Boeing 777-333ER

Service difficulty reports · 52

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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 = '777333ER'
  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 CA190812018Wire · burned(CAN) AT START OF SHIFT RECEIVED INFORMATION ABOUT DAMAGE FOUND TO R/H LANDING LIGHT AREA, NO RECORD IN TRAX, OR ON SHIFT HANDOVER PAPERWORK. UPON INSPECTION, FOUND LENS COVER AND LAMP REMOVED AND A VERY STRONG ODOR COMING FROM LANDING LIGHT LAMP COMPARTMENT. Jun 4, 2019 · Boeing 777333ER · Light System WiringSDR CA190401007Engine · failed(CAN) WHILE AIRCRAFT WAS POSITIONED AT GATE, FLIGHT-CREW STARTED THE APU AND IDENTIFIED WHAT SOUNDED LIKE A BANG. APU FAULT MESSAGES APPEARED, AND RAMP CREW REPORTED APU CONTENTS FOUND ON THE GROUND. PARTS OF APU SHOT OUT FROM APU APPROXIMATELY 20METRES FROM TMar 18, 2019 · Boeing 777333ER · APU Core EngineSDR CA160303003Relay · failed(CAN) SMOKE DETECTED IN CABIN. FLIGHT DIVERTED. DUMPED FUEL TO BE LIGHTER FOR LANDING. PAN PAN WAS DECLARED. RESOLUTION BITE TEST CARRIED OUT OF IFE SYS, SPM FAILED ON TEST. SPM REPLACED. INSPECTION C/O OF ALL SEATS AND ABOVE CEILING AND ABOVE GALLEY WITH PWRMar 3, 2016 · Boeing 777333ER · Entertainment SystemSDR CA160223006Unknown · unknown(CAN) AFTER COMPLETING DE-ICING THE ACFT, TAXIED TO RUNWAY FOR DEPARTURE. DURING THE BEFORE T/O CHECK RUDDER TRAVEL CHECK NORMAL, HOWEVER AILERON IMMOVABLE AND ELEVATORS ONLY MOVABLE VERY SLIGHTLY. ACFT TAXIED BACK TO GATE WHERE MAINTENANCE MET FLIGHT AND WERFeb 18, 2016 · Boeing 777333ER · Flight Control SystemSDR CA150930004Brake · overheated(CAN) AFTER LANDING ANOTHER ACFT ADVISED OF SMOKE COMING FROM THE LT MAIN GEAR AFTER THEY EXITED THE RUNWAY. CREW NOTICED A SMALL FLAME AND SMOKE COMING FROM THE LT MAIN GEAR VIA THE ONBOARD CAMERA. MAYDAY WAS DECLARED AND FIRE TRUCKS ATTENDED THE SCENE. BRAKSep 30, 2015 · Boeing 777333ER · BrakeSDR CA150929002Hydraulic System · low(CAN) CENTER HYDRAULIC QUANTITY LOW EICAS. CTR SYS HYD SERVICED IAW AMM 12-12-01 PB301. DELTA P INDICATOR ON CENTER SYS FILTER CHECK SERVICEABLE.Sep 28, 2015 · Boeing 777333ER · Hydraulic System, MainSDR CA150316001Fan · failed(CAN) SMOKE ODOR NOTICEABLE ON CAPTAINS SIDE OF COCKPIT, NONE IN PASSENGER CABIN. PHONE PATCH WITH MOC, TURNED OFF WEATHER RADAR, ODOR DISSIPATED. PROCEEDED AS NORMAL. RESOLUTION RT EQUIPMENT COOLING SUPPLY FAN REPACED IAW AMM 21-27-03, PB 401.Mar 14, 2015 · Boeing 777333ER · Air Distribution FanSDR CA150310013Indication Sys · malfunctioned(CAN) APPROX 5 HOURS AFTER T OFF FLIGHT CREW RECEIVED A STATUS MSG ENG EEC C1, FUEL IMBALANCE EICAS MSG, CAME UP & THERE WAS A 1900KG IMBALANCE IN FUEL BETWEEN THE RT & LT TANK. ENG PARAMETERS ALL NORMAL IAW FLIGHT CREW. FUEL DRIP CHECK CARRIED OUT ON LT TANMar 10, 2015 · Boeing 777333ER · Fuel Indicating SystemSDR CA150216003Computer · failed(CAN) AFTER TAKEOFF AT 300 AGL, WHEN AUTO PILOT WAS SELECTED ON, FLIGHT DIRECTOR COMMANDED A 30 DEGREE LEFT TURN IGNORING THE FMS SID. MTC CONTROL ADVISED. INBOUND FLIGHT DECK EFFECTS SHOWED NO FAULTS RELATED TO AUTOPILOT. PERFORMED AFDS SYS TEST, PASSED NOFeb 16, 2015 · Boeing 777333ER · Autopilot SystemSDR CA150115001Valve · failed(CAN) CREW HAD ISSUES WITH TRIM AIR VALVE. AFTER RESET ATTEMPTS (AS PER MOC), NO IMPROVEMENT IN CABIN/FLIGHT DECK TEMPERATURE HAD OCCURRED. FLIGHT ELECTED TO RETURN. FLT DECK ZONE TRIM AIR VALVE REPLACED IAW AMM 21-61-02-401 OPS CHECK OK.Jan 14, 2015 · Boeing 777333ER · Cabin Temperature Control SystemSDR CA141103016Anti-Ice Valve · failed(CAN) ENROUTE, THE RIGHT ENGINE ANTI-ICE VALVE FAIL IN THE CLOSED POSITION. WITH FORECAST AND ACTUAL ICING CONDITIONS PRESENT AT ARRIVAL, AIRCRAFT DIVERTED. EAI VALVE REPLACED IAW AMM 30-21-02-401 EAI VALVE CONTROLLER REPLACED IAW AMM 30-21-03 PB 201 ENGINEOct 31, 2014 · Boeing 777333ER · Air Intake Anti/De-Ice SystemSDR CA141022002Tee Fitting · cracked(CAN) INCIDENT DETAILS: AFTER DEPARTURE, FLIGHT ENCOUNTERED A HYDRAULIC PROBLEM AND ELECTED TO DIVERT TO FRA WHERE AN OVERWEIGHT LANDING WAS CARRIED OUT. MTC CONTROL, FLEET MANAGER AND DUTY PILOT WERE ADVISED. RESOLUTION FOUND CRACK ON TEE FITTING OF FLAPERONOct 21, 2014 · Boeing 777333ER · Hydraulic System, MainSDR CA140926013Fmc · failed(CAN) INCIDENT DETAILS:PAN PAN DECLARED AT 40W DUE TO LOSS OF 2 FMCS. AUTOPILOT SERVICEABLE.REBOOTED SYSTEM,NOW OK,CANX PAN PAN WITH ATC.CARRYING ON RESOLUTION ON THE MAT FOUND MSG 31-83172 NOT ACTIVE. GRND TEST THROUGH MAT TEST PASS. NO FAULT HISTORY.Sep 25, 2014 · Boeing 777333ER · Flight ControllerSDR CA140912004Hydraulic Line · cracked(CAN) "HYD QTY LO C" E1CAS DURING CRUISE. QTY FELL FROM .40 TO .36 BY APPROACH. AFTER GEAR EXTENSION QTY FELL TO 0.28. LHR A/C MTCE.FOUND HYD.FLUID LEAKING FROM CRACK IN CENTRE RUDDER PCU RETURN LINE,LOCATED IN FWD.VERTICAL STAB,AREA IMMEDIATE ACTIONS TAKEN: Sep 7, 2014 · Boeing 777333ER · Hydraulic System, MainSDR