N381HA

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 = 'N381HA' AND registry_match = 'registration'
  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 HALA2015082400167Fire Loop · shortedENGINE 2 FIRE LOOP A FAULT ECAM WARNING DISPLAYED IAW FLIGHT CREW. FOUND RT ENGINE LOOP A PYLON DETECTOR, 6WD2, SHORTED TO GROUND. R & R LOOP A, 6WD2, AMM 26-12-16-400 -808A, ACCOMPLISHED TO STEP 5B, 3. OPS CHECK GOOD. COMPLETED REMAINING STEPS AMM 26-12-16-Aug 24, 2015 · N381HA · Airbus A330243 · Smoke DetectionSDR HALA2015081900163Tire · wornON TAKEOFF ROLL, EXTREME NOSE WHEEL VIBRATION. T/S IAW TSM 32-20-00-810. FOUND UNEVEN WEAR BETWEEN NLG TIRE ASSY. REPLACED BOTH NLG TIRE ASSY IAW AMM 32-41-12. INSPECTED NLG ASSY FOR IRREGULARITIES. NONE NOTED.Aug 19, 2015 · N381HA · Airbus A330243 · TireSDR HALA2015082005022Tire · wornDUE TO EXTREME NOSEWHEEL VIBRATION DURING TAKEOFF ROLL. T/S IAW TSM 32-20-00-810, FOUND UNEVEN WEAR BETWEEN NLG TIRE ASSY. REPLACED BOTH NLG TIRE ASSY IAW AMM 32-41-12. INSPECTED NLG ASSY FOR IRREGULARITIES. NONE NOTED.Aug 19, 2015 · N381HA · Airbus A330243 · TireSDR HALA2015080600153Sensor · malfunctionedNR 2 ENGINE BLEED ECAM DURING DESCENT. R & R RIGHT ENGINE EXCHANGER OUTLET SENSOR IAW AMM 36-11-17-400-804-A.Aug 6, 2015 · N381HA · Airbus A330243 · Pneumatic Distribution SystemSDR HALA2015071600140Brake · overheatedDURING TAKEOFF ROLL AROUND 65 KTS, ECAM MESSAGE HOT BRAKE, NR 6 BRAKE AT 320. ALL BRAKE TEMPS AROUND 130 PRIOR TO TAKEOFF ROLL. VERIFIED WHEEL SPINS FREELY. REPLACED NR 6 TIRE AND BRAKE.Jul 16, 2015 · N381HA · Airbus A330243 · Landing Gear Brake SystemSDR HALA2015072005019Brake · overheatedDURING TAKEOFF ROLL, AROUND 65 KTS ECAM MESSAGE HOT BRAKE, NR 6 BRAKE AT 320 DEGREES. ALL BRAKE TEMPS AROUND 130 DEGREES PRIOR TO TAKEOFF ROLL. VERIFIED WHEEL SPINS FREELY, REPLACED NR 6 TIRE AND BRAKE.Jul 16, 2015 · N381HA · Airbus A330243 · Landing Gear Brake SystemSDR HALA201506230113Indicator · malfunctionedABORTED T/O, F/O AIRSPEED ERROR ABORTED AT 65 KTS. NO AIRSPEED FAULTS ON PFR, ADR2 & IR2 SYSTEM TEST OK IAW AMM 34-13-00 & 34-14-00. HA MOC REPLACED F/O PITOT PROBE IAW AMM 34-11-15, OPS TEST OK. REPLACED ADM-2, 19FP2 AND HOSE IAW AMM 34-11-17. ADR2 SYSTENJun 23, 2015 · N381HA · Airbus A330243 · Airspeed/Mach IndicatorSDR HALA2015052200092Bleed Valve · malfunctionedENGINE AIR BLEED FAULT ON CLIMBOUT. RESET NR 1 ENGINE BLEED ECAM, CLEARED. R & R NR 1 ENGINE BLEED VALVE, OPS AND LEAK CHECKED OK. OK FOR SERVICE.May 22, 2015 · N381HA · Airbus A330243 · Compressor Bleed ValveSDR HALA2015052100091Bleed Air Sys · malfunctionedNR 1 ENGINE BLEED AIR FAULT ON CLIMB OUT. RESET