Boeing 767-3CB
Service difficulty reports · 573
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 = '7673CB' 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 = '7673CB' 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 HALA2014070500103Wire · damagedRIGHT ENGINE FIRE LOOP 2 DISPLAYED ON EICAS. REPAIRED WIRE AT TS682 IAW WDM 26-11-2 & SWPM 20-30-11. OPS CHECKED OK IAW AMM 26-11-00.SDR HALA2014062500094Control Panel · failedALT WINDOW ON MCP PANEL INOPERATIVE FROZEN. REPLACED MODE CONTROL PANEL PERMORMED TESTS 1-4-30-40 MCP OPS NORMAL ACFT REMAINS LAND 3 STATUS.SDR HALA2014061600084Scuff Plate · leakingDURING CLIMBOUT, F/A REPORTED LOUD WOOSHING NOISE AT R1 DOOR. CONFIRMED AIR MOVEMENT AT AFT LOWER CORNER OF DOOR. RETURNED AS A PRECAUTION. PRESSURIZED CABIN AND CONFIRMED AIR LEAK/ NOISE COMING FROM AFT EDGE OF R1 DOOR SCUFF PLATE. EDGE SEALED R1 DOOR SCUSDR HALA2014052400069Indicator · malfunctionedLOW SPEED ABORT FOR CONFIGURATION RED INDICATOR EICAS INDICATIES STABALIZER, SPEED LESS THAN 60 KTS. R & R STAB TRIM POSITION INDICATOR IAW AMM 27-48-01-024-001 & 27-48-01-434-053. PERFORMED MCDDP GROUND TEST 65 & 66. SYS OPS NORMAL. CONFIG TAKEOFF SYS TESSDR HALA2014052400068Warning Light · false indicationLOW SPEED ABORT FOR CONFIGURATION RED INDICATION, EICAS INDICATES STABLIZER. SPEED LESS THAN 60 KTS. PERFORMED MCDP TEST 08, NO FAULTS NOTED, FIM 31-51 FAULT TREE 807, NO FAULTS NOTED.SDR HALA2014042300054Satcom · malfunctionedINTERMITTENT DATA LINK LOST MESSAGE, FOUR TIMES AND AT 1633Z DATA LINK LOST AND DATA LINK SYS MESSAGE WITH SAT NO COMM AND ACARS NO COMM.SDR HALA2014040500045Probe · malfunctionedAFTER TAKEOFF, TAT PROBE FOLLOWED BY AUTOTHROTTLE DISC DISPLAYED ILLUMINATED ON EICAS, FOLLOWED BY LT ENGINE EEC MODE. REPLACED TAT PROBE IAW WDM 30-33-11. OPS CHECKED GOOD IAW AMM 30-33-00-715-010.SDR HALA2014040400041Idg · failedAIR TURNBACK: LEFT GENERATOR FAILED, GENERATOR DRIVE DISCONNECTED. R & R LT ENGINE IDG IAW AMM 24-11-01. OPS AND LEAK CHECKED GOOD. NO FAULTS NOTED, OK FOR SERVICE.SDR HALA2014040300042Actuator · inoperativeOVERWING SLIDE INOPERATIVE. FOUND RT FWD DOOR OPENING ACTUATOR BLOWN. R & R RT FWD DOOR OPENING ACTUATOR IAW AMM 25-65-10-004-001-001 AND AMM 25-65-10-404-016-001, TEST OK.SDR HALA2014032100037Ptu · leakingPRIOR TO DEPARTURE LT HYD QTY INDICATED .97 AT APPROX 2110Z STATUS PAGE WAS CHECKED. LT HYD QTY INDICATED .74RF FROM 2110Z TO 2208Z LT HYD QTY DECREASED TO .64RF. BLOCKED IN LT HYD IND. R & R HYD POWER TRANSFER UNIT IAW 29-22-01. SECURITY CHECK GOOD. LEAK CSDR HALA2014022500029Pump · malfunctionedLEFT FWD FUEL PUMP EICAS MESSAGE AT TOP OF CLIMB. REPLACED LT FWD FUEL BOOST PUMP IAW AMM 28-22-03. OPS AND LEAK CHECKED GOOD.SDR ANZY2014021000937Pump · erodedDURING RECTIFICATION WORK TO IMPROVE BONDING RESISTANCE, FUEL BOOST PUMPS ON LT WING REMOVED. FOUND INBD PUMP HAD SIGNIFICANT EROSION ON THE IMPELLER HOUSING SUPPORT LEG, UP TO APPROX 50 PERCENT. THE OUTBD PUMP EROSION ON