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 HALA2012050600130Light · inoperativeON OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHT STRIP L1 & R1 DOOR INOPERATIVE. REPLACED FLOOR LIGHT STRIP AT CROSS ISLE BETWEEN L1 & R1 DOOR IAW AMM 33-51-10. OPS CHECKED OK.SDR HALA2012050300129Control Module · malfunctioned"RUDDER RATIO" EICAS MESSAGE & OVERHEAD ANNUNCIATOR PANEL. R & R LT RRCM IAW AMM 27-09-00. OPS CKS OK. NO EICAS MESSAGE NOTED. OK FOR SERVICE.SDR HALA2012042800128Pressure Switch · failedDURING CLIMB FAULT LIGHT ILLUMINATED FOLLOWED BY APU SHUTDOWN. ATTEMPTED RESTART IAW QRH. UNSUCCESSFUL. TROUBLESHOT IAW 49-11-00-1 FIM AND FOUND DELTA PRESSURE SWITCH FAULTY. R & R IAW AMM 49-27-15/401. OPS CKD NORMAL. ACFT OK FOR SERVICE.SDR HALA2012041100121Warning Message · illuminatedRIGHT PACK TEMP EICAS MESSAGE ILLUMINATED ENROUTE. IAW QRH, SELECTED PACK CONTROL TO STANDBY-N AND OPERATIONS NORMAL. RAN SYS AND TROUBLESHOT IAW FIM 21-51-00/101, FIG 104. ALL CHECKED GOOD. NO MESSAGES ON PACK TEMP CONTROL. OP CHECKED NORMAL, OK FOR SERSDR HALA2012032400119Wire · brokenRIGHT ENGINE NR 2 FIRE LOOP STATUS MESSAGE. FOUND BROKEN WIRE TO TERMINAL AT NR 2 LOOP ON ENGINE. RETERMINATED IAW SWPM 20-30-00, OPS CHECKED GOOD.SDR HALA2012030700108Engine · bird ingestionNR 2 ENGINE BIRD STRIKE UPON LANDING. ENGINE CHANGE IN WORK.SDR HALA2012030500100Warning Light · false activationRT ENG. PRIORITY VALVE STATUS MESSAGE AFTER PUSHBACK. TROUBLESHOT IAW FIM 36-10-00/101, FIG 123, BIT BOX & ACCOMPLISHED VERIFICATION CHECK. GREEN LIGHT AT CONTROLLER. RESET, RAN ENG. OPS CHECKED GOOD.SDR HALA2012030300098Radar · unknownLEFT WEATHER RADAR INOPERATIVE. PERFORMED OPS TEST OF WEATHER RADAR SYS IAW AMM TASK 34-43-00-501. TEST SATISFACTORY.SDR HALA2012030100092None · noneNR 1 TCAS FAIL. TEST TCAS SYS REF B767 MM 34-45-00 TCAS SYS TEST OK.SDR HALA2012022600080Warning Light · false activationETOPS SIGNIFICANT SYS -WINDSHEAR SYS EICAS DISPLAYED WITH WEATHER RADAR FAIL DISPLAYED ON NAV DISPLAY. THIS OCCURS WITH THE NR 1 RT SELECTED. WHEN NR 2 RT IS SELECTED, ALL ANNUNCIATIONS CLEAR. TROUBLESHOT IAW FIM 34-43-00/101, FIG 103 AND FIM 34-46-00/101, SDR HALA2012022200066Module · faultedRUDDER RAIO EICAS MESSAGE AND RUDDER RATIO LIGHT ILLUMINATED JUST AFTER TAKE OFF. ACCOMPLISHED FIM 27-21-00-1, FIG 104 AND 27-09-00-1, FIG 106 B. FAULTING RT RUDDER RATIO CHANGE MODULE. R & R RT RUDDER RATIO CHANGER MODULE IAW AMM 27-09-00. BITE CHECKED OK. SDR HALA2012021400061Coupler · failedHF NR 2 RT UNABLE TO TUNE & COMMUNICATE ON LOWER FREQUENCIES. ABLE TO TUNE 11282 SUCCESSFULLY. REPLACED NR 2 RT HF COUPLER IAW AMM 23 11 01. CONTACTED SFO RADIO SIGNAL STRENGTH 