B752, en route, western Ireland, 2013
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|On 20 October 2013, a Boeing 757-200 Co-Pilot believed his aircraft was at risk of stalling when he saw a sudden low airspeed indication on his display during a night descent and reacted by increasing thrust and making abrupt pitch-down inputs. Other airspeed indications remained unaffected. The Captain took control and recovery to normal flight followed. The excursion involved a significant Vmo exceedance, damage to and consequent failure of one of the hydraulic systems and passengers and cabin crew injuries. The false airspeed reading was attributed by the Investigation to transient Ice Crystal Icing affecting one of the pitot probes.|
|Actual or Potential
|Human Factors, Loss of Control, Weather|
|Type of Flight||Public Transport (Passenger)|
|Origin||Newark Liberty International Airport|
|Intended Destination||Dublin Airport|
|Take off Commenced||Yes|
|ENR / APR|
|Origin||Newark Liberty International Airport|
|Tag(s)||Inadequate Aircraft Operator Procedures,|
Deficient Crew Knowledge-automation,
Deficient Crew Knowledge-handling
|Tag(s)||Inappropriate crew response - skills deficiency,|
Inappropriate crew response (automatics),
Procedural non compliance,
AP/FD and/or ATHR status awareness
|Tag(s)||AP Status Awareness,|
Aircraft Flight Path Control Error
|Tag(s)||In Flight Airframe Icing|
|Tag(s)||Airport Emergency Medical Response|
|Damage or injury||Yes|
|Causal Factor Group(s)|
On 20 October 2013, a Boeing B757-200 (N41140) being operated by United Airlines on a scheduled international passenger flight from Newark to Dublin experienced turbulence during descent at night in IMC. Inappropriate control inputs by the co-pilot PF in response to false airspeed indications caused passenger and crew injuries and system damage also occurred. ATC were advised that medical and emergency services would be required on arrival. Thirteen of the 131 passengers and four of the six cabin crew sustained minor injuries and significant damage to one of the hydraulic systems was confirmed.
An Investigation was carried out by the Irish AAIU. Data from the FDR were successfully recovered but relevant data on the CVR had been overwritten because its CB had not been tripped. It was noted that "the non-availability of the CVR denied the Investigation the opportunity to fully understand the cockpit environment at the time of the occurrence and to accurately account for the communications, discussions and actions of the Flight Crew as they responded to the unfolding events". The Investigation noted that United Airlines' Manuals in respect of access to recorders and the tripping of the CVR CB after a Serious Incident did not correspond to the requirements of ICAO Annex 6.
It was noted that "the Commander initially appeared to be unaware of his obligations with regard to the requirements and conduct of a safety investigation in a foreign state". However, "following a briefing from an AAIU Inspector", the Commander provided a verbal statement and the First Officer provided "a frank, verbal, statement", both of these being obtained on board the aircraft shortly after its arrival in Dublin.
The 59 year old Captain informed the Investigation that he did not keep a logbook but stated that he had accumulated around 32,000 total flying hours. United Airlines were able to provide details of his hours whilst in their employment and these included 8,769 hours on type. The 43 year old First Officer had accumulated 12,010 total flying hours which included 5,384 hours on type. The First Officer was PF for the investigated flight.
It was established that whilst descending towards destination at 300 KCAS and 1500 fpm and passing approximately FL250, with the seat belt signs already selected on, turbulence had been encountered and shortly afterwards, precipitation had been entered. The First Officer stated that "when the turbulence subsided" he noticed a very low indicated airspeed on his instrument display and "believing that the aircraft was about to stall, immediately pushed the control column forward and applied full power without disengaging the autopilot or autothrottle". He stated that following this, his airspeed “went back up into the normal range”, but as soon as he began to raise the nose and reduce power, “it went back into a stall - or the indications of a stall” and he had "commenced a second pitch down manoeuvre".
It was then ascertained that (only) the First Officers airspeed indication was false and so the Captain had taken control and returned the aircraft to normal flight. When the First Officer’s airspeed indications returned to normal, he had handed control back. At this time, an EICAS indication of a loss of hydraulic pressure in the centre hydraulic system was seen and the relevant checklist was actioned. A report was received from the cabin that the excursion from normal flight had resulted in "minor impact injuries" being sustained by some passengers and some members of the cabin crew.
ATC were advised that as a result of an encounter with "severe turbulence" medical assistance was required on arrival because some passengers had been injured. AFS attendance was also requested because of the loss of the centre hydraulic system. The remainder of the flight was subsequently completed without further event. However, on inspection it was found that the aircraft had sustained "significant damage" to the structure of the centre hydraulic system servicing bay which had led to the indicated loss of system pressure (see the illustration below). One cabin ceiling panel was also found to have been impact-damaged during the event.
