air serv international – beechcraft 1900c-1 (zs-old)
Transcription
air serv international – beechcraft 1900c-1 (zs-old)
AIR SERV INTERNATIONAL – BEECHCRAFT 1900C-1 (ZS-OLD) Background Information Page 1 Background Facts and Potential Cause Analysis Aubin N.Mabanza Avocat a la Cour KLAM & Partners 4955 Avenue de la Gombe Kinshasa - Gombe Democratic Republic of Congo On the 1st of September 2008, a Beechcraft 1900C-1, registration ZS-OLD operated by Air Serv International, departed Kinshasa Airport on a humanitarian flight to Goma (GOM). En route stops were made in Mbandaka (MDK) and Kisangani (FKI). The last stop before Goma would be Bukavu (BKY), a one hour flight from Kisangani. En route to Bukavu, the aircraft flew into a steep ridge, some 15 km northwest of Bukavu. The crash site is at about 9000 ft - 10000 ft above sea level and is a steep slope of mount Kahuzi. The area is thick jungle. The 2 crew and 15 passengers were killed. Bernard Solitude Avocat a la Cour Cabinet d’avocats Bernard Solitude 7 rue de la Bourse Paris France Noel Enzouni Avocat a la Cour Cabinet NOEL ENZOUNI & Associates Immeuble Basile Local 11 avenue du Commerce Kinshasa - Gombe Democratic Republic of Congo Calehr & Associates 2700 Post Oak Boulevard, Suite 1220 Houston Texas 77056 Stewarts Law LLP 5 New Street Square London EC4A 3BF Tel: +44 (0)20 7822 8000 Fax: +44 (0)20 7822 8080 Website: www.stewartslaw.com Email: [email protected] There is very little information on what caused the crash other than the location and the fact that contact was lost. Reports indicate that the weather conditions were poor at the time meaning that if the aircraft entered cloud it would have to ensure that it stayed above its safety altitude in the mountainous terrain and fly a published instrument approach into Bukavu. The location of the crash is approximately on the track it would have been flying from Kinsangani Airport. In this location the Minimum Safe Altitude (MSA) is 12400 ft because of the line of mountains west northwest of Bukavu. The height the Beechcraft crashed was AIR SERV INTERNATIONAL – BEECHCRAFT 1900C-1 (ZS-OLD) Background Information Page 2 over 2000 ft below the MSA. The MSA is shown on the Global Navigation Satellite System (GNSS) approach chart. The GNSS approach for Bukavu (Runway 35) shows that at the starting points for the approach (OLSON and DOPEM), which are south/ southwest of the airfield, an aircraft should be at or above 11000 ft. For some reason the Air Serv Beechcraft descended early ( while over mountains) northwest of the airfield, below its safety altitude of 12400 ft and below the 11000ft starting altitude for the published approach. As a result of this descent the aircraft crashed near the top of the mountain ridge. There are no reports/ record of any emergency transmissions from the aircraft. MSA Crash site - on mountains approx 15 KM northwest of Bukavu at 9000 – 10000 ft BUKAVU AIRPORT GNSS start point GNSS start point GNSS Approach Chart - Bukavu AIR SERV INTERNATIONAL – BEECHCRAFT 1900C-1 (ZS-OLD) Background Information Page 3 Beechcraft 1900C-1 Registration ZS-OLD The accident aircraft, a Hawker Beechcraft 1900 C-1, is a 19-passenger, pressurized twin-engine turboprop airplane manufactured by the Beech Aircraft Corporation, previously the Beechcraft Division of Raytheon and now a unit of Hawker Beechcraft. It was designed as and is primarily used as a regional airliner. It is powered by two PT6A turbine engines, which are manufactured by Pratt & Whitney Canada, a Canadian aircraft engine manufacturer. Beechcraft 1900C-1 The Air Sev Beechcraft was built in 1990 and owned by CemAir, based in South Africa. It was being leased to Air Serv International which is a not for profit aviation organization based in America. Potential Causes of the accident This crash is one of 5 Beechcraft 1900 crashes in 2008. In total there have been 27 catastrophic Beechcraft 1900 crashes since 1987. The Democratic Republic of Congo is conducting an accident investigation into the Bukavu crash but the report will take some time. Fortunately the Accident Data Recorder (ADR) has been recovered which will hopefully enable the investigators to determine the cause(s) of the accident. Until the final report is made available there are limited facts, which mean any accident analysis at this stage cannot determine the exact cause of the crash. As there are many potential factors that could have contributed to the crash, this analysis will only on focus on 4 potential causes at this stage, namely, controlled flight into terrain, faulty flight instruments, weather and engine failure. 