Boeing 767-3BG
Service difficulty reports · 342
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 = '7673BG' 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 = '7673BG' 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 NACA2024050200001Warning Message · false activationL ENG HPSOV. PERFORMED AIR SUPPLY BITE TEST, STATUS MESSAGE CLEARED, NO FAULTS NOTED.SDR NACA2024050100001Controller · no testPERFORM RH AND LH PNEUMATIC HEALTH CHECK. PERFORMED RH AND LH PNEUMATIC HEALTH CHECK IAW AMM 36-00-22. REPLACED HPC PN# 773289-15 SN# 200008067 4659FH 1488 FC. REPLACED PRVC PN# 792755-16 SN# 910169 FH AND FC UNKNOWN. REPLACED PRV PN# 820170-10 SN# A95030012 4SDR NACA2024043000005Pseu · failedKMIA CONFIG WARNING ON V1 FOLLOWED BY LE SLAT ASYM, PERFORMED QRH, RETURNED TO MIA. ACCOMPLISHED FIM 27-801 FT 809 FSEU BITE SHOWS NO CURRENT FAULTS. FT 803 FOUND RIGHT CARD INTERNAL FAULT, REMOVED AND REPLACED PSEU IAW B767 AMM 32-09-04. PART INFO UNKNOWN TO SDR NACA2024043000004Apu · no discrepancyAPU WENT TO AUTO-SHUTDOWN, 2 ATTEMPTS TO START FAILED. ACCOMPLISHED APU CONTROL UNIT BITE TEST, NO FAULT FOUND IAW AMM 49-61-05.SDR NACA2024043000003Valve · failedSTATUS ON FINAL RH ENG A/O VALVE. REPLACED AIR/OIL VALVE IAW AMM 79-21-09 IDLE LEAK TEST GOOD.SDR NACA2024043000002Valve · failedSTATUS ON FINAL RT ENG EEC C1. REPLACED AIR/OIL VALVE IAW AMM 79-21-09.SDR NACA2024042000004Warning Message · illuminatedRH ENG EEC C1 STATUS MESSAGE. PERFORMED BITE CHECK, OPS CHECK OK IAW FIM 73-21 FT 828.SDR NACA2024042000003Warning Message · illuminatedRH ENG A/O VALVE STATUS MESSAGE. PERFORME BITE TEST, OPS CHECK GOOD NO MSG IAW FIM 71-01 FT 803.SDR NACA2024042000002Valve · failedRH ENGINE A/O VALVE STATUS MESSAGE. REPLACED AIR/OIL VALVE IAW AMM 79-21-09 OPS CHECK AND LEAK CHECK GOOD.SDR NACA2024042000001Heat Exchanger · failedRH ENG EEC C1 STATUS MESSAGE. REPLACED AIR/OIL HEAT EXCHANIGER IAW AMM 79-21-09 OPS CHECK GOOD.SDR NACA2024041700001Blade · nickedPILOT REPORTED ON POST FLIGHT CHECK THAT OBSERVED POSSIBLE NICKS ON #1 ENGINE BLADES 2 11 12 15 18. PERFORMED VISUAL INSPECTION, ALL NICKS ARE IN PERMITTED LIMITS WITHOUT REPAIRS PER AMM 72-31-02SDR NACA2024041500002Control Panel · faultedRIGHT HF RADIO BLANK/NO POWER. RESET HF COMM CONTROL PANEL PER AMM 23-11-00. OPS CHECK GOOD.SDR NACA2024041500001Control Panel · failedRIGHT HF RADIO BLANK/NO POWER. REMOVED AND REPLACED HF COMM CONTROL PANEL PER AMM 23-11-02.SDR NACA2024041200001Skin · crackedPOSSIBLE SKIN CRACK FOUND AT STATION 1210 STRINGER 37R. CUTOUT DAMAGE, INSTALLED REPAIR DOUBLER IAW NAC EO 767-53-004SDR NACA2024041100002Hf Comm · faultedRIGHT HF RADIO FAIL IN ITS DISPLAY WINDOW. RESET RH HF CONTROL PANEL PER AMM 23-11-00 OPS CHECK GOOD.SDR NACA2024041100001Transmitter · failedLEFT ENGINE FUEL FLOW INDICATION ZERO AFTER ENGINE START. REMOVED AND REPLACED LEFT ENGINE FUEL FLOW TRANSMITTER, REF 73-31-01 OPS TEST GOOD.SDR NACA2024040900001Door · warning messageAPU DOOR EICAS MESSAGE. APU DOOR REMAINS OPEN. REMOVED AND REPLACED C868, PERFORMED APU OPS CHECK IAW 49-11-00 OPS CHECK GOOD.SDR NACA2024040400002Sensor · inoperativeLH SEC HEAT EXCHANGER INDICATION INOP. REMOVED AND REPLACED LH TEMP SENSOR IAW B767 AMM 21-52-05SDR