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"

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SDR HALA2009122600605Warning Light · false indicationETOPS SIGNIFICANT SYS - RUDDER RATIO LIGHT ILLUMINATED INFLT EICAS MSG RUDDER RATIO DISPLAYED. TESTED IAW FIM 27-21-00, FIG 104, BLOCK 31 AND FIM 27-0900, FIG 103, SHEET 2, BLOCK 53 RUDDER RATIO CHECKS OK.Dec 26, 2009 · N586HA · Boeing 7673G5 · Rudder Control SystemSDR HALA2009122600604Transceiver · malfunctionedETOPS SIGNIFICANT SYS - SFO REPORTS RT HF RADIO (8643HZ) VERY HARD TO RECEIVE TRANSMISSIONS. LT HF OK. PERFORMED BITE OF LT AND RT HF TRANSCEIVERS. NO FAULTS NOTED. CONTACTED SFO FREQ 5574. LT AND RT HF HAVE GOOD CONTACT. LT SIDE 3X3 RT SIDE 3X4. NO HF Dec 26, 2009 · N586HA · Boeing 7673G5 · HF Communications SystemSDR HALA2009122100597Control Valve · faultedETOPS SIGNIFICANT SYS - RT PACK TEMP LIGHT CAME ON IN FLIGHT(EICAS), (PACK OFF LIGHT). FOLLOW QRH, OPERATED RT PACK CONTROL SELECTOR IN STBY-N. BITE CHECK PACK CONTROL BOX FOUND TEMP CONTROL VALVE FAULT. REMOVED AND REPLACED PACK TEMP CONTROL VALVE IAW AMM Dec 21, 2009 · N584HA · Boeing 7673G5 · Cabin Cooling SystemSDR HALA2009122100596Control Valve · faultedETOPS SIGNIFICANT SYS - RT PACK TEMP LIGHT CAME ON IN FLIGHT(EICAS), (PACK OFF LIGHT). FOLLOW QRH, OPERATED RIGHT PACK CONTROL SELECTOR IN STBY-N. BITE CHECK PACK CONTROL BOX FOUND TEMP CONTROL VALVE FAULT. REMOVED AND REPLACED PACK TEMP CONTROL VALVE IAW AMMDec 21, 2009 · N584HA · Boeing 7673G5 · Cabin Cooling SystemSDR HALA2009122100595Warning Message · illuminatedETOPS SIGNIFICANT SYS - EICAS STATUS MSG ELEV FEEL DISPLAYED. ACCOMPLISHED FIM 27-31-00 FIG 106 NO FAULTS DISPLAYED. OK FOR SERVICE.Dec 21, 2009 · N584HA · Boeing 7673G5 · Central WarningSDR HALA2009121900593Transponder · warning messageETOPS SIGNIFICANT SYS - TCAS DISPLYS NR 1 TRANSPONDER DATA BUSS MESSAGE AND CAPT/ FO USI TCAS FAIL FLAG DISPLAYED. NR 2 ATC SWITCH RESTORES NORMAL OPERATION. CYCLED PWR TO TCAS SYS. GND OPS CHECK OK.Dec 19, 2009 · N584HA · Boeing 7673G5 · Flight Management Computing Hardware SystemSDR HALA2009121800594A/C Pack · false indicationETOPS SIGNIFICANT SYS - RT PACK TEMP LIGHT ILLUMINATES INTERMITTENTLY INFLIGHT AND ON THE GRD IN AUTO ONLY. BITE CHECK COMPLETED ON RT PACK TEMP CONTROLLER. NO FAULTS NOTED. VERIFY/RESET COMPLETED ON CONTROLLER. ALL INDICATIONS NORMAL DURING TRANSIT. OK FODec 18, 2009 · N584HA · Boeing 7673G5 · Cabin Cooling SystemSDR HALA2009121300579Controller · malfunctionedETOPS SIGNIFICANT SYS - R PACK LIGHT ILLUM. EICAS MSG R PACK TEMP DISPLAYED, OPERATED NORM AFTER STBY SELECTED. TROUBLSHOT IAW FIM 21-51-00/101 BIT AND PREVIOUS FOUND FAULTS ON CONTROLLER FAULT "TEMP CONT