N596HA, cancelled Mar 11, 2014

Service difficulty reports · 251

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N596HA' AND deregistration_id = 'N596HA-2014-03-11'
  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 HALA201312250181Connector · failedFUEL QTY INDICATION STATUS MESSAGE CENTER TANK FUEL & TOTALIZER ON OVERHEAD ARE BLANK. R & R FQIS PROCESSOR IAW AMM 28-41-08 CONDITION SAME. FQIS BITE FAULT CODE 71. ACCOMPLISHED LT AUX TANK INSULATION RESISTANCE TEST AMM 28-41-00. FOUND LT AUX BUSSING PLUGDec 25, 2013 · N596HA · Boeing 767332 · Fuel System WiringSDR HALA2013111100167Pump · failedLEFT HYD PRIMARY OVERHEAT EICAS MESSAGE. IAW MOC INSTRUCTION/TSI T/S FIM 29-11, FT821. R & R ENG DRIVEN HYD PUMP IAW AMM 29-11-05. RAN LT ENGINE. LT EDP PRESSURE CHECKED GOOD AT 3000 PSI.Nov 11, 2013 · N596HA · Boeing 767332 · Hydraulic Pump (Electric/Engine), MainSDR HALA2013092600122Circuit Card · failedWARN ELEX ADVISORY DISPLAYED IN FLIGHT ALONG WITH AMBER SPLIM ON F/O ADI SPEED TAPE WITH LOSS OF RED SPEED TAPE INDICATOR BAR. REPLACED RT WARNING ELEX STALL WARNING CARD. OPS CHECK OK IAW FIM 27-32-00, FIG 105.Sep 26, 2013 · N596HA · Boeing 767332 · Stall Warning SystemSDR HALA2013072400094Transformer · inoperativeACFT DIVERTED TO AN ALTERNATE STATION. T/E FLAP DISAGREE EICAS AND CVE LIGHTS ILLUMINATED WHEN FLAPS SELECTED TO 15 DEGREES. AND STATUS T/E FLAP SHUTDOWN. ACCOMPLISHED FIM 27-51, FIG 114C, ACCOMPLISHED FSPM BITE FIM 27-58, FIG 104, ACCOMPLISHED FSEU BIJul 24, 2013 · N596HA · Boeing 767332 · Trailing Edge Flap Control SystemSDR HALA2013071500089Connector · dirtyON RIGHT ENG START EGT FLUCTUATING DID NOT INCREASE. CLEANED CONNECTOR ON RT ENG. OPS NORMAL, OK FOR SERVICE.Jul 15, 2013 · N596HA · Boeing 767332 · Engine Indicating System WiringSDR HALA2013071200087Connector · disconnectedAFTER START RT ENGINE EGT FAILED (13DEG) (BTB). INSPECTED RT ENG THERMOCOUPLES, FOUND CONNECTOR DISCONNECTED ON THE FWD SIDE OF J-BOX. CONNECTED CONNECTOR, RAN ENGINE, EGT INDICATION NORMAL. ALL WORK PERORMED IAW AMM 77-21-02 AND 71-00-00.Jul 12, 2013 · N596HA · Boeing 767332 · Engine Indicating System WiringSDR HALA2013061400081Skin · dentedDENT FOUND FWD AND LOWER OF AFT CARGO COMPT. APPROX BS 1329, BETWEEN STRINGERS S36-37. NDT INSPECTION-NO CRACKS NOTED. PERFORMED INTERNAL VISUAL INSPECTION IAW SRM 53-00-01, NO DEFECTS NOTED. ACCOMPLISHED E105-596232-IN.Jun 14, 2013 · N596HA · Boeing 767332 · Fuselage Main, Plate/SkinSDR HALA2013061400080Skin · damagedDENT FOUND FWD AND LOWER OF AFT CARGO COMPT APPROX BS 1280.5. BETWEEN STRINGERS S36-38. DENT 9"L X 12"W X .1875 DEPTH. GOUGE NOTED IN DENT .040 DEPT. NDT INSPECTION-CRACK INDICATION AT GOUGE. PERFORMED FLUORESCENT PENETRANT INSP OF AREA. NO CRACKS NOTED.Jun 14, 2013 · N596HA · Boeing 767332 · Fuselage Main, Plate/SkinSDR HALA2013042700046J-Box · failedRT PRIMARY ENGINE EGT INDICATOR READS ZERO USING LDRR ICAS COMPUTER STANDBY ENGINE INSTRUMENT ALSO READS ZERO. TROUBLESHOT IAW FIM 77-21, FAULT TREE 803 INSPECTED EGT THERMOCOUPLE CABLES TERMINALS AND BRACKET FOR DAMAGE INSPECTED CONNECTORS AND PINS AT FIREWAApr 27, 2013 · N596HA · Boeing 767332 · Engine Indicating System WiringSDR HALA2013041700039Engine · making metalAPU AUTO SHUTDOWN. LOW OIL PRESSURE FAULT ON ECU. DP POPPED ON OIL FILTER. METAL PARTICLES FOUND ON GEARBOX CHIP DETECTOR. REPLACED APU IAW M266, AUXILIARY POWER UNIT (APU) CHANGE.Apr 17, 2013 · N596HA · Boeing 767300 · APU Core EngineSDR HALA2012121000233Engine · hung startLEFT ENGINE HUNG START, N1 18.37. EGT 740. N2 56.47 F/F 1,200. REPLACED LT ENGINE MEC & LEAK CHECKED IAW AMM 73-21-01. REPLACED LT ENGINE T2 SENSOR IAW AMM 73-21-05. REPLACED CIT SENSOR. COMPLIED WITH ALL COMPONENT REPLACEMENT TESTS IAW AMM 71-00-00 TESTS Dec 10, 2012 · N596HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2012101000226Skin · damagedLIGHTING STRIKE FOUND AT BS 148.2, 6.5" BELOW & -24L. DAMAGED AREA CUT OUT IAW SRM 53-00-01-2R-16, REPAIR 14D6347210, REV. 90. REPAIR PARTS FABRICATED IAW SRM 53-00-01-2R-14 REPAIR 14, D634T210, REV 90. REPAIR PARTS INSTALLED IAW SRM 53-00-01-2R-14. REPAIROct 10, 2012 · N596HA · Boeing 767332 · Fuselage Main, Plate/SkinSDR HALA2012053000151Circuit Card · failedACFT ARRIVED SAFELY, NR 1 & 2 FIRE BOTTLES FOR RT ENGINE WERE DISCHARGED BY THE FLT CREW DURING APPROACH. WHILE LINING UP FOR APPROACH RECEIVED "FIRE WARNING" ANNUNCIATION, FLT CREW DISCHARGED NR 1 BOTTLE. "WARNING DID NOT EXTINGUISH, THEN NR 2 BOTTLE DISCHMay 30, 2012 · N596HA · Boeing 767332 · Fire DetectionSDR HALA2012052900149Wire Harness · malfunctionedRIGHT ENGINE LP2 STATUS MESSAGE WAS INTERMITTENT. R & R WIRE HARNESS ON RESPONDERS IAW AMM 26-11-02/401 AND ACCOMPLISHED LEAK CHECK ON ALL DUCTING IAW AMM 36-11-09-782-104-001, NO LEAKS, RAN ENGINE AT IDLE, NO EICAS OR STATUS MESSAGE ON RT ENGINE.May 29, 2012 · N596HA · Boeing 767332 · Engine Indicating System WiringSDR HALA2012052700148Check Valve · malfunctionedRT ENGINE FIRE LP 2 STATUS MESSAGE INTERMITTENT. FOUND & REPLACED INTERMEDIATE CHECK VALVE & DUCT ASSY. OPS & LEAK CHECKED GOOD IAW AMM 36-11-06. LEAK CK GOOD.May 27, 2012 · N596HA · Boeing 767332 · Pneumatic Distribution SystemSDR HALA2012052700147Warning Light · no indicationLEFT PACK OFF LIGHT & LT PACK OFF EICAS MESSAGE NEVER ILLUMINATED WHEN PACK SELECTOR IN OFF POSITION. PERFORMED BITE CHECK ON LT PACK CONTROLLER NO FAULTS NOTED. TRIED TO DUPLICATE PROBLEM NUMEROUS TIMES. OPS CHECKED OK IAW AMM21-51-00-705-001.May 27, 2012 · N596HA · Boeing 767332 · Cabin Cooling SystemSDR HALA2012052100143Fire Detector · false activationRIGHT ENGINE FIRE LP2 EICAS ILLUMINATED. PERFORMED FIM 26-11-00/101, FIG 104, ENGINE FIRE DETECTION SYS BITE PROCEDURE RESECURED COUPLINGS AT HIGH STAGE BLEED MANIFOLD LEAK CHECKED NORMAL AT NR 2 POS.May 21, 2012 · N596HA · Boeing 767332 · Fire DetectionSDR HALA2012051900141Unknown · warning messageRIGHT EEC EICAS ILLUMINATED, DID NOT RESET IAW QRA. TROUBLESHOOTING PERFORMED, ECC MONITOR BITE NO FAULTS NOTED. RESET EEC SWITCH RAN ENGINE FOR 10 MIN. NO FAULTS NOTED. 2ND EEC MONITOR BITE SHOWED NO FAULTS. OK FOR CONTINUED SERVICE.May 19, 2012 · N596HA · Boeing 767332 · Central WarningSDR HALA2012051900140Transceiver · not seatedA/S 192 KTS FLAP 20 DEGREE WHEN SPEEDBRAKES EXTENDED. RECEIVED RED CONFIG WARNING & GEAR NOT DOWN EICAS. RERACKED NR 1 RADIO ALT TRANSCEIVER, GROUND CHECKED OK. PERFORMED MCDP 30, NO FAULTS NOTED, TEST PASSES. ACFT LMP STATUS REMAINS LAND 3.May 19, 2012 · N596HA · Boeing 767332 · Ground Proximity SystemSDR HALA2012051400139Fire Detector · malfunctionedAFTER PARKING, STATUS MESSAGE DISPLAYED RT ENGINE FIRE LOOP. AFTER A FEW MINUTES THE STAUS MESSAGE EXTINGUISHED. INSPECTED RT ENGINE FIRE LOOP WIRE HARNESS IAW WDM 26-11-21. NO DEFECTS NOTED. REPLACED RT ENGINE FIRE DETECTORS TS44, TS45, TS46 IAW AMM 26-11May 14, 2012 · N596HA · Boeing 767332 · Fire DetectionSDR HALA2012051400138Warning Message · false activationRECEIVED A STATUS MESSAGE "RT ENGINE FIRE LP 2". PERFORMED FIM 26-11-00/101 FIG 104. CHECKED RT ENG LP2 AND LP1 CONNECTIONS AND CLEANED. SECURITY/ATTACHMENT VERIFIED. OPERATION OF FIRE TEST NORMAL. REF AMM 26-11-00. STATUS MESSAGE EXTINGUISHED.May 14, 2012 · N596HA · Boeing 767332 · Fire DetectionSDR HALA2012051300137Circuit Card · malfunctionedRIGHT ENGINE FIRE LOOP, STATUS MESSAGE ILLUMINATED ON DECENT. EXTINGUISHED AFTER LANDING. CHECKED RESISTANCE AT M684, PINS 19 & 20 - 1.5 K OHMS. CHECKED INSULATION RESISTANCE BETWEEN PING 18 & 19, & PINS 18 & 20-54 OHMS. "SHAKE CHECKED" RT ENG FIRE LOOP HARNEMay 13, 2012 · N596HA · Boeing 767332 · Fire DetectionSDR HALA2012051000132Ecu · faultedPRIOR TO ENGINE START, APU FAULTED AND AUTO SHUTDOWN. BITE CHECKED APU ECU FOUND REVERSE FLOW FAULT. PERFORMED FIM 49-11-00-1 FIG 108. GROUND OPS CHECKED OK.May 10, 2012 · N596HA · Boeing 767332 · APU Bleed Air SystemSDR HALA2012031800112Compressor · stalledNR 2 ENGINE COMPRESSOR STALL AT TOP OF CLIMB. FLT CREW DECLARED EMERGENCY AND DIVERTED BACK, WHERE AN UNEVENTFUL LANDING WAS MADE. OPEN.Mar 18, 2012 · N596HA · Boeing 767332 · Turbine Engine Compressor SectionSDR HALA2012030700107Fire Detector · malfunctionedETOPS SIGNIFICANT SYSTEM - ON COCKPIT PREFLIGHT FOUND NO AURAL WARNING WHEN WHEEL WELL AND ENG/APU/CARGO FIRE SYS