NACA2024040400001Acm · failedLH PACK INOP. REMOVED AND REPLACED LH ACM IAW 767 AMM 21-51-03, PART UNKNOWN TO TRAX.SDR NACA2024040300001Radio · failedLEFT HF RADIO FAILED. LH HF TRANSCEIVER SHOWS BITE SHOWING CONTROL INPUT FAIL. RESET LH HF CONTROL PANEL PER AMM 23-11-02, LH HF RADIO OPS CHECK GOOD.SDR NACA2024032600001Warning Message · illuminatedCABIN ALT AUTO 2 EICAS MESSAGE. DEFER PER MEL 21-31-01A ON 3/26/2024 1340ZSDR NACA2024032200002Igniter · wornDURING ENGINE 1 IGNITOR PLUGS INSPECTION FOUND IGNITOR PLUG WORN OUT. REMOVED AND REPLACED IGNITOR PLUG 1 ON ENGINE 1 PER AMM 74-21-02 OPS CHECK GOOD PER AMM 74-00-00SDR NACA2024032100001Control Panel · failedRH HF COMM CONTROL PANEL CASE DIGIT TURNING KNOB INOP. REMOVED AND REPLACED RH HF COMM CONTROL PANEL PER AMM 23-11-02 OPS CHECK GOOD. UNIT IS UNKNOWN TO TRAXSDR NACA2024030300001Warning Horn · activatedWHILE TAXIING OPERATION, AURAL WARNING FROM EQUIPMENT COOLING START HORNING AND DIDNT STOP UNTIL WE RETURNED TO GATE. OVERHEAD OVERHEAT LIGHTING ILLUMINATED. CLEARED AIR INLET FRILL AND AIR CLEANER. REMOVED AND REPLACED FWD RACK SUPPLY AND EXHAUST FANS. ACCOMPSDR NACA2024030100001Pump · failedRIGHT AFT PUMP CAUTION LIGHT CAME ON AT ONE HOUR INTO FLIGHT. RAN QRH. REMOVED AND REPLACED RIGHT AFT FUEL PUMP ASSY PER AMM 28-22-03. OPS CHECK PUMP GOOD. BUT LOW PRESSURE LIGHT REMAINS DIM WHILE RUNNING. RH AFT LOW PRESSURE LIGHT DEFERRED PER MEL 28-42-01-01SDR NACA2024022800001Display · inoperativeRH HF SELECT PANEL DISPLAY INOP. DEFERRED PER MEL 23-11-01-02B CAT C@ 0154Z 2-28-2024. REMOVED AND REPLACED HF FREQ SELECT PANEL PER AMM 23-11-02 OPS CHECK GOOD.SDR NACA2024022610001Pump · failedLH FWD FUEL BOOST PUMP LOW PRESSURE LIGHT IS ON. ACCOMPLISHED FIM 28-22 FAULT TREE 819, AND 28-22 TREE 831. FOUND LH FWD GFI OUT. REMOVED AND REPLACED LH FWD BOOST PUMP IAW AMM 28-22-03 OPS TEST NORMAL.SDR NACA2024021900001Latch Handle · out of adjustFO WINDOW OPENED DURING TO ROLL. ADJUSTED TENSION ON WINDOW LATCHING HANDLE, AND WINDOW'S INBOARD/OUTBOARD ALIGNMENT PER AMM 56-11-02. CHECKS GOOD FOR SECURITY, NO DEFECTS FOUND, ADJUSTMENTS MADE TO THE UPPER SERVICEABLE LIMITSSDR NACA2024021500001Blade · cracked#1 ENG #28TH BLADE HAS A 3.968 MM CRACK ON THE LEADING EDGE AREA F SURFACE, 8" FROM THE PLATFORM BASE. PERFORMED 1ST STAGE FAN BLADE REPAIR ON #1 ENG #28 BLADE PER AMM 72-31-02, PERFORMED FLUORESCENT PENETRANT INSPECTION, OK FOR SERVICE FINAL DEPTH 4.783 MMSDR NACA2024021400002Controller · malfunctionedCABIN DIFFERENTIAL POINTER IS IN THE RED ZONE ABOVE 35000. ACCOMPLISHED BOTH CABIN PRESSURE CONTROLLER BITE TEST IAW FIM 21-31-803 FOUND NORMAL AT THIS TIME .SDR NACA2024021300002Engine · vibrationNOTICED HIGH VIBRATION FROM LEFT ENGINE AT TAKEOFF. IN CRUISE, LEFT ENGINE SHOWS VIBRATION N1 VARIABLE BETWEEN 3.7 & 4.1 @ FL350. ACCOMPLISHED FAN LUBE PER B767 AMM 72-31-02, MID SPAN SHROUD LUBE WAS PERFORMED PER WO 1223028 TC 767-72-433-01-01SDR NACA2024021000002Light · inoperativeRH ENG GEN DRIVE LIGHTS INOP. DEFERRED PER MEL 24-11-01-01A CAT B @1015Z 2/1/2024SDR NACA2024021000001Hf Comm · malfunctionedATC REPORTED THEY COULD NOT UNDERSTAND US ON HF #1, VERY GARBLED. SWITCH TO SAME FREQ ON #2 AND TRANSMISSION WAS GOOD. PERFORMED OPS CHECK ON HF1 