Boeing 767-3G5
Service difficulty reports · 724
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 = '7673G5' 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 = '7673G5' 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 HALA2009082300387Indicator · inoperativeETOPS SIGNIFICANT SYS - RA FLAG DISPLAYED STEADY ON THE F/O ADI. REMOVED AND REPLACED RT R/A IAW AMM 34-33-01 OPS CHECK OK PERFORMED TEST 30 IAW AMM 22-00-02 AND 767 LMP TABLE 2, TEST PASS. ACFT TO REMAIN IN LAND 3 STATUS.SDR HALA2009081700368Indicator · inoperativeETOPS SIGNIFICANT SYS - FUEL QTY TOTAL PROG PAGE 2 BLANK - FUEL QTY ON CTR TANK INCREASED 5000LBS ON CLIMB OUT-SUSPECT FUEL CTR TANK QTY INCORRECT ON GROUND. PERFORMED T/S IAW FIM 28-41-00/101. BITE TEST OF FQIS NO FAULT FOUND. ALL PARAMETERS NORMAL.SDR HALA2009081600367Indicator · failedETOPS SIGNIFICANT SYSTEM - ATTITUDE INDICATION OF STANDBY ATTITUDE INDICATOR IS ABNORMAL IN ROLL. GYRO FLAG IS RETRACTED. NOTE: SEEMS NORMAL AT FIRST, BUT UPON FIRST TURN AFTER TAKEOFF, THE ROLL MODE BANKS, THEN DOESN'T RECOVER BACK TO WINGS LEVEL.//REPLACEDSDR HALA2009081200362Radar · malfunctionedETOPS SIGNIFICANT SYS - LT RADAR MADE FAINT BRIEF RUBBING SOUND WHEN SWEEPING TO LT. REPLACED WEATHER RADAR. GRD OPS CHK OK AMM 34-43-05.SDR HALA2009081100361Indicator · failedETOPS SIGNIFICANT SYS - FIM 34331302 F/O RADIO ALTIMETER FAILED RA FLAG IN
VIEW AND ADI (STEADY) NO LAND 3 ON AUTOLAND STATUS. PERFORMED F/O'S RA OPS CK OK IAW MM 34-33-00. PERFORMED MCDP GND TEST 30 CK OK IAW MM 22-00-02. LMP STATUS TO REMAIN ON LAND 3 SDR HALA2009080400349Fan Blade · damagedETOPS SIGNIFICANT SYS - FOUND NICK ON NR 2 ENG 1ST STAGE FAN BLADE APPROX 8.5" FROM ROOT AREA F. REPAIRED FAN BLADE IAW TASK 72-31-02 WITHIN LIMITS. EDDY CURRENT CHECK OK.SDR HALA2009072700331Fan Blade · bentETOPS SIGNIFICANT SYS - FOUND NR 1 ENGINE FAN BLADE NR 30 DAMAGED. BENT. INSPECTED BLADE AND DETERMINED TO BE WITHIN LIMITS IAW AMM 72-31-02-206-070-N00 ON NR 1 ENG BLADE 30. OK FOR SERVICE.SDR HALA2009072700330Fan Blade · bentETOPS SIGNIFICANT SYS - FOUND NR 1 ENGINE FAN BLADE 29 DAMAGED. (BENT) INSPECTED BLADE AND DETERMINED TO BE WITHIN LIMITS IAW AMM 72-31-02-206-070-NOO ON NR 1 ENG BLADE 29. OK FOR SERVICE.SDR HALA2009072700329Fan Blade · damagedETOPS SIGNIFICANT SYS -FOUND NR 1 ENGINE FAN BLADE 33 DAMAGED, NICKED. PERFORMED BLADE BLENDING PROCEEDURE IAW AMM TASK 72-31-02-308-003-N00 ON NBR 1 ENG BLADE 33. OK FOR SERVICE.SDR HALA2009071600301Indicator · malfunctionedETOPS SIGNIFICANT SYS - LT MAIN AND TOTAL FUEL QTY IND DISPLAYS FLUCTUATE +/- 300 LBS FUEL QTY TEST NORMAL. FLUCTUATION IS RAPID AND CONTINUOUS. RAN BITE CHECK OF FUEL QUANTITY