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 HALA2012020500051Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN STA 434 AND 456. REPAIRED IAW SRM 53-00-03, REV 88.SDR ANZY20120201Plate · crackedPRIOR TO RAISING INBD SLATS, A CAVITY CHECK FOR FOD AND CLEARANCE OF AREAS WAS CARRIED OUT. DURING THIS CHECK IT WAS FOUND THAT THE RT KRUGER FLAP SEAL ACTUATOR MOUNTING SIDE PLATE STRUCTURE HAD SNAPPED IN HALF. S/O RAISED TO REPLACE SIDE PLATE STRUCTURE ANDSDR HALA2012011900045Engine · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT ENGINE STARTED NORMALLY TILL 50 PERCENT, THEN REMAINED AT 50 PERCENT FOR 50 SECOUNDS BEFORE SLOWLY ACCELERATING - TOTAL TIME FROM FUEL ON TILL ENGINE STABLE TOOK 110 SECONDS, PEAK TEMP EGT WAS 397. TROUBLESHOT IAW FIM 73-21-00/SDR HALA2012011800042Spinner · leakingETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK FOUND OIL LEAK FROM NOSE SPINNER AREA ON NR 2 ENGINE. INLET CONE LEAKAGE WITHIN LIMITS IAW FIM 71-08-00-1, FIG 113.SDR HALA2012011700041Generator · malfunctionedETOPS SIGNIFICANT SYS - GENERATOR FIELD MANUAL RESET (RT) FIELD OFF LIGHT ON. BITE CHECKED BPCU AND NO FAULTS NOTED. RAN NR 2 ENGINE RESET NR 2 GENERATOR. OPS CHECKED OK IAW 24-20-00, OK FOR SERVICE.SDR HALA2012011600035Display · malfunctionedETOPS SIGNIFICANT SYS - F/O RADAR SCREEN FLICKERS IN WX MODE. REPLACED F/O EMSI DISPLAY. OPS CHECKED OK IAW MM 34-22-00. PERFORMED MCDP TEST 30 TEST PASSED.SDR HALA2012011500036Transceiver · failedETOPS SIGNIFICANT SYS - AMBER RADAR ALITMETER WARNING BOX ILLUMINATED ON FO ADI " NO LAND 3" APPEARS IN AUTOLAND STATUS. REPLACED RT RADIO ALTIMETER TRANSCEIVER, NOW OPS NORMAL IAW MM 34-33-01. OK FOR SERVICE.SDR HALA2012011400025Warning Light · false activationETOPS SIGNIFICANT SYS - THROUGHOUT FLIGHT EICAS MESSAGE FOR WEATHER RADAR FAILURE, DISPLAYED INTERMITTENTLY. NO EICAS MESSAGE ON ARRIVAL, PERFORM BITE PROCEDURE IAW MM34-43-00-101, BITE TESTED OK. ACFT OK FOR SERVICE.SDR HALA2012011300026Warning Light · illuminatedETOPS SIGNIFICANT SYS - RA FLAG DISPLAYED STEADY ON THE CAPT'S ADI. REPLACED NR 1 RA THRUST REVERSER IAW MM34-33-00 GROUND CK OK. PERFORMED MCDP TEST 30, NO FAULTS NOTED, TEST PASSED. ACFT LMP STATUS REMAINS LAND 3.SDR HALA2012011300024Warning Light · illuminatedETOPS SIGNIFICANT SYS - ON POST FLIGHT FOUND ENGINE NR 2 GENERATOR FIELD OFF LIGHT ILLUMINATED. ACCOMPLISHED BPCU BITE CHECK IAW AMM 24-22-00-745-071. RERACKED GCU. RESET RT GENERATOR FIELD LIGHT. RT ENGINE GROUND RUN-UP OK. SYS VOLTAGE AND FREQUENCY NORMASDR HALA2012011100038Beam · chafedCHAFING ON THE INBD SIDE OF THE RT 9-10 BEAM OF THE INBD T/E FLAP. BLENDED IAW SRM 52-53-02-1A-2, REV 88 AND FLAP ADJUSTMENT.SDR HALA2012011100018Gcu · failedETOPS SIGNIFICANT SYS - FOUND