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 HALA2009081300365Solenoid · leakingETOPS SIGNIFICANT SYS - LT ENG FOUND OIL LEAK ON COWLING. ADDED 5 PINTS ENG OIL TO FILL TO FULL AT GATE. PERFORMED FIM 71-05-00 HIGH OIL CONSUMPTION. FOUND NR 1 ENG FUEL, OIL COOLER BYPASS VALVE SOLENOID LEAKING. REMOVED AND REPLACED BYPASS VALVE SOLENOID. SDR HALA2009081100359Warning Message · false activationETOPS SIGNIFICANT SYSTEM - BTB - L OIL FILTER DISPLAYED ON STATUS PAGE- AFTER START RETURNED TO GATE. C/W FIM 79-35-00 FIG 103, NO CONTAMINATION OF METAL PARTICLES ON CHIP DETECTORS OR FILTER, REMOVED & REPLACED OIL FILTER PER AMM 79-21-05-024-001-N00. 79-21-SDR HALA2009080800356Fmc · malfunctionedETOPS SIGNIFICANT SYS - BTB - SINGLE FMC (L) OPS MESSAGE ON. AFTER LT ENG
SHUTDOWN, OPS NORMAL. RETURNED TO GATE. TROUBLESHOT IAW FIM 34-61-00 FIG 108B FMC SYS OPS NORMAL, OK TO CONTINUE.SDR HALA2009080500352Pump · malfunctionedETOPS SIGNIFICANT SYSTEM - L ENG OIL QTY 12 QTS AFTER START, 10 QTS AT TOP OF DESCENT, THEN 18 QTS AFTER SHUT DOWN. R&R LT ENG SCAVENGE OIL PUMP PER AMM 79-21-04 TO STEP 3.E.(15)08/06/09. AMM 79-21-04 STEP 3 F (1) TO (6)PENDING. ENG GRD RUN COMPLETED, NO LEAKSDR HALA2009080500351Exciter · failedETOPS SIGNIFICANT SYS - DURING OVERNIGHT MX APU FAILED TO START. IN DICATED 20 PERCENT RPM BUT NO LIGHTOFF. T/S IAW FIM 49-61-05 FIG 107. REPLACED IGN PLUG IAW MM 49-41-02 NO HELP. REPLACED LEAD IAW MM49-41-01, NO HELP. REPLACED EXCITER IAW MM 49-41-03. OSDR HALA2009080500350Tank · emptyACFT DIVERTED, DUE TO THE LOSS OF WATER PRESSURE. FOUND ON ARRIVAL H2O TANK EMPTY. SERVICED TO FULL, NO LEAKS NOTED. PRESSURE CHECKED GOOD. OK FOR SERVICE.SDR HALA2009073100345Transmitter · failedETOPS SIGNIFICANT SYS - AFTER LANDING ATTEMPTED 1 APU START. APU FAILED TO START. CHECKED APU STATUS AND APU OIL QTY INDICATED "ADD". REPLACED APU OIL QUANTITY TRANSMITTER IAW AMM 49-94-04. OPS AND UP CK, LEAK CK, OK.SDR HALA2009073000340Eadi · inoperativeETOPS SIGNIFICANT SYS - F/O'S EADI SREEN WENT GRAY IN COLOR WITH NO MARKING. REMOVED AND REPLACED F/O'S EADI IAW AMM 34-22-03-004 AND 34-22-03-404-026.SDR HALA2009072800334Warning Message · false activationETOP SIGNIFICANT SYS - BTB - EICAS MSG RT FMC FAIL DISPLAYED, OTHER MSG DISPLAYS SINGLE FMC OPERATION MSG. RT FMC RETURNED TO NORMAL TAXI IN. PILOT HAD PERFORMED A RESET OF CDU IAW QRH PROCEDURES, FMC SHOWS NO FAULTS OR DICREPANCIES, STARTED BOTH ENGS TO VERSDR HALA2009072700328Thrust Reverser · damagedETOPS SIGNIFICANT SYS -NR 2 ENGINE DAMAGE FOUND TO T/R OTBD HALF INNER