La seguridad aérea es de interés público y afecta a toda la sociedad (Javier Aguado del Moral)


In times of universal deceit, telling the truth becomes a revolutionary act (George Orwell)


Cuando el sabio señala la luna, el necio se queda mirando el dedo (Confucio)

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Mostrando entradas con la etiqueta SKYBRARY. Mostrar todas las entradas

viernes, 28 de noviembre de 2014

FALLO DE MOTOR POR CHOQUE CON AVE EN EL AEROPUERTO ADOLFO SUÁREZ DE MADRID-BARAJAS


El pasado domingo, 23 de noviembre, sobre las 20:50 hora local (19:50 UTC), el vuelo EZY58GD, un Airbus 319 de la compañía EasyJet, declaró emergencia al poco tiempo de despegar desde la pista 36R del Aeropuerto Adolfo Suárez de Madrid-Barajas, debido a la ingestión de un ave por uno de sus motores.
En el artículo de Aviación Digital (Mayday, Mayday, Bird strike!), que reproducimos a continuación, contrastan dos formas muy diferentes de gestionar, por parte de la tripulación, la emergencia de fallo de motor en despegue por ingestión de ave.

El caso del EZY58GD

Si el lector pulsa en el enlace situado más abajo su navegador le llevará directamente a la aplicación FLIGHTRADAR24.COM y asistirá al momento (19:50 UTC) en que el EZY58GD despega de Barajas, a cómo una vez notificada la emergencia recibe las primeras instrucciones del ATC para volver al aeropuerto, y a cómo un par de minutos después el controlador tiene que quitar de en medio a un vuelo de Air Europa y a otro de Ryanair (este a la misma altitud que el avión de la emergencia) para evitar males mayores, ya que la tripulación en realidad no tenía la intención de aterrizar inmediatamente porque debía realizar comprobaciones y porque determinados virajes habituales no serían posibles con un motor dañado o parado.

El video no contiene audio, pero aun sin audio se adivina que la tripulación no informó adecuadamente de la incidencia exacta que su avión tenía, salvo su intención de volver a Barajas para aterrizar. Nada de que necesitaba ir a un lugar cercano donde hacer las comprobaciones necesarias marcadas por su manual para este tipo de situaciones y nada concreto de qué motor era el afectado y qué maniobrabilidad tenía el avión. El resto fue, a buen seguro, una continua sorpresa para los controladores aéreos de Aproximación Madrid porque está claro que el avión de la emergencia cruzó los localizadores de las pistas 32R y 32L y que navegó sin previo conocimiento del ATC por un espacio aéreo que, en principio, no era previsible que ocupara y en el que se encontraban en ese momento otros aviones.

Enlace Flightradar

A continuación, aparecen unos pantallazos del video del suceso en los que se aprecia a los aviones implicados uno frente a otro, así como sus respectivas trayectorias voladas.




El caso del TOM263H

El 29 de abril de 2007, el vuelo TOM263H, un Boeing 757 de la compañía británica de bajo coste Thomsonfly con 221 personas a bordo, despegaba del aeropuerto de Manchester a las 9:30 de la mañana con destino a Lanzarote cuando justo tras la rotación dos pájaros fueron ingeridos por el motor derecho. El momento fue captado por un video aficionado.

En el siguiente enlace al video de Youtube aparece la secuencia completa de la emergencia, incluidas las comunicaciones con el control aéreo. En el mismo se puede apreciar que el comandante del avión informa en todo momento al ATC de cuáles van a ser sus siguientes movimientos así como sus necesidades tanto en vuelo como en tierra. También se adjunta un enlace a la transcripción de las comunicaciones.

Desde entonces el video y el audio de esta experiencia forman parte del material de entrenamiento de muchas compañías aéreas, aunque es evidente que no de todas. Video Emergencia TOM263H



Transcripción de las comunicaciones del video

No vamos a hacer juicios de valor respecto a este asunto porque se explica por sí mismo. Lo que sí nos preguntamos es si las autoridades británicas se interesarán por profundizar en el análisis del desarrollo de la emergencia del vuelo de Easyjet y en sacar enseñanzas que puedan contribuir a la mejora de la formación de las tripulaciones de todo el mundo.
Ya sabemos que las autoridades españolas, suponiendo que aquí tengamos de eso, no van a hacer absolutamente nada útil al respecto.


Las colisiones con aves en las cercanías del Aeropuerto Adolfo Suárez de Madrid-Barajas son un suceso más frecuente de lo que sería deseable. Incluimos los primeros párrafos del artículo Colisiones con aves en el Aeropuerto de Madrid-Barajas, publicado en Las mentiras de Barajas el 25 de mayo de 2012

COLISIONES CON AVES EN EL AEROPUERTO DE MADRID-BARAJAS

El Aeropuerto de Madrid-Barajas limita al oeste con la ciudad de Madrid, al este con el río Jarama, los cerros de Paracuellos y el espacio aéreo de Torrejón, al sur con las poblaciones Coslada y San Fernando, y al norte con los términos municipales de San Sebastián de los Reyes, Algete y Cobeña.

Los márgenes del río Jarama están densamente arboladas, y en ellas habita una variada avifauna. Para evitar incidentes con aves el Aeropuerto dispone Servicio de Control de Fauna, creado por Félix Rodríguez de la Fuente, y que desde hace 40 años controla Jesús Rero, con unos 38 halcones que se encargan de mantener libre el espacio aéreo del área de influencia aeroportuaria.

Cuando el aeropuerto opera en la llamada configuración norte, los aviones que salen atraviesan parajes naturales, como el Soto de Viñuelas a la altura de Fuente el Fresno y Ciudalcampo, la cuenca alta del Manzanares, el valle del Jarama a la altura de la urbanización Pradonorte y la Zepa de Algete, donde habitan, campean y transitan multitud de rapaces; entre ellas el buitre leonado, el buitre negro y el águila imperial. Antes de julio de 2005 los aviones atravesaban el Monte del Pardo, donde residen también estas emblemáticas especies. Desde la inauguración de la primera ampliación del aeropuerto, en noviembre de 1998, son frecuentes los incidentes cuando los aviones sobrevuelan estos espacios naturales.

En configuración sur, las aproximaciones se llevan a cabo por el pasillo que forman la carretera A-1 y el valle del Jarama, y no tenemos constancia de ninguna colisión. Además los despegues resultan más peligrosos porque los motores van a máxima potencia y el impacto de un pájaro puede causar mayores daños.


Lo ocurrido el pasado domingo fue un suceso que pudo tener consecuencias graves por diversas razones, y probablemente la más relevante sea la falta de comunicación entre la tripulación y el control. Este avión al sufrir un fallo de motor debería haber aplicado el procedimiento de fallo de motor. Recordamos que si bien son específicos de cada compañía, los aprueba la Agencia Estatal de Seguridad Aérea (AESA), lo cual no es algo tranquilizador sino todo lo contrario.

Dado que los despegues en Barajas desde las pistas 36R y 36L se producen de forma simultánea y en paralelo, el procedimiento de fallo de motor de una aeronave que despega por la pista 36R obliga a los pilotos a abandonar la salida estandarizada y a girar a la izquierda, con el riesgo de impacto contra los aviones que despegan de la pista 36L. (Ver RIESGO DE IMPACTO DE AERONAVES EN EL ESPACIO AÉREO 2).

La tripulación del Airbus 319 de la compañía Easy Jet, al no informar al control de su incidente, y abandonar la salida estandarizada y, por así decirlo de modo coloquial, ponerse a dar vueltas, provocó una situación de riesgo cierto dado que el Barajas es un aeropuerto con un tráfico muy alto. Comparada con la del vuelo TOM263H en Manchester su actuación puede ser calificada de negligente.

Finalmente adjuntamos el enlace de Skybrary en el que se describe y analiza el incidente que sufrió un Boeing 767-300 de la compañía Qantas, con origen en Melbourne y destino en Sidney (Australia), que se encontró con una bandada de pájaros durante Vr en el momento del atardecer, aunque todavía con visibilidad normal, y que sufrió varios impactos en su fuselaje y fallo en el motor del ala izquierda. Finalmente la tripulación decidió continuar con el viaje a destino y no volver al aeropuerto de Melbourne. Una decisión tomada con todas las precauciones y que pone de manifiesto que habían recibido una formación adecuada.

miércoles, 2 de abril de 2014

AQUAPLANING: A SKYBRARY ARTICLE




A SKYbrary article.

Aquaplaning

Source: www.skybrary.aero

Categories: Theory of Flight | Enhancing Safety | Overrun on Landing | Directional Control | Runway Excursion

Description

Aquaplaning, also known as hydroplaning, is a condition in which standing water, slush or snow, causes the moving wheel of an aircraft to lose contact with the load bearing surface on which it is rolling with the result that braking action on the wheel is not effective in reducing the ground speed of the aircraft.

Interestingly, Water Skiing was originally called Aquaplaning and was carried out on a simple board which underlines that the physics of aquaplaning works at very low speeds by aviation standards. Aquaplaning is also highly relevant to cars at speeds as low as 40 mph.

The continued incidence of aquaplaning reduces the braking co-efficient to that of an icy or "slippery" runway - less than 20% of that on an equivalent dry runway.

Causal Factors

A layer of water builds up beneath the tyre in increasing resistance to displacement by the pressure of the wheel. Eventually, this results in the formation of a wedge between the runway and the tyre. This resistance to water displacement has a vertical component which progressively lifts the tyre and reduces the area in contact with the runway until the aircraft is completely water-borne. In this condition, the tyre is no longer capable of providing directional control or effective braking because the drag forces are so low. If such a runway surface state prevails, then flight crew are required to make their aircraft runway performance calculations using "slippery runway" data; this specifically allows for poor deceleration. They must also take account of crosswind component limits in the AFM which make allowance for less assured directional control.