ENGINE 1 BLEED IAW MAINTENANCE CONTROL REQUEST. PACK FLOW "LOW" AND FAULT CLEARED. PERFORMED TSM 36-11-00-710-813-A. OPS CHECKED GOOD, NO FAULTS NOTED. ALSO, PERFORMED HIGH POWER RUN, OPS CHECKED GOOD, NOMay 21, 2015 · N381HA · Airbus A330243 · Pneumatic Indicating SystemSDR HALA2015052000091Bleed Air Sys · malfunctionedNR 1 ENGINE BLEED AIR FAULT DURING CLIMBOUT. RESET NR 1 ENGINE BLEED IAW MX CONTROL REQUEST. PACK FLOW "LOW" AND FAULT CLEARED. PERFORMED TSM 36-11-00-710-813-A. OPS CHECKED GOOD, NO FAULTS NOTED. ALSO PERFORMED HIGH POWER RUN, OPS CHECKED GOOD, NO FAULTSMay 21, 2015 · N381HA · Airbus A330243 · Pneumatic Indicating SystemSDR HALA2015050903174Slide · damagedLEFT EMERGENCY DOOR ESCAPE SLIDE FAILED OPERATIONAL CHECK. SLIDE DID NOT STAY INFLATED FOR 10 MINUTES. FOUND 1" HOLE IN FORWARD SIDE OF SLIDE, SUSPECT PREVIOUS REPAIR FAILED. REPLACED SLIDE. LP 1939117.May 8, 2015 · N381HA · Airbus A330243 · Escape SlideSDR HALA2015050903173Cylinder · failedDURING OPS CHECK, DOOR 1L ESCAPE SLIDE FAILED DEPLOYMENT TEST. FOUND THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FAILED INTERNALLY, SO THE SLIDE FAILED TO OPEN SUFFICIENTLY. REPLACED DOOR ACTUATOR AND SLIDE. LP 1939106, 1915911.May 8, 2015 · N381HA · Airbus A330243 · Escape SlideSDR HALA2015050800071Cylinder · failed1L DOOR ESCAPE SLIDE/RAFT TEST DEPLOYMENT FAILED. DURING SAMPLING INSPECTION IAW FORECAST 43-0525-8-0040, 1L DOOR FAILED TO OPEN SUFFICIENTLY TO FIRE THE SLIDE. FOUND THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER HAD FAILED INTERNALLY.May 8, 2015 · N381HA · Airbus A330243 · Escape SlideSDR HALA2015050800070Slide · leakingLEFT EMERGENCY DOOR ESCAPE SLIDE FAILED OPS CHECK. SLIDE DID NOT STAY INFLATED FOR 10 MINUTES. SLIDE HAD 1" HOLE IN FWD SIDE. R & R SLIDE.May 8, 2015 · N381HA · Airbus A330243 · Escape SlideSDR HALA2015050305010Valve · faultedRETURNED TO AIRPORT DUE TO AIR PACK VALVE 2 FAULT DURING CLIMB. POST FLIGHT REPORT SHOWS AIR ENG 2 BLEED FAULT PRESSURE REGULATOR MESSAGE. REPLACED PRV BLEED VALVE.May 1, 2015 · N381HA · Airbus A330243 · Cabin Cooling SystemSDR HALA2015050100069Valve · faultedAIR PACK VALVE 2 FAULT ON CLIMB OUT. POST FLIGHT REPORT SHOWS AIR ENGINE 2 BLEED FAULT PRESSURE REGULATOR V. R & R PRV BLEED VALVE IAW AMM 36-11-52. OPS CHECK NORMAL. OK FOR SERVICE.May 1, 2015 · N381HA · Airbus A330243 · Cabin Cooling SystemSDR HALA2014092900147Generator · malfunctionedIDG NR 2 LOW OIL PRESSURE DISCONNECTED IDG & TURNED OFF GENERATOR NR 2. REMOVED AND INSTALLED NR 2 ENGINE IDG IAW AMM 24-21-51. FOUND IDG FILTER DPI POPPED AND METAL PARTICLES ON FILTER. FILTER ELEMENT WAS NOT DAMAGED AND