Boeing 767-3G5

Service difficulty reports · 724

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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.

SDR HALA2010062900280Electronic Unit · malfunctionedFLAP SLAT ELEC MSG DISPLAYED. BITE CHECKED FSEU, FOUND PSEU POS SENSOR 1 MSG. 27-51002. FOUND C/B C14 AND C15 ON P11 POPPED. RESET CBS NO DEFECTS NOTED. R & R FLAP/SLAT ELECTRONICS UNIT IAW AMM 27-51-01. OPS CHECK OK.Jun 29, 2010 · N584HA · Boeing 7673G5 · Leading Edge Slat Control SystemSDR HALA2010061700260Fan · failedETOPS SIGNIFICANT SYS - RT RECIRC FAN INOP. T/S RT RECIRC FAN IAW FIM 21-25-00/101, FIG 103. OPS CK GOOD. OK FOR SERVICE.Jun 17, 2010 · N585HA · Boeing 7673G5 · Air Distribution FanSDR HALA2010061000251Guard · damagedETOPS SIGNIFICANT SYS- DUCT LEAK INDICATION ON BOTH SIDES ON O/H PNEUMATIC CONT PANEL & L&R STRUT DUCT LEAK ON EICAS. ACCOMPLISHED WIRING CHECK IAW WDM 26-18-12 FOUND STRUT TEST SWITCH GUARD SPRING WAS HITTING SWITCH ON TEST POSITION. REPOSITIONED SWITCH GUARJun 10, 2010 · N584HA · Boeing 7673G5 · Pneumatic SystemSDR HALA2010061000248Warning Light · false activationETOPS SIGNIFICANT SYS - R BLD ISLN VAL EICAS AND R ISLN VALVE LIGHT ILLUMINATED (OCCURED AFTER LDG AT IDLE PWR). RAN BOTH ENGINE AT IDLE & CYCLED RT BLD ISLN VALVE. BOTH EICAS MSG & VALVE LIGHT CLEARED. OK FOR SERVICE.Jun 10, 2010 · N586HA · Boeing 7673G5 · Pneumatic Distribution SystemSDR HALA2010060300243Circuit Card · malfunctionedETOPS SIGNIFICANT SYS- ALTITUDE ALERT LIGHT FAILED TO ILLUMINATE ON DESCENT. R & R ALTITUDE ALERT WARNING DCA CARD IAW AMM 31-51-04, OPS CHECK OK.Jun 3, 2010 · N584HA · Boeing 7673G5 · Stall Warning SystemSDR HALA2010053000235Actuator · malfunctionedETOPS SIGNIFICANT SYS - AFTER T/O & DURING CLIMB ACFT REQUIRES 4-5 RUDDER UNITS OF TRIM 2-3 UNITS OF RUDDER TRIM AS WEIGHT DECREASES. R & R RUDDER TRIM ACTUATOR IAW AMM 27-21-11, OK FOR SVC.May 30, 2010 · N585HA · Boeing 7673G5 · Rudder ActuatorSDR HALA2010052900234Trim System · unknownETOPS SIGNIFICANT SYS - RUDDER TRIM INTERMITTENTLY INOP WHEN TRIMMING TO THE RT. PERFORMED OPS CHECK IAW FIM 27-21-00/101 FIG 106 NO FAULTS FOUND SYS CHECKS GOOD AT THIS TIME.May 29, 2010 · N585HA · Boeing 7673G5 · Rudder Tab Control SystemSDR HALA2010052000229Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK RBL 54 AT STA.427, 438, 458, 535, 566, 575, 591, 604, 622,654+10, 654+29, 654, 654+42, 774 -786 AND 676 -760 AND 423 - 489. SCRATCHES ON SEAT TRACK RBL 54 AT STA 434 - 456 AND 676-760. SEAT TRACK SPLICE REPAIR CARRIED OUT FROM May 20, 2010 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010051900228Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK LBL 54 AT STA. 522 - 654+44. SEAT TRACK REPLACED FROM STA 348-654+44 IAW 767-300, SRM 51-40-02, D634T210, REV 83.May 19, 2010 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010051900227Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK LBL 88 AT STA 368 - 423. SEAT TRACK REPLACED FROM STA 344 - 423 IAW SRM 51-40-02, D634T210 REV 83 SEAT TRACK AT ALL OTHER DEFECT STATIONS CORROSION REMOVED UNTIL NO FURTHER CORROSION EVIDENT, FOUND WITHIN LIMITS IAW SRM 53-00-5May 19, 2010 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010051900218Seat Track · corrodedLEVEL 2 CORROSION AND SCRATCHES ON SEAT TRACK RBL 30, STA. 654 +44 TO 654 + 110. SEAT TRACK SPLICE REPAIR CARRIED OUT. REPAIR, REF, SRM 53-00-52 REPAIR 2.May 19, 2010 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010051800226Structure · corrodedRT INBD T/E MAIN FLAP HAS CORROSION ON UPPER REAR CHORD 18 INCHES OTBD FROM INBD END. UPPER REAR CHORD REPLACED IAW SRM 51-40-02,DWR 0634T210. REV 83.May 18, 2010 · N584HA · Boeing 7673G5 · Trailing Edge FlapsSDR HALA2010051600216Indicator · malfunctionedETOPS SIGNIFICANT SYS - CAPT LWR EFIS DISPLAY FLICKERS. REPLACED CAPT EHSI DISPLY UNIT OPS CHCK OK IAW MM 34-22-00. PERFORMED MCDP TEST 30 TEST PASSED. ACFT REMAINS IN LAND 3 LMP STATUS.May 16, 2010 · N585HA · Boeing 7673G5 · Directional Gyro and Indicating SystemSDR HALA2010050600205Panel · damagedL/E OF PANEL 511CB DAMAGED. R & R PANEL 511CB SECURITY CK & CLEARANCE CK OK.May 6, 2010 · N586HA · Boeing 7673G5 · Wing, Plate/SkinSDR HALA2010050200225Angle · brokenNR 1 STRUT AFT FAIRING, AFT "V" ANGLE, INBD ANGLE BROKEN WERE FAIRING ATTACHES TO STRUT. FABRICATION OF REPLACEMENT PARTS IAW DWG 313T3380. MATCH DRILL REPLACEMENT FRAME DWG 313T3380-303, IAW SRMS -40-02, REV 82. ASSY FRAME AND FABRICATED PARTS IAW SRM 51-40-May 2, 2010 · N584HA · Boeing 7673G5 · Nacelle/Pylon Miscellaneous StructureSDR HALA2010042800224Wedge · debondedL/E SLAT NR 4 T/E WEDGE UPPER SURFACE INBD EDGE FWD OF T/E DISBOND 2"X2". REPAIRED IAW SRM 57-43-02-2R-1 AND 51-70-10 BOTH REV 82.Apr 28, 2010 · N584HA · Boeing 7673G5 · Leading Edge DevicesSDR HALA2010042800223Wedge · debondedNR 8 SLAT T/E WEDGE HAS 2 AREAS OF DISBONDS, (1) INBOARD EDGE, T/E 3"X1.5". (2) 37" OTBD OF INBD EDGE ADJACENT TO T/E 1.5" DIA. REPAIRED IAW SRM 57-43-02-2R-1 AND 51-70-10.Apr 28, 2010 · N584HA · Boeing 7673G5 · Leading Edge DevicesSDR HALA2010042000177Circuit Card · malfunctionedETOPS SIGNIFICANT SYS - R ENG EEC MODE DISPLAYED. ALTN MODE ON R EEC CONT SWITCH. BIT PIMU. REPLACED RT ENGINE SPEED CARD IAW AMM 77-12-01. EICAS MESSAGE CLEARED. IDLE RUN OK. NO FAULTS NOTED. CLEARED PIMU.Apr 20, 2010 · N586HA · Boeing 7673G5 · Engine (Turbine/Turboprop)SDR HALA2010041800176Shutoff Valve · malfunctionedETOPS SIGNIFICANT SYS- BTB INOP AND PACK OFF LIGHT ILLUMINATED FR LT PACK - WOULD NOT RESET. R & R LT FLOW CONTROL AND SHUTOFF VALVE IAW AMM 21-51-01, RAN ENGINE ON GROUND, NO DEFECTS NOTED, OPS CHECKS GOOD.Apr 18, 2010 · N586HA · Boeing 7673G5 · Cabin Cooling SystemSDR HALA2010041800175Feeder Cable · damagedETOPS SIGNIFICANT SYS - 14 MINUTES INFLIGHT LT GEN OFF LGT ILLUMINATED, FOLLOWED BY LT GENERATOR OFF LGT EICAS. BPCU BITE LT GEN POWER SYS DP TRIP GEN/FDR PRECAU CHG 1 IDG IAW AMM 24-11-01. OPS CKS OK 7309/5755 CONF OF IRING ROUT THRU CT-T106 FOR PROP ROUTINGApr 18, 2010 · N584HA · Boeing 7673G5 · Electrical Power System WiringSDR HALA2010041500158Oil Filter · unknownETOPS SIGNIFICANT SYSTEM - TOOK 2 ATTEMPTS TO START APU ON GROUND. REPLACED OIL FILTER PER 49-27-03, NO LEAKS NOTED.Apr 12, 2010 · N586HA · Boeing 7673G5 · APU Oil SystemSDR HALA2010041500157Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - "L FMC FAIL" EICAS; RESET CB "E9" (FMCS COMPUTER) PER L FMC FAIL QRH CHECKLIST. OP NORMAL. T/S PER FIM 34-61-00, NO FAULTS. SYS OPS CHECKED OK.Apr 12, 2010 · N585HA · Boeing 7673G5 · Flight Management Computing Hardware SystemSDR HALA2010040900155Generator · malfunctionedOPEN - ETOPS SIGNIFICANT SYS - DURING PREFIGHT APU TRIPPED OFF LINE. R & R APU GENERATOR IAW AMM 24-21-01. TESTED APU GENERATOR LOAD IAW AMM 24-21-00 ALL CHKS NML.Apr 9, 2010 · N586HA · Boeing 7673G5 · AC Generator-AlternatorSDR HALA2010040800156Contactor · damagedETOPS SIGNIFICANT SYS - APU GENERATOR TRIPS WILL NOT TAKE LOAD. REPLACED APU CONTACTOR C905 IAW AMM24-22-03. OPS CK OK.Apr 8, 2010 · N586HA · Boeing 7673G5 · AC Generator-AlternatorSDR HALA2010040700154Gcu · failedETOPS SIGNIFICANT SYS - APPROX 45 MIN. AFTER ARRIVAL APU GEN KICKED OFF LINE WITH A BPCU FAULT OF "DP TRIP" AND "OVERLAP ZONE". T/S IAW FIM 24-20-00/101 STEP F (1) (B) 1 THRU 6. NO TROUBLE NOTED. INSPECTED PINS OF APU GCU, NO TROUBLE NOTED. REPLACED APU GCU IApr 7, 2010 · N586HA · Boeing 7673G5 · AC Generator-AlternatorSDR HALA2010040100147Valve · inoperativeETOPS SIGNIFICANT SYS - LT ENGINE ANTI ICE INOP. R & R ENG NR 1 VALVE THRML ANTI ICE, IAW AMM TASK 30-21-03 PB 401, SYS TEST REF AMM 30-21-00735 001.Apr 1, 2010 · N584HA · Boeing 7673G5 · Air Intake Anti/De-Ice SystemSDR HALA2010033100145Fan Blade · damagedETOPS SIGNIFICANT SYS - NR 2 ENG FAN BLADE NR 1 TIP DAMAGED. REPAIRED IAW AMM 72-31-02. EDDY CURRENT INSPECTED IAW AMM 72-31-02, NO CRACK IND.Mar 31, 2010 · N584HA · Boeing 7673G5 · Turbine Engine Compressor SectionSDR HALA2010033000141Warning Light · false activationETOPS SIGNIFICANT SYS - EICAS MSG L ENG ANTI-ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SW ON. PERFORMED 30-21-00/101. LIGHT OPERATED NORMALLY. NO DEFECTS FOUND. UNABLE TO DUPLICATE.Mar 30, 2010 · N584HA · Boeing 7673G5 · Air Intake Anti/De-Ice SystemSDR HALA2010032900139Pump · leakingETOPS SIGNIFICANT SYS- LT ENGINE HYD PUMP LEAKING. R & R PUMP. LT ENGINE HYD PUMP IAW AMM 29-11-05/401.Mar 29, 2010 · N585HA · Boeing 7673G5 · Hydraulic Pump (Electric/Engine), MainSDR HALA2010032300133Actuator · malfunctionedETOPS SIGNIFICANT SYS - FUEL CROSSFEED VALVE LIGHT ILLUMINATED WHEN CLOSED SELECTED. EICAS MESSAGE FUEL CROSSFEED DISPLAY. T.S. IAW FIM 28-22-00. R & R FUEL CROSSFEED VALVE ACTUATOR IAW AMM 28-22-12. OPS TEST OF FUEL XFEED VALVE CHK GOOD ON GROUND.Mar 23, 2010 · N586HA · Boeing 7673G5 · Fuel Transfer ValveSDR HALA2010031900131Seal · out of positionETOPS SIGNIFICANT SYSTEM - LEFT AILERON BINDS. FOUND RIGHT INBOARD AILERON OUTBOARD LOWER SEAL AT LEADING EDGE STICKING OUT FOUR INCHES. RE-SECURED SEAL, SECURITY AND OPS CHECK OK REF FIM 27-11-00 FIG 107.Mar 19, 2010 · N584HA · Boeing 7673G5 · Aileron Control SystemSDR HALA2010031800124Hf Comm · malfunctionedETOPS SIGNIFICANT SYSTEM - HF NR 2 WOULD NOT CHANNELIZE OR TRANSMIT OR USE HF DATA LINK, AT BEGINNING OF FLT, BUT WORKED AT END OF FLT. PERFORMED OPERATIONAL TEST HF COMM SYSTEM AS PER AMM TASK 23-11-00-715-001, OPERATIONAL TEST.Mar 18, 2010 · N584HA · Boeing 7673G5 · HF Communications SystemSDR HALA2010031400107Indicator · malfunctionedETOPS SIGNIFICANT SYSTEM - CAPT AIRSPEED FLAG INTERMITTENT ON SHORT FINAL AND TAXI IN. REPLACED CAPT MACH/A/S IND, OPS CHECK OK PER M/M 34-13-02.Mar 14, 2010 · N584HA · Boeing 7673G5 · High Speed WarningSDR HALA2010030800099Acars · malfunctionedETOPS SIGNIFICANT SYSTEM - HF DATA LINK LOST DISPLAYED ON EICAS (NR 1 HF USED IN DATA). FOLLOWED FIM PROCEDURES 23-22-00/101 FIG 103. ACARS COMMUNICATION PROBLEM. SYSTEM INDICATIONS/OPERATION NORMAL.Mar 8, 2010 · N584HA · Boeing 7673G5 · Communications SystemSDR HALA2010030300085Processor · malfunctionedETOPS SIGNIFICANT SYS - FUEL CONFIG LIGHT CAME ON AS FUEL QTY FLUCTUATED 1500 LBS DIFFERENCE ON TOTALIZER. FQIS PROCESSOR BITE IAW AMM 28-41-00 TABLE 101, NO FAULTS NOTED, PRECAUTIONARY CHANGE OF FQIS PROCESSOR IAW AMM 28-41-08 OPS CHECK GOOD.Mar 3, 2010 · N586HA · Boeing 7673G5 · Fuel Quantity IndicatorSDR HALA2010021000060Unknown · unknownETOPS SIGNIFICANT SYS - RA FLAG DISPLAYED STEADY. FOUND RA FLAG ON FO EADI ONLY. T/S IAW FIM 34-33-00/101 RA T/A RT TEST COMPLETE NO FAILURES. ALL INDICATIONS NORMAL. OK FOR SERVICE.Feb 10, 2010 · N586HA · Boeing 7673G5 · Navigation SystemSDR HALA2010013100044Rheostat · inoperativeETOPS SIGNIFICANT SYS - CAPT ADI DARK. LIGHTING FULL DIM ONLY. RHEOSTAT INOP. REPLACED CAPT EFIS CONTROL PANEL. OPS CHECK OK IAW MM 34-22-00 PERFORMED MCDP TEST 30 TEST PASSED. ACFT REMAINS IN "LAND 3" LMP STATUS.Jan 31, 2010 · N585HA · Boeing 7673G5 · Instrument PanelSDR HALA2010012900043Fire Loop · malfunctionedETOPS SIGNIFICANT SYS - R ENG FIRE LP-1. RESEATED FIRE AND OVERHEAT CARD IAW FIM 26-11-00/101, FIG 104. OPS CK GOOD, OK FOR SERVICE.Jan 29, 2010 · N584HA · Boeing 7673G5 · Fire DetectionSDR HALA2010012200039Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB - "RIGHT ENGINE CONTROL"EICAS MSG. DISPLAYED AFTER NR 2 ENGINE STARTED. NR 2 ENG COWLS UNLATCHED FOR MAINTENANCE. REMOVED AND REPLACED NR 2 ENG EEC PER M/M C/W EEC STATIC TEST AND ENG RUN NO STATUS OR EICAS MSG. CLOSED ENG COJan 22, 2010 · N586HA · Boeing 7673G5 · Fuel Controlling SystemSDR HALA2010011700029Coupler · damagedETOPS SIGNIFICANT SYSTEM, NR 1 HF WILL NOT CHANNEL OR TUNE. REMOVED AND REPLACED NR 1 HF COUPLER. GRD CHK OK PER AMM 23-11-01.Jan 17, 2010 · N584HA · Boeing 7673G5 · HF Communications SystemSDR HALA2010011600027Relay · malfunctionedETOPS SIGNIFICANT SYSTEM - RT ENG OIL PRESS DISPLAYED IN "RED" AFTER ENG SHUTDOWN. (W/PRESS AT EICAS STILL INDICATES RED). REPLACED K1039 CH B R ENG EEC RESET RELAY AND K169 R FUEL/IGN