Aquaplaning can occur when a wheel is running in the presence of water; it may also occur in certain circumstances when running in a combination of water and wet snow. Aquaplaning on runway surfaces with normal friction characteristics is unlikely to begin in water depths of 3mm or less. For this reason, a depth of 3mm has been adopted in Europe as the means to determine whether a runway surface is contaminated with water to the extent that aircraft performance assumptions are liable to be significantly affected. Once aquaplaning has commenced, it can be sustained over surfaces and in water depths which would not have led to its initiation.

In the case of the most common type of aquaplaning, called dynamic aquaplaning (see below), a simple formula (Horne's formula) exists for calculating the minimum groundspeed for initiation of this type of aquaplaning on a sufficiently wet runway based upon tyre pressure where V = groundspeed in knots and P = tyre inflation pressure in psi:

V = 9 x √P

This formula is based upon the validation of hydrodynamic lift theory by experimental evidence. For many modern tires the constant maybe closer to 6 or 7 rather than 9. With a typical tyre pressure of about 150 psi, √P will be 12.25 so aquaplaning is possible down to about 70 knots. The effect of the relationship demonstrated is that most jet aircraft, even relatively small ones, have a significant ‘window’ for the initiation of dynamic aquaplaning during a landing near to the maximum approved weight and an even larger one in the case of a high speed rejected take off. It assumes that tyre pressure and tread depth are both within allowable AMM limitations.

Types of Aquaplaning

• Dynamic aquaplaning is that which does not begin unless the groundspeed as given by Horne’s formula above is exceeded. It leaves no physical evidence on tyre or runway surface.

• Viscous aquaplaning arises in the same way as dynamic aquaplaning, but only on abnormally smooth surfaces such as touchdown zones contaminated with excessive rubber deposits, where it may begin and continue at any ground speed. Typically, a small amount of water may mix with a surface contaminant. a significantly thinner layer of contaminant is required in the event of viscous aquaplaning, compared to that required for dynamic aquaplaning. It too leaves no physical evidence on tyre or runway surface.

• Reverted rubber aquaplaning occurs when the heat of friction from a locked wheel in contact with the surface causes the rubber to revert to its un-cured state and 'boils' the surface moisture into steam. The pressure of the steam raises the centre of the tyre off the surface whilst the edges remain in contact, forming a seal that temporarily traps the steam. The tyre will show clear evidence of rubber reversion and the runway surface will be clearly marked with the path of the wheels as a result of ‘steam pressure cleaning’ beneath the tyre. This is the only type of aquaplaning which leaves physical evidence on the runway surface. It was much more common before anti-skid units became widespread and usually only occurs to aircraft so fitted if an emergency brake, which is applied directly rather than through the anti-skid units, is used.

Dry Runway Friction

The friction status of a dry runway surface must be assessed periodically under the terms of ICAO TPN 13. It should also be re-assessed after any maintenance which might have affected the surface smoothness. Dry runway friction is directly related to the lesser friction when a runway is wet and this affects the braking coefficient. The ICAO guidelines are not prescriptive in detail and so a range of interpretations is possible. In particular, averaging of measured friction along a whole runway or even significant lengths of it can conceal considerable variation since averaging is not always associated with extremes or with general statistical measures of variation about such an average.

Flight crew are aware that the touchdown zone (TDZ) on many runways can be affected to some degree by rubber deposits from landing aircraft. These deposits should be regularly removed to achieve a stated minimum dry friction level, but sometimes this may not happen and the actual surface friction in the TDZ can then be noticeably worse than along the rest of the runway. If a finding of low friction is made for the TDZ or any other part of a runway during regular inspections or a planned maintenance work then, unless rectification can be immediately achieved, NOTAM action to the effect that the runway is liable to be slippery when wet should be taken. Any such low friction condition is conducive to viscous aquaplaning beginning below the ‘aquaplaning speed’ and therefore ‘slippery runway’ landing performance data should be used. Crews should be wary of a contaminated Upwind or Stop End TDZ because this can cause a loss in braking just when the landing seems to have been safely completed and Reverse Thrust has been deselected. This may be Dynamic or Viscous aquaplaning.

Runway Surface State

The surface state of a wet runway can be assessed by either:

• the depth of water in the touchdown zone, or

• the measured or observed braking action.

In some parts of the world, a standard terminology which describes a runway as dry, damp, wet, wet with water patches or flooded is in use; this is often found in association with the use of 3mm water depth over a significant part of the runway as the division between a normal runway and a contaminated one for aircraft performance purposes. It is the responsibility of the Airport Operator to communicate this information, or a local equivalent, to pilts; ATC are merely the means of communication. If ATC suspect that it is inaccurate or no longer valid, they may choose to give their own assessment made from the visual control room (VCR), but this should be prefaced by the qualification 'unofficial'.

It is unlikely that the actual depth of water on a runway will be passed to an aircraft by ATC; at present, equipment which takes tactical friction measurement on wet runways (as opposed to surfaces with frozen deposits) is rarely authorised for use, so the best information a pilot is likely to get prior to landing is an informal braking action comment made to ATC by a previously landed aircraft. This should be passed by ATC with the time of the report, the aircraft type which made it and any significant change in precipitation since it was received. Prior to takeoff, direct observation should enable the pilot to form a first-hand impression of the surface state and the extent to which water is present on it. This will be particularly important in the event of a rejected take off.

The speed with which water drains from a runway surface is affected by the geometry of the surface and by whether or not it is grooved, or has a porous surface layer. Airport and runway licensing requirements limit the extremes of surface geometry, and exceptions allowed by an NAA should be published in the State AIP from where they should be replicated as Notes in the commercially published Flight Guides used by most pilots on the flight deck. Even normal surface geometry may lead to unusual water depth variation if a significant crosswind component exists; the effect of this could be periods of asymmetric braking if one main gear assembly (likely to be the downwind one) is braking normally whilst the other is aquaplaning. Where an abnormal pavement geometry is promulgated, the potential effect of the exceptions on any intended landing or take off should be assessed at the time.

It is widely recognised that the present arrangements for communicating likely runway braking action or actual surface friction measurements on wet runways are unsatisfactory and much attention continues to be given to developing an improved system.

Defences

Note: The AFM should serve as the overriding reference

Avoiding Aquaplaning

• If there is any doubt as to the probable extent of water of depth greater than 3mm on the landing runway, then an alternative runway should be chosen…if possible. (In the real world if you are landing in very stormy weather all the runways that you have enough fuel to reach may be similarly affected).

• If the flight crew become aware, just before landing, that the depth of water on the runway, especially in the touchdown zone, has increased to an extent that aquaplaning is likely, then a go-around should be flown. If this circumstance is not apparent until touchdown, then, provided it is permitted by the AFM, the landing should be promptly rejected from the runway.

• If it is decided to continue an approach to a landing, a stabilised approach is required which results in the aircraft crossing the runway threshold at the correct airspeed and height so as to achieve a touchdown within the TDZ. This is especially important when the landing distance required is close to the landing distance available. Since heavy rain is usually accompanied by rough conditions, crews should ensure they allow sufficient time to establish a stabilised approach and recognise that sustaining it may be quite demanding.

General Airmanship Considerations

• The pilot should be aware of the aquaplaning speed derived from the fully-inflated tyre pressure for both the maximum takeoff weight and maximum landing weight.

• Careful attention should be paid to the appearance of the tyres during the pre-flight external check, as far as is possible, especially the depth of tread. Even though having the tyre pressure within allowable limits is important, it can be extremely difficult to assess this visually on multi-wheel landing gear. (Note that if one tyre looks partially deflated it may be bearing the weight of the other tyre on the same axle which, with no pressure inside it to push the sides out, may not appear to be deflated.) Seek engineering advice if, after landing in heavy rain, there is any sign of rubber reversion

• The main gear touchdown on a wet runway should always be firm and made without any bounce in order to break through the surface water film and make effective contact with the runway surface to spin-up the wheels. (A stationary wheel can generate a wall of water in front of it on which it will aquaplane.)

Braking, Spoiler Deployment, Thrust Reversers and Control Column Handling

• Once touchdown on all of the landing gear has been achieved and sustained, SOPs usually recommend application of positive forward control column pressure in order to reduce the wing incidence, and therefore the lift, and thereby to assist in imposing the full aircraft weight onto the landing gear.

• A significant crosswind component may result in a difference between the amount of weight transferred onto each main gear assembly. This is because, even with the wings being held level by into-wind aileron, fuselage shielding partly blanks the downwind wing. This increases the likelihood of difficulties with directional control in a situation where the possibility of transient differential aquaplaning may also exist.

• Where available, full reverse thrust or reverse pitch should be selected whilst the ground speed is still high in order to gain maximum effect. Crews must be careful not to become so pre-conditioned to delayed selection of only Idle Reverse Thrust for noise abatement under normal conditions that they fail to select maximum retardation quickly when it is needed. Full ground spoiler deployment should also be made as soon as all wheels are on the ground if manual selection is necessary. Auto deployment of ground spoilers may be delayed until a specific wheel rotational speed, perhaps 25 kts, is sensed. Brake Units are likely to have anti-skid systems fitted so that any applied brake pressure by-passes the units until a specified wheel rotational speed is reached after touchdown. Typically, this could be 50 kts. Auto-braking selection should follow AFM requirements and Operator SOPs; manual braking may be inhibited until a specific time after the final touchdown is sensed. It is important to understand how each of these contributions to deceleration work so that if aquaplaning should occur, it is recognised as such rather than mistaken for a system malfunction. In very slippery conditions the Autobrake may appear to fail under heavy antiskid operation. Disconnecting the Autobrake prematurely is likely to increase stopping distance. Crews should be familiar with the indications of correct Autobrake/Anti-skid functioning, which is best learnt in the simulator.