PROCESSOR BOTH CH 1 AND CH 2 NO FAULTS FOUND. UNABLE TO VERIFY PROBLEM AT THIS TISDR HALA2009070700284Trim System · malfunctionedETOPS SIGNIFICANT SYS - FRM:27211102 2.5 UNITS RUDDER TRIM REQUIRED IN NOSE R DIRECTION WHILE IN CRUISE. NOTE: COMPLETED M284 PROCEDURE AND FORM. INFO NOTED: NO TRIM LIMIT FOR INSERVICE ACFT IAW AMM TASK 27-01-00. OK TO CONTINUE. INSPECTED PRIMARY FLIGHT CSDR HALA2009070700281Indicator · trippedETOPS SIGNIFICANT SYSTEM - BTB - APU AUTO SHUT DOWN. PERFORMED BITE OF APU ECU FOUND LOW OIL PRESSURE FAULT. INSP APU FOUND LUBE OIL FILTER DPI POPPED. T/S IAW FIM 49-11-00 FIG 109 REMOVED AND REPLACED LUBE AND SCAVENGE OIL FILTERS IAW MM 49-27-03, RESET DPSDR HALA2009061800253Transformer · malfunctionedETOPS SIGNIFICANT SYSTEM, APU FAILED TO START FAULT LGT ILLUM AND EICAS MSG APU FAULT DISPLAYED. ADDITIONAL START ATTEMPTS UNSUCCESSFUL. PERFORMED FIM 49-11-00, REPLACED APU TRU PER BLOCK 23 OF FIG 106B AND AMM 24-32-04. GROUND RUN OPS CHECK GOOD. APU STASDR HALA2009061700254Clutch · leakingETOPS SIGNIFICANT SYSTEM, APU LOSING OIL WHILE RUNNING DEPARTED W/QTY FULL AFTER 3:00 HRS QTY .50 AT 3:30 QTY ADD MANUALLY SHUT DOWN APU. REMOVED AND REPLACED O-RING ON APU FILTER HOUSING AND REMOVED AND REPLACED STARTER CLUTCH AND O-RING PER AMM 49-41-06 OPSSDR HALA2009061600247O-Ring · damagedETOPS SIGNIFICANT SYSTEM, APU VERIFICATION START ATTEMPT UNSUCCESSFULLY EICAS MSG APU OIL QTY DISPLAYED AND OIL QTY READS ADD. BITE CHECKED ECU FOUND AC START MESSAGE TS PER FIM 49-11-00. NO DEFECTS NOTED PHYSICALLY CHECKED APU OIL QTY FOUND OIL LEVEL LOW ADSDR HALA2009061500248Starter · failedETOPS SIGNIFICANT SYSTEM, APU VERIFICATION START ATTEMPT, UNSUCCESSFUL. REPLACED APU START RELAY K117 COND SAME. APU START CHECK FAULT PER FIM 49-11-00. REMOVED AND REPLACED STARTER AND CLUTCH ASSY PER AMM 49-41-01 AND 49-41-06. GRND RUN OPS CK GOOD. PRECSDR HALA2009061500240Trim System · malfunctionedETOPS SIGNIFICANT SYSTEM, DURING CRUISE AT FL350 RUDDER TRIM FAILED TO TRIM RT W/FULL TURN KNOB APPLICATION ON SUBSEQUENT ATTEMPTS TRIM MOVED INTERMITTENTLY. NOTE: 2 UNITS RT RUDDER TRIM TO OBTAIN .5 UNITS AILERON TRIM TO RT OF CENTER. TROUBLESHOT PER FIM 27SDR HALA2009061500237Ecu · unknownETOPS SIGNIFICANT SYSTEM, APU INOP, OIL QT ZERO. RAN APU, THEN PHYSICALLY VERIFIED OIL QTY WITH SIGHT GAUGE, LEVEL IS FULL AND QTY INDICATION IN CKPT READS FULL ALSO. BIT CHECK ECU FOUND "A/C START CIRCUIT" MSG, TROUBLE SHOT PER FIM 49-11-00, NO DEFECTS NOTESDR HALA2009061500236Fan Blade · damagedETOPS SIGNIFICANT SYSTEM, RT ENGINE FAN BLADE NR 6 FOUND WITH NICK'S ON THE LEADING EDGE, 2 1/2 INCHES FROM THE TIP. LEADING EDGE AREA "A"-3/16 INCHES BY 1/4 INCHES LONG. PERFORMED BLENDING ON RT ENGINE FAN BLADE NR 6 IAW B7
67 AMM 72-31-02.SDR HALA2009061400241Altimeter · malfunctionedETOPS SIGNIFICANT SYSTEM, INTERMITTENT RADIO ALTIMETER FLAG ON F/O'S PFD ACCOMPANIED BY A NO LAND 3 ANNUNCIATED ON THE AUTOLAND STATUS DISPLAY. F/O'S RA OPERATES NORMALLY IAW FIM REF 34-33-00 FIG 104.SDR HALA2009061000232Apu · faultedETOPS SIGNIFICANT SYSTEM, APU FAULT LIGHT ILLUM. REMOVED AND REPLACED APU PER HAL M266-767, APU CHANGE OPS AND LEAK CHECK GOOD.SDR HALA2009061000230Fire Warning · false activationETOPS SIGNIFICANT SYSTEM, CREW CALLED RT ENGINE FIRE LOOP 2 AND RT ENG O/H EICAS MESSAGE OCCURRED AFTER POWER TRANSFER. PERFORMED FIRE WARNING TEST, ALL FIRE WARNING ANNUN LIGHTS ILLUMINATED AND FIRE WARNING MESSAGE SHOWED ON EICAS SCREEN. ENDED FIRE WARNINGSDR HALA2009060300227Pressure Switch · malfunctionedETOPS SIGNIFICANT SYSTEM, R OIL FILTER EICAS STATUS MESSAGE DISPLAYED. PERFORMED FIM 79-35-00 FIGURE 103. CHIP DETECTOR CLEAN. REPLACED MAIN OIL FILTER PER AMM 79-21-05. REPLACED DIFF PRESSURE SWITCH PER AMM 79-35-01. OPS CHECKS GOOD.SDR HALA2009060300226Warning Light · false activationETOPS SIGNIFICANT SYSTEM, STATUE MESSAGE IN FLIGHT R OIL FILTER. T/S PER FIM 79-35-00 MAG CHIP DET GOOD NO METAL NOTED REPLACED MAIN OIL FILTER FOUND NO METAL IN FILTER. ENG RUN AND LEAK CHECK GOOD MSG DID NOT RETURN OK FOR SERVICE.SDR HALA2009060300225Warning Light · false activationETOPS SIGNIFICANT SYSTEM, STATUE MESSAGE IN FLIGHT R OIL FILTER. T/S PER FIM 79-35-00 MAG CHIP DET GOOD NO METAL NOTED. REPLACED MAIN OIL FILTER, FOUND NO METAL IN FILTER. ENG RUN AND LEAK CHECK GOOD MSG DID NOT RETURN. OK FOR SERVICE.SDR HALA2009060200225Charger · inoperativeETOPS SIGNIFICANT SYSTEM, ON GROUND APU FAILED TO START W/2 ATTEMPTS RECEIVED APU FAULT EICAS MSG, ACCOMP FIM 49-11-00 FIG 105 AND FIM 49-11-00 FIG 104. REMOVED AND REPLACED APU BATTERY CHARGER PER AMM 24-31-05. OPS CK OK. REMOVED AND REPLACED APU BATTERY PSDR HALA2009053000209Controller · malfunctionedETOPS SIGNIFICANT SYSTEM, EICAS MSG "R FWD WINDOW" WITH R FWD WINDOW HEAT INOP LIGHT ON OVERHEAD PANEL. BITE CHECK RT WINDOW HEAT CONTROLLER PER AMM 30-4-01-240-801. OPS CHECK GOOD, NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2009052900208Pressure Switch · failedETOPS SIGNIFICANT SYSTEM, C HYD PRIM 1 EICAS MESSAGE W/ASSOC PRESS LIGHT. REMOVED AND REPLACED PRESSURE HYD SWITCH IAW 29-11-18-004-001. OPS CK AND LEAK CK OK.SDR HALA2009052900207Unknown · unknownETOPS SIGNIFICANT SYSTEM - RIGHT ENGINE START DUCT PRESSURE LOW AT R DUCT 17 PSI L DUCT 19 PSI MAX MOTORING N2 AT 19 PERCENT. LEFT ENGINE START DUCT PRESSURE AT L DUCT 20 PSI, R 22 PSI MAX MOTORING 21 PERCENT, FRM CODE 80030502. STARTED BOTH ENGINES, RAN AT SDR HALA2009052100184Circuit Breaker · malfunctionedLT WEATHER RADAR WILL NOT TEST. RESET WX RADAR C/B FOR LT SIDE. OPERATION NOW TEST NORMAL.SDR HALA2009051900181Trim System · out of toleranceOPEN - ETOPS SIGNIFICANT SYSTEM - ACFT FLYS OUT OF TRIM, NEEDS RT AILERON 2 DEGREES RT RUDDER, 2 DEGREES FOR STRAIGHT AND LEVEL, SAME IN A/P MODE. PERFORMED AILERON TRIM CONTROL OPERATIONAL TEST PER AMM 27-11-00-715-002 STEPS A-G, PERFORMED RUDDER TRIM CONTROSDR HALA2009051800180Annunciator · no testETOPS SIGNIFICANT SYSTEM, APU/CARGO FIRE CONTROL PANEL CARGO "DISCHARGE" ANNUNCIATOR WILL NOT TEST. REMOVED AND REPLACED APU/CARGO FIRE PANEL "DISCHARGE " SWITCH OPS CHECK'S GOOD IAW AMM 26-22-03.SDR HALA2009051800178Annunciator · no testETOPS SIGNIFICANT SYSTEM, APU/CARGO FIRE CONTROL PANEL CARGO "DISCHARGE" ANNUNCIATOR WILL NOT TEST. REMOVED AND REPLACED APU/CARGO FIRE PANEL "DISCHARGE " SWITCH OPS CHECK'S GOOD IAW AMM 26-2203.SDR HALA2009051400178Warning Message · illuminatedETOPS SIGNIFICANT SYSTEM, BOTH AFT FAN EXH 1 AND FAN EXH 2 CAME ON POWER TRANSFER "EICAS MSG". RESET CB AND OPS CKD, SYS CKD OK. A/C OK FOR SERVICE.SDR HALA2009050600170Aileron · out of rigACFT FLYS OUT OF TRIM OVER 1 1/2 DEGREE RT AILERON OVER 2 DEGREE RT RUDDER. ACFT WANTS TO ROLL LEFT CONSTANTLY. REMOVED SCREWS FOR LEFT WING PANELS 561BB, 561AB, AND 552HB. RE-RIGGED LT INBD AILERON PER AMM 27-11-08. CLOSED ACCESS PANELS 561BB, 561AB AND 5SDR HALA2009042800168Unknown · unknownETOPS SIGNIFICANT SYSTEM - L PIMU MSG ON ECS/MSG. TROUBLESHOOT WITH FIM 71-00-00. BITE OF PIMU SHOWED EEC CH A/B XTRN DISAGREE. EPCS PAGE 2 DOESN'T SHOW ANY LABEL BIT INFO FOR OVERSPEED CIRCUITS. ERASED L PIMU PERFORMED BITE AND RAN ENGINE MSG DID NOT RETUSDR HALA2009042500166Indicator · intermittentETOPS SIGNIFICANT SYSTEM, CAPT A/S IND RED FLAG OVER MACH INDICATOR INTERMITTENT. REPLACED CAPT MACH/A/S IND. OPS CHECK OK PER M/M 34-13-02.SDR HALA2009042200162Indication Sys · malfunctionedETOPS SIGNIFICANT SYSTEM, RUDDER POSITION INDICATOR FAILS TO INDICATE RUDDER MOVEMENT ON EICAS LOWER SCREEN INDICATOR. RUDDER TRIM INDICATOR ON CENTER CONSOLE OK. PERFORMED OPERATIONAL TEST OF RUDDER AND RUDDER TRIM CONTROL SYSTEM IAW AMM 27-21-00. NO DEFECSDR HALA2009041100142Control Panel · malfunctionedETOPS SIGNIFICANT SYSTEM, F/O MAP RANGE SELECTOR WILL NOT REDUCE LOWER THAN 160 MILES SCALE. REMOVED AND REPLACED F/O'S EFIS CONTROL PANEL PER AMM 34-22-02. OPS CK OK. PERFORMED TEST 30 ON LMP 767 TABLE 2. TEST PASS. ACFT WILL REMAIN IN LMP STATUS LAND 3.SDR HALA2009041100140Fan Blade · nickedETOPS SIGNIFICANT SYSTEM, FOUND NICK