VLV" PERFORMED STEPS OF FIG 103 SH 5. VERIFIED FAULT Dec 13, 2009 · N584HA · Boeing 7673G5 · Cabin Cooling SystemSDR HALA2009120600571Altimeter · stickingETOPS SIGNIFICANT SYS - STANDBY ALTIMETER STICKING. JUMPS 500-700 FEET. USUALLY 900 FT ON CLIMB. REPLACED STANDBY ALTIMETER OPS CHECK OK IAW MM 34-13-06.Dec 6, 2009 · N586HA · Boeing 7673G5 · Altimeter, Barometric/EncoderSDR HALA2009120600568Generator · failedETOPS SIGNIFICANT SYS - ON ENG START RT GEN FAILED. PERFORMED FIM 24-20-00/101. NO FAULTS ON BPCU BITE. RAN ENG UNDER LOAD, NO FAULTS NOTED. RT GEN OK FOR SERVICE.Dec 6, 2009 · N584HA · Boeing 7673G5 · AC Generation SystemSDR HALA2009120400570Computer · inoperativeETOPS SIGNIFICANT SYS - FD FLAG IN VIEW AND NO FD CMD BARS ON CAP'S ADI. INSTR INDICATION NORMAL W/INSTR SOURCE SEL AT C POS. NO LAND 3 DISPLAYED REMOVED AND REPLACED LT FCC AND OPS CKD OK IAW AMM 22-11-01-004-001 AND 22-11-01-404-007. RAN A TEST 40 AND PASDec 4, 2009 · N586HA · Boeing 7673G5 · Autopilot ComputerSDR HALA2009120400566Start Valve · malfunctionedETOPS SIGNIFICANT SYS -RT ENG STARTER INDICATION VALVE LIGHT ON. REPLACED RT ENG START VALVE IAW AMM 80-11-02. OPS CHECK OK. COWLING CLOSED AND SECURED. SECURED.Dec 4, 2009 · N585HA · Boeing 7673G5 · Engine Start Valves/ControlsSDR HALA2009120300562Software · malfunctionedETOPS SIGNIFICANT SYS - AFTER T/O LOSS FLIGHT PLAN ROUTE ON BOTH FMC, NO WAYPOINTS ON LEGS PAGE ACTIVATED ROUTE 2 WHICH HAD A COPY OF ROUTE 1 CONTINUED BUT NO ETA OR FUEL PREDICTIONS FOR EACH WAYPOINT ON LEG PAGE AND PREVIOUS PAGE. PREFORMED OPS TEST AND SYS Dec 3, 2009 · N585HA · Boeing 7673G5 · Flight Management Computing Software SystemSDR HALA09F00135Fmc · malfunctionedETOPS SIGNIFICANT SYS - AFTER T/O LOSS FLIGHT PLAN ROUTE ON BOTH FMC, NO WAYPOINTS ON LEGS PAGE ACAVATED ROUTE 2 WHICH HAD A COPY OF ROUTE 1 CONTINUED BUT NO ETA OR FUEL PREDICTIONS FOR EACH WAYPOINT ON LEG PAGE AND PREVIOUS PAGE. PREFORMED OPS TEST AND SYS TDec 3, 2009 · N585HA · Boeing 7673G5 · Flight Management Computing Software SystemSDR HALA2009120100556Start Valve · malfunctionedETOPS SIGNIFICANT SYS - ON ENG START RT START FAILED TO OPEN. (STARTER VALVE LIGHT ON BUT DID NOT GO OUT.) STARTED LT ENG OK. RESTART RT ENG AFTER RECYCLING ISOLATION VALVE, OK. OPS CHECK RT START VALVE IAW 80-11-00-705 GOOD.Dec 1, 2009 · N585HA · Boeing 7673G5 · Engine Start Valves/ControlsSDR HALA2009120100555Cdu · malfunctionedETOPS SIGNIFICANT SYS - ACTIVE RTE 1 CDU FAILED 2HRS 20 MIN INTO FLIGHT. (BOTH CDU'S). PERFORMED FMS BITE PROCEDURE IAW FIM 34-61-00-1. CHECK NORMAL.Dec 1, 2009 · N586HA · Boeing 7673G5 · Flight Management Computing Hardware SystemSDR HALA2009112800554Aileron Sys · malfunctionedETOPS