Recovery from Aquaplaning

• Aquaplaning should be avoided if at all possible because, once it has begun, there is no certain way of regaining control and establishing useful deceleration.

• In the case of continued aquaplaning, deceleration can be expected to correspond to that for a slippery runway with braking coefficient of around 0.05. Around 50% more stopping distance will be needed if thrust reversers are not available and around 25% if they are (since account is not taken of their effect for normal landing performance calculations). If Heavy Rain is forecast for departure or arrival, very careful consideration should be given before accepting an aircraft with reverser(s) locked out in accordance with the MEL.

• Prior to attempting a landing on a runway where aquaplaning is likely, check that sufficient 'slippery runway' landing distance exists so that a runway excursion will not follow if aquaplaning commences.

• If there is a significant crosswind component, a landing on a potentially slippery runway should not be attempted. AFM limitations usually impose specific restrictions on allowable crosswind component for this case.

• Apart from an immediate rejected landing where AFM limitations and Operator SOPs allow it, there is little that can be done if aquaplaning begins and continues. If manual braking is being used, then briefly releasing and then reapplying pressure may succeed in increasing braking effectiveness. However, under no circumstances (except gross malfunction) should anti-skid be disabled since hard braking on a wet runway without this protection is certain to lead to reverted rubber aquaplaning and a decrease in deceleration due to locked wheels.

Example Accidents and Incidents

• B744, Bangkok Thailand, 1999 (RE HF WX) - On 23 September 1999, a Boeing 747-400 being operated by Qantas on a scheduled passenger service from Sydney Australia to Bangkok overran Runway 21L during an attempted night landing in normal visibility and came to a halt substantially intact 320 metres beyond the runway end.

• E135, George South Africa, 2009 (RE GND) - On 7 December 2009, after a relatively normal touchdown at destination in unexceptional daylight conditions, an EMB 135 being operated by South African Airlink on a scheduled passenger flight from Cape Town to George failed to decelerate normally and overran the end of the runway resulting in major damage to the aircraft and injuries to 7 of the 30 passengers on board and to all three aircrew.

• E145, Hanover Germany, 2005 (RE HF WX) - On 14 August 2005, an Embraer 145 being operated by British Airways Regional on a scheduled passenger flight from Birmingham to Hanover overran the wet landing runway by 160 metres in normal visibility after flying a daylight ILS approach with the approach lights visible from about 4 nm.

Related articles and further reading were not included but are available in the skybrary article.



What would happen in Madrid-Barajas International Airport in case of aquaplaning? Visit MADRID-BARAJAS INTERNATIONAL AIRPORT HOT SPOTS MAP.

As you read the information revealed in this link, you realize that an event of aquaplaning in any of the Madrid-Barajas International Airport runways could end up in a disastrous accident.

This is well known by the Spanish Civil Aviation Authorities, as they described it in the operation design reports. In that documents, engineers discarded the FAA Normative as too strict and unnecessary because of the low accident rate.

They even proposed a B-plan, in which collision risk could be avoided moving apart the airplanes that are on the way. In any case read this story, doesn’t it give you goose bumps?

domingo, 3 de noviembre de 2013

SUCEDIÓ EN BARAJAS EL 4 DE AGOSTO DE 2011


Adjuntamos artículo de SKYbrary sobre un incidente que sufrió un avión en su aproximación al Aeropuerto de Madrid-Barajas.

E145, en route, north east of Madrid Spain, 2011 (CFIT LB HF AGC)


Source: www.skybrary.aero

Categories: Accidents and Incidents

Description

On 4 August 2011, an Embraer ERJ 145 being operated by Luxair on a scheduled passenger flight from Luxembourg to Madrid in day VMC when its crew read back a clearance to descend to 10,000 feet as one to descend to 5000 feet, an altitude below both the STAR minimum altitude and the MRVA. The controller did not notice the read back error and when the aircraft was then transferred to the next sector, the controller there also did not notice the error when the crew advised their clearance on first call. An EGPWS ‘PULL UP’ Hard Warning was subsequently activated and recovery followed. There were no injuries to the 47 occupants during this manoeuvre.

Investigation

An Investigation was carried out by the Spanish Investigation Agency CIAIAC. It was noted that the First Officer had been acting as PF at the time of the Incident and that both pilots were experienced on the aircraft type and familiar with Madrid.

It was found that when the aircraft was cleared to descend to 10,000 feet by the controller in the ACC East Director position using the phraseology “descend to ten thousand feet”, spoken clearly and enunciated properly, the aircraft crew had wrongly read back a clearance to descend to 5000 feet which was not noticed by the controller concerned and was also below the altitude for the STAR being flown (10,000 feet), the MSA on the STAR chart (9500 feet) and the applicable MRVA. Prior to the aircraft reaching 10,000 feet, there was then a change of controller in position with the relevant strip showing a clearance to 10,000 ft. The aircraft was then transferred to the Initial Approach Director on the assumption that it was descending in accordance with the clearance issued. The receiving controller, despite advising the aircraft of “radar contact”, failed to notice the wrong cleared altitude when 5000 feet was given as well as not noticing that the aircraft was below the MRVA. He advised the Investigation that “the aircraft was transferred to him while supposedly descending through 10,000 ft and that there must have been a miscommunication since he asked the (East Sector) controller if he had cleared the aircraft to descend, to which he replied no”. The Investigation noted that “the information obtained from the (East Director) executive controllers and the planning controllers did not yield anything of relevance to the investigation of the event”.

Recorded data showed that when the aircraft was transferred to the Initial Approach controller, it was already below 8000 feet and the advice to the crew of “radar contact” was given with the aircraft descending through an altitude of 7349 feet. The aircraft EGPWS was triggered a little over half a minute later with a Terrain Alert followed about 20 seconds later by a Hard Warning “Terrain Pull Up” to which the crew responded by disconnecting the AP, increased thrust and climbing. The minimum altitude reached by the aircraft was found to have been 6290 ft. The Warning and the response to it was not reported to ATC until responding shortly afterwards to a second transmission to turn right for traffic separation when after acknowledging the instructed radar heading, the crew added “and we’ll maintain seven thousand feet due to mountain”. Subsequently, ATC instructed the aircraft to climb to 10,000 feet.

The actual altitude of the aircraft in relation to altitude clearance restrictions and key points during the event are shown in the diagram below. It can be seen that the aircraft was below the minimum altitude for the STAR for four minutes and below the MRVA for three minutes. The Investigation does not comment on the terrain clearance actually achieved during the event.


Flight profile of the aircraft during the incident (Reproduced from the Final Report)

The Investigation did note that:

• Each of the controller positions involved was manned by an “executive controller” and a “planning controller” but that “the functions of the planning controller are not documented by the service provider (AENA), meaning the exact tasks involved in the planning controller’s job are unknown.

• The radar control system installed at the ACC involved was capable of generating MSAW alerts but that according to AENA “this function is not enabled at any of Spain’s control centres because the relevant operational validation to determine which operating parameters are needed for said alert has not been performed yet”.

The formal statement of Cause made by the Investigation reads:

“The incident occurred because the aircraft descended below the minimum standard terminal arrival route, minimum radar vectoring and minimum sector altitudes. The crew, which was obligated to maintain separation with terrain and know that the minimum altitude specified by the arrival procedure was 10,000 ft, descended below said altitude without confirming with ATC whether the clearance given was correct.

The (ACC) sector controller used improper phraseology and cleared the aircraft to descend to 10,000 ft. The crew acknowledged descending to 5,000 ft and the controller did not correct the faulty readback”.

It was also noted that contributing to the incident was “the fact that (the controllers involved) noticed that the aircraft had descended below the minimum altitude in the procedure and below the minimum radar vectoring altitude. The (Initial Approach) controller only realised this fact after being informed by the crew when the aircraft’s EGPWS alerted them and they started to climb.”

Three Safety Recommendations were made as a result of the Investigation as follows:

• that AENA evaluate the incorporation of topics involving the use of standard phraseology and the recommendations issued by EUROCONTROL, as well as information concerning faulty acknowledgments and its consequences, into the continuing training programs for control personnel so as to raise controller awareness regarding the importance of these aspects. [REC 01/13]

• that AENA establish the measures needed to implement the altitude alert function in (the radar control system), at least in those posts where aircraft separation with terrain could be critical (as is the case of Madrid-Barajas when in a south configuration). [REC 02/13]

• that AENA issue a document where the operation procedure be described and the tasks of the planner controllers be defined. [REC 03/13]

It was noted that as Luxair had decided during the Investigation to "revise its procedures, to improve its training and to present this incident internally to its crews as a case study to remind them of the importance of increasing their awareness of altitude restrictions and limitations” a Safety Recommendation to the Operator was not necessary. The Final Report (in Spanish) was approved for publication on 30 January 2013 and subsequently made available in English translation: Final Report (in English).

Related articles and further readings were not included but are available in the skybrary article.


El informe publicado por la CIAIAC, con fecha de aprobación del 30 de enero de 2013, se puede consultar en el siguiente enlace: Informe técnico.

La aeronave, modelo Embraer 145, con matrícula LX-LGX y distintivo de llamada LGL 3837, realizaba un vuelo entre el Aeropuerto Internacional de Luxemburgo (ELLX) y el Aeropuerto de Madrid/Barajas (LEMD) el día 04 de agosto de 2011. A las 16:57:55 h la aeronave se encontraba en las proximidades del aeropuerto de Madrid/Barajas, en descenso.