5 BY 5 ON LOW FREQUENCIES. OPS NORMAL.SDR HALA2012020900057Blade · damagedNR 1 ENGINE HAS TIP CURL ON ONE BLADE. .250" ON L/E THRU .100 ON OUTER EDGE TIP OF BLADE. REMOVED DAMAGED AREA REF AMM 72-31-02. PERFORMED FPI AND EDDY CURRENT IAW AMM 72-31-02, NO FAULTS.SDR HALA2012012000046Warning Light · false activationETOPS SIGNIFICANT SYS - RUDDER RATIO EICAS MESSAGE ILLUMINATED. PERFORMED BITE ON RUDDER RATIO BOX NO FAULTS NOTED. PERF FIM 27-21-00/101, FIG 104. OK FOR SVC.SDR HALA2012011600031Probe · malfunctionedETOPS SIGNIFICANT SYSTEM - ALL FUEL INDICATIONS ON RT TANK FUEL GAUGE DISAPPEARED. GAUGE CAME ON AT BLOCK IN. WIRE CONTINTUITY CHECKED GOOD FROM D2706C TO D4638P TO M1949 PER WDM28-41-22. FOUND IN TANK HI-Z TO SHEILD INSULATION RESISTANCE LOW & TU2, TU4SDR HALA2012011500034Windshield · shortedETOPS SIGNIFICANT SYS - RIGHT FWD WINDOW HEAT INOP. FOUND F/O'S R1 WINDOW BAD. R & R IAW AMM 56-11-01/401 ALL TORQUES C/W. OK FOR SERVICE.SDR HALA2012011400027Windshield Wiper · inoperativeETOPS SIGNIFICANT SYS - CAPTAIN`S WINDSHIELD WIPER BLADE INOPERATIVE. R & R WINDSHIELD WIPER. OPS CHECKED GOOD IAW AMM 30-42-03.SDR HALA2012011300023Computer · failedETOPS SIGNIFICANT SYS - AFTER CLEARD TO LINE UP & WAIT - NOTICED STATUS PAGE EICAS MESSAGE FOR ELEVATOR FEEL. R & R ELEVATOR FEEL COMPUTER IAW MM27-31-19 UP TO 3.F (12). ACCOMPLISHED STEPS 3F 13 TO G3. OPS CHECKED GOOD. PERFORMED PITOT/STATIC LEAK CHECKED ISDR HALA2012011100015Clamp · brokenETOPS SIGNIFICANT SYS - ON EXTERNAL INSPECTION OF NR 1 ENGINE, FOUND TWO TCC SUPPORT BRACKET CLAMPS BROKEN. REPLACED TCC SUPPORT BRACKET CLAMPS AT 3 O'CLOCK POSITION. OK FOR SERVICE.SDR HALA2012011000016Warning Light · false activationETOPS SIGNIFICANT SYS - EICAS MESSAGE RT GPS DISPLAYED. CW FIM 34 58 00, FIG 10 TEST OF THE MMR GPS SYS, GPS SYS OK FOR SERVICE.SDR HALA2012011000013Altimeter · inaccurateETOPS SIGNIFICANT SYS - ALTIMETERS DIFFERENCE BETWEEN CAPT AND CO-PILOT IN RVSM 130' DIFFERENCE. IAW DISPATCH-ACFT FLT PLAN HAS FLT LEVELS FROM 37,000 FT TO 38,000 FT AT CRUISE. REF FIM CHART CHAPTER 34 FAULT CODE DIAGRAM ALTIMETER TOLERANCES FIG 6, SHEET 1.SDR HALA2012010900014Transceiver · failedETOPS SIGNIFICANT SYS - WXR FAIL DISPLAYED ON HSI W/RT SYS SELECTED. WX TEST NOT ATTEMPTED. REPLACED RT WEATHER RADAR TRANSCEIVER, GROUND CK OK IAW