SIGNIFICANT SYS - AIL LOCK LIGHT ILLUMINATED AT LOW SPEED. EICAS MESSAGE AILERON LOCKOUT DISPLAYED. OTBD AILERONS DID NOT INDICATE MOVEMENT. AT FLAPS 20 MESSAGE CLEARED. TROUBLESHOT IAW FIM 27-11-00 FIG 104 SHEET 3 BLOCK 67. THE SYS IS OK OPS CHECK NORNov 28, 2009 · N585HA · Boeing 7673G5 · Aileron Control SystemSDR HALA2009112600549Display · malfunctionedETOPS SIGNIFICANT SYS - PRIOR TO ENGINE START RT ENGINE N2 DISPLAY DOES NOT INDICATE MIN FUEL INTRODUCTION MAGENTA LINE. ON ARRIVAL AT SFO MAGENTA LINE WAS INDICATING ON N2. PERFORMED EICAS BITE IAW FIM 31-41-00-1. NO FAULTS. ON ENG START AND TAXI OVER TO THNov 26, 2009 · N585HA · Boeing 7673G5 · Central DisplaySDR HALA2009112500548Radio Altimeter · faultedETOPS SIGNIFICANT SYS - RA FLAG DISPLAYED STEADY ON CAPT'S ADI. REMOVED AND REPLACED NR 1 RADIO ALTIMETER UNIT GND CK OK IAW AMM34-33-01. MCDP GND TEST 30 PASSED IAW LMP COMPLIANCE REF FIM 22-0003.Nov 25, 2009 · N586HA · Boeing 7673G5 · Ground Proximity SystemSDR HALA2009112300538Transceiver · intermittentETOPS SIGNIFICANT SYS - TRANSMISSION ON RT HF IS INTERMITTENT AND NO SIDE TONE AT ALL STATIONS. TROUBLESHOT IAW FIM 23-11-00. VERIFIED VOICE. SIDE TONE, AND DATA OPERATIONS. ALL OK. PERFORMED BITE RT HF TRANCEIVER IAW 23-12 FIM. NO FAULTS EXIST.Nov 23, 2009 · N584HA · Boeing 7673G5 · HF Communications SystemSDR HALA2009112200537Transceiver · malfunctionedETOPS SIGNIFICANT SYS - RT HF WILL RECEIVE BUT UNABLE TO TRANSMIT. WILL NOT RECEIVE DATA. TROUBLESHOT IAW FIM 23-11-00. ALL OPS CHECKS NORMAL IN TRANSMIT/RECEIVE/DATA RECEIVE. OK FOR SERVICE.Nov 22, 2009 · N584HA · Boeing 7673G5 · HF Communications SystemSDR HALA2009112100540Connector · dirtyETOPS SIGNIFICANT SYS - MX STATUS MESSAGE "R IDG TEMP SENSE". INSPECTED AND CLEANED IDG RECEPTACLE AND PLUG. NO DEFECTS NOTED. OPS CK OK, NO MAINT STATUS MESS. OK FOR SERVICE IAW FIM 24-20-00/101.Nov 21, 2009 · N586HA · Boeing 7673G5 · Electrical Power System WiringSDR HALA2009112100539Transceiver · intermittentETOPS SIGNIFICANT SYS - RA FLAG DISPLAYED INTERMITTENT ON THE CAPT ADI. REPLACED RADIO ALTIMETER TRANSCEIVER IAW AMM 34-33-01.Nov 21, 2009 · N585HA · Boeing 7673G5 · Ground Proximity SystemSDR HALA2009112100536Transceiver · malfunctionedETOPS SIGNIFICANT SYS - HF2 WILL NOT TUNE TO 8843 (OR A NR OF OTHER FREQS IN 8000 RANGE) EACH TIME TRANSMIT BUTTON IS PUSHED THE TUNING TONE SOUNDS OFF FOR 15 SECONDS HF2 DOES RECEIVE IN THIS RANGE INCLUDING SEL CAL BUT DATA MODE DID NOT WORK. DID OPS CHECK ONov 21, 2009 · N584HA · Boeing 7673G5 · HF Communications SystemSDR HALA2009111900533Electronic Unit · inoperativeETOPS SIGNIFICANT SYS - FLAP/SLAT ELECTRIC STATUS MESSAGE DISPLAYED. FOUND FLAP SLAT ELECTRIC UNIT