Boeing 767-3G5

Service difficulty reports · 724

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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 HALA2010102600494Generator · malfunctionedETOPS SIGNIFICANT SYS- RT GENENERATOR NEEDED TO BE RESET AFTER ENG START. ACCOMPLISHED RT ENGINE GENERATOR CHECK ON BPCU BITE. NO FAULTS NOTED RT. GENERATOR SYS CHECK GOOD IAW FIM 24-20-00 OK FOR SVC.Oct 26, 2010 · N584HA · Boeing 7673G5 · AC Generator-AlternatorSDR HALA2010102500491Stringer Splice · corrodedLEVEL 2 CORROSION ON STRINGER SPLICE AT BS 434, S17L. SPLICE REPLACED IAW SRM 51-40-02, REV 84 AND DWG 140T0115.Oct 25, 2010 · N585HA · Boeing 7673G5 · Fuselage Main, Longeron/StringerSDR HALA2010102500490Stringer Splice · corrodedLEVEL 2 CORROSION ON STRINGER SPLICE AT BS 434, S18L. SPLICE R & R IAW SRM 51-40-02 REV 84 AND DWG 140T0115.Oct 25, 2010 · N585HA · Boeing 7673G5 · Fuselage Main, Longeron/StringerSDR HALA2010102200516Seat Track · corrodedLEVEL 2 CORROSION AT SECTION 45 SEAT TRACK, BS 787, 804, 816, 836, 848, 867, 890 -915 ,918, 935, 952, 970, 1033, 1045, 1065, 1092, 1093, AT LBL 88.5. BLENDED AREAS AT BS 787-893 IAW SRM 53-00-52 REV 84. SEAT TRACK REPLACED FROM BS 893-1098 IAW SRM 53-00-52, Oct 22, 2010 · N585HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010102200514Seat Track · corrodedSEAT TRACK SECTION 46, LBL 88.5 HAS 16 AREAS OF CORROSION IN THE BOTTOM OF THE TRACK. REWORKED AND PROTECTED IAW SRM 53-00-52-1A-1 DETAIL VII, REV 84, AND SEAT TRACK REPLACMENT AT STATION 1100 TO 1197+120 AND 1429,TO 1444,LBL 88.5. CPC APPLIED.Oct 22, 2010 · N585HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010101800522Floorbeam · corrodedLEVEL 2 CORROSION ON FLOORBEAM TOP CHORD AT BS 654+66 - 654+100,LBL 55. BLENDED BEYOND LIMITES IAW SRM 51-10-02-00-0, REV 84. STRAP REPLACED IAW SRM 51-04-02, REV 85. CPC APPLIED.Oct 18, 2010 · N585HA · Boeing 7673G5 · Fuselage Main, Floor BeamSDR HALA2010101800515Floorbeam · corrodedLEVEL 2 CORROSION ON FLOORBEAM TOP CORD AT BS 325, LBL 55. BLENDED OUT (0.030")BEYOND SRM 53-00-51-1A.1 REV 84 LIMITS. REPAIR CARRIED OUT IAW SRM 53-00-51,FIG 201, REV 84. CPC APPLIED.Oct 18, 2010 · N585HA · Boeing 7673G5 · Fuselage Main, Floor BeamSDR HALA2010101400532Structure · corrodedGALLEY A1 UPPER AND LOWER UNITS HAVE NUMEROUS DEFECTS AND EXTENSIVE CORROSION IN EXTRUSIONS. EXTRUSIONS FABRICATED AND REPLACED IAW SELL CMM 25-38-73, REV 4, SRM 25-32-03 AND SRM D634T210 REV 84, AND AIR NZ TI190136349-0001, HAL M105 FILE NR 585167 TO UPPER FOct 14, 2010 · N585HA · Boeing 7673G5 · Fuselage Miscellaneous StructureSDR HALA2010101400513Floorbeam · corrodedLEVEL 2 CORROSION ON FLOORBEAM TOP CHORD, AT BS 654+88,LBL11 - LBL20. BLENDED AND ASSESSED BEYOND SRM 53-00-51.1A.1, REV 84 LIMITS, (0.028"). REPAIR CARRIED OUT IAW SRM 53-00-51 REV.84.Oct 14, 2010 · N585HA · Boeing 7673G5 · Fuselage Main, Floor