Las condiciones meteorológicas informadas por el METAR de las 17:00 h indicaba que la intensidad media del viento era de 8 kt y la dirección 210°, variable entre 190° y 260°, con ráfagas de hasta 20 kt. Según el informe proporcionado por la AEMET la visibilidad era de 10 km o más, sin fenómenos de tiempo significativo y sin nubes de importancia para las operaciones.

Según se indica en el informe el incidente se produjo porque la aeronave descendió por debajo de las altitudes mínimas del procedimiento de llegada normalizada, mínima de Guía Vectorial radar y mínima de sector, como consecuencia de que la tripulación, que debía mantener su separación con el terreno y conocer que la altitud mínima marcada por el procedimiento era 10.000 ft, descendió por debajo de ésta, sin confirmar con ATC si la autorización proporcionada era correcta. El controlador de Sector RES, utilizando una fraseología inadecuada, había autorizado a la aeronave a descender a 10.000 ft, ésta colacionó que descendía a 5.000 ft y el controlador no corrigió esta colación incorrecta. Además, contribuyó al incidente el hecho de que los controladores de Sector RES y Sector AIS tampoco detectaron que la aeronave había descendido por debajo de la altitud mínima del procedimiento y la de Guía Vectorial radar. El controlador de Sector AIS fue consciente de este hecho tras ser informado por la tripulación, después de que se activara el EGPWS de la aeronave y comenzaran el ascenso.

Sirva este incidente no sólo para modificar procedimientos, sino para valorar lo importante que es disponer de controladores bien formados, bien descansados y sin presiones externas (léase políticas, laborales, mediáticas, etc.), que puedan inducirles a cometer fallos. Los responsables políticos y sus jefes de AENA tienen la obligación de proporcionarles el adecuado ambiente de trabajo, para que puedan desempeñar sus funciones con las garantías debidas, en lugar de arrojarlos al circo mediático en el que llevan lidiando desde hace varios años.

jueves, 3 de octubre de 2013

AIRSPACE INFRINGEMENT: A SKYBRARY ARTICLE





A SKYbrary article.

Airspace Infringement

Source: www.skybrary.aero

Categories: Airspace Infringement, General Aviation, Operational Issues

Description

Airspace infringement occurs when an aircraft enters notified airspace without previously requesting and obtaining clearance from the controlling authority of that airspace, or enters the airspace under conditions that were not contained in the clearance.

Notified Airspace includes controlled airspace structures in ICAO airspace classes A to E, such as Airways, Terminal Control Areas (TMAs), Control Zones (CTRs) or aerodrome traffic zones (ATZ) outside controlled airspace, as well as restricted airspaces, such as danger areas, restricted areas, prohibited areas and temporary reserved airspaces (TRA).

It should be noted that VFR traffic cannot infringe class E airspace because under ICAO rules neither an ATC clearance nor radio communication is required to enter or operate within it, unless filed national differences call for one or the other (or both). Traffic following instrument flight rules (IFR) can infringe class E airspace when not in receipt of a clearance to enter it.

Although VFR flights do not require clearance to enter Class E airspace, serious incidents have occurred between VFR and IFR flights in such airspace due largely to limitations in the “see-and-avoid” principle. Therefore this type of incident is also being addressed by airspace infringement prevention initiatives.

All classes of aircraft are prone to airspace infringement, but the majority of incidents recorded involve General Aviation. This is unsurprising, as most GA VFR flights are conducted outside controlled areas and zones, and are in general flown by less trained and experienced leisure pilots; whereas IFR flights are usually conducted within controlled airspace and carried out under the supervision of ATC units.

Effects

• Mid-Air Collision
• Loss of Separation from other aircraft. An infringement leading to loss of separation may also cause Loss of Control due to wake vortex encounter and even injuries to passengers or crew when violent manoeuvres are needed to avoid the other aircraft.
• Disruption to flight operations. An infringement can significantly increase controller and pilot workload due to the need to break-off an approach, change aircraft sequence for landing or implement other contingency measures. Any disruption to flight operations is likely to have adverse environmental and economic impact due to increased fuel burn by aircraft, both in the air and on the ground, which are subject to delays .
• Exposure to danger from military hazards, e.g. radiation, gun-firing or manoeuvring high-performance aircraft.
• Perceived security risk of flight contrary to clearance which may result in a military response.
• Disruption of military or other special activities within restricted, danger or prohibited airspace.

Defences

• Enhanced Flight Information Service (FIS), based on the use of radar, provides services to VFR flights outside controlled airspace. Examples include Traffic Service (provides the pilot with traffic information on conflicting aircraft) and Deconfliction Service (provides the pilot with traffic information and deconfliction advice on conflicting aircraft) provided in the UK airspace.
• Accurate aircraft navigation systems, including conventional, BRNAV and PRNAV systems
• Hand held or mounted GPS equipment used in VFR flying on board light aircraft, provided that the pilot has a proper understanding of the right way to use it and is aware of its limitations.
• Use of aircraft transponders, especially those associated with encoding altimeters which enable ATC to identify traffic and can facilitate TCAS-based avoiding action.
• Ground based Safety Nets, such as Short Term Conflict Alert (STCA) and Area Proximity Warning (APW) that can alert controllers to hazardous sitations and help mitigate the effects of infringements.
• Knowledge of and strict adherence to RTF procedures.

Typical Scenarios

• Aircraft flying outside controlled or restricted airspace, etc. enters the airspace without clearance due to:

o Lack of awareness of existence of the airspace (lack of, or out-of-date maps, deficient briefing, etc.); or,
o Lack of awareness of the activation of airspace restriction; or
o Poor navigation performance (equipment or technique); or,
o Poor air-ground communication technique; or,
o Lack of understanding of procedure for obtaining clearance to enter.

• Aircraft flying outside controlled or restricted airspace enters it with or without awareness as a result of adverse weather avoidance
• Aircraft flying outside controlled or restricted airspace enters it as a result of misunderstanding or misinterpretation of ATC instructions or clearance.

Contributory Factors

• Poorly equipped aircraft (navigation and communication equipment).
• Inexperienced or inadequately trained pilots.
• Poor pre-flight preparation (out-of-date or inappropriate maps, NOTAM briefing, etc.).
• Over-reliance on GPS equipment
• Adverse Weather.
• Absence of enhanced Flight Information Service.
• Airspace design which constrains uncontrolled air traffic into corridors of limited horizontal and/or vertical dimension.
• Unfavourable attitude of ATC controllers to VFR flights, leading to poor comunication.
• Routine (assumption that airspace restrictions on a familiar route will not change) or Complacency.

Solutions

• Improve airspace infringement awareness;
• Improve pilot's navigation and communication skills by raising the standard of pilot training, emphasising the importance of and developing the ability to ensure:

o Effective Pre-flight briefing;
o Accurate Navigation;
o Appropriate and effective Air-Ground communications;

• Enhance Flight Information Services to VFR flights based on the use radar in areas where airspace infringement is common;
• Implement safety nets, such as Area Proximity Warning (APW) that can alert controllers of potential or actual infringements;
• Improve the availability and accessibility of aeronautical and meteorological information to VFR flights;
• Review airspace design where repetitive airspace infringement occur with the objective of removing features which appear to have contributed to such incidents;
• Encourage or mandate the use of high quality aircraft systems for navigation and communication, including transponders;
• Improve cooperation at local level between ATS providers, GA establishments and the military.

SKYbrary Toolkit

We recommend visiting and experiencing the Airspace Infringement Prevention Toolkit

Related articles and further readings were not included but are available in the skybrary article.


This event is very likely to happen in the Madrid-Barajas International Airport because of the unsafe operation that is implemented by the airport operator, AENA, and the Spanish Civil Aviation authorities, ever since it started to operate the four runways configuration.

In the Plan Director de Barajas defences to prevent airspace infringement are not clear, and an accident is likely to occur in case of human error (e.g., misoperation due to fatigue) or equipment failure (e.g., communications failure).

What would happen in Madrid-Barajas International Airport in case of airspace infringement? Visit MADRID-BARAJAS INTERNATIONAL AIRPORT HOT SPOTS MAP.

miércoles, 24 de julio de 2013

UNEXPECTED EVENTS TRAINING: A SKYBRARY ARTICLE


Adjuntamos artículo de SKYbrary sobre el entrenamiento y formación de pilotos y tripulaciones para aprender a reaccionar y actuar ante sucesos imprevistos.


Se trata de procedimientos de fácil aprendizaje que tienen como objetivo que la reacción reflejo ante un imprevisto sea adecuada y lo más certera para evitar los posibles riesgos de una acción errónea o demasiado tardía. Actuar correctamente sin necesidad de pensar. Haciendo una analogía, en el entrenamiento de la defensa personal se practica hasta la saciedad qué hacer en caso de agresión hasta integrar la respuesta óptima en la reacción primaria o reflejo ante una situación imprevista. No se trata de analizar la situación, buscar la mejor solución y aplicarla, sino en actuar y anular el intento de agresión de una manera efectiva y contundente.


Estas técnicas, heurísticas o reglas de oro (rules of thumb en inglés) están basadas en la experiencia y en cómo reaccionamos ante un imprevisto; por ejemplo, ante una caída colocamos las manos para evitar daños en la cabeza, aunque no siempre es la mejor opción por el riesgo de dañar gravemente las muñecas, una articulación muy delicada; sin embargo con un entrenamiento concienzudo podemos aprender a caer y reducir el riesgo de roturas, como hacen en determinadas artes marciales.

Se trata de técnicas sencillas basadas en la experiencia y el comportamiento humano primario que inciden en la inmediata reacción ante un suceso imprevisto.