CONT RELAY PER SSM 76-11-01. ACCOMPLISHED IDLE RUN RT ENG OIL PRESS IND NJan 16, 2010 · N585HA · Boeing 7673G5 · Engine Indicating SystemSDR HALA2010011600026Circuit Card · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB: ON ENGINGE START, STATUS MSG "R ENG SPEED CARD" DISPLAYED. REPLACED RT ENGINE SPEED CARD PER AMM 77-12-01-404. ALL TEST PASSED. ENGINE RUN GOOD.Jan 16, 2010 · N586HA · Boeing 7673G5 · Engine Indicating SystemSDR HALA2010011400025Unknown · unknownOPEN - ETOPS SIGNIFICANT SYSTEM - CREW REPORTED THAT AFTER FUELING WAS COMPLETED, THE TOTAL FUEL DECREASED FROM 68.3K TO 66.7K IN ABOUT 15 MIN AND CONTINUE TO DROP.Jan 14, 2010 · N586HA · Boeing 7673G5 · Fuel StorageSDR HALA2010011300019Pump · leakingETOPS SIGNIFICANT SYSTEM - ON WALK AROUND FOUND NR 1 ENG HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED HYDRAULIC PUMP AT NR 1 ENG PER AMM 29-11-5. LEAK CHECK AND SECURITY CHECK OK.Jan 13, 2010 · N586HA · Boeing 7673G5 · Hydraulic Pump (Electric/Engine), MainSDR HALA2010010800011Warning Light · illuminatedETOPS SIGNIFICANT SYS - RT ENG OIL PRESS & RT ENG BLEED OFF LIGHTS ON. PERFORMED ENG SHUTDOWN INPUT REMOVAL IAW AMM 31-41-00-912-037. GROUND RUN ENG CK OK.Jan 8, 2010 · N585HA · Boeing 7673G5 · Engine Oil Indicating SystemSDR HALA2010010600006Cdu · inoperativeETOPS SIGNIFICANT SYS - BTB: RT FMS FAIL, CDU BLANK. REMOVED & REPLACED NR2 MCDU. GRD CHK OK IAW AMM 34-61-02.Jan 6, 2010 · N586HA · Boeing 7673G5 · Flight Management Computing Hardware SystemSDR HALA2010010300002Fuel Control · malfunctionedETOPS SIGNIFICANT SYS - ATB - APU FAIL AT ALT 350, DURING APU VERIFICATION FLIGHT. BITE CHECK ECU, NO FAULT NOTED, REMOVED AND REPLACED FCU IAW AMM 49-31-01 IAW MFG APU T/S GUIDE AND PRECAUTIONARY CHANGE APU ECU IAWAMM 49-61-05, OPS AND LEAK CHECK OK.Jan 3, 2010 · N586HA · Boeing 7673G5 · APU Engine Fuel and ControlSDR HALA2010010300001Ecu · faultedETOPS SIGNIFICANT SYS - DURING REQUIRED INFLT APU START RECEIVED EICAS MESSAGE "APU FAULT" AND OVERHEAD PANEL APU "FAULT" LIGHT. SECOND START ATTEMPT YIELDED SAME RESULT. FL 380, SAT -50 DEGREE, TAT -20 DEGREE, START TIME WAS LESS THAN 1 MINUTE, MAX EGT WAS Jan 3, 2010 · N586HA · Boeing 7673G5 · APU Start/Ignition SystemSDR HALA2010010200003Warning Message · false activationETOPS SIGNIFICANT SYS - ON ENG SHUTDOWN EICAS STATUS ALERT-EICAS MSG'R ENG EEC C1' DISPLAYED AND RT ENG OIL PRESS SHOWS RED BOX. PERFORMED OPS CHECK OF OIL PSI INDICATING SYS IAW MM79-32-00 OPS CHECK OK PERFORMED EICAS ERASE PROCEDURE FOR EEC C1 MSG. MSG CLEJan 2, 2010 · N585HA · Boeing 7673G5 · Engine Indicating SystemSDR HALA2009122900609Gcu · failedETOPS SIGNIFICANT SYS - LT GENERATOR FAILED/RESET/FAILED. BITE BPCU FAULT MSG, DP TRIP GEN/FDR, DP TRIP MAIN BUS/OVERLAP ZONE. CHK IAW FIM 24-20-00/101 & WDM 24-21-11. ALL CHECKED GOOD. REMOVED AND REPLACED LT GCU AS A PRECAUTION. OPS CHK NML. OK FOR SERDec 29, 2009 · N584HA · Boeing 7673G5 · Alternator-Generator Drive
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