1. Controlled Flight into Terrain (CFIT). CFIT describes an accident whereby an airworthy aircraft, under pilot control, inadvertently flies into terrain, an obstacle, or water. The pilots are generally unaware of the danger until it is too late. The incidents often involve AIR SERV INTERNATIONAL – BEECHCRAFT 1900C-1 (ZS-OLD) Background Information Page 4 impact with significantly raised terrain such as hills or mountains, and may occur in conditions of clouds or otherwise reduced visibility. CFIT often occurs during aircraft descent to landing, near an airport. If the pilot is using automated systems to fly and navigate the aircraft, he must ensure that the data he inputs into those systems is correct. If it is incorrect, the pilot may mistakenly believe that he is over low ground when in fact he is on a collision course with high ground. An example of this situation is Air New Zealand Flight 901, a McDonnell Douglas DC-10-30 that crashed into Mount Erebus, killing all 237 passengers and 20 crewmembers aboard because the crew made a mistake when entering the flight coordinates into the aircraft computer. CFIT can also occur when a pilot descends into cloud believing, through visual illusion/ mistake, that below (or between a break in the cloud) there is good clearance from terrain and good visibility, enabling him to fly visually below the cloud. An example of a pilot mistakenly flying a Beechcraft into terrain in similar circumstances is a Raytheon Aircraft Ferry Flight of a Beechcraft 1900C on 9 December 2002. This case involved the pilot descending and crashing into a mountain ridge which was below a layer of cloud. 2. Flight Instrument Fault CFIT may be associated with equipment malfunction. Malfunction of the flight instruments or navigation equipment can confuse/ distract crew and cause them to fly the aircraft into the ground. Beechcraft 1900C-1 flight instruments Pilots rely on the flight instruments to fly the aircraft safely. The primary flight instruments display information to the pilot so that he knows what the aircraft is doing in terms of roll, pitch, speed, height and heading. Attitude Indicator (AI) – shows roll and pitch Airspeed Indicator (ASI) Horizontal Situation Indicators (HSI) Show heading/ navigation information Altimeter – displays height In good visibility, the pilot is not totally reliant on the flight instruments but can also use visual cues to fly. AIR SERV INTERNATIONAL – BEECHCRAFT 1900C-1 (ZS-OLD) Background Information Page 5 While in cloud he will be totally reliant on the instruments. If the Air Serv Beechcraft entered cloud and there was a fault with any of the flight instruments, the aircraft could have ended up in an unusual flight parameter which would have been difficult to recover from and or distracted the pilots, resulting in a loss of height and possible descent below the safety altitude. Beechcraft Autopilot/ Global Positioning System (GPS). The pilots engage these systems to fly the aircraft automatically and to navigate in all weather conditions. If there is a fault in these systems that is not noticed promptly, the aircraft can end up in a dangerous flying attitude and/ or stall causing it to descend. Furthermore, if there is a fault in the GPS/ navigation systems the displayed position of the aircraft may be incorrect which could lead the crew to start a descent too early. As with many other passenger aircraft, the Air Serv Beechcraft 1900C-1 had a Ground Proximity Warning System (GPWS), probably manufactured in the USA by Sundstrand/ Honeywell, which uses a Radar Altimeter to assist in calculating terrain closure rates. When this system senses the aircraft is going to collide with the ground, it gives an audible warning and tells the pilot to “pull up”. Unfortunately, there have been previous accidents in a number of different types of aircraft where the GPWS systems have not given the prior warning they were designed to, resulting in the aircraft crashing into the ground. Examples of this are the Ansett New Zealand DHC-8-102 flight on 9 June 1995 and the Garuda Airbus A300 crash on 26 September 1997. Ansett New Zealand DHC-8-102: During an instrument approach in cloud to Palmerston North Airport(PMR), New Zealand, the aircraft descended below the glideslope and crashed. The Sundstrand GPWS audio alarm sounded only 5 seconds before impact when it should have given a 17 second warning. 1 crew and 3 passengers were killed. Garuda Airbus A300 Flight 152: All 224 occupants were killed when this aircraft crashed 18 miles from its destination airfield. There has been a successful lawsuit by the Wisner Law firm concerning the late proximity warning by the Sundstrand GPWS system because it only gave a 5 seconds warning instead of an 18 – 23 seconds warning. Further information on how well the flight instruments, autopilot, GPS and GPWS were performing in the Air Serv Beechcraft is required to determine if a fault in these systems caused/ contributed to the crash. 