Boeing 767-33A

Service difficulty reports · 1,978

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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 = '76733A'
  ORDER BY difficulty_date DESC"

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SDR HALA2008122400901Starter · inoperativeETOPS SIGNIFICANT SYSTEM - BTB - LEFT ENG N2 FAILED TO ROTATE WITH STARTER IN GND START VLV LIGHT WAS EXTINGUISHED AND DUCT PRESSURE WAS NORMAL. FOUND NR 1 ENG STARTER DEFECTIVE. REPLACED STARTER PER AMM 80-11-01. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.Dec 24, 2008 · N593HA · Boeing 76733A · Engine StarterSDR HALA2008122000897Fan Blade · damagedETOPS SIGNIFICANT SYSTEM, NR 2 ENG HAS A NICK ON ONE OF THE N1 FAN BLADES. BLENDED BLADE PER AMM 72-31-02. EDDY CURRENT INSP. NO CRACKS NOTED. DIMENSIONS .093 BY 5/8 INCH IN AREA "D" OF BLADE.Dec 20, 2008 · N587HA · Boeing 76733A · Turbine Engine Compressor SectionSDR HALA2008121700893Wire · damagedETOPS SIGNIFICANT SYSTEM, STATUS MSG L ENG FIRE LP1 INTERMITTENTLY COME ON. REPAIRED WIRING AT LEFT ENG UPPER AFT DETECTOR ASSY. OPS CK OK PER FIM 26-11-00.Dec 17, 2008 · N589HA · Boeing 76733A · Fire Protection System WiringSDR HALA2008121500892Fire Warning · false indicationETOPS SIGNIFICANT SYSTEM, "L ENG FIRE LP 1" ON LOWER STATUS PAGE. PERFORMED ENG FIRE TEST. TEST OK. MESSAGE CLEARED.Dec 15, 2008 · N589HA · Boeing 76733A · Fire DetectionSDR HALA2008121500887Fmc · inoperativeETOPS SIGNIFICANT SYSTEM, AFTER FMC INITIALIZATION AT GATE. LEFT FMC BLANKED THEN DISPLAYED "FMC L OUTPUT LOSS". REPLACED RIGHT FMC, LOADED NEW SOFTWARE FROM BINDER AND CROSSLOADED TO LEFT FMC MONITORED FOR MSG. NO MSG DISPLAYED AMM 34-61-01. PERFORMED FMCDec 15, 2008 · N587HA · Boeing 76733A · Flight Management Computing Hardware SystemSDR HALA2008121400891Connector · looseETOPS SIGNIFICANT SYSTEM, STANDBY ALTIMETER HANGS UP PASSING ZERO ON CLIMB/DESCENT THEN JUMPS 300-500 FT. STANDBY ALTIMETER TESTS GOOD PER AMM 34-13-06. CLEANED AND RE-SEATED CONNECTOR. VIBRATOR OPS CK GOOD.Dec 14, 2008 · N581HA · Boeing 76733A · Navigation System WiringSDR HALA2008121400890Idg · underservicedETOPS SIGNIFICANT SYSTEM, EICAS MX LEVEL MSG L IDG OUT TEMP DISPLAYED AT TOP OF CLIMB. IDG OUT 86, 115 IDG RISE 10,11. FOUND LEFT IDG UNDERSERVICED. SERVICED IDG, TO INSP IDG NO LEAKS NOTED. T/S PER FIM 24-20-00. NO FAULTS ON BPCU BITE.Dec 14, 2008 · N581HA · Boeing 76733A · AC Generator-AlternatorSDR HALA2008121400884Transceiver · malfunctionedETOPS SIGNIFICANT SYSTEM, TRANSMISSIONS ON RT HF