NO SIGNS OF BYPASS WERE FOUND. OPSep 29, 2014 · N381HA · Airbus A330243 · AC Generator-AlternatorSDR HALA2014092300152Structure · damagedAFT CARGO DOOR INTERIOR SIDE RIVET HEAD DAMAGED 4PT AFT OF FWD DOOR EDGE 1.5 FEET FROM BOTTOM DOOR EDGE. BETWEEN FRAME 62 AND FRAME 62A BEAMS. REPAIRED IAW E105-381000. OK FOR SERVICE.Sep 23, 2014 · N381HA · Airbus A330243 · Cargo/Baggage DoorsSDR HALA2014092100142Warning Message · false activationDURING CRUISE FLT, RECEIVED ECAS ELEC CIRCUIT BREAKER TRIPPED. BITE TEST APU, NO FAULTS. RESET OIL/SERVICE CIRCUIT BREAKER. FUCTIONAL CHECKED OF APU OK. LEAK TEST OF APU OIL HEATER OK. NO LEAKS. OK FOR SERVICE.Sep 21, 2014 · N381HA · Airbus A330243 · APU Bleed Air SystemSDR HALA2014092100141Circuit Breaker · trippedDURING CRUISE, RECEIVED ECAM ELEC CIRCUIT BREAKER TRIPPED AND CIRCUIT BREAKER PAGE MESSAGE APU 5000VU. BITE TEST APU. NO FAULTS. RESET OIL SERVICE CIRCUIT BREAKER. FUNCTIONAL CHECKED OK. LEAK TEST OF APU OIL HEATER OK. NO LEAKS. OK FOR SERVICE.Sep 21, 2014 · N381HA · Airbus A330243 · APU ControlsSDR HALA2014070400100Jettison System · malfunctionedACFT DIVERTED DUE TO FUEL JETTISON NOT CLOSED, X4, LT TANK FUEL JETTISON VALVE. SHOWED OPENED.Jul 4, 2014 · N381HA · Airbus A330243 · Fuel Dump SystemSDR HALA2013091700119Windshield · failedAPPROXIMATELY 1.5 HRS INTO THE FLT ECAM MESSAGE A. "ICE RT WINDSHIELD HEAT". SIMULTANEOUSLY WITH APPEARENT SHORT OF RT WINDSHIELD, BLACK MARK WITH DELAMINATION LAYER BELOW. R & R F/O WINDSHIELD IAW AMM 30-42-34, OPS CHECKED GOOD.Sep 17, 2013 · N381HA · Airbus A330243 · Flight Compartment WindowsSDR HALA2013091700118Windshield · failedAPPROX 1.5 HRS INTO THE FLIGHT, ECAM MESSAGE A ICE RT WINDSHIELD HEAT. SIMULTANTOUSLLY WITH APPEARENT SHORT OF RT WINDSHIELD, BLACK MARK WITH DELAMINATING LAYER BELOW. R & R F/O WINDSHIELD IAW AMM 30-42-34, OPS CHECKED GOOD.Sep 17, 2013 · N381HA · Airbus A330243 · Flight Compartment WindowsSDR HALA2013050200053Adiru · malfunctionedAT APPROX 95 KTS DURING TAKEOFF ROLL. F/O AIRSPEED INDICATOR TAPE LOST SPEED INDEXES AND BEGAN FLASHING RED. MOVED NR 3 ADIRU INTO NR 2 POSITION AND REPLACED NR 3 ADIRU. OPS AND LEAK CHECKED GOOD.May 2, 2013 · N381HA · Airbus A330243 · Inertial Guidance SystemSDR HALA2013042100042Indicator · inoperativeCAPTAINS AIR SPEED INOPERATIVE RTO -80 KTS. ON ARRIVAL AT GATE PFR SHOWED NO FAULTS. ADR-1, SYS TESTS OK, NO FAULTS IAW AMM 34-13-00. AFS BITE TEST FAULTS FMGEC-1 AND FMGEC-2 RESET BOTH FMGEC, AFS BITE TEST OK IAW AMM22-96-00. INSPECTED PITOT PROBE 1, NO DEApr 21, 2013 · N381HA · Airbus A330243 · Airspeed/Mach IndicatorSDR HALA2012041800124Warning Light · false