3. Weather As the Air Serv Beechcraft was flying over mountainous terrain, adverse weather may have caused it to lose height. Two factors that can cause this are thunderstorms and airframe icing. If an aircraft enters a thunderstorm, it can experience severe updrafts and downdrafts and in addition to large hailstones, damaging lightning, torrential rain and airframe icing, all of which are potentially hazardous to aircraft. AIR SERV INTERNATIONAL – BEECHCRAFT 1900C-1 (ZS-OLD) Background Information Page 6 Due to the dangers, pilots should avoid flying within 5 miles of a thunderstorm. They do this by analysing the weather forecast before flight and monitoring the weather radar during flight. If the Beechcraft pilots flew close to a thunderstorm and encountered severe turbulence, this could be the reason it ended up descending over 2000 ft below safety altitude. Also, when flying in cloud the droplets of water in the cloud can be at a temperature lower than zero degrees Celsius, known as “super cooled”. When these droplets come into contact with the surface of the aircraft they freeze onto the surface. In severe icing this can adversely affect the aerodynamics of the aircraft, restrict the movement of flying controls and cause the engines to lose power. This can lead to a descent/ departure from controlled flight. In-flight icing on the leading edge of a wing Because of the dangers of icing, the Beechcraft 1900C-1 has an airframe anti-icing system manufactured by Goodrich, USA. Analysis of the ADR should reveal whether the Air Serv Beechcraft was in icing conditions and whether the anti-icing system was working correctly. 4. Engine problems. Aircraft engines can fail for a number of reasons such as mechanical failure, fuel contamination/ blockage, and fire. Twin engine passenger aircraft are designed so that they can fly safely on one engine. Single engine (asymmetric) flight is more difficult because there is much less thrust available and the aircraft thrust vector is out of balance, meaning the aircraft always wants to veer (yaw) towards the side where the failed engine is – e.g. if the failed engine is on the left wing the aircraft will want to veer left and vice versa. Properly trained and experienced flight crew are constantly practicing this kind of emergency in flight simulators and should have no difficulty in flying the aircraft by applying appropriate rudder (controls yaw), aileron (controls roll) and power inputs. If the flight crew of the Beechcraft had the appropriate experience and training, a single engine failure on its own would not have caused the crash – there would have to be an additional failure such as problems with both AIR SERV INTERNATIONAL – BEECHCRAFT 1900C-1 (ZS-OLD) Background Information Page 7 engines, adverse weather, or fire. Alternatively, if the crew were inexperienced and/ or not properly trained, the handling pilot may have mishandled the aircraft by not controlling the asymmetric thrust induced yaw and or not efficiently managing the 50% reduction in thrust, resulting in an uncontrolled descent or the aircraft stalling and dropping out of the sky. Two examples of Beechraft 1900C engine failures are Southern Air Charter in October 2004 and Southern Sudan Air Connection in May 2008. Southern Air Charter Flight 204: During flight the right engine lost power and eventually the engine failed. Unfortunately, while approaching to land , the left engine also lost power resulting in the aircraft ditching short of the runway. Fortunately all occupants survived. Southern Sudan Air Connection: The Beechcraft 1900C-1 departed Wau, Sudan on a flight to Juba, Sudan via Rumbek. Near Rumbek the pilot reported engine problems then the aircraft crashed killing all 21 on board. The accident investigation is ongoing and there is speculation that both engines failed. As for Air Serv International, this Southern Sudan Air Connection Beechcraft was owned by CemAir. Stewarts Law is representing the families of 15 passengers. Other factors As has already been explained, there is not yet enough evidence to say exactly what caused the crash – other factors such as fire, electrical problems, flying control malfunctions etc could have caused/ contributed to the accident. The scenarios set out in paragraphs 1 – 4 above are possibilities based on the limited evidence that is available at this time. Liability Investigation The families of those who were killed have the right to seek compensation for the damage they have suffered against various potential defendants. Viable potential targets for liability include the following: 1. 2. 3. 4. 5. 6. 7. Hawker Beechcraft – the designer and manufacturer of the Beechcraft 1900C-1, based in the USA. Pratt & Whitney – as the manufacturer of the engines, based in the USA. Various component/ sub-component manufacturers of flight instruments and flight critical products on the Beechcraft 1900C-1. Air Serv International, based in the USA – as air carrier and lessee of the aircraft, Air Serv International have specific responsibilities for their passengers and crew. CemAir – the owner of the aircraft, based in South Africa. Atlantic Turbines – the company responsible for the maintenance and overhaul of aircraft engines for CemAir, based in Canada and the USA. Insurers and re-insurers of the potential targets, mostly based in London, UK.