INTERMITTENT AT ALL STATIONS. REMOVED AND REPLACED NR 2 HF TRANSCIEVER GROUND CHECKED OK PER AMM 23-11-03.Dec 14, 2008 · N583HA · Boeing 76733A · HF Communications SystemSDR HALA2008121400883Transceiver · malfunctionedETOPS SIGNIFICANT SYSTEM, TRANSMISSIONS ON RT HF INTERMITTENT AT ALL STATIONS. REMOVED AND REPLACED NR 2 HF TRANSCEIVER GRND CHK OK PER AMM 23-11-03.Dec 14, 2008 · N583HA · Boeing 76733A · HF Communications SystemSDR HALA2008121300889Computer · malfunctionedETOPS SIGNIFICANT SYSTEM - ATB - VNAV/LNAV WOULD NOT ENGAGE WITH CENTER AUTOPILOT ENGAGED. CAPTAIN SPEED LIMIT INOP DISPLAYED ON CAPTAINS ADI. REPLACED NR 1 FMC. GND OPS CHK OK AMM 34-61-02. ACCOMPLISHED MCDP TEST 30 TEST PASS A/C OK TO REMAIN AT LMP STATUDec 13, 2008 · N587HA · Boeing 76733A · Autopilot SystemSDR HALA2008120700880Control Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT ENGINE FAILED TO START. NO ROTATION. R & R LT ENGINE STARTER CONTROL VALVE PER AMM 80-11-02 OPS AND LEAK CHK GOOD.Dec 7, 2008 · N587HA · Boeing 76733A · Engine Start Valves/ControlsSDR HALA2008120500888Keelbeam · corrodedLEVEL "2" CORROSION AT FASTENER HOLES ON KEEL LOWER CHORDS FROM STA 785.9 - 950 AND LBL 9.5 - RBL 9.5. CORROSION BLENDED OUT ON KEEL CHORDS LOWER SURFACE AROUND FASTENER HOLES IAW SRM 58-50-12/1AO1 REV 77.Dec 5, 2008 · N593HA · Boeing 76733A · Fuselage Main, KeelSDR HALA2008112600876Skin · corroded11 AREAS OF LEVEL 11 CORROSION, ON HORIZONTAL STABILIZER UPPER SURFACE OF CENTER SECTION SKIN. REWORKED IAW AIRNZ TI 190120092-0001.Nov 26, 2008 · N582HA · Boeing 76733A · Horizontal Stabilizer, Plate/SkinSDR HALA2008112500875Transceiver · failedCAPT RADAR ALTIMETER FAIL FLAG ILLUMINATED SEVERAL TIMES DURING GLT. REMOVED AND REPLACED NR 1 RADIO ALTIMETER T/R UNIT GROUND CHECK OK PER AMM34-33-01. TEST 30 PASSED ACFT REMAINS IN LAND 3 STATUS.Nov 25, 2008 · N581HA · Boeing 76733A · Ground Proximity SystemSDR HALA2008112500874Bypass Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB - APU SHUTDOWN ON TOW OUT. BITE CK ECU FOUND OIL TEMP HOT FAULT. REPLACED OIL COOLER BYPASS VALVE PER MM49-27-10 REF FIM 49-11-00.Nov 25, 2008 · N581HA · Boeing 76733A · APU Oil SystemSDR HALA2008112400869Fmc · malfunctionedETOPS SIGNIFICANT SYSTEM -ATB - MCP STUCK IN VERTICAL SPEED MODE WHILE BOTH LNAV AND VNAV INDICATE ENGAGED. UNABLE TO DISENGAGE VERTICAL SPEED. ABLE TO DISENGAGE VNAV BUT NO EFFECT ON VERTICAL SPEED MODE. CHECK LAST FLT FAULTS WITH MCDP FOUND A/T DISC FMC LNov 24, 2008 · N587HA · Boeing 76733A · Navigation SystemSDR HALA2008112300870Unknown · vibrationATB - OUT OF 18000 MSL FELT VIBRATION IN AIRFRAME. FLT CONTROLS NO VIBRATION. CONTINUED TO 25 MSL THEN SLOWED IN INTENSITY. FL 320 STILL SLIGHT VIBRATION. RETURN TO LAS. INSPECTED AIRCRAFT PANELS, FOUND SECURED INSPECTED ALL DOOR SEAL AND PRESSURIZED TO 6Nov 23, 2008 · N581HA · Boeing 76733A · Standard Practices/StructuresSDR HALA2008112200868Apu · shutdownETOPS SIGNIFICANT SYSTEM, APU AUTOSHUTDOWN AT GATE. REMOVED AND REPLACED APU PER HAL M266-767.Nov 22, 2008 · N587HA · Boeing 76733A · APU Core EngineSDR HALA2008112100866Sensor · malfunctionedETOPS SIGNIFICANT SYSTEM, APU FAULT LIGHT AND AUTO SHUTDOWN AT FL 340. RESTART AND RAN OK AT FL 300 PRIOR TO AUTO SHUTDOWN, APU DID START AND RUN FOR APPROX 10 MIN AT FL 340. PERFORMED FIM 49-11-00, NO DEFECTS NOTED. PRECAUTIONARY REPLACED AIR TEMP SENSOR PNov 21, 2008 · N587HA · Boeing 76733A · Pneumatic Distribution SystemSDR HALA2008112000865Eec · failedETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE LT ENG EEC C1 DISPLAYED. PIMU BITE SHOWS EEC CH-A/B B25 FD-BK FAIL. PERFORMED CORRECTIVE ACTION PIMU MSG INDEX AND FIM 73-21-00. REMOVED CONNECTOR FROM 2.5 BLEED VALVE AND CHECKED PINS NO TROUBLE FOUND. RESEATED CONNov 20, 2008 · N591HA · Boeing 76733A · Fuel Controlling SystemSDR HALA2008111900860Skin · puncturedOPEN - HOLE PUNCHED IN BELLY OF FUSELAGE AT STA 1777 BETWEEN STRINGERS S-36L AND S-36R. HOLE MEASURES 4" LONG BY 3" WIDE. OK TO CONTINUE PER HALM105 FILE NR 589034.Nov 19, 2008 · N589HA · Boeing 76733A · Fuselage Main, Plate/SkinSDR HALA2008111700877Panel · debondedLT WING T/E PANEL AT WS314.3 TOP SURFACE RAISED AND RIVET PULLED. SUSPECTED CORROSION UNDER PANEL. FOUND TO BE DISBOND OF COMPOSITE PANEL. REPAIRED PANEL IAW SRM 57-51-01 AND 51-70-07, PARA 5K REV 77.Nov 17, 2008 · N582HA · Boeing 76733A · Wing, Plate/SkinSDR HALA2008111700864Skin · damagedFRETTING DAMAGE ON RT WING AT RBBL 97.42 LOWER SPLICE PLATE. FRETTING DAMAGE BLENDED IAW 767 SRM 57-20-90/1AO1, THEN ROTO-PEEING 767 CM 20-10-03. SURFACE ALODINED AND PRIMED, SEALENT RE-APPLIED TO EDGES.Nov 17, 2008 · N582HA · Boeing 76733A · Wing, Plate/SkinSDR HALA2008111700854Connector · looseETOPS SIGNIFICANT SYSTEM, RT HYD PRIME PUMP ANNUNCIATED ON EICAS ASSOC SWITCHED LIGHT (PRESS) ILLUMINATED BTB. C/W FIM 29-11-00, SECURED RT ENG HYD PUMP CONNECTOR D10980, OPERATED RT ENG PER MM 71-00-00, R ENG PRIMARY PRESS LIGHT EXTINGUISHED, NO MESSAGE ON ENov 17, 2008 · N583HA · Boeing 76733A · Hydraulic Power System WiringSDR HALA2008111400853Totalizer · reads highTOTALIZER