BeamSDR HALA2010101400467Starter · failedETOPS SIGNIFICANT SYS - APU FAILED TO START UPON ARRIVAL. APU ECU BITE IAW FIM 49-11-00. NO FAULTS, NO FLAGS. TRIED APU START ATTEMPT UNSUCCESSFUL, RPM ONLY 20 PERCENT. R & R APU START ASSY. OPS CK GOOD. AMM 49-41-01. SECURED APU DOOR. APU STARTED SUCCOct 14, 2010 · N584HA · Boeing 7673G5 · APU Start/Ignition SystemSDR HALA2010101100530Bracket · crackedBRACKETS AT CTR WING UPPER SURFACE TO FRAME AT STA 852, BL 94, LT AND RT SIDES CRACKED. REPLACEMENT FITTINGS, PN 145T1928 -15-16, FABRICATED AND INSTALLED IAW AIR NZ TI190136220-0001.Oct 11, 2010 · N585HA · Boeing 7673G5 · Wing, Center BoxSDR HALA2010101100498Structure · corrodedLEVEL 2 CORROSION, ON UPPER CHORD, STA 347 BETWEEN LBL 33 TO LBL 55. BLENDED OUTSIDE LIMITS, IAW SRM 53-00-51-1A-1, REV 84. DAMAGED SECTION R & R IAW SRM 53-00-51, REPAIR 1.Oct 11, 2010 · N585HA · Boeing 7673G5 · Fuselage Structure (General)SDR HALA2010101000504Bracket · corrodedLEVEL 2 CORROSION FOUND ON BRACKET AT BS 544, S17R. FABRICATED REPLACEMENT BRACKET PN 143T8006-R, IAW DWG 143T8006, AND INSTALLED IAW SRM 51-40-02. CPC APPLIED.Oct 10, 2010 · N585HA · Boeing 7673G5 · Fuselage Main, Attach FittingsSDR HALA2010093000477Seat Track · corrodedLEVEL 2 CORROSION SEAT TRACK AT STA 1435, RBL 88.5 BEYOND LIMITS. SEAT TRACK REPLACED IAW SRM 51-40-02, REV. 84 AT RBL 88.5, STA 1324 - STA 1444. ALODINED, PRIMED, PAINTED, AND APPLIED CPC.Sep 30, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010092900446Seat Track · corrodedLEVEL 2 CORROSION ON END OF TRACK AT STA 346 LBL 88.5. REMOVED FABRICATED AND REPLACED TRACK IAW SRM 53-00-51-2R1, REPAIR 1.Sep 29, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010092900447Seat Track · corrodedLEVEL 2 CORROSION AT SEAT TRACK LBL 88.5, STA.1370. SEAT TRACK SECTION PN 146T5215-3 FABRICATED IAW DWG 146T5215. SEAT TRACK INSTALLED IAW SRM 51-40-02, REV 84.Sep 29, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010092100482Strap · corrodedLEVEL 2, CORROSION ON STRAP AT STA 927, S20R. REPLACED STRAP IAW SRM 51-40-02 REV.84 AT STA 927,S20R.Sep 21, 2010 · N586HA · Boeing 7673G5 · Fuselage Miscellaneous StructureSDR HALA2010092100445Floorbeam · corrodedLEVEL 2 CORROSION AT STA. 1540, RBL 21. REMOVED, FABRICATED FLOORBEAM AND INSTALLED IAW SRM 53-00-51-2R1, REPAIR 1.Sep 21, 2010 · N586HA · Boeing 7673G5 · Fuselage Main, Floor BeamSDR HALA2010092000483Mount · corrodedLEVEL 2 CORROSION ON GALLEY FEET MOUNTS AT STA 1588, LBL76,STA.1592 LBL45, AND RBL 45, STA.1614, RBL45. R & R FEET IAW SRM 51-10-02, REV 84.Sep 20, 2010 · N586HA · Boeing 7673G5 · Fuselage Structure (General)SDR HALA2010092000426Warning Light · false activationETOPS SIGNIFICANT SYS - FMC LIGHT STAYED ON ENTIRE FLIGHT. FINALLY WENT OUT WHEN ENGINES SHUTDOWN AT GATE. INBOUND FLT CREW REPORTED NO FMC PROBLEMS DURING FLIGHT. DID MCDP LAST FLT AND PREVIOUS FLT FAULTS AND