ON NR 2 ENGINE 1ST STAGE FAN BLADE. BLENDED AREA, WITHIN LIMITS PER AMM 72-31-02, EDDY CURRENT ACCOMPLISHED.SDR HALA2009040900150Access Panel · corrodedCORROSION ON FUEL TANK PANEL 541WB, ON CUT-OUT MATING SURFACE. PANEL REPLACED, CORROSION OUTSIDE SRM 57-20-01/201 REV 79 LIMITS.SDR HALA2009040800159Skin · damagedLIGHTING STRIKE ON FUSE CROWN AT BS 929, S 4/5. DAMAGED AREA REWORKED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01/101 SHEET 6, REV 79. IFEC INSPECTION IAW NDT MANUAL PT 6 51-00-19 REV 92. NO CRACKING EVIDENCE.SDR HALA2009040800152Skin · damagedLIGHTING STRIKE ON FUSE CROWN AT BS 871-54L. REPAIRED BY RIVET REPLACEMENT IAW B767-300-01, SRM 53-00-01 FIG 201, SECTION 2, SHEET 2 REV 79. IFEC INSPECTION IAW NDT 767 MANUAL PT 6 510049 REV 92, NO CRACKS NOTED.SDR HALA2009040800134Radar · inoperativeETOPS SIGNIFICANT SYSTEM, ON PREFLT, FOUND RADAR AND WINDSHEAR ALERT SYSTEM INOP, TEST FAILED. TESTED WEATHER RADAR PER FIM 34-43-00. SYSTEM TESTS OK PER FIM. RADAR AND WINDSHEAR NOW TEST OK IN FLIGHT DECK.SDR HALA2009032900116Indicator · malfunctionedETOPS SIGNIFICANT SYSTEM, RECAGED. OPS NORMAL. ATTITUDE INDICATION OF STANDBY ATTITUDE INDICATOR IS ABNORMAL IN PITCH AND ROLL. GYRO FLAG RETRACTED, INTERMITTENT. REPLACED STANDBY ATTITUDE IND, OPS CHECK OK PER M/M 34-24-01.SDR HALA2009032800115Indicator · malfunctionedETOPS SIGNIFICANT SYSTEM, STAND BY ATTITUDE INDICATOR INOP (TUMBLED ON APP TO SYD). STAND BY ATTITUDE INDICATOR GROUND CHECK NORNAL NO FLAGS AND NOT TUMBLED IAW AMM 34-26-1.SDR HALA2009032800114Iru · malfunctionedETOPS SIGNIFICANT SYSTEM, AFTER LANDING RECEIVED RIGHT IRS FAULT EICAS MSS. REPLACED RT IRU. GND OPS CHECK OK PER AMM 34-21-01. ACCOMPLISHED MCDP TEST 30. TEST PASSED A/C LMP STATUS TO REMAIN AT LAND 2.SDR HALA2009032700113Iru · misalignedETOPS SIGNIFICANT SYSTEM, AFTER LANDING RECEIVED RIGHT IRS FAULT EICAS AND FAULT LIGHT ILLUM ON RIGHT IRU. REALIGNED IRU'S PERFORMED OPERATIONAL CK PER M/M 34-21-00, NO FAULTS NOTED OK FOR CONT SERVICE.SDR HALA2009032500102Trim System · malfunctionedETOPS SIGNIFICANT SYSTEM, INFO NOTE, IT TAKES +2 UNITS OF RUDDER TRIM TO THE RIGHT TO CENTER AILERON TRIM ON CONTROL YOKES (MARKINGS). THE ADI BALL IS TO THE LEFT OF CENTER. EICAS SURFACE POSITION INDICATOR SHOWS RUDDER CENTERED AND AILERON (ALL) ABOVE CENTESDR HALA2009032200099Generator · malfunctionedETOPS SIGNIFICANT SYSTEM, LT GENERATOR TRIPPED OFF AT CRUSE FL 370 CYCLED PER QRH RESET OK. TROUBLE SHOT PER FIM 24-11-00 FIG 101, HAD FAULT D9 THAT FAULTED GCU. RAN BITE TEST FOR GCU, ALL TESTS WERE NORMAL. NO PREVIOUS FLIGHT FAULTS, NO CURRENT FLIGHT FAUL
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