CA140818008Tee Fitting · broken(CAN) APPROXIMATELY 5 HOURS INTO THE FLIGHT THE CREW REPORTED A RIGHT HYDRAULIC LOW QUANTITY INDICATION. FOUND THE RT HYD SYS TEE BROKEN. REPLACED THE TEE AND RT EDP.Aug 15, 2014 · Boeing 777333ER · Hydraulic System, MainSDR CA140602034Brake · overheated(CAN) ONCE ACFT ARRIVED AT GATE, FLIGHT CREW ADVISED OF HOT BRAKES AND 4 BLOWN TIRES. BLOWN TIRES, HAPPENED ON THE GATE NOT ON LANDING OR TAXI. ALL PASSENGERS, AND FLIGHT CREW WERE ON-BOARD, AND CRF WAS NOT REQUIRED. FOUND FUSE PLUG MELT ON WHEELS NR 1, 5, Jun 1, 2014 · Boeing 777333ER · Landing Gear Brake SystemSDR CA140522018Line · failed(CAN) DURING WALK AROUND FOUND HYD FLUID LEAKING FROM AFT BELLY DRAIN NEAR POTABLE WATER SERV PANEL. UPON FUTHER INSPECTION BULK CARGO, RT SIDE BEHIND WATER TANKS, FOUND HYD SYS RETURN LINE LEAKING. PN 272W4690-56. BS 2150 PIN HOLE IN RADIUS NEAR UNION RESOMay 10, 2014 · Boeing 777333ER · Hydraulic System, MainSDR CA140508006Lens · melted(CAN) LIGHTNING STRIKE ON CLIMBOUT AT APPROXIMATELY FL160 IN CLOUD AND LIGHT RAIN. MOST LIKELY THE NOSE AREA. MOC FOUND LT REAR WHITE NAV LIGHT- LENS COVER GLASS MELTED. REPLACED LT REAR WHITE NAV LIGHT LENS ASSY IAW AMM 33-43-02-960-802. SYSTEM CHECKED SMay 8, 2014 · Boeing 777333ER · Exterior LightingSDR CA140508001Control Unit · failed(CAN) EICAS ANTI-SKID MESSAGE, POSSIBLE HYDRAULIC LEAK TO 1 BOGEY. LANDING 15L WILL STAY ON RUNWAY FOR INSPECTION. FAULTED BRAKE SYS CONT UNIT. REPLACED IAW AMM 32-42-01, PB401 MAT TEST PASSED.May 7, 2014 · Boeing 777333ER · Brake Anti-Skid SectionSDR CA140407004Controller · failed(CAN) AFTER DEPARTURE, FROM PEAK FLIGHT HAD A LT ENGINE ANTI-ICE VALVE FAILURE ON ECAM. RE-SET INFLIGHT UNSUCCESSFUL. QRH PRECLUDED OPERATION INTO ICING CONDITIONS. EXPERIENCING ICING CONDITIONS AT ARRIVAL TIME. DECIDED TO DIVERT. LT ENGINE ANTI-ICE CONTROLApr 4, 2014 · Boeing 777333ER · Air Intake Anti/De-Ice SystemSDR CA131015002Unknown · odor(CAN) ACFT WAS ON THE GATE WITH THE ENGINE SHUTDOWN, SWITCHING TO EXTERNAL POWER WHEN THE EXTERNAL PLUG FELL OUT. THERE WAS AN ABRUPT POWER CHANGE, AND AN ELECTRICAL BURNING ODOR WAS NOTICED IN THE GALLEY AND CABIN. THE CREW BUNK SMOKE DETECTOR ALSO WENT OFFOct 12, 2013 · Boeing 777333ER · Air Distribution SystemSDR CA131007021Fan · failed(CAN) APPROXIMATELY 7 HRS IN TO FLIGHT, AN ELECTRICAL BURNING ODOR, OR AN ODOR OF MELTING PLASTIC WAS DETECTED IN THE MID GALLEY. ODOR RAPIDLY DISSIPATED. OCCURED CONCURRENTLY WITH