INOP- UNABLE TO BITE. REMOVED AND REPLACED FLAP SLAT ELECTRONIC UNIT IAW AMM 27-51-01-024-001. OPS CHECK GOOD.Nov 19, 2009 · N586HA · Boeing 7673G5 · Trailing Edge Flap Control SystemSDR HALA2009111700531Trim System · malfunctionedETOPS SIGNIFICANT SYS - 5 UNITS RUDDER TRIM REQUIRED IN NOSE DIRECTION WHILE IN CRUISE, 265 KTS, 6.5 UNITS RUDDER TRIM REQUIRED IN NOSE RT WHILE IN CLIMB AT 300KTS. INFO NOTED MOC AND TECH SVC NOTIFIED. OK FOR SERVICE IAW AMM 27-01-00-501.Nov 17, 2009 · N585HA · Boeing 7673G5 · Rudder Tab Control SystemSDR HALA2009111300525Throttle · misalignedETOPS SIGNIFICANT SYS - FRM 73032501 IN CRUISE FL300 A/C THROTTLES ARE MISALGINED 7/8 OF KNOB DIFFERENCE TO GET ENG PARAMETERS THE SAME WE ADJUSTED LT SIDE IT WAS 7/8 BEHIND R SIDE. INFO NOTED MOC NOTIFIED ACCOMP FIM 73-21-00 FIG 107 BITE PIMU LT AND RT OK INov 13, 2009 · N586HA · Boeing 7673G5 · Power LeverSDR HALA2009111300524Throttle · misalignedETOPS SIGNIFICANT SYS - FRM 73032501 IN CRUISE FL300 ACFT THROTTLES ARE MISALGINED 7/8 OF KNOB DIFFERENCE TO GET ENG PARAMETERS THE SAME, ADJUSTED LT SIDE IT WAS 7/8 BEHIND R SIDE. INFO NOTED MOC NOTIFIED ACCOMP FIM 73-21-00 FIG 107 BITE PIMU LT AND RT OK IANov 13, 2009 · N586HA · Boeing 7673G5 · Power LeverSDR HALA2009111000518Track · obstructedR4 SLIDE WILL NOT ARM. CLEARED DEBRIS FROM DOOR TRACK, SLIDE R4 ARMS NORMALLY.Nov 10, 2009 · N586HA · Boeing 7673G5 · Escape SlideSDR HALA2009110800513Indicator · faultedETOPS SIGNIFICANT SYS - F/O'S RADIO ALTIMETER 'AMBER' RA ON HSI AND NO AUTO DISPLAYED ON AUTOLAND STATUS. TROUBLESHOT IAW FIM 34-33-00/101 FOUND SINGLE INTERMITTENT FAULT NO CORRECTED ACTION RECOMMENDED "FIG 104 SHEET 3 BLOCK 23. PERFORMED TEST 40. TEST PASS.Nov 8, 2009 · N586HA · Boeing 7673G5 · Ground Proximity SystemSDR HALA2009110400505Autothrottle Sys · malfunctionedETOPS SIGNIFICANT SYS - BTB- ABORTED TAKEOFF AT APPROX 75KTS DUE TO AUTO THROTTLE NOT ENGAGEING. ON TAXI BACK TO GATE, ENGAGED OK. PERFORMED MCDP TEST 2, 10,30 AND NO FAULTS NOTED. COMPLETED BRAKE CHECK, NR 1 AND 2 ENG TEST 3 AND PERFORMED THE ETOPS * ITEMSNov 4, 2009 · N585HA · Boeing 7673G5 · Autopilot SystemSDR HALA2009110400503Display · inoperativeETOPS SIGNIFICANT SYS - F/O'S MCDU WENT BLANK AFTER ENGINE SHUTDOWN. REPEAT WRITE UP. REPLACED F/O'S MCDU IAW AMM 34-61-02.Nov 4, 2009 · N586HA · Boeing 7673G5 · Flight Management Computing Hardware SystemSDR HALA2009110100499Transceiver · failedETOPS SIGNIFICANT SYS - RA FLAG ON F/O ADI. RT RADIO ALT TRANSCEIVER FAILS BITE. REMOVED AND REPLACED TRANSCEIVER IAW AMM 34-33-01. TEST NRML.Nov 1, 2009 · N586HA · Boeing 7673G5 · Ground Proximity SystemSDR HALA2009103100500Packing · leakingETOPS SIGNIFICANT SYS - ATB - DURING FLIGHT