Boeing 767-33A
Service difficulty reports · 1,978
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 = '76733A' 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 = '76733A' 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 HALA0300785Housing · damagedPAE - LEFT WING MAIN TANK FUEL BOOST PUMPS SHOWS EVIDENCE OF ARCING BETWEEN PUMP HOUSING AND SHUTOFF SLEEVES. REPAIRS IN WORK. (M)SDR HALA0300786Housing · damagedPAE - RIGHT WING MAIN TANK BOOST PUMPS SHOWS EVIDENCE OF ARCING BETWEEN PUMP HOUSING AND SHUTOFF SLEEVES. REPAIR IN WORK. (M)SDR HALA0300647Pseu · inoperativeTRAILING EDGE FLAP LIGHT ON. FLAPS SELECTED TO 5 DEGREES, FLAPS ONLY EXTENDED TO 1 DEGREE. PSEU CODE 27-81041. REPLACED NR 1 OUTBOARD RDVT IAW MM 27-31-11 OPS CHECK FLAP/SLAT OK.SDR HALA0300632Control Unit · malfunctionedTE FLAP DISAGREE LIGHT ILLUMINATED WHEN SELECTING MORE THAN FLAPS ONE. FSUE FAULTS OUTBOARD FLAP RVDT NR 1 M544. REPLACED O/B FLAP RVDT NR 1 IAW MM 27-81-11. OPERATE FLAPS AND SLATS NORMAL AND ALTERNATE, ALL INDICATIONS AND OPERATIONAL NORMAL. SYSTEM OPS NSDR HALA0300292Switch · inoperativeAPU FAULED TO START. APU DOOR LIGHT CAME ON, NO APU FAULT LIGHT, NO RPM OR EGT. T/S PER FIM 49-11-00/101, FIG 104 BLOCK 24A HIGH RESISTANCE AT PIN 7 OF RELAY DS47. REPLACED DOOR SWITCH, RESISTANCE NOW NORMAL. APU STARTED NORMAL THREE TIMES. SWITCH REPLACEDSDR ANCF200300006Packing · brokenL HYD QTY DECREASE TO 0.06 WITH EDP PRESSURIZED AND ACMP OFF; HYD QTY CONTINUED DECREASING. AIRCRAFT RETURNED TO BOGOTA.CORRECTIVE ACTION:LH DIFFERENTIAL PRESSURE INDICATOR WAS FOUND WITH LEAK. DIFFERENTIAL PRESSURE INDICATOR WAS REMOVED AND BOTH PACKINGS WESDR HALA0300029Relay · failedLAX - BOTH AC AND DC STANDBY POWER LOST AND EICAS MESSAGE STANDBY BUS OFF DISPLAYED. STANDBY POWER BUS OFF LIGHT ILLUMINATED, BOTH INDICATORS SAME WHEN STANDBY POWER MOMENTARILY SELECTED TO BAT. REPLACED K-109 STANDBY POWER RELAY. PERFORMED STANDBY POWER. SDR HALA0300008Duct · blownHNL - FOUND BLOWN AIR SUPPLY DUCT FOR FORWARD CARGO HEAT SYSTEM. REPLACED DUCT ASSEMBLY. (M)SDR AUS20021061Door · separated(AUS) LH MAIN LANDING GEAR TRUNNION DOORS MISSING. DAMAGE CAUSED TO BRAKE AND LANDING GEAR HYDRAULIC LINES. LH HORIZONTAL STABILISERHAD MINOR IMPACT DAMAGE TO THE LEADING EDGE.SDR AUS20020941Chip Detector · contaminated(AUS) NR 1 ENGINE CHIP DETECTOR CONTAINED METAL PARTICLES. METALLURGICAL INVESTIGATION FOUND THAT THE METAL WAS NOT FROM ANY ENGINE COMPONENT AND IT IS SUSPECTED TO BE BUILD SWARF.SDR AUS20020809Module · failed(AUS) RUDDER RATIO MODULE FAILED.SDR AUS20020709Connector · damaged(AUS) FORWARD CARGO DOOR CONNECTOR PLUG DAMAGED BEYOND REPAIR. SHORT CIRCUIT IN PLUG CAUSED FAULT IN PSEU AND PROXIMITY SWITCH.SUSPECT PLUG DAMAGED BY CONTAINER DURING UNLOADING.SDR AUS20020543Oil System · contaminated(AUS) LH ENGINE NO6 BEARING SCAVENGE FILTER BLOCKED WITH CARBON PARTICLES AND D' SUMP SCAVENGE LINES COKED CAUSING OIL TO BE VENTED OVERBOARD. ENGINE OIL TYPE HAD BEEN CHANGED FROM EXXON 2380 TO MOBIL JET II.SDR HALA0200156Relay · failedETOPS SIGNIFICANT SYSTEM: F/O PITOT HEAT WOULD NOT RESET. REPLACED AIR/GROUNG RELAY K528. PITOT HEAT CHECKS GOOD. NO FAULT MESSAGES.SDR AUS20020520Oil System · contaminated(AUS) RH ENGINE D SUMP OIL SCAVENGE LINES AND D