activationSMOKE, FWD & AFT BOTTLE FAULT 1 & 2 WARNING LIGHTS. PERFORMED MCDU TEST IAW AMM 26-10, SYS TESTED OK. MESSAGE CLEARED.Apr 18, 2012 · N381HA · Airbus A330243 · Detection SystemSDR HALA2012022200068Warning Light · false activationSMOKE AFT CARGO BOTTLE 1(2) FAULT CARGO AFT CARGO DETECT FAULT 1(2) DISPLAY ECAM. RESET SDF1 AND SDF2 IAW SUPPLEMENTAL MANUAL. NO FAULTS NOTED. OK TO CONTINUE.Feb 22, 2012 · N381HA · Airbus A330243 · Extinguishing SystemSDR HALA2012010100001Smoke Detector · malfunctionedFWD & AFT CARGO SMOKE BOTTLES 1 & 2 FAULT DURING PREFLIGHT. PERFORMED CARGO SMOKE TEST IAW AMM 26-16-00, NO FAULTS NOTED.Jan 1, 2012 · N381HA · Airbus A330243 · Smoke DetectionSDR HALA2011100500430Unknown · unknownETOPS SIGNIFICANT SYS - BTB -NR 2 ENGINE OVERSPEED PROTECTION LOST. ENGINE NR2 LP SHAFT PROTECTION LOST. ACCOMPLISHED FIM 73-21-89. NO FAULTS NOTED. ACFT OK FOR SERVICE.Oct 5, 2011 · N381HA · Airbus A330243 · Fuel Controlling SystemSDR HALA2011080800358Smoke Detector · malfunctionedETOPS SIGNIFICANT SYS - SMOKE FWD/AFT CARGO BTL1 FAULT, SMOKE FWD/AFT CRG BTL2 FAULT, SMOKE BULK DET FAULT, SMOKE BULK REST FAULT, SMOKE BULK REST DET FAULT, SMOKE BAND DET FAULT DISPLAYED. RESET SDF 1 & 2. MESSAGES CLEARED. SMOKE DETECT SYS TEST OK. NO DEFEAug 8, 2011 · N381HA · Airbus A330243 · Smoke DetectionSDR HALA2011072700336Iru · malfunctionedETOPS SIGNIFICANT SYS - NR3 INERTIAL REF, ALTHOUGH RE-ALIGNED TWICE, FAULT LIGHT CONTINUOUSLY FLASHES. RE-RACKED & RE-ALINGED NR3 IRU, GND CHECKED GOOD.Jul 27, 2011 · N381HA · Airbus A330243 · Central WarningSDR HALA2011072500333Warning Light · false activationETOPS SIGNIFICANT SYS - BTB - ENG 2 BLEED FAULT ECAM MESSAGE, CAME ON SHORTLY AFTER ENG START. PERFORMED FIM 36-11-81, BMC 2 BITE CHECKED, NO FAULTS FOUND, RAN ENGINES, NO FAULTS FOUND, SWAPPED NR 1 & NR 2 PACK CONTROLLERS IAW AMM 21-51-00. OPS CHECK GOOD.Jul 25, 2011 · N381HA · Airbus A330243 · Engine Bleed Air SystemSDR HALA2011072100332Smoke Warning · false activationACM MEMO ALERT APPEARED AT TOP OF DESCENT, SMOKE FWD CARGO BLT 1 FAULT, AFT CARGO BLT 1 FAULT, FWD CARGO BLT 2 FAULT, AFT CARGO BLT 2 FAULT, THE MESSAGE CLEARED ABOUT 10 MIN LATER. PERFORMED A FWC BITE, NO FAULTS FOUND, INFO NOTED. RECORDED MSG REAPPEARED. PJul 21, 2011 · N381HA · Airbus A330243 · Smoke DetectionSDR HALA2011072100331Smoke Detector · malfunctionedECAM MEMO ALERT APPEARED AT TOP OF DESCENT SMOKE FWD CARGO BLT 1 FAULT, AFT CARGO BLT 1 FAULT, FWD CARGO BLT 2 FAULT AFT CARGO BLT 2 FAULT, THE MESSAGE CLEARED ABOUT 10 MIN LATER. PERFORMED A FWC BITE NO FAULTS FOUND, INFO NOTED. RECORDED MESSAGE REAPPEARED. Jul 21, 2011 · N381HA · Airbus A330243 · Smoke DetectionSDR HALA2011061200259Smoke Detector · malfunctionedSMOKE FWD CARGO BLT FAULT "AFT" "FWD" "2" AFT. RESET SDF 1 AND SDF 2 PERFORMED SDF TEST, TEST PASS, NO FAULT NOTED. OK FOR SERVICE.Jun 12, 2011 · N381HA · Airbus A330243 · Smoke DetectionSDR HALA2011061100258Decoder · malfunctionedSLIDE ICE PROTECTION NO DATA AVAILABLE AT DOOR L1, 1R, AND 2R MSG ON FWD FAP. CIDS GROUND SCANNING FAULT IPCU FWD 14DS DEU B 300 RT 4. R & R DEU B300RH4 IAW AMM 23-73-47. BITE OK. FAP MSG CLEARED. OK FOR SVC.Jun 11, 2011 · N381HA · Airbus A330243 · Ice/Rain Protection SystemSDR HALA2011060800254Adc · malfunctionedABORTED T/O BELOW 100 KTS, LOSS OF CAPT'S IAS. VISUALLY INSPECTED PITOT PROBE FROM FRONT OF TUBE, NOTHING OBVIOUS FOUND. PRESSURIZED 2 OUT OF 3 PITOT SYS AT THE SAME TIME. TRIED SEVERAL DIFFERENT COMBINATIONS AND DIFFERENT SWITCH SELECTIONS IN COCKPIT. NO Jun 8, 2011 · N381HA · Airbus A330243 · Air Data ComputerSDR HALA2011060800253Adiru · inoperativeETOPS SIGNIFICANT SYS - ATB - ON T/O RUN, ABOVE 100 KTS, CAPT'S IAS WENT ROD/INOP/UNRELIABLE. TRANSFERED CONTROL. BOTH F/O & ISIS ACCURATE. CAPTS ALTIMETER OK CHANGED AIRDATA TO "CAPT ON 3" - DISPLAY OK. OK TO CONT IAW MEL 34-10-1B. PLACARDED AND ENTERED ONJun 8, 2011 · N381HA · Airbus A330243 · Airspeed/Mach IndicatorSDR HALA2011060800251Skin · damagedSUB-FOUND DAMAGE ON LT FUSELAGE BETWEEN STA 18698 AND 19228, AND BETWEEN STRINGER 28 AND 30. BLENDED UPPER AND LOWER GOUGED AREA. UPPER AT .040 MATERIAL REMAINING. LOWER AT 0.062 REMAINING UPPER BLEND 1.2500" W X .7500"H LOWER BLEND 1" W X .7500". HFEC OF Jun 8, 2011 · N381HA · Airbus A330243 · Fuselage Main, Plate/SkinSDR HALA2011060800250Skin · damagedFOUND DAMAGE ON LT FUSELAGE BETWEEN STA 18698 AND 19228, AND BETWEEN STRINGER 28 AND 30. BLENDED UPPER AND LOWER GOUGED AREA. UPPER AT .040 MATERIAL REMAINING. LOWER AT 0.062 REMAINING UPPER BLEND 1.2500" W X .7500" H LOWER BLEND 1" W X .7500". HFEC OF FUSEJun 8, 2011 · N381HA · Airbus A330243 · Fuselage Main, Plate/SkinSDR HALA2011060100250Connector · corrodedAFTER START EMERGENCY LIGHTS SIGN ON AND FLASHING CYCLED EMERGENCY LIGHTS NO CHANGE. FOUND MOISTURE AND LITE CORROSION AT CONNECTOR PLUG LOCATED AT 5158VC CLEANED AND RESECURED IAW AWM 33-51-05 AND AMM 33-31. OPS CK OK.Jun 1, 2011 · N381HA · Airbus A330243 · Light System WiringSDR HALA2011051300198Battery Pack · dischargedPERFORMED OPS TEST OF EMERGENCY POWER SUPPLY UNIT, FORECAST 43-0533-8-0001. FOUND 4L DOOR POWER SUPPLY BATTERY INOP. R & R DOOR 4L 300R7 POWER SUPPLY IAW AMM 33-57-38,OPS CK NORMAL, OK FOR SERVICE.May 13, 2011 · N381HA · Airbus A330243 · Emergency