Minor injuries were found to have been sustained by 13 passengers and four of the cabin crew.
The Investigation obtained written statements from both pilots. It was noted that the Captain "made no mention in any of his reports, of any communications between himself and the Co-Pilot regarding the manoeuvres performed by the Co-Pilot during the event". The Co-Pilot stated that he had mistaken the overspeed warning which had occurred during the event for a stall warning. Neither pilot reported noticing the EICAS 'IAS DISAGREE' Alert during the event or the Master Caution annunciation which would have accompanied it. It was considered that although the FDR had no record of this, the recording of such activation was only sampled on a discrete basis every 64 seconds so "it is probable that (such an Alert) was generated". It was noted that previously investigated unreliable airspeed events had also found that pilots' "have not recognised" this annunciation.
FDR data showed that the rate of descent during the First Officer's intervention had briefly reached 12,000 fpm. Airspeed had reached 380 KCAS (30 knots above the AFM Vmo), pitch attitude ranging between -4.4º and -16.2º and the maximum negative 'g' loading had reached -0.36g. Control column pitch inputs had begun around 2 minutes after the initial encounter with turbulence which had all but ceased prior to the onset of a series of abrupt thrust lever and control column inputs, which had then lasted about 20 seconds. The AP and A/T were recorded as having remained engaged throughout. The airspeed had remained above Vmo for most of a period lasting just over a minute and the Master Caution activated by the 'IAS DISAGREE' Alert had annunciated for just over 20 seconds.
Boeing was reported to have noted that since the event had been an "unreliable airspeed" occurrence it should have triggered the corresponding response detailed in the QRH. They also considered that the aircraft had "behaved as expected" in response to the control inputs and control surface deflections.
United Airlines stated that the crew had recently completed a self study portion of the "Continuing Qualification Training Programme" which covered unreliable airspeed events. However although Boeing stall guidance was found to direct pilots to initiate the Approach to Stall or Stall Recovery manoeuvre as published in the QRH, United Airlines informed the Investigation that their QRH did not contain Stall Recovery procedures which were instead provided in the "Operator’s Flight Manual".
Weather conditions in the vicinity of descent flight path at the time of the event were confirmed by the Irish Meteorological Service as having been conducive to at least moderate turbulence and concluded that "ice crystals were likely to have been present at the time the incident occurred and at the levels at which the incident occurred" and that they "would have been the predominant water phase”. In respect of the likely size of water droplets also present, they noted that the available evidence suggested they would have been "large" and therefore capable of detection using aircraft weather radar. Boeing noted that the recorded SAT at FL235 had been -37º C and that the aircraft had probably flown through "a small cold core thunderstorm" which had significant ice crystal content present in its core.
The Investigation noted that that the aircraft type involved benefited from 'Grandfather Rights' in respect of its airworthiness certification and was not required to comply with the current FAA standard for pitot probe ice protection which has extended the definition of icing conditions requiring system protection to include convective cloud ice crystal conditions.
In respect of Human Factors, the following were considered:
- CRM and in particular the apparently limited extent of any meaningful communication between the two pilots once a problem had manifested itself.
- The likely effect of startle or surprise on the First Officer's clearly inappropriate response to the sudden drop in his indicated airspeed. It was noted that "given the reliability of modern aircraft and their systems, pilots are rarely exposed to failures and malfunctions, and may become conditioned to an expectation of normality during everyday operations" so that "sudden, serious events may elicit a startle response" during which "pilots’ perception and reaction to certain sudden failures or instrument displays may not be appropriate" and may lead to the affected individual "focusing […] on the causal stimulus to the exclusion of other events taking place […] such as warnings, alerts and communications".
- the circumstances which may encourage ineffective pilot use of airborne weather radar which it was considered had been the case in this event.
- the possible effects of the 'window of circadian low' as relevant to the event.
The considerable history of inappropriate flight crew response to the sudden onset of one or more unreliable airspeed indications attributed to ice crystal icing or other causes was noted during the Investigation and a number of these events were explicitly identified, including:
- the 1996 unrecovered loss of control of a Boeing 757 after a night departure from Lima, Peru when all pressure-dependent flight instruments were giving false readings because the static ports still covered by tape after repainting.
- the 2005 temporary loss of control of a Boeing 717 in the USA after the crew failed to notice that thrust was reducing after the engine inlet pressure sensors iced up because the engine anti icing was not on.
- the 2009 continued night take-off of a Boeing 757 from Accra Ghana with a known airspeed discrepancy which led to crew confusion after unsuccessful attempts to deal with the fault during the climb.