SUMP OIL FILTER COKED WITH CARBON BUILDUP CAUSING SUMP TO FILL WITH OIL AND VENTOVERBOARD. OIL TYPE HAD BEEN CHANGED FROM 2830 TO MJ2 SIX MONTHSPREVIOUSLY.SDR HALA0200111Apu · failedETOPS SIGNIFICANT SYSTEM: APU FAILED TO START IN AIR. OAT-52, FL 360. APU EGT REACHED 594 DEGREES AND ONLY 8 RPM. THEN ADD OIL LIGHT AND APU FAULT. VISUALLY CHECKED APU OIL QUANITY. OIL LEVEL WAS FULL, NO OIL ADDED. PERFORMED BITE CHECK OF APU ECU PER 7SDR AUS20020363Hose · ruptured(AUS) RH MLG WOULD NOT RETRACT DURING CLIMB. GROUND INVESTIGATION FOUND THE HYDRAULIC HOSE CONNECTED TO THE 'UP' ACTUATOR HAD RUPTURED.SDR HALA0100315Pump · damagedETOPS SIGNIFICANT SYSTEM, PER EO 28-01-03-71, LEFT AFT FUEL BOOST PUMP CONDUIT OUTER SLEEVE HAS A HOLE APPROX 44 INCHES FROM TERMINAL END. REPLACED LEFT AFT BOOST PUMP CONDUIT OUTER SLEEVE PER EO 28-01-0371 REV A. (M)SDR HALA0100314Pump · damagedHNL - ETOPS SIGNIFICENT SYSTEM, PER EO 28-01-03-71 LT AUX TANK BOOST PUMP CONDUIT OUTER SLEEVE HAS A HOLE APPROX 14 INCHES FROM TERMINAL END. REPLACED LEFT OVERRIDE AUX PUMP CONDUIT OUTER SLEEVE PER EO 28-01-03-71 REV A. (M)SDR HALA0100280Fire Loop · damagedHNL - FLT 32 - RIGHT ENGINE FIRE LOOP FAILED. TROUBLE SHOT RIGHT ENGINE FIRE DETECTOR SYSTEM PER FIM 29-11-00 PAGE 101 FIG 104. FOUND AFT UPPER FIREWALL 'B' LOOP HAS HIGH RESISTANCE LOOP P/N 2520545. REPLACED UPPER AFT FIRE WALL ELEMENT ASSY, OPS CHECK OK PSDR ANCF200100006Hose · leakingDURING CLIMB, PASSING 25,000 FT, THE STANDBY ALTIMETER SHOWED 17,000 FT AND THE AIRSPEED INDICATORS SHOWED 320 KNTS WHILE THE STANDBY AIRSPEED INDICATOR SHOWED 220 KNTS. WITH 28,000 FT IN THE CAPTAIN AND F/O ALTIMETER THE STANDBY ALTIMETER SHOWED 18,000 FT. SDR ANCF200100003Computer · looseDURING TAKE OFF ROLL CAPT'S ADI AND HSI SCREENS WENT BLANK WHEN AIRCRAFT ROLLED OVER IRREGULARITIES ON RUNWAY, DURING TAXI BACK TO GATE INSTRUMENTS WENT BACK TO NORMALCORRECTIVE ACTIONTHE EICAS COMPUTER AND LH SYMBOL GENERATOR WERE ADJUSTED ON RACK, ALSO WERE SDR AU001004Door · separated(AUS) RT MAIN LANDING GEAR STRUT AND TRUNNION DOORS MISSING.INVESTIGATION FOUND OTHER DAMAGE INCLUDING RH BRAKE LINES AND BOGIE TILT ACTUATOR HYDRAULIC LINES. IMPACT DAMAGE OCCURRED TOTHE WING TO BODY FAIRING (PANEL 196KR) AND UNDERWING PANEL 615SB. THE RH HORSDR AU991015Rod · worn(AUS) FOLLOWING REMOVAL OF THE RT PYLON BOAT FAIRING FOR REPAIR THE FOLLOWING DEFECTS WERE FOUND: 1. RT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE AND SUPPLY LINE ELBOW JAM NUTS BACKED OFF AND ELBOW FRETTING IN PYLON RECEPTACLES2S. 2. INBOARD VERTICAL STRAKESDR AU970155Bracket · cracked(AUS) RH WING OUTBOARD FLAP DEFLECTION CONTROL TRACK FITTING CRACKED ON LH AND RH SIDES - SLIGHT DAMAGE TO RH WING CLOSE-OUT PANELSDR AU961143Skin · cracked(AUS) FUSELAGE SKIN CRACKED - CRACK LENGTH 38.1MM (1.5IN) - FURTHER INVESTIGATION OF REAR CARGO FLOOR REVEALED EXFOLIATION CORROSIONSDR AU960756Circuit Board · faulty(AUS) RH ENGINE FIRE DETECTION SYSTEM PRINTED CIRCUIT CARD M683 IN P54 CARD RACK FAULTY - FALSE FIRE WARNING ON RH ENGINE RESULTED IN DISCHARGE OF BOTH FIRE BOTTLESSDR AU960417Switch · faulty(AUS) RAM AIR TURBINE (RAT) AIRSPEED SWITCH FAULTY - SUSPECT FAULTY DIODE - RAT FAILED TO AUTODEPLOY
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