Boeing 767-33AER
Service difficulty reports · 288
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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 = '76733AER' 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 = '76733AER' 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 HALA2010112600565Idg · malfunctionedETOPS SIGNIFICANT SYSTEM, EICAS MX LEVEL MSG IDG OUT TEMP DISPLAYED AT TOP OF CLIMB L/R IDG OUT 82 113, L/R IDG RISE 812. T/S PER FIM 24-20-00 FIG 103. BITE CK OF BPCUNO FAULTS NOTED. SERVICED IDG. MSG IS NUISANCE MSG. OK FOR SERVICE.SDR HALA2010112300564Ptu · failedWHILE TESTING SPOILERS, AILERONS AND FLAPS A LARGE HYDRAULIC LEAK WAS NOTICED FROM THE HORIZONTAL STAB COMPARTMENT. CONDITIONS IMMEDIATELY PRIOR TO SHUTDOWN OF HYDRAULIC. LT HYD PUMP OFF (QTY. 1.4), THEN RT HYD PUMP ON(QTY.0.70), BIG PUDDLE ON THE FLOOR, HORSDR HALA2010111900552Indicator · malfunctionedETOPS SIGNIFICANT SYSTEM, F/O ANALOG AIRSPEED COMMAND BUG FLAG IN VIEW, BUG WILL NOT MOVE. EADI AIRSPEED TAPE WAS NORMAL. REPLACED F/O MACH AIRSPEED IND. OPS CKD GOOD PER AMM 34-13-02.SDR HALA2010111800548Computer · malfunctionedETOPS SIGINIFICANT SYSTEM, EICAS MSG TCAS DISPLAYED TCAS FAIL. REMOVED AND REPLACED TCAS COMPUTER PER AMM34-45-01. OPS CK OK FOR SVC.SDR HALA2010111700544Warning Light · illuminatedETOPS SIGNIFICANT SYSTEM, EICAS TCAS DISPLAYED. PERFORMED FIM 34-53-00 SYSTEM TEST NORMAL. OK TO CONTINUE.SDR HALA2010111500562Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK AT BS 348, RBL 55, ON UPPER CROWN, WHERE IT CONTACTS, DIVIDER SUPPORT FITTING. ASSESSED BEYOND LIMITS, IAW SRM 53-00-52 1A-1. TRACK REPLACED.SDR HALA2010100600457Indicator · inoperativeETOPS SIGNIFICANT SYS - LT MAIN FUEL TANK INDICATOR INOP (ON LT WING FUEL PANEL). (FUEL QTY INDIATOR) R & R LT FUEL TANK INDICATOR ON LT WING PANEL IAW AMM28-41-06 OPS CK OK, OK FOR SVC.SDR HALA2010100600456Throttle · out of adjustETOPS SIGNIFICANT SYS - THROTTLE HANDLES MUST BE SPLIT ONE FULL WIDTH TO HAVE PARALLEL. INFO NOTED NO EXCEEDENCE NOTED NO EICAS MESSAGE IAW POWERPLANT ENGINEER. OK TO CONTINUE. THROTTLE SPLIT WHEN LIVING UP ENG. PARAMETER OTHER THAN EPR.SDR HALA2010100500448Sensor · inoperativeETOPS SIGNIFICANT SYS - ATB - LT PACK INOP. PERFORMED FIM 21-51-00, FIG 103. LT PACK CONTROLLER FAULTS COMPRESSOR SENSOR. REPLACED LT PACK COMPRESSOR OUTLET TEMP SENSOR IAW AMM21-51-06-401. TESTS OK. TROUBLESHOOTING WITH FIM21-51-00FIG104B USING APU AIR SHOSDR HALA2010091700427Aileron Sys · malfunctionedETOPS SIGNIFICANT SYS - 