FUEL DISAGREES WITH CALCULATED FUEL ON BOTH CDU'S. CALCULATED FUEL SHOWS HIGHER AND INCREASES AS FLIGHT PROGRESSED. CDU TOTALIZER FUEL AGREES W/FUEL GAUGE. PERFORMED FIM 28-41-00 SYS IS OK.Nov 14, 2008 · N581HA · Boeing 76733A · Fuel Indicating SystemSDR HALA2008111400849Adapter · crackedRT ENGINE GEAR BOX STARTER MOTOR ADAPTER PLATE CRACKED HORIZONTALLY IN TWO POSITIONS ACROSS TOP AND BOTTOM OF ADAPTER. POSSIBLE FATIGUE CAUSED BY IMBALANCE OF STARTER FAILURE. REPLACED IAW ENGINE MANUAL, SUBTASK 72-61-00-430-061.Nov 14, 2008 · N581HA · Boeing 76733A · Turbine Engine Accessory DriveSDR HALA2008111300848Skin · corrodedHORIZONTAL STABILIZER CENTER SECTION LOWER SKIN EXTERNAL SURFACE CORRODED AT LBL 3.3 AND RBL 6.5 AT REAR SPAR. BLEND REPAIR IAW SRM 55-10-01 FIG 101 AND ANZ TI 190119901-0001.Nov 13, 2008 · N581HA · Boeing 76733A · Horizontal Stabilizer, Plate/SkinSDR HALA2008111300847Support Angle · corrodedFAIRING 139C SUPPORTING CROSSMEMBER CORRODED AROUND SWAGE NUTS, CROSSMEMBER (P/N:145T8629-2). REPLACED, PAINT AND CPC APPLICATION PRIOR TO RE-INSTALLATION.Nov 13, 2008 · N581HA · Boeing 76733A · Aerodynamic FairingsSDR HALA2008111300846Keelbeam · corrodedCORRISION ON KEEL BEAM STA 920. REMOVED IAW SRM 53-50-12, OPEN HOLE INSPECTION FPI, ROTO REEMED, PAINT CPC.Nov 13, 2008 · N581HA · Boeing 76733A · Fuselage Main, KeelSDR HALA2008111300845Keelbeam · corrodedCORRISION, TOP SURFACE OF KEELBEAM RT INNER FAIRING ATTACHMENT FLANGE AT STA 965. CORRISION REMOVED IAW SRM 53-50-12 FPI, OPEN HOLE INSPECTION, ROTO REEMED, PART AND CPC APLICATION.Nov 13, 2008 · N581HA · Boeing 76733A · Fuselage Main, KeelSDR HALA2008111200850Lamp · inoperativeETOPS SIGNIFICANT SYSTEM, APU SQUIB WOULD NOT TEST. RELAMPED APU SQUIB TEST SWITCH. OPS OK, TEST OK.Nov 12, 2008 · N580HA · Boeing 76733A · Extinguishing SystemSDR HALA2008111100843Seat Track · damagedTHE B-ZONE, SEAT TRACK AT RBL 11 STN 545 HAS DAMAGE TO TOP OF TRACK BEYOND REPAIR LIMITS. DEPTH MEASURED AFTER BLEND AT 0.052 INCH (SRM LIMIT 0.020). DAMAGED SECTION OF TRACK CUT & REMOVED IAW SRM 53-00-52 FIG 201 REPAIR 1. REPAIR PARTS FABRICATED IAW SRM 5Nov 11, 2008 · N581HA · Boeing 76733A · Fuselage, Seat/Cargo Attach FittingsSDR HALA2008110400840Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM - DURING CLIMB OUT TCAS FAIL LIGHT ILLUMINATED WENT OUT APPROX 2HRS LATER WORKED FINE FOR REST OF FLIGHT. PERFORMED BITE CHECK PER FIM 34-45-00, SYSTEM CHECKS OK TO CONTINUE.Nov 4, 2008 · N593HA · Boeing 76733A · Air Collision Avoidance SystemSDR HALA2008110300837Oil