LightingSDR HALA2010112300560Idg · faultyETOPS SIGNIFICANT SYSTEM - ATB: FLIGHT ELECTRIC IDG 2 OIL LO PR ECAM. REMOVED AND REPLACED NR 2 IDG ASSY PER AMM 24-21-51. OPS AND LEAK CHECKS OK.Nov 23, 2010 · N381HA · Airbus A330243 · AC Generator-AlternatorSDR HALA2010112000556Warning Light · illuminatedETOPS SIGNIFICANT SYSTEM - APROX 3+15 INTO FLT ECAM STATED CTR TO INR: MAN ONLY PLUS INOP SYS - "FUEL AFT XFR" ANNUNCIATED. CTR TANK 0 QTY, ALL TAIL TANK FUEL XFR TO INNER WING TANKS UNTIL CTR TANK EMPTY. PERFORMED TSM TASK 28-26-00-810-801. SYSTEM TESTS ONNov 20, 2010 · N381HA · Airbus A330243 · Fuel Indicating SystemSDR HALA2010111800555Warning Message · illuminatedETOPS SIGNIFICANT SYSTEM - ECAM MESSAGE FUEL CENTER TO INNER FAULT APPROX AT ATTEMPTED TRIM TANK TRANSFER. MESSAGE DISAPPEARED AFTER 2 MIN. PERFORMED AMM 28-51-00-740-801. NO FUEL CENTER TO INNER FAULT MESSAGE FOUND. OK FOR SERVICE.Nov 18, 2010 · N381HA · Airbus A330243 · Fuel Indicating SystemSDR HALA2010101400468Fcu · failedETOPS SIGNIFICANT SYS - UNSUCCESSFUL INFLT APU START. REPAIRED CLASS 1 FCU FLOW DIVIDER. BITE CHECK AND CLASS 1 FAULT CLEARED.Oct 14, 2010 · N381HA · Airbus A330243 · APU Engine Fuel and ControlSDR HALA2010081200363Computer · malfunctionedETOPS SIGNIFICANT SYS - BTB - ECAM (AMBER) WARNING - FLT CONTROL AIL FAULT LIGHT. CHECKED SV SIGNAL WIRING FROM FCPC1 AD/12J, 12K TO SERVO CTL (8CS1) A /E,F AND SV CTL WIRING FROM FCPC-1 AD/12G, 12H TO AB/1J, 1K CONTINUITY CHECKS GOOD, NO SHORTS TO GND. SHAKAug 12, 2010 · N381HA · Airbus A330243 · Flight Management Computing Hardware SystemSDR HALA2010081200362Computer · faultedETOPS SIGNIFICANT SYS - BTB - F/CTL AIL SERVO FAULT. REPLACED FCPC1 IAW 27-93-400-801, PG 400, ALL INDICATIONS NORMAL, ACFT OK FOR SERVICE.Aug 12, 2010 · N381HA · Airbus A330243 · Flight Management Computing Hardware SystemSDR HALA2010072200318Hydraulic System · malfunctionedETOPS SIGNIFICANT SYSTEM - ATB - AFTER T/O GREEN HYD PRESS 'O'. GREEN HYD SYS QTY NORMAL. DUMPED FUEL BELOW MAX LANDING WT AND RETURNED TO DEPARTURE AIRPORT. REPLACED GREEN HYD RESERVOIR LOW LEVEL SWITCH PER AMM 29-31-12-000-801-0. REPLACED HSMU PER AMM 29Jul 22, 2010 · N381HA · Airbus A330243 · Hydraulic System, MainSDR HALA2010071800305Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - ATB - GREEN HYD SYS ECAM SHOWS LOW QTY. ACCOMPLISHED TSM 29-11-00-810-832 STEP 4, A, (1), (A), 1, A IAW DELTA TECH SVC. FOUND NO FAULTS, CONTINUITY OF 0.8 OHM & NO SHORTS TO GROUND. G RSVR LO LVL SW 10JS1 HAS A SHORT OF 2.5K OHM FROJul 18, 2010 · N381HA · Airbus A330243 · Hydraulic System, Main
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