SEC 5 OCLOCK POS REPETITIVE INSP REQUIRED. ACCOMPLISHED DPM P319305-38 REPETITIVE INSP ON NR 2 ENG T/R OTBD 5 OCLOCK POS NO FURTHER DAMAGE NOTED.SDR HALA2009072400325Valve · malfunctionedETOPS SIGNIFICANT SYS- BTB -AFTER ENGINE START RT PACK OFF LIGHT ILLUMINATED WITH RT PACK EICAS MESSAGE - PACK APPEARS TO BE OPERATING. PERFORMED FIM 21-51-00 FIG 105D, FOUND RT FLOW CONTROL AND SHUTOFF VALVE. REPLACED FLOW CONTROL AND SHUTOFF VALVE IAW AMM SDR HALA2009072300323Warning Light · false activationETOPS SIGNIFICANT SYS - L PACK LIGHT ON EICAS MESSAGE CAME ON IN FLIGHT ACCOMPLANIED BY A LOUD HUM AND VIBRATION. PACK CAME ON AND HUM WENT AWAY AFTER ABOUT 1 MINUTE. PERFORMED FIM 21-51-00 BITE CHECK LFT PACK TEMP CONT ROLLER NO FAULTS NOTED. VISUALLY INSPSDR HALA2009072100320Circuit Card · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB: RT AIR CONDITIONING PACK ILLUMINATES "INOP" PACK OFF. ACCOMP FIM 21-50-00 & WDM 21-51-24. REPLACED RT FLOW CONTROL CARD (M864) PER AMM 21-51-09 /5743. OPS CK PEND. OPS TEST PER AMM 21-51-09 CKS OK. RAN PACK WITH NUMEROUS TEMPSDR HALA2009071600303Connector · dirtyETOPS SIGNIFICANT SYSTEM - ON OVERNIGHT CHECK FOUND C PIMU MESSAGE ON EICAS ECS/MSG PAGE, TROUBLESHOT PER FIM 71 PIMUINX BITE OF LT PIMU REVEALS MESSAGE EEC CH B REVERSER RING FAIL. T/S PER PIMU MESSAGE INDEX 352-25 CODE RESISTANCE CHECK OF EEC HARNESS GOOD SDR HALA2009071400300Liner · crackedETOPS SIGNIFICANT SYS - IAW BORESCOPE NR 1 S/N 729023 - MULTIPLE CRACKS ON INNER LINER COMBUSTION CHAMBER NR 6 AND 7 LOUVERS VIEW THRU AP-9. CRACKS W/IN LIMITS IAW AMM 72-00-00-206-357-N00 TABLE 602A.SDR HALA2009071400294Connector · dirtyETOPS SIGNIFICANT SYS - FOUND ON OVERNIGHT CHECK EICAS MAINT MSG RT PIMU BITE RT PIMU FAULT EEC CH A AOC TR-CK FAIL. T/S IAW FIM PIMU MAINT INDEX CODE 351-23 REMOVED, INSPECTED AND CLEANED AOC CONNECTOR W3P17 AND REINSTALLED CONNECTOR, PERFORMED REPAIR CONFISDR HALA2009071300295Indication Sys · failedETOPS SIGNIFICANT SYS - ON THE GROUND, L FUEL QTY AND TOTAL FUEL QTY INDICATORS WENT BLANK. STATUS MSG DISPLAYED. AFTER A COUPLE OF MINUTES INDICATORS OPERATED NORMALLY. WORKED OK FOR REST OF FLIGHT. ACCOMPLISHED FUEL QTY BITE CHECK IAW AMM 28-41-00 TEST PASDR HALA2009071100291Shutoff Valve · malfunctionedETOPS SIGNIFICANT SYS - RT DUCT PRESS SURGES TO 40 PSI FROM 20 PSI. LT DUCT PRESS STEADY AT 20 PSE, THEN RT DUCT PRESSURE REMAINED AT 40 PSI-CRUSE PWR 86 PERCENT N1. REMOVED AND REPLACED NR1 ENGINE PRSOV IAW AMM 36-11-09. ACCOMPLISHED HIGH POWER ENG RUN ON LSDR HALA2009070800287Relay · unknownETOPS SIGNIFICANT SYSTEM - EICAS MESSAGE HYD GEN VAL ON STATUS PAGE.