Filter · unknownETOPS SIGNIFICANT SYSTEM - L OIL FILTER ADVISORY LIGHT EICAS MESSAGE L OIL FILTER. DISAPPEARED WITH THRUST REDUCTION, ADVISORY REMAINED. ACCMP FIM TASK 79-35-00, REPLACED THE MAIN OIL FILTER, RAN ENG OPER NORMAL. LEAK CHECKED OK PER AMM 79-21-05/401.Nov 3, 2008 · N591HA · Boeing 76733A · Engine Oil Distribution (Airframe Furnished)SDR HALA2008103100833Generator · malfunctionedETOPS SIGNIFICANT SYSTEM - PER FLT CREW APU GEN FELL OFF LINE. REMOVED & REPLACED APU GENERATOR PER MM 24-21-01-424-002 REF LOG PAGE 272631 ITEM 94 FOR VERIFICATION FLT.Oct 31, 2008 · N582HA · Boeing 76733A · AC Generator-AlternatorSDR HALA2008102600829Battery · unknownETOPS SIGNIFICANT SYSTEM - UPON PUSHBACK BEFORE ENG START APU AUTO SHUT DOWN. REMOVED & REPLACED APU BATTERY PER AMM24-31-04. OPS CHECK OK. PERFORMED APU ECU BITE CK. NO FAULTS NOTED. OK FOR SERVICE. FOUND NO APU ELECTRICAL. REPLACED APU GCU PER AMM24-2Oct 26, 2008 · N582HA · Boeing 76733A · Battery/Charger SystemSDR HALA2008102300832Keelbeam · corrodedCORROSION ON KEEL BEAM AT PANEL FIXING ANCHOR NUT AT BS 933. CORROSION BLENDED IAW SRM 53-50-12 FIG 101, SHEET 10. WORKED AREA, ROTO PEENED IAW SRM 51-20-06 & PAINTED IAW SRM 51-20-01.Oct 23, 2008 · N580HA · Boeing 76733A · Fuselage Main, KeelSDR HALA2008102300831Keelbeam · corrodedCORROSION ON KEEL BEAM AT PANEL FIXING ANCHOR NUT AT BS 933. CORROSION BLENDED IAW SRM 53-50-12 FIG 101 SHEET 10. WORKED AREA, ROTO PEENED IAW SRM 51-20-06 & PAINTED IAW SRM 51-20-01.Oct 23, 2008 · N580HA · Boeing 76733A · Fuselage Main, KeelSDR HALA2008102300823Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - RETURNED TO GATE. RIGHT ENGINE STARTER FAILED TO ACCELERATE PAST N2 10 PERCENT. MAINT REQUESTED TO EXAMINE PROBLEM. REMOVED AND REPLACED STATER ASSY PER AMM 80-11-01. OPS CHECK OK.Oct 23, 2008 · N581HA · Boeing 76733A · Engine StarterSDR HALA2008102300814Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - RETURNED TO GATE. RIGHT ENGINE STARTER FAILED TO ACCELERATE PAST N2 10 PERCENT. MAINT REQUESTED TO EXAMINE PROBLEM. REMOVED AND REPLACED STARTER ASSY PER AMM 80-11-01. OPS CHECK OK.Oct 23, 2008 · N581HA · Boeing 76733A · Engine StarterSDR HALA0800817Clamp · looseETOPS SIGNIFICANT SYSTEM - LT DUCT LEAK. FOUND LOOSE CLAMP ON HEAT EXCHANGER DUCT, RESECURED CLAMP. OPS CHECK, LEAK CHECK GOOD PER AMM 21-51-02 AND 21-51-00.Oct 17, 2008 · N583HA · Boeing 76733A · Air Distribution SystemSDR HALA0800811Processor · malfunctionedETOPS SIGNIFICANT SYSTEM - OVERHEAD FUEL QUANTITY TOTALIZER INTERMITTENT. ACCOMPLISHED