RT GENERATOR FIELD LIGHT ILLUMINATED ON P61. SERVICED IDG RESET FIELD LIGHT IAW AMM 24-22-00. PERFORMED IDLE ENGINE RUN. FAULT DID NOT RETURN. DUE TO HISTORY, REPLACED RT GCU IAW AMM 24-22-02. TESTED OK IAW AMM. OK FOR SERVICE.SDR HALA2012010500007Altimeter · malfunctionedETOPS SIGNIFICANT SYS - STANDBY ALTIMETER HANGS AT 0 THEN JUMPS IN 500' INCREMENTS. VERIFIED VIBRATOR INTERMITTENT. REPLACED STBY ALTIMETER IAW AMM 34-13-06. NO LEAKAGE NOTED.SDR HALA2012010500004Altimeter · malfunctionedETOPS SIGNIFICANT SYS - F/O ALTIMETER DIFFERS FROM CAPTAINS BY 120-150 FT DURING CRUISE. IAW DISPATCH- ACFT FLT PLAN HAS FLT LEVELS FROM 35,000 FT TO 37,000 FT AT CRUISE. REF FIM CHART CHAP 34 FAULT CODE DIAGRAM ALTIMETER TOLERANCES FIG 6 SHEET 1, ALTIMETER SDR HALA2012010400008Display · failedETOPS SIGNIFICANT SYS - F/O EHSI BLANK. SWAPPED DISPLAY FROM MFD POSISTION, OPS NORMAL IAW AMM 34-22-04.SDR HALA2012010100002Warning Light · illuminatedETOPS SIGNIFICANT SYS - EICAS MESSAGE TRACK FAIL ILLUMINATED AFTER TAKEOFF. PERFORMED TROUBLESHOOTING, PLACED IECAS COMPUTER SELECTED SWITCH TO ALTERNATE POSITION, OPENED AND RESET CIRCUIT BREAKER TO EICAS COMPUTER. ALL CHECKED GOOD.SDR HALA2011123100623Probe · malfunctionedETOPS SIGNIFICANT SYS. F/O PILOT EICAS MESSAGE AND OVERHEAD PANEL ANNUNCIATOR LIGHT ON. R & R F/O PITOT TUBE AND RELAY K310 CURRENT SENSING RELAY, IAW AMM 34-11-01. R & R PROBE AND WDM 30-31-21 RELAY. OPS TEST GOOD IAW AMM 30-31-00.SDR HALA2011122700612Battery Pack · dischargedFOUND RT AFT EMERGENCY LIGHTS INOPERATIVE. R & R RT AFT EMERGENCY LIGHTING BATTERY POWER SUPPLY. OPS CHECKED GOOD IAW AMM 33-51-09.SDR HALA2011122600618Warning Light · false activationETOPS SIGNIFICANT SYS - AFTER ENGINE SHUTDOWN, NOTE GENERATOR FIELD TRIP ON RT ENG. ACCOMPLISHED FIM 24-20-00. NO FAULTS NOTED. RESET RT GEN FIELD SWITCH. GROUND RUN CHECK OK IAW AMM 24-11-00. OK FOR SERVICE.SDR HALA2011122500611Warning Light · false activationETOPS SIGNIFICANT SYS - AUX PANEL HAS GENERATOR FIELD OFF INDICATOR ON AFTER LANDING. PERFORMED BPCU BITE ON NR 2 BPCE IAW FIM 24-20-00, FIG 101. INSPECTED WIRING, NO DEFECTS NOTED. RESET FIELD OFF LIGHT, OPS NORMAL ON ENG RUN UP.SDR HALA2011122200606Sensor · out of positionON TAXI OUT LT FWD ENTRY DOOR, EICAS AND ENTRY DOORS WARNING LIGHT ILLUMINATED. UPON BEING TUGGED IN LIGHT WENT OUT BY ITSELF. FOUND LT FWD ENTRY DOOR OPEN SENSOR BINDING. REPOSITIONED SENSOR. SECURITY CHECK AND OPS CHECK OK. OK FOR SERVICE.SDR HALA2011122200605Connector · dirtyETOPS SIGNIFICANT SYS - ON 5 MILE FINAL, RT GEN DRIVE EICAS MESSAGE CAME ON. SECURED RT ENG ON LANDING. FOUND MESSAGE "RT IDG TEMP SENS". PFMD FIM 24-20-00. CLEANED CONNECTOR AND ENG RUN. OPS CHECKED OK. ACFT OK FOR SVC.SDR HALA2011121100579Radar · malfunctionedETOPS SIGNIFICANT SYS - WX RADAR AUTO GAIN SETTING SHOWS INDICATION EQUIVALENT TO MAX GAIN EXCESSIVE CLUTTER, EVEN IF POINTED UP. RAN TEST OF WX RADAR IAW AMM 34-43-00-715-001 AND 34-43-00-725-319. NO FAULTS NOTED. SYS OPS NORMAL.SDR HALA2011120800573Switch · inoperativeETOPS SIGNIFICANT SYS - LEFT AFT BOOST PUMP SWITCH INOPERATIVE. R & R LEFT AFT BOOST PUMP SWITCH, SECURITY CHECKED AND OPS CHECKED OK.SDR HALA2011120200596Support Channel · corrodedINTERNAL SUPPORT CHANNEL CORRODED, BS 1425 AT DRAIN MAST FOR WASTE WATER. FITTED NEW SKIN STIFFENER IAW SRM 53-00-03.SDR HALA2011120200581Floor Support · crackedFLOOR SUPPORT CRACKED 1 INCH, BETWEEN BS 742 AND 764 AT RBL 40. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, D634T210, REV 87.SDR HALA2011120100584Floorbeam · corrodedAFT CARGO HOLD, FLOOR STRUCTURE, UPPER HORIZONTAL FLANGE A FRAME STA 1197+66, HAS CORROSION OUTSIDE SRM LIMITS AND NUMEROUS CORRODED ANCHOR NUTS. INNER CHORD PN 146T1060-2, REPLACED IAW SRM 51-40-02, REV 87, CORRODED ANCHOR NUTS REPLACED IAW SRM 51-40-02, REVSDR HALA2011113000583Floorbeam · corrodedNET CARGO FLOOR STRUCTURE, UPPER HORIZONTAL FLANGE AT BS 1175, HAS CORROSION AS MARKED. REPLACED IAW SRM 51-40-02, REV 87.SDR ANZY20111120102Stringer · corrodedON C CHECK, CORROSION OF STRINGER AT S34R HAD CAUSED MULTIPLE HOLES IN EXTRUSION TO THE POINT THAT NO STRUTURAL MATERIAL WAS LEFT. REPAIR UNDER WAY AT THIS TIME.SDR HALA2011112900597Mechanism · corrodedNLG FWD DOOR OPERATING MECHANISM FOUND CORRODED BS 180.5. REPLACED NLG FWD DOOR OPERATING MECHANISM ON LT SIDE IAW AMM 32-22-04, REV 77.SDR HALA2011112900580Stringer Clip · crackedCRACK IN STRINGER CLIP AT STA. 1678, S3R, 1". REPLACED STRINGER CLIP IAW SRM 51-40-02.SDR HALA2011112800602Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 605. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.SDR HALA2011112800600Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 594. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.SDR HALA2011112800601Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 594. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.SDR HALA2011128000600Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 575. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.SDR HALA2011112800599Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5, AT STA. 565. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.SDR HALA2011112800598Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT BS 544. REPLACED SEAT TRACK IAW 53-00-52-REV 87.SDR HALA2011112800592Wedge · debondedNR 8 SLAT OTBD END HAS A T/E WEDGE AREA OF DISBOND. REPAIRED IAW SRM 57-43-02-2R-1, REV 87 AND 51-70-10, REV 87.SDR HALA2011112800591Skin · damagedLIGHTING STRIKE NEAR RIVET HEAD AT BS 395, 1 INCH BELOW S33L. DAMAGE REMOVED IAW SRM 53-00-01-2R-8 REV 88. FASTENER REPLACED IAW SRM 51-40-02, REV 88.SDR HALA2011112800582Tee Fitting · corrodedCORROSION ON TEE FITTING BETWEEN STA 808 & 933, BETWEEN RBL 10 & LBL 10. REPLACED TEE FITTING IAW SRM 51-40-02.SDR HALA2011115000519Power Supply · inoperativeFIRST CLASS RT SIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED M730 POWER PACK. CHECKED GOOD IAW AMM 33-51-05.SDR HALA2011113000512Engine · malfunctionedETOPS SIGNIFICANT SYS - LEFT ENGINE HESITATED AT 50 PERCENT N2 DURING ENGINE START AFTER START VALVE CLOSED AND STARTER CUTOUT WITH SELECTOR BACK IN AUTO. OTHER PARAMETERS NORMAL. GROUND RAN LT ENGINE, FOUND WITHIN LIMITS OF AMM 71-00-00. OK FOR SERVICE.SDR HALA2011112000513Fire Warning · no testWHEEL WELL FIRE TEST AUDIO INOPERATIVE. RESET MASTER CAUTION SWITCH GROUND CHECKED OK.SDR HALA2011111000510Switch · failedETOPS SIGNIFICANT SYS - LT PACK SHUTDOWN IN AUTO AND STBY AT GATE. R & R LT PACK COMPRESSOR OUTLET OVERHEAT SWITCH IAW AMM 21-51-19. LT PACK OPERATES NORMAL ON GROUND.SDR HALA2011111000509Warning Light · false activationETOPS SIGNIFICANT SYS - LT DUCT LEAK LIGHT ILLUMINATED, EXTINGUISHED AFTER ENGINE BLEED SUPPLY AND ISOLATION VALVES CLOSED. ACCOMPLISHED FIM 26-18-00 WING DUCT LEAK DETECTION BITE, NO FAULTS NOTED. SYS CHECKED GOOD, OPS NORMAL. ACCOMPLISHED FIM 36-10-00,M NOSDR HALA2011110900507Transponder · false indicationETOPS SIGNIFICANT SYSTEM - NR 1 & NR 2 TRANSPONDER DATA BUSS DISPLAYED ON TRAFFIC DISPLAY TCAS FLAG ON CAPT/FO'S VSI. RECYCLED TCAS CIRCUIT BREAKER TCAS SYS TESTED OK, IAW MM34-45-00, NO NR 1 & NR 2 TRANSPONDER DATA BUSS DISPLAYED ON TRAFFIC DISPLAY.SDR HALA2011110200501Indication Sys · unknownETOPS SIGNIFICANT SYS - TOTAL FUEL DIFFERS FROM CAPT & F/O FMC CALCULATED FUEL QTY "FUEL DIS AGREE-PORG 2" ALERT MSG DISPLAYED ON CDU AND FUEL FLOW WAS NORMAL. TOTAL FUEL EXCEED CALCULATED FUEL BY MORE THAN 3000 LBS IAW FIM PGBLK 28-41/101, FIG 107, BLK 1 FUELSDR HALA2011110100500Unknown · unknownETOPS SIGNIFICANT SYS - HF DATALINK INOPERATIVE BOTH RADIOS, VOICE OK. PERFORMED A BITE TEST ON BOTH HF TRANSCEIVERS, NO FAULTS NOTED. PERFORMED A SYS TEST IAW 23-11-00-735-042, ALL CHECKED ARE GOOD.SDR HALA2011102800523Angle · crackedNR 1 ENGINE PYLON AFT FAIRING LOWER ATTACHMENT CLOSE OUT ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-40-02 REV.87SDR HALA2011102500491Fmc · malfunctionedETOPS SIGNIFICANT SYS - FMC- ENROUTE WAY POINT TIME (ETA'S) ESTIMATES WERE IN ERROR UP TO 20 MIN ONLY HAPPENED ONCE AT (1) WAY POINT THE LAST ONE (COAST IN WAY POINT FIX) AT END OF FLT. C/W FIM 34-61-00, FIG 108A AND FIG 111. NR 10000. REPLACED LT FLIGHT MAN
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