TEST 30 IAW FIM 22-00-03-1. NO FMC FAULTS. T/S Sep 20, 2010 · N584HA · Boeing 7673G5 · Central WarningSDR HALA2010091900423Fmc · malfunctionedETOPS SIGNIFICANT SYS - DURING CRUISE BOTH FMC LOCKED UP. BOTH FMC DISPLAYED STANDBY 1. AFTER CHECKLIST FMC NORMAL. PERFORMED FIM 34-61-00/101 NO FAULT NOTED. OPS CHECK OK.Sep 19, 2010 · N584HA · Boeing 7673G5 · Flight Management Computing Hardware SystemSDR HALA2010091600487Seat Track · corrodedLEVEL 2 CORROSION AT SEAT TRACK STA 1197+132, RBL 88.5. CORROSION IN SEAT TRACK. R & R SEAT TRACK AT STA 1197+132, IAW SRM 53-00-52 REV 84.Sep 16, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091600478Slat Track · damagedNR 3 L/E SLAT INBD AUX TRACK ARM IS CRACKED IN FWD UPPER RADIUS. SLAT NR3 AUX TRACK ARM DAMAGE FOUND BEYOND LIMITS, R & R AUX TRACK ARM IAW SRM 57-43-02-1A-1, REV 84.Sep 16, 2010 · N586HA · Boeing 7673G5 · Leading Edge DevicesSDR HALA2010091600444Stringer · corrodedLEVEL 2 CORROSION AT STA 478 STRINGER 18L. CORRODED ON UNDERSIDE BEYOND SRM LIMITES. STRINGER REPAIRED IAW SRM 53-00-03, FIG. 201, REV. 84.Sep 16, 2010 · N586HA · Boeing 7673G5 · Fuselage Main, Longeron/StringerSDR HALA2010091600443Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK 1197+132, RBL 88.5. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-51.Sep 16, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091500486Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK AT STA 1090, LBL54.75, DAMAGE BEYOND LIMITS. R & R SEAT TRACK AT STA.1070 - STA.1444, LBL54.75, IAW SRM 53-00-52 REV.84. ALODINE, PRIMED AND PAINTED. CPC APPLIED.Sep 15, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091500485Seat Track · corrodedLEVEL 2 CORROSION ON FWD END OF SEAT TRACK AT STA 346, LBL 88.5. DAMAGE OUT OF LIMITES. R & R SEAT TRACK IAW SRM 51-40-02 REV.84 AT 340 LBL88.5 - STA. 423.45.Sep 15, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091500479Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK AT STA 1180, RBL 54.75. SECTION OF SEAT TRACK REPLACED IAW SRM 53-00-52 REV 84 AT RBL 54.75, STA 1070 - 1190.Sep 15, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091500442Seat Track · corrodedLEVEL 2 CORROSION ON SEAT TRACK AT STA. 1180, RBL 54.75. REMOVED AND REPLACED SECTION OF SEAT TRACK IAW SRM 53-10-51.Sep 15, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091400484Seat Track · corrodedLEVEL 2 CORROSION ON FLOOR STRUCTURE UNDER INTERCOSTAL AT STA. 654+6, LBL20. R & R SEAT TRACK IAW SRM 51-40-02, REV.84 AT LBL 20, STA. 654+66.Sep 14, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091400441Structure · corrodedLEVEL 2 CORROSION ON FLOOR STRUCTURE UNDER INTERCOSTAL AT STA. 656+66 LBL 20. REPAIRED BY REPLACEMENT OF FLOOR STRUCTURE, IAW SRM 53-10-51.Sep 14, 2010 · N586HA · Boeing 7673G5 · Fuselage Miscellaneous StructureSDR HALA2010091300481Structure · corrodedLEVEL 2 CORROSION ON NR9 