BITE OF FQ PROCESSOR PER FIM 28-41-00 FIG 104 PROCESSOR FAULTED. REPLACED PROCESSOR PER AMM 28-41-08. OPS CHECK OK.Oct 16, 2008 · N587HA · Boeing 76733A · Fuel Quantity SensorSDR HALA0800617Channel · crackedTHE VERTICAL U-CHANNEL IS CRACKED AT AFT INBOARD EDGE OF NR 2 ENG PYLON, 7: INBOARD OF THE DIAGONAL BRACE AFT MOUNT FITTING. REMOVED AND REPLACED VERTICAL U-CHANNEL AT AFT INBOARD EDGE OF NR 2 ENG PYLON PER SRM 54-53-70/ 101 AND SRM 51-70-11-06-0 FIG 1. (S)Jun 3, 2008 · N589HA · Boeing 76733A · Nacelle/Pylon Miscellaneous StructureSDR HALA0800602Unknown · odorELECTRICAL ODOR IN COCKPIT AND MID GALLEY. TURNED OFF UTILITY BUSSES ODOR DISIPATED. ATB TO SEA. PERFORMED THE FOLLOWING TEST WITH APU, ENGINES 1 AND 2 PACKS AND RECIRC FANS ON AND RUNNING. IFE OPS CHECK (23-34-00-715-001)GALLEY OPS TEST (25-31-03-764-020)May 24, 2008 · N581HA · Boeing 76733A · Air Distribution SystemSDR HALA0800600A/C Pack · malfunctionedETOPS SIGNIFICANT SYSTEM, PACK INOP LIGHT ILL EICAS MESSAGE L PACK TEMP DISPLAYED. OPERATED NORMAL AFTER STBY SELECTED. BITE CHECK LEFT PACK, NO FAULTS NOTED. RESET LEFT PACK GND, OPS CHECK OK.May 22, 2008 · N593HA · Boeing 76733A · Cabin Cooling SystemSDR HALA0800601Antenna · failedETOPS SIGNIFICANT SYSTEM, WXR FAIL DISP ON HSI (CAPT AND F/O) WITH BOTH SYS 1 AND SYS 2 SELECTED WXR TEST NOT ATTEMPTED. REPLACED WXR ANT DRIVE. GND OPS CHK OK 34-43-05.May 22, 2008 · N593HA · Boeing 76733A · Weather Radar SystemSDR HALA0800593Rib · crackedCRACK, JUST INBOARD OF VENT BOX, RIGHT WING FIXED T/E FORE AND AFT RIB. REPAIRED RIGHT WING FIXED T/E RIB I/B OF VENT BOX. ALL WORK ACCOMPLISHED PER SRM 51-20-11-OG-0 AND SRM 51-40-01-OG-0.May 17, 2008 · N581HA · Boeing 76733A · Wing, Rib/BulkheadSDR HALA0800592Stiffener · crackedCRACK ON RIGHT WING FIXED T/E, JUST FORWARD OF O/B AILERON LENGTH WISE STIFFENER. REPAIRED RIGHT WING T/E, JUST FWD OF O/B AILERON STIFFENER PER SRM 51-20-11-OG-0, AND SRM 51-01-OG-0.May 17, 2008 · N581HA · Boeing 76733A · Wing StructureSDR HALA0800591Seal · tornBLADE SEAL TORN ON RIGHT WING O/B AILERON UPPER BLADE. REPLACED UPPER BLADE SEAL ON RIGHT WING O/B AILERON AT TORN AREA IAW SRM 51-40-02-OG-0.May 17, 2008 · N581HA · Boeing 76733A · Wing Miscellaneous StructureSDR HALA0800590Skin · damagedRIVETS SHEARED ON RIGHT WING FIXED T/E UPPER SURFACE (9). REMOVED AND REPLACED SHEARED RIVETS ON RIGHT WING FIXED T/E UPPER SURFACE PANEL IAW SRM 51-40-04-OG-O.May 16, 2008 · N581HA · Boeing 76733A · Wing, Plate/Skin
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