AMM34-43-00.SDR HALA2012010900010Pump · inoperativeETOPS SINGIFICANT SYS - ELEVATOR FEEL STATUS MESSAGE ANNUNCIATED DURING FLIGHT. TROUBLESHOT IAW FIM 27-31-00/101, FIG 106 AND MESSAGE IS ASSOCIATED WITH ADP INOPERATIVE, NOT PROVIDING ENOUGH HYD SYS PRESSURE, MESSAGE CLEARED, OK FOR SERVICE.SDR HALA2012010800012Indicator · inoperativeETOPS SIGNIFICANT SYS - F/O VERTICAL SPEED OFF FLAG IN VIEW. ALTERNATE AIR DATA DOES NOT CORRECT. REPLACED F/O VERTICAL SPEED INDICATOR IAW AMM 34-22-06-004-001. GROUND OPS CHECKED OK IAW AMM 34-22-06-064.SDR HALA2012010400006Transceiver · malfunctionedETOPS SIGNIFICANT SYS - TRANSMISSION ON RIGHT HF, INOPERATIVE AT ALL STATIONS. RERACKED RT HF TRANSCEIVER. GROUND OPS CHECKED OK IAW AMM 23-11-03.SDR HALA2011122900621Connector · failedETOPS SIGNIFICANT SYS - RT ENGINE FIRE LP2 ON EICAS. ACCOMPLISHED FIM 26-11-00. REPLACED BAD FIRE LOOP 2 CONNECTOR PLUG. OPS CHECKED OK ON GROUND. OK FOR SVC.SDR HALA2011122600610Bearing · failedSTEERING TILLER BINDING DURING TAXI. F/A REPORTED "BANGING NOISE" IN FORWARD CABIN AREA. UPON ARRIVAL FOUND NR 6 WHEEL SPARKING. REMOVED NR 6 WHEEL FOUND REAR BEARING DAMAGE. INSPECTED AXLE IAW AMM 05-51-17, NO DAMAGE NOTED. R & R NR6 BRAKE AND TIRE ASSY IASDR HALA2011122500614Warning Light · illuminatedETOPS SIGNIFICANT SYS - ON STATUS PAGE ON LOWER EICAS, LT EEC ENGINE C1 LIGHT CAME ON, NO OTHER INDICATIONS. TROUBLESHOT IAW FIMM 73-21-00-101, FIG 115 TO PIMU MESSAGE INDEX. PERFORMED BITE TEST, FAULT DOT 3 CR CHECK FAILED. CHECKED CONNECTION, EEC M198 TO NSDR HALA2011122000603Warning Light · illuminatedETOPS SIGNIFICANT SYS - APU FAULT LIGHT ON AFTER APU START AND RUN LIGHT ON. APU SHUTDOWN WITH APU FAULT LIGHT ON AND EICAS MESSAGE. PERFORMED BITE TEST, STARTED NORMALLY, NO FAULTS, STARTED BOTH A/C ENGINES, NO FAULTS. APU OPS NORMAL IAW AMM 49-11-00-802.SDR HALA2011121100578Warning Light · false activationETOPS SIGNIFICANT SYS - RUDDER RATIO LIGHT ILLUMINATED IN FLIGHT. EICAS MESSAGE "RUDDER RATIO" DISPLAYED. PERFORMED FIM 27-21-00. NO FAULTS NOTED. ACFT IS OK TO CONTINUE. ACFT IS OK FOR SERVICE.SDR HALA2011120900574Warning Message · false activationETOPS SIGNIFICANT SYS, DURING LANDING ROLLOUT LEFT IRS FAULT MESSAGE ON EICAS. PERFORMED LEFT IRS TEST IAW AMM 34-21-00, NO FAULT-FOUND. PERFORMED FIM 34-21-00/101, FIG 107, NO FAULT FOUND. SYS OK.SDR HALA2011120300566Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - RT PACK RUNNING HOT. R & R LOW LIMIT VALVE IAW AMM 21-51-11 ON RT PACK. NO LEAKS NOTED. OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2011120300564Start Valve · failedETOPS SIGINIFICANT SYS - RT ENGINE START VALVE WOULD NOT OPEN. REPLACED RT ENGINE START VALVE IAW MM 80-11-02, REPLACED RT ENGINE STARTER IAW MM 80-11-01. ROTATION GOOD.SDR HALA2011120200559Transponder · failedETOPS SIGNIFICANT SYS - NR 1 TRANSPONDER ATC FAIL LIGHT ON. TROUBLE SHOT IAW FIM SUSPECT NR 1 TRANSPONDER. R & R TRANSPONDER IAW AMM 34-53-01. OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2011112900548Terminal · brokenETOPS