STATUS MESSAGE RECIRCULATION FAN. REPLACED FWD UPPER RECIRCULATION FAN IAW Oct 5, 2013 · Boeing 777333ER · Air Distribution FanSDR CA131009009Unknown · odor(CAN) APPROXIMATELY 30 MINUTES BEFORE ARRIVAL THE CREW REPORTED THERE WAS AN ELECTRICAL ODOR IN THE CABIN FOR BRIEF DURATION. ON ARRIVAL THE CREW REPORTED NO FURTHER OCCURRENCE AFTER THE INITIAL REPORT OF THE ELECTRICAL ODOR IN THE CABIN. THEY DID REQUEST A PSep 30, 2013 · Boeing 777333ER · Air Distribution SystemSDR CA130906004Engine · leaking(CAN) WHILE ENROUTE, AN OIL LEAK DEVELOPED FROM THE LT ENGINE. THE CREW OBSERVED THE EICAS QUANTITY DECREASE BY 16 LITRES DURING CRUISE. RESULTING IN ENGINE CHANGE.Sep 1, 2013 · Boeing 777333ER · Turbine Engine Oil SystemSDR CA130604005Circuit Board · shorted(CAN) SHORTLY AFTER PUSHBACK, SMOKE STARTED COMING INTO THE CABIN THROUGH THE VENTS. CREW RETURNED TO GATE FOR DEPLANING OF PASSENGERS AND MAINTENANCE INVESTIGATION. FOUND QSEB 11K AT AFT RT J CLOSET INTERNAL CIRCUIT BOARD SHORTED DUE TO EVIDENCE OF DRIPPINGJun 3, 2013 · Boeing 777333ER · Electrical Power SystemSDR CA130313004Circuit Breaker · overheated(CAN) AFTER PUSHBACK AND PRIOR TO ENGINE START, A FAILURE OF THE CAPTAIN`S PFD, MFD, FMC, AUDIO PANEL, UPPER EICAS AND VHF-L WAS EXPERIENCED. THE ACFT RETURNED TO GATE AND THE FLIGHT WAS CANCELLED. MAINTENANCE INVESTIGATION FOUND EVIDENCE OF HEAT DAMAGE AND Mar 11, 2013 · Boeing 777333ER · AC Power Distribution SystemSDR CA130128016Outflow Valve · failed(CAN) THE FLIGHT CREW WAS UNABLE TO PRESSURIZE THE ACFT DURING DEPARTURE. IN CONJUNCTION WITH MAINTENENCE, FLIGHT DISPATCH & FLIGHT OPERATIONS, THE ACFT WAS DIVERTED BACK. THE FLIGHT MAINTAINED 9000FT ALTITUDE, WHILE "DUMPING" APPROXIMATELY 70,000 KG OF FUELJan 26, 2013 · Boeing 777333ER · Pressure Regulator/Outflow ValveSDR CA121217005Pump · failed(CAN) FUEL EMERGENCY DECLARED ON APPROACH. CENTER TANK FUEL SYS WOULD NOT SCAVENGE WITH 900 KGS, FUEL TRAPPED IN CENTER TANK. MINIMUM FUEL WAS 7.1 INCLUDING CENTER TANK TRAPPED FUEL, LANDED WITH 6.9 FOB. ASR TO FOLLOW IAW L4880810 CENTER TANK SCAVENGE BURNEDDec 14, 2012 · Boeing 777333ER · Fuel Boost PumpSDR CA121123004Regulator · corroded(CAN) ENGINEERING REQUEST A REGULATOR REPLACEMENT ON PASSENGER O2 BOTTLE NR 10. ON INSPECTION FOUND CORROSION ON THE REGULATOR AND SURROUNDING O2 BOTTLE AND SYSTEM COMPONENTS. THE CORROSION IS DUE TO LEAKING LAV WASTE LINE SITUATED ABOVE AFFECTED AREAS. DRIPJul 11, 2012 · Boeing 777333ER · Passenger Oxygen SystemSDR CA120626012Turbine · damaged(CAN) IAW CAMPAIGN 7-0018 CARRY OUT BORESCOPE INSPECTION OF THE HPT STAGE 2 NOZZLE AND HPT STAGE 1 STATOR SHROUD. IAW AMM 72-00-00-290-805, ITEM 7, N 4. HOLE FOUND IN FLOWPATH SURFACE GREATER THAN 31.61 MM AT TIME STOP 2.44 MINUTES OF THE VIDEO. L4601970 RAJun 25, 2012 · Boeing 777333ER · Turbine SectionSDR CA120529002Blades · damaged(CAN) REPORTED BY GROUND PERSONNEL SOMETHING HAS FALLEN OFF AN ACFT, HAS SHUTDOWN AN ENGINE AND IS IN THE PROCESS OF DUMPING FUEL AND RETURNING. AT 1000` AGL, RAPID EGT RISE RT ENGINE RAPID POWER LOSS. ENGINE SHUTDOWN. STAGE 6 TURBINE BLADES DAMAGED, AND TMay 28, 2012 · Boeing 777333ER · Turbine SectionSDR CA120525009Electrical Box · odor(CAN) CREW REPORTED A VERY STRONG ACRID ODOR AROUND SEAT 11A. QRH WAS CARRIED OUT AND A PHONE PATCH WITH MAINTENANCE CONTROL WAS ESTABLISHED. POWER WAS DISCONNECTED FROM THE AREA AND THE ODOR DISSIPATED. THE CREW INCREASED SPEED AND ELECTED TO DECLARE A PANMay 25, 2012 · Boeing 777333ER · Passenger Compartment EquipmentSDR CA120403004Line · leaking(CAN) RETURNED TO GATE DUE TO HYD QTY LOW LT EICAS DURING TAXI OUT. THE LT HYD SYS RESERVOIR WAS CONFIRMED TO BE PHYSICALLY LOW, BUT THERE WAS NO OBVIOUS EXTERNAL HYDRAULIC LEAKAGE SEEN. THE AIRPLANE WAS THEN ROUTED TO THE HANGAR FOR INVESTIGATION. DURING TRMar 31, 2012 · Boeing 777333ER · Hydraulic System, MainSDR CA110815005Oven · odor(CAN) CREW ADVISED FLIGHT DISPATCH AND MOC OF A BURNING ODOR COMING FROM NR 2 GALLEY. ALL OVENS AND CHILLERS WERE SHUTDOWN, ODOR DISSIPATED. ELECTRICAL ODOR FROM GALLEY NR 2 5HRS INTO FLT. OVENS TURNED OFF AND CHILLER OFF ODOR DISSIPATED. LT NR 2 GALLEY SHAug 13, 2011 · Boeing 777333ER · Buffet/GalleysSDR CA110718014Pitch Control · malfunctionedTAKEOFF REJECTED AT 30KTS DUE TO A FLIGHT CONTROL FAULT, FULL NOSE DOWN TRIM ON TAKEOFF ROLL. RETURNED TO GATE. WHEN T/O THRUST APPLIED CONFIG STABILIZER SOUNDED. TRIM WAS VERIFIED TO GREEN BAN AT 3.5 DURING T/O CHECK. FIM TASK 27-41-00-810-809 CARRIED OJul 12, 2011 · Boeing 777333ER · Stabilizer Position IndicatingSDR CA110708008Switch · failedSMOKE COMING FROM SEAT ROW 31 HJ. POWER REMOVED WITH IFE/PAX SWITCH. SMOKE STOPPED AND ELECTRICAL ODOR DECREASED AFTER REMOVAL OF POWER. DISPATCH AND MX ADVISED FOUND QSEB 31J AT FAULT. PART REPLACED SWITCH DOWNLOAD C/O. OPS OK. NO DAMAGE TO WIRING.Jun 27, 2011 · Boeing 777333ER · Equipment/Furnishings WiringSDR CA110615001Charger · failedODOR OF SMOKE IN THE COCKPIT, MAIN BATTERY & BATTERY CHARGER MAIN STAUS MESSAGES APPEARED. RETURNED TO LAND. DUMPED FUEL. FOUND MAIN BATTERY CHARGER AT FAULT MAIN 7 APU BATTERY, MAIN & APU BATTERY CHARGER. APU BATTERY DFD MEL 24-31-01B.Jun 14, 2011 · Boeing 777333ER · Battery/Charger SystemSDR CA110429003Line · leaking(CAN) FLIGHT CREW CALLED STATION TO REPORT THAT THEY LOST HYDRAULIC PRESSURE DURING TAXI TO THE GATE. MAINTENANCE AND TOW CREW CALLED FOR ASSISTANCE. MAINTENANCE HAD TO CAP THE NR 12 LINE AND THE ACFT WAS TOWED TO THE GATE. THE SPILL WAS 2 FT X 2 FT AND Apr 28, 2011 · Boeing 777333ER · Landing Gear Brake SystemSDR CA110127004Receptacle · burned(CAN) AIRCRAFT ARRIVED ON GATE WHILE CONNECTING THE GPU TO THE AIRCRAFT THERE WAS AN ELECTRICAL ARCH CAUSING DAMAGE TO THE GPU PANEL OF THE AIRCRAFT. MTCE WAS PRESENT AT THE AIRCRAFT AT THE TIME OF THE INCIDENT. MDC/GTAA WAS ADVISED. MTC HAS PUT THE AIRCRAFT OJan 25, 2011 · Boeing 777333ER · AC Power Distribution SystemSDR CA101224001Electrical Box · burned(CAN) DURING THE FLIGHT, A BRIEF FIRE STARTED UNDER SEAT THE 63E ELEX BOX. TWO (2) HALON BOTTLES WERE USED TO EXTINGUISH THE FIRE. ONCE OUT, A MEMBER OF THE CABIN CREW WAS ABLE TO REACH IN UNDER THE SEAT AND PULL THE WIRING OUT. THERE WAS NIL ADVERSE PASSENGERDec 23, 2010 · Boeing 777333ER · Entertainment SystemSDR CA101220004Cable · overheated(CAN) JUST NORTH OF DESTINATION THE CREW DETECTED AN ELECTRICAL BURNING SMELL FROM THE AREA OF SEAT 11A. POWER TO GALLEY AND ENTERTAINMENT SYSTEM WAS SHUT OFF AND THE SMELL DISSIPATED DETECTED LIGHT SCENT OF ELECTRICAL COMPONENTS AT STOWAGE COMPT INBD OF SEATDec 19, 2010 · Boeing 777333ER · Communications System WiringSDR CA101214004Window · cracked(CAN) APPROXIMATELY 4 HOURS AFTER DEPARTURE THE CREW REPORTED THE INSIDE PANEL OF THE FIRST OFFICERS WINDOW HAD CRACKED. THERE WAS NO ARCING AND NO PRESSURE LOSS. RT WINDSHIELD REPLACED AS PER AMM 56-11-00-200-801. WINDOW HEAT OPS TEST C/O, NO FAULTS FOUND.Dec 12, 2010 · Boeing 777333ER · Flight Compartment WindowsSDR CA101019013Wire Harness · chafedDURING TROUBLESHOOTING FOR MULTIPLE AUTOTHROTTLE DISCONNECT SNAGS FOUND WIRES W0770-2008B-20, W0770-2008R-20, W0770-2006B-20 AND W0770-2006R-20 CHAFED ON NR 2 ENG FAN CASE AT THE 12 O`CLOCK POSITION. WIRES TEMPORARILY REPAIRED UNDER PRODUCTION PERMIT B777-73-Oct 16, 2010 · Boeing 777333ER · Engine Control System WiringSDR CA100920002Elevator · unknownON DEPARTURE