2711XA09 - IN CRUISE, LT INBD AILERON INDICATES UPWARD DEFLECTION OF APPROX 2.5" RAIL IS NORMAL. ACFT TRIMMED ALL NORMAL (ZERO). VISUAL INSP CONFIRMED LT INBD AILERON DEFLECTED UPWARDS APPROX 2" AT OTBD EDGE, RT INBD AILERON FLUSH. PESDR RYNA2010009020029Control Unit · malfunctionedROOT CAUSE: LIGHT FLICKERED DURING CRUISE. LEFT GEN DRIVE. REMOVED AND REPLACED BPCU PER MM 24-41-03 DUE TO FAULT MESSAGE "REPLACE BPCU", SERVICED LT IDG PER MM 12-13-01. VERIFIED WIRING FROM D10964 TO 4216P FOR OBVIOUS DEFECTS, VISUALLY CHECKS OK. LT GENSDR HALA2010090200388Engine · leakingETOPS SIGNIFICANT SYS - DURING ETOPS INSP FOUND OIL ACCUMULATION APPROX 1 OZ IN NR 2 ENG INLET, NO OIL WAS REQUIRED TO BE SERVICED AND NO OTHER LEAKS NOTED IAW AMM 71-00-00-795-003-N00, PERFORMED GROUND TEST AT IDLE POWER NO FURTHER LEAKS NOTED, OK FOR SERVICSDR HALA2010090200387Oil Filter · trippedETOPS SIGNIFICANT SYS - DURING ETOPS INSP FOUND DPI POPPED ON APU OIL PUMP FILTER. R & R OIL FILTER. NO METAL FOUND, RESET DPI, RAN APU NO LEAKS, DPI DID NOT TRIP, OK FOR SERVICE.SDR HALA2010081000360Priority Valve · malfunctionedETOPS SIGNIFICANT SYS - EICAS MESSAGE LT ENGINE BLEED OFF DISPLAYED LT ENGINE BLEED OFF & BLEED LGT ILLUMINATED. R & R NR 1 ENG PRV IAW AMM36-11-18. OPS & LEAKS CHECKS OK.SDR RYNA2010007020025Brake Assy · disintegratedUPON POST FLIGHT INSPECTION THE NR 6 BRAKE WAS FOUND CATASTROPHICALLY DISINTEGRATED. REMOVED AND REPLACED NR 6 MAIN LANDING GEAR BRAKE ASSEMBLY. OPERATIONAL CHECKED GOOD. INSPECTED LEFT MAIN LANDING GEAR FOR DAMAGE, NONE FOUND AMM REF 32-41-08 AND 32-45-01.SDR RYNA2010007020022Smoke Detector · intermittentAFT LT LAVATORY SMOKE DETECTOR RINGS INTERMITTENTLY UPON DESCENT. CAN BE RESET, BUT WILL RING AGAIN SOON. REMOVED AND REPLACED AFT LT SMOKE DETECTOR PER MM 26-13-01. OPERATIONAL CHECKED GOOD.SDR HALA201007090300Apu · failedETOPS SIGNIFICANT SYSTEMS - APU QUIT ON PUSHBACK. REMOVED & REPLACED APU ASSY IAW TASK HAL M266-767. LEAK CHECK AND OPS CHECKS GOOD. ITEM CLEARED FROM MIC SHEET.SDR HALA2010033100144Warning Light · illuminatedETOPS SIGNIFICANT SYS - RUDDER RATIO LIGHT ON AFTER ENGINE START. PERFORMED FIM 27-09-00 FIG 106. OPS CK GOOD. OK FOR SERVICE.SDR HALA2010032100128Monitor · malfunctionedETOPS SIGNIFICANT SYSTEM - FWD EQUIP COOLING FAN STATUS MSG ILLUMINATED. REPLACED FWD EQUIP SUPPLY FAN MONITOR PER AMM 21-58-06, GROUND OPS CHECK OK.SDR HALA2010032100127Apu · malfunctionedETOPS SIGNIFICANT SYSTEM - APU FAILED TO START AFTER TWO ATTEMPTS. BOTH APU START ATTEMPTS MADE