SLAT AT 2 LOCATIONS ON INTERNAL STRUCTURE 60" FROM INBD END, BEHIND PANEL 673CB AND 107" FROM INBD END BEHIND 624EB. CORROSION OUT OF LIMITS. R & R SLAT INTERNAL PANEL SUPPORT STRUCTURE, IAW SRM 57-43-02-1A-1, REV. 84. R & R SLAT INTSep 13, 2010 · N586HA · Boeing 7673G5 · Leading Edge DevicesSDR HALA2010091300439Seat Track · corrodedLEVEL 2, CORROSION FOUND ON SEAT TRACK RBL 54.75, STA.344 TO 424, IN 32 AREAS. R & R SEAT TRACK, RBL 54.75 STA. 344 TO 424, IAW SRM 51-40-02.Sep 13, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010091000440Seat Track · corrodedLEVEL 2 CORROSION AT SEAT TRACK LBL 88.5, CORROSION/DAMAGE AT STA. 634,STA. 654+10 - 654+15AND STA. 654+28. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-02.Sep 10, 2010 · N586HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010090200389Computer · malfunctionedETOPS SIGNIFICANT SYS - IN CRUISE FLIGHT "FUEL USED" DISPLAY ON PROGRESS PAGE 2 WENT BLANK FUEL FLOW INDICATORS AND FUEL QTY INDICATORS BOTH TOTALIZER AND CALCULATED APPEAR NORMALLY DISPLAYED VALUE BLANK FOLLOWING MOMENTARY A/T DISCONNECT PROMPT. PERFORMED FUSep 2, 2010 · N585HA · Boeing 7673G5 · Engine Fuel Indicating SystemSDR HALA2010082300378Circuit Card · failedETOPS SIGNIFICANT SYS - L ENG OH LP 2 STATUS MESSAGE. TROUBLESHOT IAW FIM 26-11-00-1, FIG 104, PERFORMED FIRE/OVHT TEST AND TEST PASSED, NO FAULTS FOUND. ACFT OK FOR SERVICE. R & R FIRE OVER HEAT DETECTION CARD OPS CHK GOOD, OK FOR SVC.Aug 23, 2010 · N585HA · Boeing 7673G5 · Overheat DetectionSDR HALA2010082100376Transmitter · inoperativeETOPS SIGNIFICANT SYS - APU OIL QTY INOP. R & R APU OIL QUANTITY TRANSMITTER. IAW MM 49-94-04-004-001. OPS CK GOOD.Aug 21, 2010 · N586HA · Boeing 7673G5 · APU Oil SystemSDR HALA2010081700374Sensor · failedETOPS SIGNIFICANT SYS - APU AUTO SHUTDOWN ON SHORT FINAL APPROACH. RESTARTED AFTER LANDING OPS NORMAL. ACCOMP APU ECU BITE FOUND APU INLET PRESSURE (P2) SENSOR AT FAULT R & R APU INLET PRESS SENSOR IAW AMM49-61-04. OPS CKS OK FOR SVC.Aug 17, 2010 · N586HA · Boeing 7673G5 · APU Core EngineSDR HALA2010081500367Connector · dirtyETOPS SIGNIFICANT SYS - LT ENG O/H LP 2. CLEANED CONNECTORS ON LT ENG OVERHEAT/FIRE LOOPS. ENG FIRE TEST GOOD. OK FOR SERVICE.Aug 15, 2010 · N585HA · Boeing 7673G5 · Fire Protection System WiringSDR HALA2010080700354Circuit Card · malfunctionedETOPS SIGNIFICANT SYS - LT ENG O/H LP2 STATUS LIGHT. REF FIM 26-11-00, FIG 104 , RE-RACKED CARD, CYCLED ALL SYS, ALL CK GOOD.Aug 7, 2010 · N585HA · Boeing 7673G5 · Overheat DetectionSDR HALA2010073100348Transceiver · inoperativeETOPS SIGNIFICANT SYS - F/O "RA" ILLUMINATED ON HSI. REPLACED NR 2 RA TRANSCEIVER. GRD OPS CHK OK 34-33-01.Jul 31, 2010 · N585HA · Boeing 7673G5 · Ground Proximity SystemSDR HALA2010073000349Spacer · missingETOPS SIGNIFICANT SYS - ON ETOPS WALK AROUND FOUND BOTH NLG AXLE NUTS SPACERS (OUTER) MISSING. R & R LT & RT NLG