654 TO BS 1674 STR 13A FOUND CRACK AT SKIN APPROX 3/4" IN LENGTH FUSELAGE BS1654 TO BS 1674 STR 13A CRACKED AREA REPAIR CARRIED OUT AS PER SRM 53-80-01 REPAIR 7 FORM 44.0008 ITEM 1-20 ATTACHED DIP RAISDR CALA2019050300690Wire · damagedDURING CLIMB PAX SAW A FLASH ABOVE ROW 20 FOLLOWED BY SMOKE AND FUMES. REF AMM05-51-56 SMOKE INSPECTION. REMOVED CABIN CEILING PANELS AT 19-20 ABC AND 19-20 KL. CONFIRMED HEAT DAMAGE ON LEFT SIDE CEILING BETWEEN STATION 764 AND 808 REQUIRING FURTHER INVESTIGATSDR CALA2019050300685O-Ring · leakingTHE AIRCRAFT DIVERTED FOR PLACARD ON ANTI-SKID SYSTEM 3242A. DISPATCH RELEASED AIRCRAFT BASED ON WEATHER PREDICTION OF DRY RUNWAYS IN ORD AT TIME OF ARRIVAL. RAIN LASTED LONGER THAN FORECAST, MEL RESTRICTIONS PROHIBIT LANDING ON WET RUNWAYS. REQUIRED DIVERSIONSDR CALA2019042900670Seal · leakingFWD LEFT OVERWING EXIT DOOR HAS LEAKING SEAL. VERY NOISY. LEFT WING FWD OVERWING EXIT HATCH SEAL FOUND IN POOR CONDITION, SEAL REPLACED IAW AMM 52-09-03-401. DOOR REMOVED AND INSTALLED IAW AMM 52-21-01-002-201/52-21-01-402-202 RESPECTIVELY. EXCESSIVE PRESSURISSDR CALA2019041900601Floorbeam · corrodedSTA LBL54 FLOOR SUPPORT FOUND CORRODED, CABIN STA 325 FLOOR BEAM BETWEEN LBL44 AND LBL58 REPAIRED PER SRM 53-00-51 REPAIR 4 FIG 201. HFES INSP CARRIED OUT PER NTM PART 6 51-00-19, NO CRACK FOUND AT TRIMMED EDGE.
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