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Accident Bulletin 1/2010 - Preliminary Report on Airbus A330-342 ...

Accident Bulletin 1/2010 - Preliminary Report on Airbus A330-342 ...

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Aircraft <str<strong>on</strong>g>Accident</str<strong>on</strong>g> <strong>on</strong> CPA 780 <strong>on</strong> 13 April <str<strong>on</strong>g>2010</str<strong>on</strong>g>(<strong>Airbus</strong> <strong>A330</strong>-<strong>342</strong> Registrati<strong>on</strong> Mark B-HLL)(All times are in UTC.hours.)Surabaya time is UTC+7 hours and H<strong>on</strong>g K<strong>on</strong>g time is UTC+81. Cathay Pacific Airways (CPA) flight number CPA 780 was scheduled to operate fromthe Juanda Internati<strong>on</strong>al Airport (WARR), Surabaya, Ind<strong>on</strong>esia to the H<strong>on</strong>g K<strong>on</strong>gInternati<strong>on</strong>al Airport (VHHH) <strong>on</strong> 13 April <str<strong>on</strong>g>2010</str<strong>on</strong>g> with a scheduled time of departure(STD) at 0120 hours (hr) and scheduled time of arrival (STA) at 0600 hr. The actualand forecast weather al<strong>on</strong>g the flight plan route, including the departure and arrivalairports, were c<strong>on</strong>sidered acceptable by the flight crew. There was no enginesystem-related or fuel system-related defect reported in the maintenance log of theaircraft prior to departure. The actual Take Off Weight (TOW) was around 198,700kilograms (kg), with a total of 33,400 kg of Jet A-1 fuel, including 24,400 kg of fueluplifted at stand number 8 at WARR where the aircraft was parked before departure.2. The aircraft took off from runway 28 at 0124 hr. The departure was uneventful andwas away from any significant weather. During the climb, the flight crew noticedsome minor Engine Pressure Ratio (EPR) fluctuati<strong>on</strong>s <strong>on</strong> No. 2 engine. No. 1 enginealso had EPR fluctuati<strong>on</strong>s but within a narrower range.3. At 0158 hr, when the aircraft was leveling off at Flight Level (FL) 390 (i.e. 39,000 feetabove mean sea level at standard atmosphere), the Electr<strong>on</strong>ic Centralised AircraftM<strong>on</strong>itoring (ECAM) message “ENG 2 CTL SYS FAULT” was annunciated. Theflight crew followed the ECAM procedures. They also c<strong>on</strong>tacted the “MaintenanceC<strong>on</strong>trol” (MC) of the CPA Engineering Department for technical advice. Thecompany’s Operati<strong>on</strong>s Manuals were reviewed. As parameters <strong>on</strong> both engines werenormal except the slight fluctuati<strong>on</strong> of the EPR indicati<strong>on</strong>s, both the flight crew and theMC were satisfied that it was safe for the flight to c<strong>on</strong>tinue.4. At 0316 hr, ECAM message “ENG 2 CTL SYS FAULT” reappeared. CPA 780c<strong>on</strong>tacted MC to discuss and review the issue again. As all engines parametersremained normal except the EPR fluctuati<strong>on</strong>s, both the flight crew and the MC weresatisfied that it was safe for the flight to c<strong>on</strong>tinue to VHHH.

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