Unexpected Events Training (OGHFA BN)

Source: www.skybrary.aero


Categories: Organizational influences

Introduction

This briefing note provides a prescriptive outline that identifies human factors practices and practical techniques to be integrated into advanced aeronautical training programs. The integration of these rules of thumb can help optimize responses to unexpected events and upset-recovery training for individual pilots and for flight crews. Ineffectively managed surprises, which often accompany unexpected airborne events, can otherwise exacerbate problems. A number of training strategies can help mitigate risk exposure by fostering adaptability and resiliency in the aviator.

Applying practical techniques and integrating human factors principles into the training syllabus allows evaluators to expand typical performance measures (e.g., time and proficiency scores) to include “soft evaluations” that account for individual reactions. These expanded criteria can more inclusively measure and manage how pilots improve during training and recover from a variety of upsets.

Definitions

Unexpected or surprising event:

• An event incongruent with expectations as determined by base rate probabilities — that is, the average probability of the event occurring — and the contextual information available surrounding the event; it may be normal, abnormal or emergency in nature; it may also be frequent, infrequent or novel, or,

• the absence of an expected event.

In aviation, surprise often results when something that is expected to happen, in fact, does not. This creates a twofold problem: First, if the expectation is great enough, one may “see” or “hear” what is expected, even if it is not there. For example, many pilots in “gear-up” accidents claim the gear-down-and-locked indicator lights were illuminated and the gear warning horn was not on. In some cases, the area microphone for the cockpit voice recorder clearly recorded the gear warning horn.

In the other case, if a pilot does not know what to expect in a situation, then informational cues may be ignored or a large number will be viewed as unexpected. This potentially creates distractions to, and interruptions of, the primary task of flying the aircraft.

Surprising situations can include:

• System malfunctions
• Weather or environmental threats
• Crew member incapacitation
• Loss of Situational Awareness
• Air traffic control (ATC) or other crew member communications problems
• Aerodynamic anomalies

Aircraft upset or loss of control

Unexpected events and their associated factors contribute to loss of control.

Upsets include: unintentional aircraft pitch attitudes greater than 25 degrees nose-up or 10 degrees nose-down; bank angles greater than 45 degrees; airspeeds inappropriate for the conditions of flight; or any other aircraft state that is not intended by the pilot.

Unexpectedness and the associated pilots’ reactions to an upset are major contributors to loss of control in flight, the largest category of fatal commercial air carrier accidents between 1994 and 2003 (Boeing Commercial Airplanes, 2004).

Aircraft upsets occur for a variety of reasons. The following list of causes was compiled from the Airplane Upset Recovery Training Aid, developed by the aviation industry and the U.S. Federal Aviation Administration (FAA):

• Environmentally induced upsets
• Systems failure induced upsets
• Pilot induced upsets

Data

Factors commonly associated with unexpected and surprising events

A review of 638 accidents and incidents shows the following factors to be frequently involved in surprising and unexpected events:

Factor and percent present: Aircraft Position: 55.8; Air Traffic Control: 51.1; Other Crewmember Actions: 42.3; Aircraft State: 31.7; System Status: 19.3; Automation: 14.9; In-Flight Turbulence: 11.5; Low Visibility: 10.0.

Elements Involved in Surprise

Surprise is governed by four principles:

• Surprise can be insidious (gradually and subtly causing harm).
• Surprise can be subliminal (not conscious).
• Surprising events are typically common, trivial and mundane.
• More often than not, there are cues available to suggest that the unexpected should have been expected.

The process of surprise

A person’s reaction to a surprising or unexpected event may contribute to an interruption of his or her ongoing thought processes and motor activities, thus creating an error chain.

External behaviour:

• The first sign of imbalance creeps in as a decrease in accuracy. For example, discrepancies appear between targeted headings and altitudes, and those actually flown.

• Second, the aviator may become increasingly distracted by the worsening developments, thus neglecting to monitor the automation or cross-check instruments.

• In extreme cases, panic may set in. The aviator may even lapse into a state of resignation due to not knowing what action to take next.

Consequences of expected and unexpected events

Events in the cockpit, good or bad, that affect the equilibrium of the person, the system or the situation can be considered stressors.

• Psycho-physical stress: Aviators should strive for optimal stress/arousal levels — too little (complacency) or too much (overload) leads to poor performance.

• Psycho-emotional stress: Strive for a measured emotional response. Do not completely ignore your own senses or internal dialogue. Be sensitive to visceral reactions and the “hair standing up on the back of your neck.”

Behavioural responses

Regardless of the nature of the event or perceived severity, pilots respond in one of two ways:

1. Focus on the unexpected situation, address the condition and return to pre-event duties; or,
2. Focus on the unexpected situation and fixate on one aspect, without returning to the ongoing activities in a timely manner.

Fixation is particularly detrimental because the ongoing task of flying the aircraft must be attended to continuously. Otherwise, the following tasks may be neglected:

• Aircraft handling
• Monitoring
• Procedures
• Communication

Combating Unexpectedness

Flight instruction and training

Flight instructors must recognize what is happening internally with students and either reinforce positive reaction strategies and attitudes, or identify where restricted thinking exists in order to optimize the students’ capabilities. Flight instruction should emphasize the following:

• Realistic scenario-based training.

• Recognizing and responding to ill-defined events.

• The inability to train for all possible surprising situations.

• Integration of thinking skills and emotional control, with the requisite “stick-and-rudder” skills necessary to successfully perceive, process and respond to any unexpected situation.

• If necessary, use maximum available flight control inputs and power. Employ alternate control strategies as required.

• Modify know procedures to novel situations.

Mental processes for maintaining situational awareness

The following mental processes should be considered during training and continuously revisited during flight operations:

• Reflexive — The reflexive process is purely instinctive, involving automatic reactions learned by the pilot.

• Reflective — The reflective process is a conscious, systematic thought process aimed at problem solving.

• Repeated reviewing — The repeated reviewing process involves intelligence gathering in which the pilot looks for changes in the flight environment that might affect the safety of the flight.

Improving judgement

Poor planning leads to poor judgement. Lack of familiarity with the airplane, the flight environment, operating procedures, the route of flight and the destination airport can contribute to bad decisions.

• By deliberately seeking all available information in flight and during preflight planning, potential surprises may be discovered and remedied before they lead to unmanageable unexpected events.

• Continually evaluate the unfolding situation by consciously thinking and communicating about the condition of the environment, the aircraft, the pilots and the interactions occurring. Practice monitoring thoughts and actions by asking, “What am I focusing on now; what is the state of the situation (e.g., aircraft attitude, flight path, altitude, velocity)?”

• Continuously ask, “What if?” What should be done in the event of a flight control malfunction? What should be done during a dual engine failure? What if …?

Airmanship attitude

• Maintain cognitive flexibility, which is keeping an open mind to alternatives and possibilities at all times. Approach flying with an appropriate attitude (mental, physical and social) so that when you are faced with a surprising event, solutions become more apparent. Being cognitively flexible helps to counteract fixation tendencies and enhances your ability to handle unexpected events.

Example Scenarios

These scenarios may not, at first glance, seem to be so unexpected. However, research has demonstrated that these seemingly everyday occurrences indeed contribute to unwanted situations and outcomes. Most aviators have had experiences in similar situations.

A. Takeoff clearance

A takeoff clearance while holding for departure usually would not be regarded as surprising. However, as the following report to the U.S. National Aeronautics and Space Administration Aviation Safety Reporting System (ASRS) illustrates, given the right circumstances, even the ordinary may turn into a surprising event.

The controller advised us to be ready to go. We acknowledged OK. And then, there was about a three-minute break in the arriving traffic. Nothing happened. No takeoff clearance. We were spring-loaded to go and then nothing happened. Finally, out of the clouds pops another aircraft on final. As I watched him get closer, I realized that we weren’t going to be released. I relaxed, my copilot relaxed. Big mistake. Tower cleared us for an immediate takeoff. You can’t even begin to imagine our total surprise. Both crew and engines weren’t spooled up to go. As we were turning the corner for a rolling takeoff, tower comes back and asks if we are rolling! As soon as we replied affirmative, the controller sent the arriving aircraft around. The controller wasn’t happy, the arrival wasn’t happy, and I wasn’t happy. (ASRS report no. 598909)

• What the crew was thinking: The crew convinced themselves that an immediate takeoff was unlikely. They were “surprised” by the takeoff clearance and rushed into a potentially dangerous departure.

• What the crew may have considered: The controller advised the crew to be ready for takeoff. The crew should have either been prepared for an immediate departure, or they should have elected to decline the takeoff clearance, given what they knew.


B. Runway change


Another event reported as creating surprise in pilots is issuance of a runway change. Once again, this is a fairly common event that can indeed result in a poor process (e.g., approach) and/or a poor outcome (e.g., landing). The following is an example:

A crew has briefed the approach and landing to Runway 25R at a major airport configured with two sets of parallel runways. It is a clear night and the runways are clearly visible. Approximately seven miles from the runway, at approximately 2,000 feet AGL [above ground level], air traffic control requests that the flight change to Runway 25L and issues clearance to land on 25L.

• What most crews do: The majority of pilots comply with such a request. However, problems are created by a surprising request, even when it happens frequently at certain airports.

• What many crews do not consider: The controller requested the runway change, but there is always the option to decline and accept the possible consequences (including a go-around). The programming of the automation and flight management system (FMS) may be such that there will be no go-around guidance for the “new” runway. There may be additional notices to airmen (NOTAMs) such as taxiway closures that may affect the flight landing on the “new” runway.

Here’s another example:

The flight is approaching the airport from the north, and the crew has prepared to land to the north. When the flight is approximately seven miles north of the airport, air traffic control “offers” the flight the option to land to the south.

• What most crews do: The majority of pilots accept the challenge and attempt to take air traffic up on the offer. Why not? They will land sooner and not have to fly all the way around the airport to land.