RECEIVED LOW QTY CTR HYD SYS-IAW QRH TURNED OFF CTR SYS. C HYD QTY DECREASED TO .12 UPON LANDING. REMOVED AND REPLACED PACKING DPI PRESSURE FILTER CTR SYS, OPS AND LEAK CHECK GOOD. RE-SERVICED CTR HYD SYS IAW AMM12Oct 31, 2009 · N585HA · Boeing 7673G5 · Hydraulic Indicating SystemSDR HALA2009102800490Connector · damagedETOPS SIGNIFICANT SYS - EICAS MSG 'L GEN DRIVE' DISPLAYED INTERMITTENTLY BELOW 15,000 FT IDG OUT/ RISE TEMPS WERE NORMAL55/11 DEGREES. REPLACED LT ENG IDG IAW AMM TASK 24-11-01-004-001 AND 24-11-01-404-34. NO HELP. T/S IAW WDM 24-11-11 FOUND PIN 6 OF CONNECOct 28, 2009 · N585HA · Boeing 7673G5 · Engine Indicating System WiringSDR HALA2009102800489Connector · damagedETOPS SIGNIFICANT SYSTEM - EICAS MSG 'L GEN DRIVE' DISPLAYED INTERMITTENTLY BELOW 15,000 FT IDG OUT/ RISE TEMPS WERE NORMAL55/11 DEGREES.//REPLACED LT ENG IDG IAW AMM TASK 24-11-01-004-001 AND 24-11-01-404-34. NO HELP. T/S PER WDM 24-11-11 FOUND PIN 6 OF CONNEOct 28, 2009 · N585HA · Boeing 7673G5 · Electrical Power System WiringSDR HALA2009102700489Idg · malfunctionedETOPS SIGNIFICANT SYS - LT GEN DRIVE EICAS AND LT DRIVE LIGHT CAME STEADY THEN WENT OUT ABOUT 30 NM FROM AIRPORT. LIGHTS CAME ON TWICE(10-20 SEC) THEN OUT, PRIOR TO ANY DISCONNECT. DID A BITE CHECK FOR THE BPCU, NO FAULTS FOUND. DELTA P PRESS CK'S NML. CHEOct 27, 2009 · N585HA · Boeing 7673G5 · Alternator-Generator DriveSDR HALA2009102600481Idg · warning lightETOPS SIGNIFICANT SYSTEM - INFO TO MAINT LEFT GEN DRIVE LIGHT ON FINAL - BEFORE DISCONNECTING LIGHT WENT OFF. PER TASK 24-11-00-745-001 BITE OF BPCU SHOWED SERVICE IDG. SERVICED IDG PER OVERNIGHT CHECK CARD M271-767. RAN LT ENGINE AT GATE-IDG DRIVE LIGHT OPOct 26, 2009 · N585HA · Boeing 7673G5 · Alternator-Generator DriveSDR HALA2009102600479Test Panel · malfunctionedLT EMERGANCY ESCAPE TEST 1, SLIDE ON P.61 PANEL WILL NOT TEST. REMOVED AND REPLACED SQUID TEST PANEL PER AMM 26-21-04, OPS CHECK OK. OK FOR SERVICE.Oct 26, 2009 · N584HA · Boeing 7673G5 · Fire Protection SystemSDR HALA2009102200473Iru · out of alignmentETOPS SIGNIFICANT SYSTEM - UNABLE RNP ANNUNCIATED EICAS. RAN QRH CHECKLIST, MSG REMAINED TIL ENGS SHUTDOWN AT GATE. PERFORMED REALIGNNENT OF IRU'S. REALIGNMENT CHKS OK AND ALL 3 IRU'S GME LOCATION OK RAN ENG'S MSG DID NOT RETURNED, A/C OK FOR SERVICE.Oct 22, 2009 · N586HA · Boeing 7673G5 · Inertial Guidance SystemSDR HALA2009100400449Irs · faultedETOPS SIGNIFICANT SYS - R IRS FAULT.F10 SELECTED IRS ALT AND COMPLIED WITH Q RT. PERFORMED BITE TEST IAW FIM 34-20-00, FIG 107. OPS NML. ACCOMPLISHED TEST 30 IAW 22-00-02 NO FAULTS.Oct 4, 2009 · N586HA · Boeing 7673G5 · DME/TACAN SystemSDR HALA2009092900442Blade · damagedETOPS SIGNIFICANT SYS - ON ETOPS 