//REPLACED RELAY K859 OPS CK OK PER DPM24-20-05.SDR HALA2009070800286Bypass Valve · leakingETOPS SIGNIFICANT SYSTEM - FOUND NR 1 ENGINE FUEL BYPASS VALVE LEAKING. REPLACED NR 1 ENGINE FUEL BYPASS VALVE PER AMM 73-11-07.LEAK CHECK GOOD.SDR HALA2009070700282Sensor · faultyETOPS SIGNIFICANT SYS - RT PACK TEMP / R PACK OFF LIGHT ILLUMINATED, FOLLOWED QRH, RESET LIGHTS (EICAS) CAME BACK ON AFTER APPROX 8 MINS. BITE CK RT PNEUMATIC CONTROLLER FOUND RT PACK TEMP SENSOR FAULT. REPLACED RT PACK
TEMP SENSOR IAW AMM 21-51-08. OPS SDR HALA2009070700277Connector · dirtyETOPS SIGNIFICANT SYS - MX LEVEL EICAS MSG 'R ENG EEC C2' DISPLAYED. AOC FIELD BLANK ON B COLUMN OF EPCS DISPLAYED FOR RT ENGINE. PERFORMED RT PIMU BITE. HAS CH A AND CH B AOC TR-CK FAIL (351-23) AND EEC CH B AOC FD-BK FAIL. INSPECTED AND CLEANED AIR OIL COOSDR HALA2009070700276Warning Message · false activationETOPS SIGNIFICANT SYS - RT ENG DUCT PRESSURE WAS INTERMITTENTLY HIGH AT CRZ THRUST AND ABOVE. PRESS NORM AT LOW THRUST.( L DUCT PRESS 23 PSI)( R DUCT PRESS 38 PSI). PERFORMED AIR SUPPLY BITE IAW FIM 36-20-00. LT ENG
HPC FAULT. INSPECTED HPC CONNECTOR AND SDR HALA2009070600283Unknown · unknownOPEN - ETOPS SIGNIFICANT SYS - APU SHUTDOWN WHILE PUSHING BACK. RETURNED TO GATE. T/S IAW FIM49-11-00 FG 110, REM OIL COOLER IAW AMM 49-27-09-004-001 REM OIL COOLER BYPASS VLV IAW AMM 49-27-10-004-001 DISCONNECTED ELEC CONN FROM APU OIL TEMP SENSOR IAW AMM 4SDR HALA2009070600280Thrust Reverser · damagedETOPS SIGNIFICANT SYS - NR 2 BO T/R HALF HAS GROUND DAMAGE. REPAIRED AREA IAW SRM 51-70-04, FIG 2, PERM REPAIR, ENTERED IN ADL.SDR HALA2009070600278Thrust Reverser · damagedETOPS SIGNIFICANT SYS - NR 2 BO T/R HALF HAS GROUND DAMAGE. REPAIRED AREA IAW SRM 51-70-04, FIG 2, PERM REPAIR.SDR HALA2009070500274Inlet · obstructedETOPS SIGNIFICANT SYS - APU SHUTDOWN DURING PUSHBACK. RETURNED TO GATE. T/S IAW FIM 49-11-00 FIG 1110. FOUND DEBRIS BUILDUP ON INLET OF OILER COOLER. REMOVED DEBRIS IAW LETTER DATED 7-5-09. CHECK APU OPS. CHECKS OK. NO FURTHER FAULTS NOTED.SDR HALA2009070400275Controller · unknownETOPS SIGNIFICANT SYS - AT GATE RT PACK TEMP LIGHT ILLUMINATED. T/S PACK TEMP CONTROLLER IAW FIM 21-51-00 FIG 103. SYS RESET. SYS CHECKS OK IAW FIM.SDR HALA2009070100271Indication Sys · malfunctionedETOPS SIGNIFICANT SYS - BTB L ENG OIL PRESSURE WENT TO ZERO DURING PWR FAILURE AT IDLE. PRESSURE RECOVERED WHEN POWER WAS RESTORED TEMPORARLY. PERFORMED FIM 79-33-00 FIG 105, NO DEFECTS NOTED AND