IMPELLOR HOUSING LEG APPROX 10 PERCENSDR HALA2014020800016Valve · failedDURING CLIMB AND DESCENT THE LT PNEUMATIC DUCT PRESSURE SURGES 25PSI TO 40 PSI REPEATEDLY. R & R AIR SUPPLY PRESSURE REGULATING AND SHUTOFF VALVE, PRSOV, IAW AMM 36-11-09.SDR HALA2014012600013Sensor · malfunctionedLEFT PACK TEMP, LT PACK OFF ILLUMINATED, COOLED FIVE MINUTES THEN RESET. LEFT PACK TEMP, TEMP OFF ILLUMINATED AGAIN. R & R LT PACK COMPRESSOR OUTLET SENSOR IAW AMM 21-51-06. OPS CHECKED GOOD, OK FOR SERVICE.SDR HALA2013122900184Warning Light · false activationRAM AIR TURBINE "UNLOCK" LIGHT ON IN OVERHEAD PANEL RAT UNLOCKED CAS MESSAGE. PERFORMED TEST IAW FIM REF 29-21, FAULT TREE 808, TEST PASSED, OPS CHECKED GOOD.SDR HALA2013122000180Pressure Switch · malfunctionedAFTER TAKEOFF, APU FAULT LIGHT ILLUMINATED, APU SHUTDOWN, COMPLIED WITH QRH PROCEDURE. APU WOULD NOT RESTART. R & R APU GEN OIL PRESSURE DIFFERENTAL PRESSURE SWITCH IAW AMM 49-27-16. OPS, LEAK AND SECURITY CHECK GOOD. OK FOR SERVICE. PLACARD REMOVED, MIC SDR HALA2013120500176Shutoff Valve · malfunctionedDURING CLIMBOUT, THERE WAS A LARGE SPLIT BETWEEN DUCT PRESSURE INDICATIONS-LT-35 & RT-19 PSI. ALL OPS WERE OTHER WISE NORMAL AND PRESSURES WERE EQUAL DURING CRUISE. REMOVED PRSOV ON ENGINE NR 2. REPLACED RT PRSOV IAW MM 36-11-09. RAN ENGINE ON HIGH POWER ISDR HALA2013120100174Fan · inoperativeSTRONG ELECTRICAL ODOR THROUGHOUT CABIN. LEFT RECIRCULATION FAN INOPERATIVE. LEFT RECIRCULATION FAN REMOVED AND REPLACED IAW AMM 21-25-01. OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2013111800168Controller · malfunctionedRIGHT ENGINE AT 77.0 N1, 101 EPR, IS CYCLING. AP BLEED, AT FLT IDLE, ITS NORMAL. SWING 20-40 ON INDICATOR. R & R HIGH PRESSURE CONTROLLER IAW AMM 36-11-08. OPS CHECK GOOD LEAK CHECK GOOD. ACCOMPLISHED AMM 36-0001.SDR HALA2013100900133Idg · failedAFTER ENGINE START RT GENERATOR CONTROL TRIPPED OFF, ONE RESET DID NOT GET GEN BACK ON LINE. REPLACED NR 2 GENERATOR CONTROL UNIT IAW AMM 24-22-02. CONDITION SAME. R & R 2 IDG IAW AMM 24-11-01. OPS CHECK OK.SDR HALA2013100900132Gcu · malfunctionedAFTER ENGINE START, RIGHT GENERATOR CONTROL TRIPPED OFF, ONE RESET DID NOT GET GENERATOR BACK ONLINE. REPLACED NR 2 ENG GENERATOR CONTROL UNIT IAW AMM 24-22-02 HISTORY: 0 EVENTS LAST 30 DAYS.SDR HALA2013100400127Light · inoperativeFIVE EMERGENCY SLIDE LIGHTS INOPERATIVE, 3 ON RT, 2 ON LEFT. REPLACED LAMPS, ESCAPE PATH LIGHTS IAW AMM 33-51-06. OPS TESTED GOOD.SDR HALA2013100400125Connector · failedON SERVICE CHECK, FOUND ASILE STRIP EMERGENCY LIGHTING INOP FROM ROW 29J-39J. INSPECTED LIGHT RUN AND FOUND BAD POWER STRIP CONNECTOR NEAR 28J. REPLACED CONNECTOR. OPS CHECKED GOOD.SDR HALA2013081300101Door · damagedFOUND DAMAGE TO FUSELAGE AFT OF RT MLG DOOR, AT HYD SERVICE PANEL. OPENSDR HALA2013070200084Blade · nickedDURING PDC CHECK, FOUND NUMEROUS BLADES NICKED ON NR 2 ESN: 729046. REF L/P 516463, ITEM 1: BLADE NR 30 ON NR 2 ESN 729046 IS NICKED BEYOND REPAIRABLE LIMITS. ACCOMPLISHED BLADE BLEND REPAIR IAW AMM 72-31-02-308-003-N00 TO AFFECTED BLADES. HFEC INSP ACCOMPLISDR HALA2013061700078Control Panel · failedALL THREE FLIGHT DIRECTORS FAILED. AFTER SECOND ATTEMPT GOT RT FD BACK. NEITHER L OR C FD OPERATED FOR 20 MINUTES. THEN BOTH OPERATED INTERMITTENTLY FOR ABOUT 10 MINUTES. AFTER THIS ALL THREE FD'S (L,C,R) OPERATED NORMALLY. FD MALFUNCTION AND RETURN TO OPS WSDR HALA2013050200052Filter · failedON CLIMBOUT, LT HYD QTY EICAS MESSAGE DISPLAYED. STATUS PAGE SHOWED ZERO QTY. RAN QRH PROCEDURE AND RETURNED TO DEPARTURE. FOUND DPI FOR PRESSURE FILTER ON EDP (L) MODULE BLOWN. REPLACED DPI IAW AMM 29-11-17. REPLACED CASE DRAIN AND PRESSURE FILTERS ON EDP SDR HALA2013041000036Fmc · failedFMC HAS A FAIL MESSAGE. REPLACED NR 2 FMC. GROUND CHECK OK IAW MM 34-61-01.SDR HALA2013031500031Switch · failedTHREE APU ATTEMPTED STARTS FAILED, PON LANDING "APU FAULT" EICAS MESSAGE. REPLACED LOW OIL TEMP SWITCH IAW AMM 49-27-14, FUNCTIONAL AND LEAK CK NORMAL ON GROUND, OK TO CONTINUE, RESERVICED APU OIL TO FULL.SDR HALA2013021600021Window · failedRT FWD WINDOW ARCED IN UPPER LT CORNER AND BEGAN TO GLOW. TURNED OFF WINDOW HEAT. THE OUTER PANEL SHATTERED. RETURNED TO BASE, R & R RT FWD WINDOW IAW MM 56-11, PERFORMED INITIAL TORQUE, AND SECOND TORQUE IAW AMM 56-11 IAW AMM 56-11. DUE TO RT FWD WINDOW ASDR HALA2012101900222Terminal · damagedLT ENGINE FIRE LOOP L1 DISPLAYED ON EICAS AFTER PDC FIRE/ OVHT LOGIC TEST. REPAIRED TERMINAL ON UPPER AFT ELEMENT. OPS TEST OK IAW FIM 26-11-804, FIG 104.SDR HALA2012101700219Terminal · damagedLEFT ENGINE FIRE LOOP LP1 DISPLAYED ON EICAS AFTER PDC FIRE/OVHT LOGIC TEST. REPLACED TERMINAL LUG ON UPPER AFT ELEMENT OPS TEST OK IAW FIM 26-11-804, FIG 104.SDR HALA2012101700218Display · inoperativeF/O MCDU BLANK. RESET F/O FMC CDU AND COMPUTER CIRCUIT BREAKERS, OPS CHECK OK IAW MM 34-61-00. SUSPECT POWER TRANSFER CAUSED GLITCH.SDR HALA2012101000217Connector · dirtyICAS MESSAGE "LT ENG FIRE" LP1 DISPLAYED. CLEANED LUG ON LOWER AFT ENG FIRE DETECTOR CHANNEL A. FIRE OVERHEAT BITE TESTED OK. READINGS OK IAW FIM 26-11-804, FIG 104.SDR HALA2012091300213Attach Fitting · corrodedCORROSION ON FLOOR ATTACH FITTINGS AND SEAT TRACK SECTIONS GALLEY/CABIN DIVIDER STA 911. SEAT TRACK SECTIONS REPLACED IAW SRM 51-40-02 REV 90 ATTACH FITTINGS REPLACED.SDR HALA2012091100212Heat Shield · corrodedNR 1 ENGINE AFT FAIRING LOWER EXHAUST HEAT SHIELD CORROSION ON SPLICE PLATE. FABRICATED REPLACEMENT STRAP IAW 313T3380 AND INSTALLED IAW SRM 1-40-02, REV 90. REPLACED SOLID EXISTING FASTENERS AT 6 LOCATIONS WITH BLIND FASTENERS IAW AIR NZ TI 1901-54328-0001.SDR HALA2012082900198Tee Fitting · corrodedCORROSION ON TEE BRACKET SUPPORT PANEL FOR KEEL BEAM ACCESS PANEL. REPLACED TEE BRACKET.SDR HALA2012082700196Latch · no testDURING EO 14.25-02-34-71D EMERGENCY OFF WING SLIDE COMPARTMENT DOOR LATCH INSPECTION, RT INTEROGATOR FAILED ITS TORQUE CHECK. THE FORCE REQUIRED TO OPEN INTEGRATOR WAS 240 IN LBS, LIMIT WAS 175 IN LBS. EO 25-02-34-71, AD2000-11-19R.1, REV D, SB-767-25A0260,SDR HALA2012070500167Oil System · leakingAPU OIL PPH IS AT 0.294. REPLACED APU IAW M266-767 LEAK & OPS CHECKED OK. OK FOR SERVICE.SDR HALA2012070200166Starter · seizedNR 2 ENGINE WOULD NOT START, NO N1 OR OIL PRESSURE NOTED. PNEU PRESSURE WAS NORMAL & START VALVE OPENED AND CLOSE NORMAL. FOUND NR 2 ENGINE STARTER SEIZED. R & R NR 2 ENGINE STARTER IAW AMM 80-11-01. NR 2 ENGINE START, OPS GOOD. ALL ENGINE INDICATIONS NORMSDR HALA2012041500123Drive Assy · failedWINDSEHAR ALERT EICAS ON TAKE OFF, THEN DURING CLIMB 1 RADAR SYS FAILED (WXR SYS STATUS H.) SWITCHED TO 2ND RADAR WHICH THEN ALSO FAILED. REFERED TO QRH FCOM, MEL. CONTECTED DISPATCH & MOC. DETERIORATING WEATHER AT DESTINATION & ALT FORCED RETURN. R & R WESDR HALA2012031400111Blade · damagedON OVERNIGHT FOUND NR 2 ENGINE BLADE DAMAGE AT THE TIP .0652 X .1250 X .2500" FROM TIP OF BLADE. REPAIRED BLADE IAW AMM 72-31-02 FOUND WITHIN LIMITS, EDDY CURRENT CHECKED OK. OK FOR SERVICE.SDR HALA2012031300110Battery Pack · inoperativeFOUND EXTERIOR EMERGENCY LIGHT AFT R1 DOOR INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07. OPS CHECKED GOOD.SDR HALA2012030400104Warning Message · false activationETOPS SINGIFICANT SYS - EICAS MESSAGE, RT PACK TEMP ACCOMPLISHED ORT, SELECTED STBY OPS NORMAL. COMPLIED WITH FIM 21-51-00/101, FIG 103 ALL AREAS NO FAULTS. RAN SYS IAW FIM ABOVE SYSTEM CHECKED NORMAL.SDR HALA2012030200095Filter · bypassing"APU FAULT" DISPLAYED ON FIRST START WHICH WAS UNSUCCESFUL. "APU FAULT" EXTINGUISHED AND SECOND START WAS NORMAL. BITE CHECKED APU CONTROL BOX. FOUND LOW OIL PRESSURE FAULT. FOUND OIL FILTER BYPASS INDICATOR OUT. R & R OIL SCAVENGE FILTER. LEAK AND OPS CSDR HALA2012022800089Heater · unknownCAPTAIN`S FWD WINDOW HEAT FAILED, NO EICAS OR WINDOW HEAT LIGHT INDICATED. CHECKED WINDOW HEATER ELEMENT LOOP RESISTANCES, CHECKED OK, 11 OHMS IAW AMM 34-41-00-765. SWAPPED TEMP CONTROL SENSOR WITH SPARE IAW AMM 30-41-00-968-001. BITE CHECKED CONTROLLER, OPSSDR HALA2012022100067Pump · leakingHYDRAULIC FLUID LEAKING FROM NR 1 ENGINE. R & R NR 1 ENGINE HYDRAULIC EDP IAW AMM 29-11-05. OPS & LEAK CHECKED OK.SDR HALA2012021100058Symbol Generator · failedCAPTAIN`S ADI AND HSI WENT BLANK WITH SG FAIL MESSAGE DISPLAYED IN BOTH INDICATORS. CYCLED "ALTN EFI" OPS RETURNED TO NORMAL/GOOD. R & R NR 1 SYMBOL GENERATOR, GROUND CHECKED OK IAW AMM 34-22-01, GROUND TEST 30 PASSED. ACFT REMAINS IN LAND 3 STATUS.SDR HALA2012021000059Module · malfunctionedSTAB TRIM EICAS "ON" DURING SHORT FINAL,TRIM WAS NORMAL. RERACKED STAB TRIM MODULES LT AND RT. ACCOMPLISHED FIM 22-00-04/101, FIG 108A, NO FAULTS NOTED. ACCOMPLISHED LMP MCDP TEST 65 AND 30, TEST PASS. ACFT OK TO REMAIN AT LMP STATUS "L AND 3".SDR HALA2012020900060Warning Light · false activationLEFT FMC FAIL LIGHT ILLUMINATED AFTER ENGINES SHUTDOWN. LT FMC OPS CHECKED OK IAW MM 34-61-00.
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