• What many crews do not consider: In this case, the problems begin to multiply. There is no mandate to accept the runway change, only the opportunity to “help out” the controller or accept the challenge of “going down and slowing down” in short order. Once again, there is always the option to decline and continue with the original plan. The programming of the automation and the FMS may be such that there will be no go-around guidance for the “new” runway. There may be additional NOTAMs, such as taxiway closures, that may affect the flight landing on the “new” runway. In addition, accepting the closer runway may result in an unstabilized approach. Many pilot reports indicate they were surprised that the approach and/or landing resulted in an unwanted outcome after accepting such an offer from ATC.

• What crews may want to consider: Pilots need to remember how we tend to fixate on a surprising event (e.g., an offer to change runways) and may fail to consider all of the factors surrounding the event. Can the approach still be accomplished within the parameters of a stabilized approach? If the airplane is high and fast, how fast is too fast? If it looks questionable whether the approach and landing to the closer runway can be accomplished with the same, or better, margin of safety, what are the alternatives? How “tight” is too tight for an approach? What are the risks and what are the benefits of accepting the closer runway? Does the crew even have time to evaluate the risks and rewards?

Surprise and unexpected events alter the decision-making process and may influence how a situation is perceived. Pilots should take extra care in situations where the element of surprise may play a part in the process of the flight.

Key Points

• There are many types of surprising events in aviation. Potentially any event or combination of events can produce a situation that can result in an unwanted outcome.

• Unexpectedness and the pilots’ associated reaction to it are major contributors to loss of control in flight.

• By deliberately seeking all available information in flight and during preflight planning, potential surprises may be discovered and remedied before they become debilitating unexpected events.

• Flight training should integrate mental skills and emotion management, with the requisite stick-and-rudder skills necessary to successfully perceive, process and respond to any unexpected situation.

Associated OGHFA Material, additional reading material and related articles, were not included but are available in the SKYbrary article.


El Aeropuerto de Madrid-Barajas presenta un escenario de riesgos tan amplio que la formación de pilotos y tripulaciones antes situaciones de riesgo imprevistas es una necesidad que las compañías aéreas no pueden ni deben obviar. Por supuesto no seguir en ningún caso las recomendaciones de los gestores de AENA y los ideólogos, diseñadores y ejecutores de la ampliación del aeropuerto, que tienen ocurrencias como ésta:



Mientras no se implante una operación segura en el aeródromo madrileño, saber cómo reaccionar ante los riesgos a los que se enfrentan pilotos y tripulaciones puede ser la garantía de un vuelo con final feliz.

domingo, 17 de febrero de 2013

LECCIONES DESDE PHUKET, TAILANDIA

Adjuntamos el artículo de SKYbrary sobre el accidente de un MD-82 de One Two Go Airlines, con 130 tripulantes a bordo, ocurrido en el Aeropuerto de Phuket (Tailandia) el 16 de septiembre de 2007. La aeronave tras una aproximación fallida a la pista 27 no fue capaz de remontar y se estrelló contra el suelo dentro del perímetro del recinto aeroportuario, con un balance final de 90 muertos, 26 heridos graves y 14 leves.



Adjuntamos también la noticia publicada en El Mundo y un vídeo sobre el accidente.



MD82, Phuket Thailand, 2007 (LOC HF)

Source: www.skybrary.aero

Category: Accidents and Incidents

Description

On 16 September 2007, a McDonnell Douglas MD-82 being operated by One Two Go Airlines on a scheduled passenger flight from Bangkok to Phuket attempted a missed approach from close to runway 27 in day VMC but only climbed briefly before a steep descent into the ground occurred within the airport perimeter. The impact and subsequent fire led to the destruction of the aircraft and to the deaths of 90 of the 130 occupants, serious injury to 26 others and minor injuries to the other 14.

Investigation

An Investigation was carried out by the AAIC of Thailand with significant assistance from the NTSB. The DFDR and CVR were recovered and successfully replayed and the non-volatile memory (NVM) from various equipment, including especially the EGPWS unit, also yielded important information.

It was established that the aircraft commander, an Indonesian National, had taken the role of PM for the flight with the First Officer, a much younger Thai National acting as PF. There was a very considerable disparity between the level of both the overall flying experience and the specific aircraft type experience of the two pilots. The First Officer, whilst having been operating on the MD82 for some time, had gained most if not all of his multi crew jet experience on the type.

It was established that the ILS approach in VMC had been made with the AP out but the A/T (autothrottle) engaged in conditions which clearly indicated that a temporary deterioration in the weather was imminent and which had included awareness of the preceding inbound aircraft reporting that there “was a Cb over the airport”. Nevertheless, the aircraft commander had allowed the First Officer to remain as PF and even when it became apparent that he was not able to achieve a stabilised approach as the wind velocity and variation increased, did not take control. Eventually, as the auto call out of 40 feet height occurred, an EGPWS Mode 1 Sink Rate Alert was annunciated and the First Officer called a go around. This was confirmed by the commander and the First Officer called for Flap 15 and manually pushed the thrust levers forward - but failed to set or call for TO/GA to be set - before ‘transferring control’ to the commander. Since the A/T was still engaged when the go around was called, retard mode had become active and since the DFDR showed that the thrust had returned to idle after the initial manual override by the First Officer, it was surmised that when control was passed to the commander without prior warning, the First Officer had removed his hand from the thrust levers and the commander was initially using both his hands on the control column. All other go around actions were completed including the necessary pitch up but at no subsequent stage was the TO/GA switch pressed. The aircraft reached a height of almost 300 feet aal before it ceased to climb as a consequence of lack of engine thrust. Further EGPWS alerts and a final PULL UP warning were found to have occurred in the descent shortly before impact, upon which a fire immediately broke out. Four minutes after the impact, the weather had deteriorated further to 800 metres visibility in heavy rain and conditions below landing minima. It was noted that the aircraft had been fitted with a reactive wind shear alerting system which it was established had been serviceable, but no activation of it had occurred until the final second prior to impact.

It was noted that there was no provision in the Operations Manual for a handover of control at the point of go around and considered that confusion about system status would have been exacerbated by this sudden and unplanned / unanticipated handover. It was considered that the aircraft commander could reasonably have taken control at a much earlier stage of the approach and/or called an earlier go around. The Investigation also noted general non compliance with SOPs by the accident aircraft flight crew (although no conflict between them) as well as considerable deficiencies in practices of the aircraft operator. It was also found that both accident flight crew had exceeded various elements of the applicable flight time limitations scheme, although no hard evidence that either was fatigued as a consequence of this in a way that affected the accident outcome was presented by the Investigation.

In respect of the Airport, the effective but non notified unserviceability of the LLWAS due to it being powered by solar cells which had run down after a period of cloudy weather was noted. Aspects of the emergency response were also considered unsatisfactory.

The Commission determined the Probable Causes of the Accident to be as follows:

• The flight crew did not follow the SOPs (for) Stabilised Approach, Call Out, Go Around and Emergency Situations as specified in the airline’s FOM
• The Take Off / Go Around (TO/GA) switch was not activated, resulting in the inability of the aircraft to increase in airspeed and altitude during the go around. Also, there was no monitoring of the change in engine power and movement of throttle levers, especially during the critical situation.
• The flight crew co-ordination was insufficient and the flight crew had heavy workloads.
• The weather condition changed suddenly over the airport vicinity
• The flight crew had accumulated stress, insufficient rest and fatigue
•The transfer of aircraft control took place at a critical moment during the go around

A total of 17 Safety Recommendations were issued as a result of the Investigation as follows:

• that One Two Go Airlines Company should establish (a) Cockpit Resource Management (CRM) course, approved by the DCA, for all related personnel in every concerned section. The course should comprise of initial and recurrent training, having content according to ICAO requirements.
• that One Two Go Airlines Company should strictly train flight crew according to the flight crew training course and flight procedures in SOP.
• that One Two Go Airlines Company should amend the Operating Procedures on ‘Transfer of Control during Critical Phase of Flight’ in SOP to be most clear and definite.
• that One Two Go Airlines Company should perform the pilot training check, as appointed by the DCA, to meet applicable standards, especially the pilot proficiency check.
• that One Two Go Airlines Company should use a flight simulator that (can) simulate the systems, equipment and instruments of the aeroplane with the same configuration (that) the Airline operates.
• that One Two Go Airlines Company should arrange the crew schedule, according to the requirements in Flight Time and Flight Duty Period Limitations, by establishing a checking system with advance warning function before exceeding the limitation. The system should also enable the flight crew to check their status.
• that One Two Go Airlines Company should establish a Safety Management System (SMS) in order to identify and mitigate the risk leading to any accident or incident and to improve the safety of flight operations to meet the required standards.
• that One Two Go Airlines Company should direct all management levels to encourage personnel to have unique corporate culture in having values and beliefs to perform their jobs, in accordance with laws and regulations, and to report any wrongful misconduct (which) may (be) of use for improving task efficiency and increasing safety performance. This could be done through training and motivation.
• that the Airport of Thailand Public Company Limited should expedite the improvement of (the) runway strip to meet the Standard prescribed in Annex 14 of ICAO or revise the category of instrument approach procedure to suit the current runway strip. The Company shall also establish a Safety Management System (SMS) in order to identify and mitigate the risk.
• that in respect of Rescue and Fire Fighting the Airport of Thailand Public Company Limited should construct more access roads across the ditch along runway 27 to inaccessible areas at Phuket International Airport to facilitate rescue and fire fighting team (access) to any accident area in due time. The Company should also arrange the rescue and fire fighting exercise in those areas in order to mitigate the difficulties in rescue and fire fighting.
• that in respect of Rescue and Fire Fighting the Airport of Thailand Public Company Limited should include the Emergency Medical Institute of Thailand (formerly Narenthorn Centre), which is the government institute that co-ordinate(s) and provide(s) medical emergency service, in the Airport Emergency Plan.
• that in respect of Rescue and Fire Fighting the Airport of Thailand Public Company Limited should perform a full scale emergency exercise which should cover the participation of all responsible sectors and personnel to comply with the Airport Emergency Plan in (the) most efficient way when an accident (occurs).
• that the Department of Civil Aviation of Thailand should oversee the operation of One Two Go Airlines Company Limited….in order to improve their safety efficiency. The DCA should also issue regulations indicating the guidelines and practices of CRM training.
• that the Department of Civil Aviation of Thailand should improve the measure for regulating and overseeing the air operators under DCA supervision to achieve the most efficiency.
• that the Department of Civil Aviation of Thailand should coordinate with the Aero Thai Company Limited in order to specify operational guidelines (for) ‘Crash on Airport’ into (the) ‘Manual of Air Traffic Services. The guidelines should also be detailed in accordance with Doc 9137/An 898 Airport Service Manual, Part 7: Airport Emergency Planning, Chapter 4, Responsibility and Role of Each Type of Emergency.
• that the Department of Civil Aviation of Thailand should coordinate with the Meteorological Department to review all LLWAS installation(s) to identify possible deficiencies I performance, similar to those identified at Phuket International Airport and correct such deficiencies to ensure optimum performance of the LLWAS. Furthermore, the DCA should consider the installation of efficient LLWAS with advance system(s) to cover other airports, as considered necessary.
• that the Department of Civil Aviation of Thailand should coordinate with the following medical centres that perform post accident medical examinations on involved flight crew.
o The Institute of Aviation Medicine, RTAF to perform physical examination on surviving post accident flight crew.
o The Institute of Aviation Medicine, RTAF to perform an autopsy and collect samples for laboratory examination by physicians from (the) Ministry of Public Health and/or physicians from the Institute of Forensic Medicine, Royal Thai Police.
o The Institute of Forensic Medicine, Royal Thai Police to collect and send samples of autopsy to the Institute of Aviation Medicine, RTAF for further laboratory examination, in case(s) where the Institute of Forensic Medicine, Royal Thai Police arrive at the accident site first.
o The Institute of Forensic Medicine, Royal Thai Police to perform an autopsy and collect samples for laboratory examination with the Institute of Aviation Medicine, RTAF and / or physicians from (the) Ministry of Public Health.
o The Ministry of Public Health to collect and send samples of autopsy to the Institute of Aviation Medicine, RTAF for further laboratory examination, in case(s) where physicians from (the) Ministry of Public Health arrive at the accident site first.
o The Ministry of Public Health to perform an autopsy and collect samples for laboratory examination with the Institute of Aviation Medicine, RTAF and / or the Institute of Forensic Medicine, Royal Thai Police.

The Final Report of the Investigation was published in June 2010.

Related articles and further readings were not included but are available in the skybrary article.


¿Cuáles serían las consecuencias de un accidente de estas características en el Aeropuerto de Madrid-Barajas?
Catastróficas. Lo vemos en los siguientes Riesgos de Barajas:

RIESGO 2

El aterrizaje frustrado por la pista 33L en categorías ILS II y III, según operaciones publicadas en el AIP en la actualidad, es susceptible de impactar contra la terminal T4.

RIESGO 3

El aterrizaje frustrado por la pista 18R en ILS CATII y III, es susceptible de impactar contra la Torre de Control Norte que invade sus OAS de frustrada, al haberla ubicado a escasos 400 metros, cuando precisamente por este motivo la pista 33R se tuvo que desplazar y distanciar de la 33L 1900 metros, a fin de cumplir con la distancia legal de seguridad de 950 metros equidistantes que sí existen para la 33R y 33L.

RIESGO 4

Los embudos o espacios de Seguridad establecidos para los aterrizajes frustrados por las pistas 33R y 33L en categoría ILS II y III, que deberían permanecer libres de objetos para cumplir su función de seguridad, son sistemáticamente invadidos por las aeronaves que despegan desde las pistas 36R y 36L con el riesgo de colisión, precisamente por no cumplir la Normativa del Anexo 14 de OACI de operar en PISTAS PARALELAS O CASI PARALELAS. Esta situación es contemplada para cuando Barajas opera en configuración Norte y vuelve a reproducirse exactamente igual cuando se opera en configuración Sur.

RIESGO 5

El aterrizaje frustrado por la pista 18R en categorías ILS II y III está sujeto a riesgo de accidente provocado por una frustrada fallida (al igual que lo han previsto para la T4) por colisión contra los depósitos de combustible CLH, las terminales T1, T2 y T3 y el pueblo de Barajas, que se encuentran ubicados en la zona de seguridad (OFA extended) y dentro de la franja de protección de 3.500 metros recomendada por la Universidad de Cranfield.

Este accidente debería servir también de advertencia a todos aquellos que piden incrementar las cargas de trabajo de tripulaciones y controladores, en aras de la competitividad y del control de costes, y que desprecian la seguridad aérea como el valor máximo que puede ofrecer el servicio de transporte por avión; porque una de las causas del accidente fue el cansancio de la tripulación, consecuencia directa de la tensión y cargas de trabajo excesivas, aparte del mal momento escogido para realizar la trasnferencia en el control de la aeronave.

Es increíble la capacidad que tiene el ser humano para cerrar los ojos a la evidencia, o mirar hacia otro lado, y luego rasgarse las vestiduras exigiendo responsabilidades; porque evidentes son los riesgos que entraña la operación en el Aeropuerto de Madrid-Barajas y cínicas serán las voces que luego se alzarán pidiendo las testas de los culpables, como si ahora desconocieran quienes son, los unos y los otros.

miércoles, 23 de enero de 2013

ATR 42 RUNWAY INCURSION EVENT, AN SKYBRARY ARTICLE, Y LO QUE PODRÍA SUCEDER EN BARAJAS

Adjuntamos artículo de SKYbrary sobre el incidente ocurrido en el Aeropuerto de Zurich (Suiza) el 18 de junio de 2010, en el que estuvieron cerca de colisionar un Avión de Transporte Regional 42-320, operado por Blue Islands Airline, que iba a despegar por la pista 28, y un Airbus A340-600, operado por Thai Airways, que iba a despegar por la pista 16. Se da la circunstancia que ambas pistas se cortan. El accidente lo evitó la tripulación de una aeronave de British Airways, a la espera de realizar el despegue por la pista 28, que alertó a control de la situación.

En el esquema siguiente se observa la configuración de las pistas y la maniobra de despegue que iban a efectuar ambos aviones.


ATR 42 Runway Incursion Event

Source: www.skybrary.aero

AT43/A346, Zurich Switzerland, 2010 (RI HF)


Category: Accidents and Incidents

Description

On 18 June 2010, an Avions de Transport Régional ATR 42-320 being operated by Blue Islands Airline on a scheduled passenger service from Zurich to Jersey, Channel Islands, began take off in normal ground visibility and in daylight on runway 28 at Zurich without ATC clearance at the same time as an Airbus A340-600 being operated by Thai Airways on a scheduled passenger service from Zurich to Bangkok began take off from intersecting runway 16 in accordance with ATC clearance. ATC were unaware of this until alerted to the situation by the crew of a British Airways aircraft which was waiting to take off from runway 28, after which the ATR 42 was immediately instructed to stop. It did this in time to clear the runway before the intersection with runway 16 whilst the A340 continued departure on runway 16 in accordance with the issued clearance.

Investigation

A Serious Incident Investigation was carried out by the Swiss AAIB. The FDR and CVR recorders were found to have both been overwritten and therefore of no assistance to the Investigation. However, recordings of all ATC media were preserved and provided sufficient information to conduct a full investigation.

It was established that the ATR 42 had received ATC clearance to taxi to the full length take off position on runway 28 from the south side one minute after the A340 had received ATC clearance to taxi to the take off position on runway 16. However, the ATR 42 had also been previously advised that take off clearance should not be anticipated for a further seven minutes after the line up and wait instruction. A British Airways aircraft was stationary at the runway 28 holding point on the north side of the threshold at this time. One minute after the ATR 42 had received line up clearance, the A340 on runway 16 had been given take off clearance and read it back before starting to roll. Unknown to ATC, the ATR 42 flight crew had also wrongly read back the take off clearance as being for them and begun to roll on runway 28. The British Airways crew had heard the A340 readback but had also heard the words “cleared for take off” from a distinctively different voice and when the ATR 42 began take off, had called TWR to alert them to the apparent risk of simultaneous take offs. It was noted that “the reaction of the (TWR) controller to the (this) report…..was immediate and resolved the situation”. It was found that the ATR 42 had been accelerating through 54 knots when told to stop and had reached a speed of 74 knots before beginning to decelerate. It had been able to clear the runway at a point 950 metres along the 2500 metre long runway and approximately 750 metres prior to the intersection of runway 28 with runway 16. The A340 had continued take-off on runway 16 and proceeded as planned to destination.


LSZH Aerodrome chart for illustration purposes ONLY.

In respect of the lack of situational awareness of the ATR 42 crew, it was considered that their failure to appreciate that the take-off clearance was unlikely to be for them was “surprising, since the take-off clearance from the air traffic controller both included the radio callsign and named runway 16”. It was also noted that they had been on the TWR frequency for nearly three minutes prior to their line up clearance and had also been advised at frequency transfer “that they could expect a take-off clearance in seven minutes”. Had they been monitoring other transmissions on the TWR frequency, it was considered that they would have recognised that another aircraft had received a conditional clearance to taxi onto runway 16 and was also awaiting a take-off clearance, especially as the previous clearance to taxi onto runway 16 was subsequently repeated without condition. Finally, since the radio transmission by the ATR 42 accepting take off clearance was shorter than the parallel transmission made by the A340, it was concluded that the end of the read back from the latter would have been “clearly audible to the (ATR 42) crew after releasing (their) microphone button”.