TESTED. RE-SET MASTER WARNING CAUTION SWITCH, OPS CHECKED GOOD. W/W & ENG/APU,CARGO FIRE SYS CK GOOD.Mar 7, 2012 · N596HA · Boeing 767332 · Fire DetectionSDR HALA2012030500105Connector · looseETOPS SIGNIFICANT SYS - F/O RADIO ALTIMETER IS INMT ON ADI. CONDITION NORM WITH ALTERNATE EFI SELECTED. PERFORMED BITE OF RT RADIO ALTIMETER. NO FAULTS INDICATED. INSPECTED ANTENNA CONNECTOR FOUND RECEIVE ANTENNA CONNECTOR LOOSE, CLEARED AND RESEATED CONNMar 5, 2012 · N596HA · Boeing 767332 · Navigation System WiringSDR HALA2012022900093Engine · hung startLEFT ENGINE HUNG START, FUEL FLOW AND DUCT PRESSURE WERE NORMAL. HUNG AT 56 PERCENT N2 AND EGT 710 DEGREES WHEN START ABORTED. SECOND START NORMAL. GROUND START 1 & 2, NO DEFECTS NOTED ON NR 1 ENGINE.Feb 29, 2012 · N596HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2012022700085Connector · dirtyETOPS SIGNIFICANT SYS - ON INITIAL CLIMB EICAS MESSAGE, RT ENG HIGH STAGE, DISPLAYED RT HI STAGE LIGHT ILLUMINATED, QRH PROCEDURES C/W, LIGHT EXTINGUISHED. CONDUCTED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00 FAULTED FAMV. TROUBLESHOT FAN AIR MODULATING VALFeb 27, 2012 · N596HA · Boeing 767332 · Pneumatic System WiringSDR HALA2012022400073Control System · malfunctionedFLAP /SLAT, ELEVATOR EICAS MESSAGE, UNABLE TO LOWER FLAPS. PERFORMED FSEU, FSPM BITE, NO FAULTS NOTED. CYCLED POWER FROM ENGINE TO APU, FLAP/SLAT ELEVATOR EICAS MESSAGE CLEARED. CYCLED FLAPS SEVERAL TIMES, NO FAULTS NOTED. ACFT OK FOR SERVICE.Feb 24, 2012 · N596HA · Boeing 767332 · Leading Edge Slat Control SystemSDR HALA2012011800043Irs · splitETOPS SIGNIFICANT SYS- FMC MESSAGE SPLIT IRS OPERATION LT IRS 034/0.5, CENTER IRS. RT IRS 350/0.6. REMOVED POWER FROM ACFT RE-ESTABLISHED POWER AND ALIGNED TRU'S IAW SUB TASK 34-45-00, 745-075-003 AMM, NO SPLIT NOTED, OPS CHECKED OK.Jan 18, 2012 · N596HA · Boeing 767332 · Flight Management Computing Hardware SystemSDR HALA2011122100604Control Unit · out of rigCALLED FOR FLAPS 20 AT APPROX 8-10' OF FLAP GOT FLAP DISAGREE, T/E LIGHT AND T/E FLAP SHUTDOWN. STATUS MESSAGE. FOLLOWED QRH AND EXTENDED FLAPS TO 20' WITH ALTERNATE METHOD. BITE FSEU IAW FIM 27-51-00, FIG 104. FOUND FAULT M548 MISRIGGED. REPLACED M548 IAW Dec 21, 2011 · N596HA · Boeing 767332 · Trailing Edge Flap Control SystemSDR HALA2011120700577Relay · failedEICAS MESSAGE T/E FLAP DISAGREE DISPLAYED, T/E LIGHT ILLUMINATED WHEN ANY T/E FLAP POSITION WAS SELECTED. FLAPS FAILED TO MOVE TO SELECTED POSITION. DECLARED AN EMERGENCY AND LANDED SAFELY. PERFORMED FIM27-51-00-1, BLOCK 26, FIG 105, SHEET 3. R & R RELAY Dec 7, 2011 · N596HA · Boeing 767332 · Trailing Edge Flap Control SystemSDR HALA2011120400565Warning Message · multiple failFLAP ASSY MESSAGE ON GROUND. ON GEAR RETRACTION, RECEIVED A GEAR UN-SAFE