AND HF2 PER AMM 23-11-00 BOTH HF 1 AND 2 SYS TRANSMIT AND RECEIVE GOOD.SDR NACA2024020900002Isolation Valve · failedISOLATION VALVE EICAS MESSAGE. NO DUCT PRESSURE. REPLACED CENTER ISOLATION VALVE IAW AMM 36-11-04 OPS CHECK GOOD. PART UNKNOWN TO TRAX.SDR NACA2024020900001Isolation Valve · faultedLEFT ISOLATION VALVE EICAS MESSAGE. NO DUCT PRESSURE INDICATED AND ASSOCIATED L ISLN LIGHT. SWAPPED LEFT AND CENTER ISOLATION VALVES PER AMM 36-11-04 INSTALLATION TEST PASSED.SDR NACA2024020600001Pump · warning messageL FWD FUEL PUMP EICAS MSG. DEFERRED LEFT FWD MAIN FUEL BOOST PUMP PER MEL 28-22-01 CAT C 2/8/24 1745ZSDR NACA2024020500002Warning Light · inoperativePILOT REPORTED R1 WINDOW HEAT LIGHT INOP DURING FLIGHT. FLIGHT DECK WINDOW HEAT SYSTEM #2 SIDE DEFERRED IAW MEL 30-41-01.SDR NACA2024012800002Hf Comm · malfunctionedR HF UNREADABLE. ACCOMPLISHED FIM 23-11 TASK 804. NFF. ACCOMPLISHED COMMUNICATION TEST IAW AMM 23-11-00 TEST GOOD.SDR NACA2024012800001Hf Comm · faultedLEFT HF DOES NOT TRANSMIT OR TUNE. RERACKED LH HF TX IAW AMM 23-11-03 OPS TEST AND COMMUNICATION TEST GOOD.SDR NACA2024012600002Hf Comm · weakRIGHT HF VERY WEAK, COULD NOT CONTACT SFO WHEN IN ETOPS. RIGHT HF OPS CHECK GOOD PER FIM 23-11 FAULT TREE 804 AND AMM 23-11-00 OPS CHECK NORMAL.SDR NACA2024012600001Hf Comm · inoperativeLEFT HF WONT TRANSMIT. LEFT HF SYSTEMS DEFERRED IAW MEL 23-11-01-028 @ 1707Z 01-26-2024 CAT CSDR NACA2024012930001Anti-Ice Valve · failedLEFT ENGINE ANTI-ICE. REMOVED AND REPLACED ENGINE THERMAL ANTI-ICE VALVE IAW AMM 30-21-03 OPS CHECK OK. UNIT IS UNKNOWN TO TRAX.SDR NACA2024012620001Control Unit · failedWINDOW HEAT RT SWITCH INOP LIGHT CAME ON DURING FLIGHT. REMOVED AND REPLACED RT WHCU IAW B767 AMM 30-41-01 TESTS OK. PART UNKNOWN TO TRAX.SDR NACA2024012510003Indicator · trippedON SERVICE CHECK INSPECTION FOUND APU LUBE OIL DIFFERENTIAL PRESSURE INDICATOR POPPED OUT. REMOVED AND REPLACED LUBE FILTER ELEMENT AS PER REF B767 AMM 49-27-03. PERFORMED OPS CHECK FOUND NORMAL.SDR NACA2024012100002Spinner · crackedRIGHT ENGINE SPINNER FOUND WITH CRACKS AROUND MOUNTING BOLT HOLES. REMOVED AND REPLACED RIGHT ENG CONE SEGMENT INLET IAW AMM 72-31-04SDR NACA2024012100001Blade · nicked#2 ENGINE BLADES # 4, 9, 17, 23, 25, 27, 30 31, FOUND WITH NICKS IN VARIOUS LOCATIONS. ALL NICKS BLENDED IAW AMM 72-31-02 AND FOUND WITHIN LIMITS. PERFORMED NDT HFEC AND FPI INSPECTION PER AMM 72-31-02 AND 70-11-06 NO DEFECTS NOTED.SDR NACA2024012390001Warning Message · illuminatedEICAS MESSAGE CABIN ALT AUTO 2 UPON CONNECTING GROUND POWER. DEFERRED PER MEL 21-31-01A CAT CSDR NACA2024012217002Warning Light · illuminatedR AFT FUEL PRESSURE LIGHT ILLUMINATED. DEFERRED PER MEL 28-42-01-01 CAT C AT 1/17/24 AT 1033Z.SDR NACA2024011500003Outflow Valve · failedCABIN ALT AUTO 2 IN STATUS MSG. REMOVED AND REPLACED OUTFLOW VALVE AS PER B767 AMM 21-31-03. PART INFO UNKNOWN TO TRAX.SDR NACA2024011700002Fairing · damagedIMPACT DAMAGE FOUND AT LH AFT WING/BODY FAIRING 195PL, STA 1222-1230, WL-160. COMPLETED TEMP REPAIR PER NAC EO 767-53-0040. DVI OF TAPE ONCE PER FLIGHT DAY, REPLACE IF DETERIORATED. ONCE PER WEEK TAP TEST, ANY GROWTH IN DAMAGE MUST NOTIFY NAC ENGINEERING.
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