- the 2009 unrecovered loss of control of an Airbus A330 when there was a very brief period of loss of airspeed indications in the cruise at night due to ice crystal icing.
- the 2009 temporary loss of control of a Boeing 767 when the crew responded to a faulty airspeed display without realising that only one display was faulty.
The significant Conclusions of the Investigation included the following:
- The aircraft flew through, or close to, an area of convective cloud activity, in which ice crystals were the predominant water phase. Although prior to this, the Flight Crew reported that they had observed nothing more than light precipitation on the weather radar display, the convective weather in the vicinity should have been visible on the weather radar if it had been appropriately adjusted.
- Following a short period of air turbulence, the First Officer noticed that his airspeed indication was low and concluded - on that basis alone - that there was a real loss of airspeed caused by the turbulence and that the aircraft was in danger of stalling. He then carried out what he termed was a “stall recovery manoeuvre” of his own volition which involved lowering the aircraft nose of the aircraft and increasing the engine power. He did not use the prescribed Standard Call “Max thrust, stow speed brake”, at the commencement of this action, and the Commander was unaware that the pitch down was being made because the First Officer believed that the aircraft was stalling. The First Officer then observed a second reduction in airspeed on his display and in response made further pitch down inputs. During these manoeuvres the aircraft exceeded Vmo by 30 KCAS.
- Following these manoeuvres, it was recognised that there was a problem with the First Officer's airspeed indication and the Commander took over as PF and recovered the aircraft to normal flight path control.
- The actions of the First Officer in response to the sight of a sudden drop in the indicated airspeed on his display may be attributed to ‘startle effect’.
- It is probable that the loss of airspeed indicated on the First Officer's ASI was caused by a temporary blockage of the right main pitot probe by ice crystals. At the time the B757 received its Type Certificate the possibility of ice crystal icing was not considered. However, the event occurred at an altitude and temperature that was within the Ice Crystal Icing envelope which current certification requirements require to be considered in respect of Airspeed Indicating Systems.
- Although the United Airlines ‘Stall Recovery’ and ‘Unreliable Airspeed’ checklists both included the instruction to disconnect the AP and the A/T, both remained engaged throughout the upset whereas disconnecting them may have assisted the Flight Crew in analysing the status of the aircraft.
It was determined that the Probable Cause of the event was "non-standard Flight Crew response to an unreliable low airspeed indication resulting from a temporary blockage of the right main pitot probe due to ice crystal icing".
A Contributory Factor was determined as "startle effect due to a sudden unexpected indication of low airspeed, following an encounter with turbulence".
Eight Safety Recommendations were made as a result of the Investigation as follows:
- that United Airlines should review its guidance material to Flight Crew on the optimal use of Airborne Weather Radar during flight in or near areas of actual or forecast convective cloud activity. [IRLD2016-004]
- that the FAA should conduct a study to establish whether a safety deficiency exists in pitot probe icing protection for aircraft certified under CFR Part 25 prior to 5 January 2015, and address any deficiencies that may be identified. [IRLD2016-005]
- that United Airlines should review its Unreliable Airspeed Training, including theoretical and simulator training, for all phases of flight. [IRLD2016-006]
- that the Boeing Aircraft Company should review the effectiveness of the current IAS DISAGREE warning as a means of alerting Flight Crews to an unreliable airspeed condition. [IRLD2016-007]
- that the Boeing Aircraft Company should review the status of the Boeing Fleet Team Digest relating to erroneous airspeed with a view to reissuing the guidance material. [IRLD2016-008]
- that United Airlines should review their guidance material on aircraft upset recognition and startle factor in its recurrent and CRM training programs in the context of the recently published documents, ‘High Altitude Operations, Supplement #1 to the Airplane Upset Recovery Training Aid’, and FAA AC 120-111, ‘Upset Prevention and Recovery Training’. [IRLD2016-009]
- that United Airlines should emphasise to flight crew the importance of using Standard Calls, especially during non-normal flight manoeuvres. [IRLD2016-010]
- that United Airlines should review its Operations Manual to ensure that the procedures associated with the preservation of Flight Recorders following an Accident or Incident are in accordance with the provisions of ICAO Annex 6. [IRLD2016-011]
The Final Report of the Investigation was published on 10 May 2016.
- Unreliable Airspeed Indications
- Ice Crystal Icing
- In-Flight Icing
- Weather Radar
- Human Factor in Emergencies
- Hindsight 15: Surprising Situations
- Cockpit Automation - Advantages and Safety Challenges
- Aerodynamic Stall Awareness and Avoidance
- Recovery from Unusual Aircraft Attitudes
- Crew Resource Management
- Airbus FOBN: Optimum Use of the Weather Radar, Airbus, Feb 2007.