LIGHT. OPEN.Dec 4, 2011 · N596HA · Boeing 767332 · Central WarningSDR HALA2011112800544Control Unit · malfunctionedFLAPS WOULD NOT EXTEND BEYOND 15DEG ACCOMPANIED BY T/E FLAP ASSYMETRY ANNOUNCIATION. USED ALTERNATE FLAPS TO EXTEND TO 30 DEG, NORMAL LANDING. ACFT ARRIVED WITH NO ASSYM MSG. HOWEVER T/E FLAP SHUTDOWN MESSAGE ON EICAS, ACCMO FIM 27-58-00/101 FIG 104 AND AMM Nov 28, 2011 · N596HA · Boeing 767332 · Trailing Edge Flap Control SystemSDR HALA2011114000518Bulb · missingON OVERNIGHT CHECK, FOUND SEAT 1H FWD AISLE EMERGENCY LIGHT MISSING LENS & BULBS AND SEAT 2H BOTH AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED LENS AND BULBS. OPS CHECKED OK IAW AMM 33-51-00.Nov 14, 2011 · N596HA · Boeing 767332 · Emergency LightingSDR HALA2011114000517Blade · damagedETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK, FOUND NR 2 ENGINE, NR 33 BLADE FR. INDEX ON SPINNER HAS FOD DAMAGE. ACCOMPLISHED AMM 72-31-02, NR 2 ENGINE NR 33 BLADE FROM INDEX ON SPINNER.Nov 14, 2011 · N596HA · Boeing 767332 · Turbine Engine Compressor SectionSDR HALA2011111100516Blade · damagedETOPS SIGNIFICANT SYS - FOUND .2500 X .2500 BLADE DAMAGE ON NR 2 ENGINE FAN. IAW AMM 72-31-02-801 WITHIN LIMITS AREA B, 4" BELOW BLADE SHROUD. BLENDED IAW AMM 72-31-02-801. OK FOR SERVICE.Nov 11, 2011 · N596HA · Boeing 767332 · Turbine Engine Compressor SectionSDR HALA2011111000511Flap System · malfunctionedON APPROACH, SELECTED FLAPS 15 DEGREE, GOT EICAS FLAP DISAGREE MSG HANDLE IN DETENT AND FLAP GAUGE SHOWED APPROX 10 DEGREE. FOLLOWED PROCEDURE AND LANDED WITHOUT INCIDENT, ON FINAL ALL ALERTS OFF AND SEL FLAP 25 DEGREE, FLAPS MOVED TO 25 DEGREE NORMALLY. TRONov 10, 2011 · N596HA · Boeing 767332 · Trailing Edge Flap Control SystemSDR HALA2011102800497Fmc · unknownETOPS SIGNIFICANT SYS - FMC BOTH WHILE IN ATC MODE ON ATC INDEX PAGE PRINTING IS ILLUMINATED ON ATC LOG PAGE. ALL INFO UPLINK WILL NOT PRINT, L6 INDICATES PRINT BUSY. CANNOT DUPLICATE ATC LOGGED IN CONDITION ON GROUND. FMC CHECKED GOOD IAW AMM 34-61-00-735-Oct 28, 2011 · N596HA · Boeing 767332 · Flight Management Computing Hardware SystemSDR HALA2011102400486Oil System · lowETOPS SIGNIFICANT SYS - AT GATE APU AUTO SHUTDOWN. BITE CHECKED ECU FOUND LOW OIL PRESSURE FAULT, SERVICED APU WITH 2.5 QTS, RAN APU NO LEAKS NOTED, OK FOR SVC.Oct 24, 2011 · N596HA · Boeing 767332 · APU Oil SystemSDR HALA2011101400461Engine · hung startETOPS SIGNIFICANT SYS - LT ENGINE HUNG START AT EGT 739 DEG; N2 53 PERCENT; FUEL FLOW 1500; OAT 14DEG C. ABORTED START, RESTARTED SUCCESSFUL. ACCOMPLISHED LT ENG START & IDLE RUN TEST 3 IAW AMM 71-00-00, ALL LT ENG PARAMETERS WITHIN LIMITS IAW AMM 71-00-00-8Oct 14, 2011 · N596HA · Boeing 7673G5 · Engine (Turbine/Turboprop)SDR HALA2011091500403Indicator · malfunctionedETOPS SIGNIFICANT SYS - ATTITUDE INDICATION OF STANDBY ALTITUDE INDICATOR IS ABNORMAL IN PITCH & ROLL. GYRO FLAG RETRACTED. REPLACED STANDBY ATTITUDE INDICATOR - CHECKS OK IAW AMM 34-24-01.Sep 15, 2011 · N596HA · Boeing 767332 · Attitude Gyro and Indicating SystemSDR HALA2011081600368Circuit Card · malfunctionedETOPS SIGNIFICANT SYS - C DEMAND PUMP EICAS "ON" WITH CTR AIR DEMAND PUMP "PRESS" LIGHT "ON" INTERMITTENTLY FROM INITIAL DESCENT TO LANDING. T/S IAW FIM 29-11-00-1, FIG 10. REPLACED SPEED CARD (P50) ALSO SUSPECT SPOILER ISSUE REF L/P 358540 ITM 30. OPS CK CAug 16, 2011 · N596HA · Boeing 767332 · Hydraulic System, MainSDR HALA2011072300335Totalizer · inaccurateETOPS SIGNIFICANT SYS - CALC & TOTALIZER HAS A 2,300 LB DIFF IAW FIM 28-41-00, FIG 107 TOTAL FUEL & FMC CAL FUEL CHECKED OK.Jul 23, 2011 · N596HA · Boeing 767332 · Fuel Quantity IndicatorSDR HALA2011070600315Processing Unit · faultedETOPS SIGNIFICANT SYS - INTERMITTENT FUEL QTY BITE EICAS MESSAGE. BITE CHECKED FUEL QTY PROCESSOR UNIT. FOUND "D2" FAULT. PERFORMED RESET VERIFY CONFIRMED NO FAULTS MESSAGE. OK FOR SVC.Jul 6, 2011 · N596HA · Boeing 767332 · Fuel Indicating SystemSDR HALA2011070200303Overheat Loop · malfunctionedETOPS SIGNIFICANT SYS - STATUS EICAS WARNING ON DESCENT. "R ENG OH LP 2". REPLACED DAMAGED RT ENGINE OVERHEAT LOOP DETECTOR AND OPS CHECK OK IAW MM 26-11-02.Jul 2, 2011 · N596HA · Boeing 767332 · Overheat DetectionSDR HALA2011062500291Circuit Card · malfunctionedETOPS SIGNIFICANT SYS - EICAS STATUS MSG: RT ENG OH LP2 DISPLAYED. ACCOMPLISHED FIM DAL D633T605 AND WDM 26-11-22. REPLACED RT ENG LP2 OVERHEAT DETECTION CARD (M690). ENG GROUND RUN CHECKED OK.Jun 25, 2011 · N596HA · Boeing 767332 · Overheat DetectionSDR HALA2011061800269Computer · unknownTCAS COMPUTER FAILURE NR 1 & NR 2 TRANSPONDER DATA BUSS FAILURE. 1 & 2 PROCESSER FAILURE RA DISPLAY NR2 RADIO ALT NR1. RECYCLED TCAS C/B. GROUND CHECK OK.Jun 18, 2011 · N596HA · Boeing 767332 · Flight Management Computing Hardware SystemSDR HALA2011051700207Line · looseETOPS SIGNIFICANT SYS - ON DESCENT WITH POWER IDLE LEFT ENGINE BLEED VALVE LIGHT ON. TROUBLESHOT IAW FIM 36-10-00, FIG 111. FOUND & SECURED LOOSE SENSE LINE AT HPSOV. PERFORMED HIGH PWR ENG RUN NO PROBLEMS NOTED. OK FOR SERVICE.May 17, 2011 · N596HA · Boeing 767332 · Pneumatic Distribution SystemSDR HALA2011041900163A/C Pack · malfunctionedETOPS SIGNIFICANT SYS - RT PACK INOP LIGHT ILLUM, EICAS MESSAGE RT PACK TEMP DISPLAYED NORMAL AFT STBY SELECTED. T/S IAW FIM 21-51-00/101, FIG 103. DID PACK TEMP CONTROLLER BITE CHECK. NO FAULTS. RAN PACKS FOR APPROX 30 MINS. PACK OPEN AND TEMP NORMAL. RApr 19, 2011 · N596HA · Boeing 767332 · Cabin Cooling System
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