AFTER A/C TURNED TAIL INTO THE WIND ALLOWED APU TO DRY. CHECKED & SERVICED OIL. ADDED 1.5 PINTS, OK. SECURED OIL CAP. ACCOMPLISHED BITE CHECK PER FIM 49-11-00 SDR HALA2010031800122Apu · malfunctionedETOPS SIGNIFICANT SYSTEM - APU FAULT APU DID NOT START WHILE TAXI UPON ARRIVAL. OPERATIONAL CHECK PERFORMED. APU OK FOR SERVICE REF: FIM 49-11-00/101 FIG 103 AMM TASK 49-11-00-802-002.SDR HALA2010031700121A/C Pack · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT PACK INOP LIGHT ON. RESET LEFT PACK. NO OTHER FAULTS NOTED. OPS CHECK GOOD.SDR HALA2010031700120Circuit Breaker · trippedETOPS SIGNIFICANT SYSTEM - R FMC FAIL. RESET NR 2 MCDU C/B. GROUND CHECK OK PER MM 34-61-01.SDR HALA2010021000061Apu · shutdownETOPS SIGNIFICANT SYS - AFTER PUSHBACK AND BEFORE START, APU SHUTDOWN. DID ONE RESTART AND IT RAN NORMALLY DURING START UP. BITE CHK APU IAW FIM 49-11-00/101. CLEARED FAULT IAW FIM. RESTARTED APU OPS CHECKED IS GOOD. NO FAULTS NOTED.SDR HALA2010021000059Skin · damagedLIGHTING STRIKE AT STATION 682,36R. BLENDED WITHIN SRM LIMITES IAW SRM 53-00-01 FIG 101, D634T210 REV.82.SDR HALA2010021000058Skin · damagedLIGHTING STRIKE AT ST.678,37R. BLENDED WITHIN LIMITS IAW SRM 53-00-01, FIG 101, D634T210 REV 82.SDR HALA2010021000057Skin · damagedLIGHTING STRIKE AT ST. 670 & 38R. BLENDED WITHIN SRM LIMITS IAW SRM 53-00-01, D634T210 REV 82.SDR HALA2010021000056Skin · damagedLIGHTING STRIKE AT STA 654+60, S36R. BLENDING WITHIN SRM LIMITS IAW SRM 53-00-00, FIG. 101, D634T210 REV. 82.SDR HALA2010020800054Controller · malfunctionedETOPS SIGNIFICANT SYS - FRM 21300900 CABIN PRESSURIZATION UNBALE TO MAINTAIN SCHEDULE ALTITUDE AT FL 380 W/ENT ANTI ICE ON. DUCT PRESS 15 PSI, OUTFLOW VLV FULLY CLOSED, CABIN CLIMB AT 300 FPM REACHED 8500'(SCHED IS 6500') COND SAME IN AUTO 1 OR AUTO 2 W/ENG ANSDR HALA2010020700052Controller · failedETOPS SIGNIFICANT SYSTEM -CABIN PRESSURIZATION UNBALE TO MAINTAIN SCHEDULE ALTITUDE AT FL 380 W/ENG ANTI ICE ON. DUCT PRESS 15 PSI, OUTFLOW VLV FULLY CLOSED, CABIN CLIMB @300 FPM REACHED 8500'(SCHED IS 6500') COND SAME IN AUTO1 OR AUTO2 W/ENG ANTI ICE OFF CABISDR HALA2010020700051Heat Exchanger · leakingETOPS SIGNIFICANT SYSTEM - DURING ETOPS 2 CHECK - NOTICED LOUD AIR LEAK COMING FROM LT A/C PACK COMPARTMENT. FOUND LT HEAT EXCHANGER CRACKED AT WELD.