TIRES & INSTALLED OUTTER SPACERS ON BOTH AXLES. SPIN CK GOOD. AMM32-45-02 & HAL CARD M296-767. OK FOR SVC. ALL SPACERS INSTALLED ON BOTH NLG AJul 30, 2010 · N586HA · Boeing 7673G5 · Main Landing Gear Strut/Axle/TruckSDR HALA2010073000342Connector · dirtyETOPS SIGNIFICANT SYS - MX LEVEL EICAS IDG OUT TEMP DISPLAYED AT TOP OF CLIMB L IDG OUT 95 IDG RISE 8, LT IDG OUT 112 IDG, RISE 23. T/S IAW FIM 24-20-00, FIG 103, CLEANED AND RESEATED CONNECTOR D4216. OPS CK GOOD.Jul 30, 2010 · N586HA · Boeing 7673G5 · Electrical Power System WiringSDR HALA2010072600338Warning Light · illuminatedETOPS SIGNIFICANT SYS - EICAS MX LEVEL MSG R PIMU R ENG EEC C2 DISPLAYED. BIT PIMUE FAULT CLEARED OK FOR SVC- NO OTHER MSGS IAW FIM 73-21-00, FIG 116.Jul 26, 2010 · N586HA · Boeing 7673G5 · Central WarningSDR HALA2010072600337Warning Light · illuminatedETOPS SIGNIFICANT SYS - MX LVL EICAS RT IDG OUT/RISE TEMPS HIGH IDG OUT L-81 R-97 IDG RISE L-7 R-20 SERVICED IDGS RAN ENGS NO FAULTS NOTED IAW FIM 24-20-00, FIG. 103.Jul 26, 2010 · N586HA · Boeing 7673G5 · Central WarningSDR HALA2010072500333Apu · malfunctionedETOPS SIGNIFICANT SYS - AFTER LANDING APU WOULD NOT START. AUTO SHUTDOWN TWICE. TEMP OK. HUNG UP AT 30 RPM AND SHUTDOWN. PERFORMED VISUAL INSP OF APU. NO DISCREPANCIES NOTED. PERFORMED ECU BITE IAW AMM 49-11-00-1, FIG 103. APU ELECTRICAL AND PNEUMATIC LOADS NJul 25, 2010 · N585HA · Boeing 7673G5 · APU Core EngineSDR HALA2010072200322Warning System · false activationETOPS SIGNIFICANT SYSTEM - RIGHT PACK INOP LIGHT ILLUMINATED EICAS MESSAGE RIGHT PACK TEMP DISPLAYED. OPERATED NORM AFTER STANDBY SELECTED. ACCMP FIM 21-51-00 FIG 103. NO FAULTS NOTED. OPERATED RIGHT PACK SEVERAL TIMES, NO FAULTS NOTED. OK FOR SERVICE. GJul 22, 2010 · N584HA · Boeing 7673G5 · Cabin Cooling SystemSDR HALA2010072000323Oil Filter · dirtyETOPS SIGNIFICANT SYSTEM - APU FAILED TO START ON 1ST ATTEMPT, APU FAULT EICAS APU START NORMAL ON 2ND ATTEMPTS. BITE ECU AND SHOWN FAULT LOW OIL PRESS. CHANGED BOTH OIL FILTERS ON APU WHICH DPS POPPED. RESET DPS, RUN APU AND OPS CHECK GOOD. NO LEAKS OR FAJul 20, 2010 · N586HA · Boeing 7673G5 · APU Oil SystemSDR HALA2010071900309Pressure Switch · malfunctionedETOPS SIGNIFICANT SYSTEM - APU AUTO SHUTDOWN AT GATE WHEN ENGINES SHUT DOWN. FIRST RESTART ATTEMPT GOOD. REMOVED AND REPLACED APU OIL PRESSURE SWITCH PER AMM 49-94-02, OPS AND LEAK CHECKS OK.Jul 19, 2010 · N586HA · Boeing 7673G5 · APU Oil SystemSDR HALA2010071700312Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - TOTAL FUEL DIFFERS FROM FMC'S CALCULATED FUEL QTY, FUEL QTY ERROR-PROG2/2 ALERT MSG DISPLAYED ON CDU AND EICAS MSG, FMC MESSAGE DISPLAYED FUEL FLOW WAS NORMAL. TOTAL FUEL 71.9, FMC CALCULATED FUEL 67.8, NO EVIDENCE FUEL LEAK. PERFOJul 17, 2010 · N586HA · Boeing 7673G5 · Flight Management Computing Hardware System
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