SIGNIFICANT SYSTEM - EICAS STATUS "RT PRV". FOUND TERMINAL BROKE-REPLACED TERMINAL IAW SWPM 20-30-11, RAN NR 2 ENG NO FAULTS. CHECKS OK AT RT PRV.SDR HALA2011112400539Warning Message · illuminatedETOPS SIGNIFICANT SYS - RUDDER RATIO EICAS MESSAGE DISPLAYED IN FLIGHT. PERFORMED BITE PROCEDURES OF RUDDER RATIO CONTROL MODULE, IAW FIM 27-09-00/101 FIG 106B. NO FAULTS AT THIS TIME.SDR HALA2011111500557Splice · crackedNR 2 ENGINE PYLON AFT FAIRING, AFT SPLICE FOUND CRACKED. REPAIRED IAW SRM 51-40-02.SDR HALA2011111500556Stiffener · crackedNR 2 ENGINE AFT FAIRING, INBD STIFFENER CRACKED. REPAIRED IAW SRM 51-40-02.SDR HALA2011111500555Structure · crackedNR 2 ENGINE PYLON AFT FAIRING, OTBD CHORD FOUND CRACKED. REPAIRED IAW SRM 51-40-02.SDR HALA2011111500554Channel · crackedNR 2 ENGINE PYLON AFT FAIRING, AFT CHANNEL, FOUND CRACKED. REPAIRED IAW SRM 51-40-02.SDR HALA2011111500553Web · crackedNR 2 ENGINE PYLON AFT FAIRING, AFT WEB CRACKED. REPAIRED IAW SRM 51-40-02.SDR HALA2011111500552Skin · crackedENGINE PYLON AFT FAIRING, INBD COMPOSITE PANEL CRACKED. REPAIRED IAW SRM 51-40-02.SDR HALA2011112000514Light · inoperativeRIGHT SIDE MID CABIN PATH WAY LIGHTING INOPERATIVE. REPLACED RT SIDE MID CABIN PATH WAY LIGHT STRIP SYS, OPS CHECKED GOOD IAW AMM 33-51-00.SDR HALA2011110400504Starter · failedETOPS SIGNIFICANT SYS - SECOND ATTEMPT: RT ENGINE N2 SHOWS 0 DURING START, START VALVE INDICATED OPEN. FIRST ATTEMPT: N2 SHOWED 19 PERCENT THEN DELAYED TO ZERO. FOUND METAL IN STARTER NR 2. R & R STARTER IAW AMM80-11-01, SECURITY AND OPS CHECKED OK.SDR HALA2011110200524Frame · corrodedCORROSION ON AFT CARGO FRAME UPPER TEE AT STA 1197 & 88. REPLACED TEE IAW SRM 51-40-02.SDR HALA2011115000523Angle · crackedNR 1 ENGINE PYLON AFT FAIRING LOWER ATTACHMENT CLOSE OUT ANGLE CRACKED PN 313T3380-54, 0.5 INCHES. REPLACED IAW SRM 51-40-02, REV 87.SDR HALA2011102600536Pulley Bracket · crackedETOPS SIGNIFICANT SYS - RUDDER SYS PULLEY BRACKET ANGLE CRACKED ON FLOORBEAM 246+BL .0. ANGLE BRACKET REPLACE WITH A NEW 1 IAW SRM 51-40-02.SDR HALA2011102600526Skin · debondedNR 11 SLAT UPPER SKIN ON T/E WEDGE DEBONDED & CORRODED. REPAIRED IAW SRM 57-43-02-01 & 57-43-02-2R-1 FIG 201 & 51-70-2R-0, PARA 6 & 8.SDR HALA2011102600524Skin · corrodedNR 11 SLAT UPPER SKIN ON T/E WEDGE, DEBONDED & CORRODED. REPAIRED IAW SRM 57-43-02-01 & 57-43-02-2R-1, FIG 201 & 51-70-10-2R-0 PARA 6 & 8.SDR HALA2011102300482Warning Message · illuminatedETOPS SIGNIFICANT SYS - RUDDER RATIO EICAS WARNING AFTER ENGINE START. RESET RUDDER RATIO SYS CB G10 CHECKED RRCM TEST NORMAL ALL FOUND TO BE NORMAL. OPS CHECKED NORMAL IAW AMM 27-21-00.
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