FIM 79-33-00 FIG 104 NO DEFECTS NOTED. ACCOMPLISH ENGINE RUNSDR HALA2009062000257Warning Light · false activationETOPS SIGNIFICANT SYSTEM, L PACK TEMP EICAS ILLUM IN FLIGHT. ACCOMP LEFT PACK TEMPERATURE CONTROLLER BITE, NO FAULTS NOTED PER FIM 21-51-00 OK FOR SERVICE EICAS MSG EXTINGUISHED LEFT PACK, OPS CK GOOD.SDR HALA2009061100235Transceiver · inoperativeETOPS SIGNIFICANT SYSTEM, VHF ACARS NO COMM MSG DISPLAYED. REPLACED CTR VHF TRANSCEIVER ACARS, OPS CK OK PER MM 23-22-00.SDR HALA2009061000231Start Valve · failedETOPS SIGNIFICANT SYSTEM - RIGHT ENG START VALVE LIGHT CAME ON STAYED ON, NO ENG ROTATION. RT STARTER VALVE EICAS MESSAGE. NO N2 DUCT PRESSURE. REMOVED AND REPLACED NR 2 ENGINE STARTER AND START VALVE PER AMM 80-11-01. OPS AND LEAK CHECK OK. OK FOR SERVICSDR HALA2009060900233Pump · failedETOPS SIGNIFICANT SYSTEM, FRM 2911XD00 C HYD ADP DEMAND PUMP DOES NOT PROVIDE FULL PRESS IN AUTO MODE. PRESS NORMAL W/SW IN ON POSITION. EICAS MSG "C HYD DEM PUMP' ILLUM W/CENTER SYSTEM DEMAND. PERFORMED FIM 29-11-00 REPLACED MODULATING VALVE FOR THE AIR DRSDR HALA2009060800228Warning Light · false activationETOPS SIGNIFICANT SYSTEM, R FMC FAIL ON L ENG START. PERF FIM 34-61-00 FIG 108A. PERF ENGINE START AT GATE. OPS NORMAL.SDR HALA2009060200218Wire · brokenETOPS SIGNIFICANT SYSTEM - EICAS MSG L ENG PRV DISPLAYED DURING ENGINE START. RIGHT ENG BLEED LGT ILLUM MSG DISPLAYED DURING BOTH ENG STARTS AND OPS NORMAL AFTER ENGINES STABILIZED. T/S PER FIM 36-10-00 FIG 124 BIT AND VERIFY ON AIR SUPPLY MODULE FAULT RIGHTSDR HALA2009053100210Warning Message · illuminatedETOPS SIGNIFICANT SYSTEM - INTERMITTENT, STATUS MSG "FUEL QTY INOP " DUE TO FUEL QTY C INOP. PERFORMED FIM 28-41-00 FIG 104 FUEL QTY BITE, NO FAULTS FOUND.SDR HALA2009053000211Blade · nickedETOPS SIGNIFICANT SYSTEM - FOUND NR 1 ENG BLADE NR 34 HAS SMALL NICK ON LEADING EDGE 2 INCHES FROM TIP (AREA A). INSP AND BLENDED BLADE PER AMM 72-31-02. EDDY CURRENT CK OK.SDR HALA2009052600199Transceiver · failedNR 2 DME INOP. REPLACED DME T/R UNIT, OPS CHECK OKAY PER MM 34-55-00.SDR HALA2009052500198Filter · cloggedDURING CABIN WALK THROUGH, NOTED ALL 5 CABIN ZONE TEMP SENSE FILTERS HEAVILY BLOCKED WITH DIRT. REMOVED CLEANED AND REINSTALLED FILTERS PER MM 21-61-09.SDR HALA2009052400197Engine · unknownAPU BLEED AIR PRESSURE FOR ENGINE START WAS AT MINIMUM 20 PSI TOOK 2.5 MINUTES TO START ENGINE NR 2. DRY MOTORED BOTH ENG MAINTAINED 34 PSI LEFT 35 PSI RIGHT WITH 26 PERCENT N2 LIMIT 20-35 PSI IAW AMM 36-00-00 RAN NR 2 ENG ON GROUND. MAINTAINED 34 PSI ON STASDR