In respect of the crucial role of the British Airways aircraft in mitigating the potentially disastrous consequences of the error made by the ATR42 crew, the Investigation commented:

“The conflict situation caused by the simultaneous take-offs on two intersecting runways was recognised by the crew of (the British Airways aircraft) and reported without delay to aerodrome control, which had not detected the impending danger. This behaviour shows that the flight crew had a very good overview of the situation. This may have been facilitated by careful monitoring of the radio traffic, the realisation that there had been a double transmission and an active intellectual engagement with the problem posed by intersecting runways.”

In respect of the absence to the TWR controller of any sign if simultaneous transmission of take off clearance acceptance, the Investigation noted that:

“Air traffic controllers questioned were of the unanimous opinion that they would recognise a multiple transmission due to a superimposed whistling tone. This opinion is based on experience with older aircraft-side transmission equipment, which in the event of dual transmission generally caused a superimposed whistling tone in the receiver in the audible frequency range. However, this is no longer the case with modern transmitters equipped with frequency synthesizers, because these transmit very precisely on the nominal carrier frequency. However, this does cause a superimposed whistling tone (but it) is below the audible range of human hearing.”

It was also noted that the automatic selection of ground receiver location for the feed of each aircraft transmission to TWR had significantly favoured the relatively stronger signal from the A340 over the simultaneous one from the ATR 42.

In respect of ground safety nets available to ATC, it was noted that as part of the upgrade of the A-SMGCS to Stage II, a RIMCAS system had been introduced on 31 May 2010 which might been expected to have given a useful warning to the TWR of the conflict. However, it was found that a Stage 2 RIMCAS Alert had not been activated until the ATR 42 had already started to reject their take off and was moving at 61 knots and the A340 was accelerating through 71 knots. This was because this activation required that both aircraft must be, on the basis of the calculated projection, in the "critical circle". It was calculated that if the ATR 42 had not rejected its take off, then a Stage 2 RIMCAS alert would only have been triggered when the accelerating ATR 42 was “in the critical speed range for aborting take-off”.

It was noted that at the time of the incident, a building programme was under way in and around the TWR VCR which caused an obstruction to the view towards the threshold of runway 28 and caused abnormal changes in the background noise level. However, whilst a specially installed telephone hotline had been installed to report any interference caused by construction work, this had not been used in the period prior to the investigated event.

The Conclusion of the Investigation was that:

(this) serious incident is attributable to the fact that on runway 28 the crew of an aircraft initiated a take-off without a corresponding clearance; this led to a significant risk of collision with an aircraft taking off on runway 16.

It was found that the following factors contributed to the serious incident:

• The crew of the aircraft on runway 28 did not notice the readback of the take-off clearance by the crew of the aircraft on runway 16.

• The readback of the presumed take-off clearance by the crew of the aircraft on runway 28 was not audible to the air traffic controller because the chosen location of the receivers of the normal radio operation system favoured the suppression of this clearance.

• Air traffic control did not notice the aircraft beginning its take-off roll on runway 28.

• The air traffic control conflict alert system was inappropriate for defusing the impending conflict.

It was also noted that “the occurrence of the serious incident was favoured by the complex operation on two intersecting runways, which has only a small error tolerance in the event of a high volume of traffic”.

One Safety Recommendation was made as a result of this Investigation:

• The Federal Office of Civil Aviation should ensure that double transmission is detectable on the radio operation systems used in Switzerland. (No. 439)

Safety Action noted by the Investigation to have been taken since the occurrence included:

• Following advice from ANSP Skyguide to the airport operator that construction above ground level should be subject to the same procedure as underground civil engineering works so as to ensure that potential impact on TWR operations caused by work on superstructures is always foreseen, a new process was introduced on 1 April 2011.

• The usefulness to ATC of the SAMAX/RIMCAS system which had been introduced shortly before the incident was reviewed and the settings subsequently adjusted. The possibility of a slight increase in nuisance alerts until a corrective software modification, which was expected to be available by the end of 2011 was accepted.

The Final Report of the Investigation No. 2113 by the Aircraft Accident Investigation Bureau was published on 8 September 2011. The event was categorised by the Swiss AAIB as an ICAO Category ‘A’ AIRPROX (a high risk of collision).

Related articles and further readings were not included but are available in the skybrary article.


El incidente fue provocado por fallos humanos, el primero y más importante de la tripulación del ATR 42 que consideró que el mensaje iba dirigido a ellos, y el segundo de los controladores que no vieron cómo las dos aeronaves iban directas al encuentro en la intersección de las pistas 16 y 28, y no lo vieron por las obras que se estaban realizando dentro y alrededor de la torre de control y que impedían la visión normal del umbral de la pista 28, además del ruido ambiente que provocaba la misma y que seguramente no permitía tener la concentración y atención que requiere su trabajo. Y se evitó la tragedia gracias a la tripulación del avión de British Airways que alertó al control.

De la información que se ofrece en el artículo de SKYbrary extraemos unos párrafos que tienen un especial significado pensando en la peligrosa operación implantada en el Aeropuerto de Madrid-Barajas:

The British Airways crew had heard the A340 readback but had also heard the words “cleared for take off” from a distinctively different voice and when the ATR 42 began take off, had called TWR to alert them to the apparent risk of simultaneous take offs.

It was also noted that “the occurrence of the serious incident was favoured by the complex operation on two intersecting runways, which has only a small error tolerance in the event of a high volume of traffic”.


Recordamos que en el Aeropuerto de Madrid-Barajas se llevan a cabo Operaciones Simultáneas y Segregadas en Pistas Cruzadas (las prolongaciones de los ejes de las pistas 32/14 se cruzan con los ejes de las pistas 36/18), lo que implica un riesgo cierto de colisión entre aeronaves que despegan y las que aterrizan y podrían frustrar (recordamos que toda operación de aterrizaje en ILS categoría II y III lleva implícita un despegue.)

La diferencia con Zurich es que la colisión tendría lugar en el campo de vuelo y los aparatos podrían caer en cualquier lugar a unos kilómetros del Aeropuerto de Madrid-Barajas, lo que es un riesgo para las poblaciones del área de influencia, incluida la capital Madrid.

Este riesgo que lo evita la Normativa de OACI en su Anexo 14, diseñando pistas paralelas o casi paralelas (inexistentes en el nuevo Barajas), está además contemplado en el propio Plan Director en su Anexo XIII/Anexo II al hablar de cálculos de procedimientos operativos en el que expresamente se especifica que en configuración norte "Las aproximaciones frustradas directas a las pistas 33R bloquean a las salidas por las pistas 36R y 36L". En configuración sur …"las llegadas a la pista 18L bloquean las salidas por la 15R y 15L." Este riesgo podría resultar agravado por el hecho de que en las 4 pistas sus umbrales para los aterrizajes hayan sido acortados en 500 y 1.050 metros como medida de restricción operativa para paliar el ruido sobre Santo Domingo (en configuración sur) y San Fernando de Henares y Coslada (en configuración norte).

Además, y recordando que este riesgo se agrava en caso de un gran volumen de tráfico aéreo como es el caso del Aeropuerto de Madrid-Barajas:

De respetarse por la actual operatividad del aeropuerto los tiempos de bloqueo establecidos en el Plan Director (normativa al parecer propia de la DGAC y no de OACI), en la que extrañamente los tiempos aparecen como distancias, está claro que jamás se podrán alcanzar las 120 operaciones por hora contempladas desde que se inició el Plan Barajas, por otra parte ridículas si se compara con la capacidad de un aeropuerto con CUATRO PISTAS PARALELAS (por ejemplo Charles de Gaulle en París). Por este motivo y dado que hasta en la Resolución de 27 de enero de 2006 por la que se autoriza la puesta en funcionamiento de las 2 nuevas pistas la finalidad de la ampliación es aumentar el número de operaciones con respecto a las llevadas a cabo antes de la ampliación nos tememos que esta aumento de capacidad sólo podrá lograrse a base de violentar peligrosamente aún mas las operaciones segregadas simultáneas. AENA todavía no ha confirmado si realmente se están haciendo operaciones segregadas simultáneas y si se están respetando los tiempos (DISTANCIAS) de bloqueo previstos en el Plan Director para evitar colisiones de aeronaves.

Además en el Aeropuerto de Madrid-Barajas se dan varias circunstancias agravantes y concurrentes. Por un lado la presión a la que someten a los controladores, sin importar la fatiga que soporten. Quien considere que los tiempos de trabajo y de descanso son demasiado laxos o benévolos, habría que recordarles que el trabajo que desempeñan requiere la máxima atención en todo momento, y que un error o descuido puede ser fatal. Por otro lado la falta de visibilidad, reconocida en el AIP de los umbrales de las pistas y que es suplida con cámaras.


Desde Las mentiras de Barajas insistimos: Los fallos humanos han sucedido, suceden y siempre sucederán; la mejora de lo que esté mal y no se sepa evitará los incidentes o accidentes futuros; pero lo que está mal y se sabe ahora será causa en los accidentes futuros.

No nos gustaría, y no dejaría en buen lugar a muchos, que fueran los de British quienes pusieran orden en la operación del Aeropuerto de Madrid-Barajas, cuando todos saben lo que se cuece en sus pistas, ni tampoco leer en un informe:

The occurrence of the serious accident was mainly due to the complex operation on two crossing runways, which has only a small error tolerance in the event of a high volume of traffic, as in Madrid-Barajas International Airport.