//R/R LT PACK HEAT EXCHANGER (SECONDARY HALF) PER AMM 21-51-02 OPS AND LEAK CHECK OK. BITE CHECK LT PACK TEMP CSDR HALA2010020300048A/C Pack · false indicationETOPS SIGNIFICANT SYS - LT PACK INOP LIGHT ILLUMINATED EICAS MESSAGE LT PACK TEMP DISPLAYED. OPERATED NORMAL AFTER STBY SELECTED. ACCOMP LT PACK BITE CHECK NO HARD FAULTS. RAN PACKS OPS CHECKS GOOD.SDR HALA2010010900013Idg · malfunctionedETOPS SIGNIFICANT SYS - RT GEN OFF ILLUM. RT GEN SW FAILED TO CLOSE (LATCHED IN) GEN BREAKER RT OFF LIGHT ILLUMINATED AND EICAS MSG GEN OFF DISPLAYED. BITE BPCU IAW FIM 24-20-00 FOUND RT FAULTS POR/FDR GEN. REMOVED RT ENG IDG IAW AMM 24-11-01-004-002-004,INSDR HALA2010010700007Warning Light · illuminatedETOPS SIGNIFICANT SYS - L OFF PACK LT ILLUMINATED. PERFORMED BFIM 21 51 00 FIGURE 104A NO FAULTS NOTED, SYS OPS NORMAL.SDR RYNA200911170023Battery Pack · dischargedDURING AIRCRAFT INSPECTION FOUND THE R3 AND R4 EMERGENCY EXTERIOR DOOR LIGHT INOP. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK M733 PER AMM 33-51-07, OPS CHECK GOOD.SDR HALA2009091400404Starter · failedETOPS SIGNIFICANT SYS - VERIF FLIGHT FOR APU NOT COMPLETED, APU LOAD START UNSUCCESSFUL. "APU FAULT" DISPLAYED APU SPOOLED UP TO 71 PERCENT THEN QUIT. IAW FIM 49-41-00 & INFO NOTED, TROUBLESHOT APU IAW FIM. APU ECU HAD APU START ABORTED MESSAGE. APU VERY SLSDR HALA2009050800172Oil System · leakingAPU AUTO SHUTDOWN DURING START. FAULT LIGHT AND APU OIL QTY STATUS MESSAGE. T/S PER FIM FOUND OIL COMING OUT OF FUEL DRAIN LINE. ADDED 4 QTS OF OIL. PER ENGINEERING REMOVED APU PER TASK CARD M266-767. DUE TO APU AUTO SHUTDOWN AND EXCESSIVE SMOKE COMING OUSDR HALA2009031500086Aru · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB, CAPTAIN'S HEADING SELECTOR INOP, IRS SWITCH TO ALT RESETS PROPER HEADING. REMOVED AND REPLACED NR 1 ARU GROUND CHECK OK AMM 34-21-01 TEST 30 PASSED. ACFT OK FOR SERVICE AND ACFT REMAINS IN TRIPLE LAND STATUS.SDR HALA2009020500042Starter · failedETOPS SIGNIFICANT SYSTEMS, APU FAILED TO START ON ARRIVAL, APU FAULT. CONFIRMED APU CLUTCH DISENGAGES, PERFORMED TROUBLESHOOTING IAW FIM 49-11-00 FIG 103/104 BITE APU STARTER. CHECK APU STARTER, FOUND BURNED HOLE ON BYPASS WEAR INDICATOR AREA. CHECK APU CSDR HALA2009020600041Coil · burned1.5 HOURS OUTSIDE OF PDX, 39KFT, A/T DISCONNECT MESSAGE, ENGINE STARTED TO SPOOL DOWN. PDX MX FOUND CHIP DETECTORS CLEAN, SMALL AMOUNT OF METAL IN MAIN OIL FILTER, FUEL FILTER CLEAN. TRIED TO MOTOR ENGINE, HAD N1 INDICATION BUT NO N2 INDICATION. REMOVED PMASDR HALA0700046Pin · ground damageON PUSHBACK TO RELOCATE A/C, HEARD 2 LOUD BANGS FROM NOSE GEAR. FOUND TOW BAR EXTENDED BEYOND LIMITS AND SHEAR PIN BROKEN AND DAMAGE TO LOWER GEAR. REPLACED NOSE GEAR TOW FITTING PER AMM 32-21-12/401. INSPECTED NOSE WHEEL SYSTEM PER AMM 32-51-00-735-072. NSDR HALA0600512Starter · damagedETOPS SIGNIFICANT SYSTEMS - GTB LT ENGINE N2 DECAYED AFTER START WOULD NOT MOTOR ABOVE 5 PERCENT, N2 ON MOTORING. FOUND LT ENGINE STARTER DAMAGED. REMOVED AND REPLACED LT ENGINE STARTER IAW AMM 80-11-01. GROUND CHECKED OK.SDR HALA0600390Controller · malfunctionedETOPS SIGNIFICANT SYSTEM RIGHT PACK TEMP EICAS MESSAGE PACK OPERATES IN STANDBY. REMOVED AND REPLACED RIGHT PACK CONTROLLER PER AMM TASK 21-51-14-004-001, ALL CHECKS NORMAL.SDR HALA0500889Ground Wire · shortedREMOVED AND REPLACED APU STARTER IAW AMM. DID NOT FIX DISCREPANCY. (LOANER STARTER FROM DELTA). TROUBLESHOT WIRING TO STARTER AND FOUND STARTER GROUND LEADS SHORTED AT TERMINAL/ AIRFRAME SIDE. REPAIRED, REPLACED GROUND LEADS AND TERMINAL ENDS, AND FABRICATSDR DL76L050426Brake · leakingLEFT BRAKE REPORTED SMOKING BY RAMP ON ARRIVAL. FOUND NR 2 BRAKE LEAKING AT LOWER PISTON CAUSING BRAKE FIRE. FLT DECK BRAKE TEMP INDICATES 4. REPLACED NR 2 MAIN BRAKE AND WHEEL ASSY PER MM. PERFORMED HEAT DAMAGE INSP PER MM 05-51- 14 PAGE 201. NO FURTHER MSDR 35505Floorbeam · corrodedCABIN FLOORBEAM AT STA 1480 LBL 70 CORROSION OUT OF LIMITS B767 SRM 53-00-51. REPAIR REQUIRED. FLOORBEAM CORRODED BECAUSE OF LAY AREA LEAKS. LAY AREA NEEDS TO BE PROPERLY SEALED.SDR TIP2004F00000Floorbeam · corrodedCABIN FLOORBEAM STA 1480, RBL 42, CORRODED. CORROSION OUT OF LIMITS IAW B767 SRM REPAIR REQUIRED. FLOORBEAM IS NEAR GALLEY AREA WHERE SPILLS OCCUR. NEED TO MAKE SURE OF PROPER CIC APPLICATION. AIRCRAFT WAS IN STORAGE FOR APPROX 2 YEARS.SDR TIP2004F00004Floorbeam · corrodedCABIN FLOORBEAM AT STA 303, RBL 54 THRU RBL 82. CORROSION OUT OF LIMITS. REPAIR REQUIRED. SRM 53-00-51. FLOORBEAM IS IN WET/GALLEY AREA, SPILLS IN AREA CORRODED BEAM. GALLEY NEED TO BE PROPERLY SEALED AND VAPOR BARRIER INSTALLED. TASK CARD NR S53-027-02.SDR TIP2004F00003Floorbeam · corrodedCABIN FLOORBEAM AT STA 287, RBL 20 THUR 82. CORROSION OUT OF LIMITS IAW B767 SRM REPAIR REQUIRED. FLOORBEAM UNDER WET AREA, SPILLS AND LEAKS CORRODED FLOORBEAM. GALLEY AREAS NEED MILAR VAPOR BARRIER INSTALLED AND SEALED AREA PROPERLY. AIRCRAFT WAS IN STORASDR TIP2004F00002Floorbeam · corrodedCABIN FLOORBEAM AT STA 325 RBL 24 THRU 54, CORROSION OUT OF LIMITS. B767 SRM, REPAIR REQUIRED. FLOORBEAM CORRODED BECAUSE OF GALLEY AREA LEAKS. GALLEY AREA NEEDS TO BE PROPERLY SEALED. AIRCRAFT WAS IN STORAGE FOR APPROX 2 YEARS. (TASK CARD NR S53-027-02)
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