CREW ADVISED PROBLEM WITH LOAD/TRIM ON ROTATION. TAIL HEAVY, REQUIRED CHECK FWD TO STOP RAPID ROTATION. COLUMN FORCE TRANSDUCER TEST OK. ELEVATOR FEEL SYS TEST, OK. CARGO WEIGHT CHECK OK. UNABLE TO LOCATE EARLIER SNAG SERV.Sep 16, 2010 · Boeing 777333ER · Elevator Control SystemSDR CA100119004Housing · worn(CAN) THE DAMAGED FUEL FILTER WAS FOUND ON ALIAS B34/SN 906537. THIS ENGINE IS CURRENTLY INSTALLED ON 731 POSITION NR 1. PRODUCTION PERMIT 777-73-39874 HAS BEEN ISSUED TO COVER THE FRETTING FOUND. THE DAMAGE FOUND ON THE POWER PLANT WHEN IT WAS OFF WING. (THDec 15, 2009 · Boeing 777333ER · Engine Fuel DistributionSDR CA100119003Housing · worn(CAN) NR 1 ENGINE LP FUEL FILTER HSG AND FILTER SHOWING SIGNS OF WEAR. ATTACHED POWER POINT PRESENTATION SHOWS THE DAMAGED FOUND ON ENGINE NR 2. ENGINE NR 2 ALSO SHOWED SIGNS OF ARCHING AND THE PICTURE SHOWS WHAT APPEARS TO BE A BLACK HOLE. THE NR 1 ENGINE DIDec 15, 2009 · Boeing 777333ER · Engine Fuel DistributionSDR CA091215003Housing · damaged(CAN) DURING ROUTINE MAINTENANCE, IT WAS FOUND THAT BOTH LT AND RT ENGINE LP FUEL FILTER BOWLS HAD ARCHING DAMAGE. A REPLACEMENT HOUSING WAS ROBBED FROM A SERVICEABLE SPARE POWERPLANT BUT WAS FOUND WITH EVEN MORE SEVERE DAMAGE. ALL DAMAGED HOUSING REPLACED WDec 15, 2009 · Boeing 777333ER · Engine Fuel DistributionSDR CA091022003Software · malfunctioned(CAN) IN CRUISE AT FL380 ENROUTE TO YVR, AIRCRAFT HAD TEMPORARY LOSS OF BOTH PACKS. BOTH PACKS RETURNED WITHIN APPROX 10 SECONDS. P/N FOR ASCPC AND S/W GIVEN ABOVE. OUTFLOW VALVE PART NUMBER IS 2119160-2. PER IPC 21-31-03-01, THIS IS AN UNAPPROVED COMBINATIOct 7, 2009 · Boeing 777333ER · Cabin Pressure Control SystemSDR CA090811001Transmission · failedAFTER TAKE-OFF THE FLIGHT HAD A FLAPS GEAR DRIVE FAILURE WITH THE FLAPS IN A POSITION BETWEEN 5 AND 20. FLIGHT WAS UNABLE TO CONTINUE TO DESTINATION AND RETURNED TO DEPARTURE. THE FLIGHT WAS APPROX 75000K OVERWEIGHT AND CREW CALLED A PAN PAN EMERGENCY FOR LAJul 23, 2009 · Boeing 777333ER · Trailing Edge Flap Control SystemSDR CA090408003Transmission · malfunctioned(CAN) ACFT DEFECT LOG SNAG RAISED FOR FLAP DRIVE FAILURE WHEN RETRACTING FLAPS FROM 20 UNITS TO 5 UNITS. DURING FAULT ISOLATION, FOUND NR 8 TRANSMISSION WITH (TRIPPED) TORQUE INDICATOR. INDICATOR RESET. HIGH LIFT SYS GROUND TEST CARRIED OUT AND TRIP INDICATORApr 6, 2009 · Boeing 777333ER · Trailing Edge Flap Control System
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