2 CHK FOUND ENGINE NR 2 BLADE NR 27 WITH NICK 0.500 LONG, 0.200 DEEP. ON NR 2 ENG - BLENDED FAN BLADE IAW AMM 74-31-02. OK FOR SERVICE.Sep 29, 2009 · N585HA · Boeing 7673G5 · Turbine Engine Compressor SectionSDR HALA2009092600440Engine · malfunctionedETOPS SIGNIFICANT SYS - N1 SLOW TO INDICATE DURING START NR 2 POS. PERFORMED START OF NR 2 ENG AT GATE, START OPS NORMAL IAW AMM 73-21-00.Sep 26, 2009 · N585HA · Boeing 7673G5 · Power Indicating SystemSDR HALA2009092500438Engine · leakingETOPS SIGNIFICANT SYS - SMALL AMOUNT OF OIL FOUND PUDDLING IN NR 1 ENG INLET COWL. JUST UNDER SPINNER CONE. OIL LEAK OK AND WITHIN LIMITS IAW AMM71-00-00-795-003 PD10. PERFORMED GROUND IDLE TEST 71-00-00-120. NO FURTHER LEAKS FOUND. OK FOR SVC.Sep 25, 2009 · N586HA · Boeing 7673G5 · Turbine Engine Oil SystemSDR HALA2009092400434Fire Warning · false activationETOPS SIGNIFICANT SYS -BTB -R ENG FIRE LP2 EICAS DISPLAYED AFTER ENGINE START. PERFORMED TROUBLESHOOTING IAW FIM 26-11-00/101, FIG 104. PERFORMED OPS CHECK, NORMAL.Sep 24, 2009 · N585HA · Boeing 7673G5 · Fire DetectionSDR HALA2009092100431Wire · brokenETOPS SIGNIFICANT SYSTEM - LT DUCT LEAK WILL NOT TEST. T/S PER FIM 26-18-00-1 FOUND WIRE BROKEN AT CONNECTOR D10586 REPLACED AND RESECURED CONNECTOR D10586. LT DUCT LEAK TEST NORMAL- OKAY TO CONTINUE.Sep 21, 2009 · N584HA · Boeing 7673G5 · Fire Protection System WiringSDR HALA200909150407Charger · failedETOPS SIGNIFICANT SYSTEMS - APU AUTO SHUTDOWN FRM 49111600. REMOVED AND REPLACED APU MAIN BATTERY PER AMM 24-31-04. REMOVED AND REPLACED APU BATTERY CHARGER PER AMM 24-31-05. OPS CHECK OK. NO FAULT NOTED. APU STARTED ON FIRST ATTEMPT.Sep 15, 2009 · N585HA · Boeing 7673G5 · Airborne Auxiliary Power Unit (APU) SystemSDR HALA2009082800389Ecu · faultedETOPS SIGNIFICANT SYS - APU FAILED TO START. APU FAULT EICAS MSG DISPLAYED AND APU FAULT DISCRETE ILLUM WHEN START SW SELECTED OFF. APU BITE FAULTS ECU. REPLACED APU ECU IAW AMM 49-61-05-404-008. APU CKS OK.Aug 28, 2009 · N584HA · Boeing 7673G5 · APU Start/Ignition SystemSDR HALA2009082700390Engine · leakingETOPS SIGNIFICANT SYS - ON PREFLT FOUND OIL PUDDLE 6 OCLOCK POSITION LT ENG. PERFROMED GROUND TEST AT IDLE POWER IAW AMM 71-00-00 TEST NR 3. TEST OK. NO OIL LEAKS NOTED. OK FOR SERVICE.Aug 27, 2009 · N586HA · Boeing 7673G5 · Turbine Engine Oil SystemSDR HALA2009082600388Warning System · false indicationETOPS SIGNIFICANT SYS - L FWD BOOST PUMP LOW PRESS LGT FAILED TO ILLUM AND EICAS MSG FAILED TO DISPLAY WITH SWITCH OFF. OPS CHECKED LT FED BOOST PUMP LOW PRESS LIGHT ON GROUND IAW AMM 28-22-00. OPS CHECK OK.Aug 26, 2009 · N586HA · Boeing 7673G5 · Engine Fuel Indicating System
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