HALA2009052400196Indication Sys · malfunctionedFUEL QTY BITE DISPLAYED ON EICAS. PERFORMED FIM 28-41-00 FIG 104 FUEL QUANTITY BITE, NO MESSAGES ITEM CLEARED. OK FOR SERVICE.SDR HALA2009052400191Shutoff Valve · leakingAPU SHUTOFF VALVE LEAKING FUEL, LT REAR SPAR. REMOVED FUEL ACCESS DOOR 531BB. REMOVED AND REPLACED LEAKING APU SHUTOFF VALVE (VALVE BODY ). REINSTALLED FUEL ACCESS DOOR 531BB. OPS CK GOOD. NO LEAKS NOTED IAW MM 28-25-02 AND MM 28-11-02. CONFIRMATION PERFSDR HALA2009052000183Packing · leakingON WALKAROUND, FOUND HYD LEAK COMING FROM TAIL OF ACFT. FOUND PACKING ON RUDDER ON RATIO SERVO VALVE TORN. REMOVED AND REPLACE O-RING ON RUDDER RATIO SERVO VALVE SECURITY AND LEAK CHK OK.SDR HALA2009051600175Shutoff Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, ATO, DUE TO HPSOV LIGHT AND EICAS MSG, ABORTED AT 40 KNTS NR 1 ENG. REPLACED HPSOV PER AMM 36-11-07. LEAK CK GOOD. PERFORMED ENG PWR RUN PER AMM 71-00-00 AND AR 767-36-001. TEST GOOD. NO LIGHTS, NO MSGS.SDR HALA2009051400177Radome · delaminatedDURING ETOPS INSPECTION WALKAROUND FOUND EVIDENCE OF BIRDSTRIKE ON NOSE RADOME AT APPROX 8:00 PO APPROX 12 INCHES FROM CENTER AS VIEWED FROM FRONT OF ACFT. INSPECTED PER BIRD STRIKE INSP IN AMM 05-51-18 FOUND EVIDENCE OF DELAMINATION ON INSIDE OF RADOME FORWASDR HALA2009051400176Generator · failedETOPS SIGNIFICANT SYSTEM, APU GENERATOR FAILED AT GATE. REPLACED APU IN ACCORDANCE WITH HAL M266-767. GROUND OPS AND LEAK CHECK OKAY.SDR HALA2009051300179Oil Filter · dirtyETOPS SIGNIFICANT SYSTEM - BTB - RIGHT AFTER ENGINE START RECEIVED AMBER EICAS MESSAGE "L OIL FILTER". THIS WENT AWAY AFTER 15 SECONDS TO BE REPLACED BY A WHITE EICAS MESSAGE "L OIL FILTER. T/S PER FIM 79-35-00 MAG CHIP DET CK'D CLEAN. REMOVED AND REPLACED SDR HALA2009051300174Pump · leakingETOPS SIGNIFICANT SYSTEM, DURING WALK AROUND FOUND NR 1 ENGINE DRIVEN HYD PUMP LEAKING. REPLACED EDP PER AMM 29-11-05. PERFORMED OPERATIONAL AND LEAK CHECK. CHECKS OK. OK FOR SERVICE.SDR HALA2009043000169Warning Light · false activationETOPS SIGNIFICANT SYSTEM, NO LAND 3 DISPLAYED 3 HOURS AFTER TAKEOFF WOULD NOT RESET WHEN SELECTED ILS FREQ F/O SIDE SHOWED NO G/S OR LOC (BOTH AMBER ALERTS) ON ADI. TS MMR PER AMM 34-31-00, PERFORMED OPERATIONAL CHECK OPS NORMAL NO FIM WITH MMR PERFORMED MCDPSDR HALA2009042700165Isolation Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, BLEED VALVE ISOLATION VALVE LIGHT ILLUMINATED AFTER LANDING. REMOVED AND REPLACED LEFT ISO VLV AS PER AMM 36-11-04 PG 401.
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