Incident Overview

Description
Tuninter flight 1153, an ATR 72-202, crashed into the sea after a los of engine power due to fuel exhaustion, killing 16 occupants; 23 survived the accident. On August 5, 2005 Tuninter’s ATR-72 TS-LBB arrived at Tunis Airport with 790 kg of fuel left in the fuel tanks. During maintenance the Fuel Quantity Indicator (FQI) was changed. Erroneously the FQI for ATR-42 aircraft was installed. The normal operation of the FQI is to processes the signal coming from the capacitance probes installed in the tanks with an algorithm typical for each aircraft, depending on tank shape, size and number of probes installed. The indication of the amount of fuel on board the airplane now read 3050 kg instead of 790 kg. On August 6 the airplane was prepared for flight 152F to Bari. An amount of 465 kg fuel was added for the flight (total fuel: 1255 kg, with 3800 kg indicated). Upon landing at Bari only 305 kg were left in the tanks. Normally this should have triggered a ‘LO LVL’ warning, but the FQI read 2300 kg, which made the crew believe they had plenty of fuel left. In preparation for the flight to Djerba, just 265 kg of fuel was added. The flight departed with 2700 kg of fuel indicated by the FQI (actual amount: 570 kg). En route, at 15:24 the crew contacted Palermo for an emergency landing. They had run out of fuel and both engines had quit. Their FQI nevertheless showed 1800 kg of fuel. They did not make it to Palermo and ditched in the sea around 15:40. CAUSE AND CONTRIBUTING FACTORS: The accident under examination, as most aviation accidents, has been determined by a series of events linked one another, which caused the final ditching. The ditching was primarly due to the both engines flame out because of fuel exhaustion. The incorrect replacement of the fuel quantity indicator (FQI) was one of the contributing factors which led irremediably to the accident. The accident’s cause is therefore traceable firstly to the incorrect procedure used for replacing the FQI, by means of the operator’s maintenance personnel. This shall be considered the disruptive element, which caused the final ditching of the aircraft due to the lack of fuel that caused the shutdown of both engines. As said before the accident was determined by a series of events (contributing factors) linked one another. Hereafter are listed some considered of major importance. – Errors committed by ground mechanics when searching for and correctly identifying the fuel indicator. – Errors committed by the flight crew: non-respect of various operational procedures. – Inadequate checks by the competent office of the operator that flight crew were respecting operational procedures. – Inaccuracy of the information entered in the aircraft management and spares information system and the absence of an effective control of the system itself. – Inadequate training for aircraft management and spares information system use and absence of a responsible person appointed for managing the system itself. – Maintenance and organization standards of the operator unsatisfactory for an adequate aircraft management. – Lack of an adequate quality assurance system; – Inadequate surveillance of the operator by the competent Tunisian authority. – Installation characteristics of fuel quantity indicators (FQI) for ATR 42 and ATR 72 which made it possible to install an ATR 42 type FQI in an ATR 72, and viceversa. The analysis of various factors that contributed to the event has been carried out according to the so called Reasons “Organizational accident” model. Active failures, which had triggered the accident, are those committed both by ground mechanics/technicians the day before the event while searching for and replacing the fuel quantity indicator, and by the crew who did not verify and fully and accurately complete the aircrafts documentation, through which it would have been possible to perceive an anomalous situation regarding the quantity of fuel onboard. Latent failures, however, remained concealed, latent in the operator’s organizational system until, some active errors (by mechanics and pilots) were made, overcoming the system’s defence barriers, causing the accident. Analysing latent and active failures (errors) traceable to various parties, involved in the event in several respects, it clearly emerges that they were operating in a potentially deceptive organizational system. When latent failures remain within a system without being identified and eliminated, the possibility of mutual interaction increases, making the system susceptible for active failures, or not allowing the system to prevent them, in case of errors. Active failures were inserted in a context characterised by organizational and maintenance deficiencies. The error that led to the accident was committed by mechanics who searched for and replaced the FQI, but this error occurred in an organizational setting in which, if everybody were operating correctly, probably the accident would not have occurred. Inaccuracy of information entered in the aircraft management and spares information system, particularly regarding the interchangeability of items and the absence of an effective control of the system itself, has been considered in fact one of the latent failures that contributed to the event. The maintenance and organization standards of the operator, at the time of event, were not considered satisfactory for an adequate management of the aircraft. The flight crew and maintenance mechanics/technicians involved in the event,
Source of Information
http://www.skybrary.aero/index.php/AT72,_en-route,_Mediterranean_Sea_near_Palermo_Italy,_2005_(AW_LOC_HF)http://www.skybrary.aero/index.php/AT72,_en-route,_Mediterranean_Sea_near_Palermo_Italy,_2005_(AW_LOC_HF)Primary Cause
Incorrect fuel quantity indicator replacement by the operator’s maintenance personnel. The faulty FQI caused an erroneous reading of 3050 kg, which was subsequently compounded by additions of 465 kg and 265 kg of fuel, leading to the aircraft’s ditching.Incorrect fuel quantity indicator replacement by the operator’s maintenance personnel. The faulty FQI caused an erroneous reading of 3050 kg, which was subsequently compounded by additions of 465 kg and 265 kg of fuel, leading to the aircraft’s ditching.Share on: