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B733, vicinity Sharm El-Sheikh Egypt, 2004

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Summary
On 3 January 3 2004, a Boeing 737-300 being operated by Flash Airlines on a passenger charter flight from Sharm el-Sheikh Egypt to Cairo for a refuelling stop en route to Paris CDG crashed into the sea 2½ minutes after a night take off into VMC and was destroyed and all 148 occupants killed. The Investigation was unable to establish a Probable Cause but found evidence of AP status confusion and the possibility of distraction leading to insufficient attention being paid to flight path control.
Event Details
When January 2004
Actual or Potential
Event Type
Human Factors, Loss of Control
Day/Night Night
Flight Conditions VMC
Flight Details
Aircraft BOEING 737-300
Operator Flash Airlines
Domicile Egypt
Type of Flight Public Transport (Passenger)
Origin Sharm el-Sheikh International Airport
Intended Destination Cairo International Airport
Take off Commenced Yes
Flight Airborne Yes
Flight Completed No
Flight Phase Climb
ICL / ENR
Location - Airport
Airport vicinity Sharm el-Sheikh International Airport
General
Tag(s) Root Cause Not Determined
HF
Tag(s) Authority Gradient,
Distraction,
Ineffective Monitoring,
Manual Handling,
Spatial Disorientation
LOC
Tag(s) AP Status Awareness,
Flight Management Error,
Flight Control Error"Flight Control Error" is not in the list (Airframe Structural Failure, Significant Systems or Systems Control Failure, Degraded flight instrument display, Uncommanded AP disconnect, AP Status Awareness, Non-normal FBW flight control status, Loss of Engine Power, Flight Management Error, Environmental Factors, Bird or Animal Strike, ...) of allowed values for the "LOC" property.,
Extreme Bank,
Last Minute Collision Avoidance
Safety Net Mitigations
Malfunction of Relevant Safety Net No
GPWS Available but ineffective
Outcome
Damage or injury Yes
Aircraft damage Hull loss
Fatalities Most or all occupants ()
Causal Factor Group(s)
Group(s) Aircraft Operation
Safety Recommendation(s)
Group(s) Aircraft Operation,
Aircraft Airworthiness
Investigation Type
Type Independent

Description

On 3 January 2004, a Boeing 737-300 being operated by Flash Airlines on a passenger charter flight from Sharm el-Sheikh Egypt to Cairo for a refuelling stop en route to Paris CDG crashed into the sea 2½ minutes after a night take off into VMC and was destroyed and all 148 occupants killed.

Investigation

An Investigation was carried out by the Egyptian Ministry of Civil Aviation (MCA). FDR and CVR data was successfully downloaded from the recovered recorders. It was noted that the prevailing weather conditions were benign and that both pilots were operating their first jet transport type, the Captain having accumulated less than 500 hours on type and the First Officer less than 250 hours on type. The Captain had previously had a long military flying career, acquiring most of his flying hours on the C130. The First Officer was in his first post as an airline pilot.

After departure from runway 22R, the aircraft was found to have been cleared for a climbing left turn to intercept the 306° radial from the Sharm el-Sheikh VOR to which allows departing flights to gain sufficient altitude before proceeding over higher terrain located along the flight path to Cairo. As shown in the diagram below, this left turn was achieved, but as the aircraft passed 5000 feet, a progressive right bank developed which was not corrected until after a steep descent at increasing airspeed had begun by which time it had exceeded 110°. Almost all the flight was conducted without the AP engaged and it was not clear whether both pilot had the same awareness of AP status during the flight. A very late attempt at recovery was evident but by then a high speed impact was inevitable.

Aircraft estimated ground track (reproduced from the Official Report)


Despite considerable efforts, this Investigation was not able to determine a Probable Cause from the evidence available and the analysis thereon.

The formal Conclusion of the Investigation was as follows:

"No conclusive evidence could be found from the findings gathered through this investigation to determine a probable cause. However, based on the work done, it could be concluded that any combination of these findings could have caused or contributed to the accident. Although the crew at the last stage of this accident attempted to correctly recover, the gravity of the upset condition with regards to attitude, altitude and speed made this attempt insufficient to achieve a successful recovery."

Nine Safety Recommendations were made as a result of the Investigation:

  • that Manufacturers and Operators should make a joint effort to minimise MEL-CDL-DDL allowances to avoid lowering safety standards by overloading pilots, and ensure that whenever found necessary to maintain such items, very clear procedures addressing pilots and maintenance crews to be made available.
  • that Manufacturers and Operators should make a joint effort to enhance the function and reliability of FDR and CVR due to the importance of the data obtained to the safety of the aviation industry.
  • that Manufacturers and Operators should make a joint effort to ensure that a clear engagement status indication for the autopilot is available to the crew to avoid any possibility of incorrect perception or ambiguity.
  • that Manufacturers and Operators should make a joint effort, based on data collected from different operators using this autopilot and the number of reports of unexpected autopilot behavior some of which are unexplained, re-assessment of this autopilot system is recommended and operators should be made aware of any problems and manufacturers' analysis actions and recommendations.
  • that the Civil Aviation Authority should ensure that all operators strictly adhere to CAA regulations and requirements, especially in remote stations.
  • that (those responsible for) pilot training should emphasise early detection and recognition of conditions that could lead to upset condition.
  • that (those responsible for) pilot training should emphasise timely and appropriate recovery action from upset conditions to counteract sudden unknown abnormal conditions.
  • that (those responsible for research into) human factors carry out in depth studies of Spatial Disorientation, ways of early recognition between crew members and appropriate crew action to overcome it and increase crew awareness of this phenomena.
  • that (those responsible for pilot training in) human factors note that it is clear that more emphasis in this area of training will achieve earlier recognition and recovery from abnormal conditions.

The Final Report was published in three parts:

One of the Comments on the draft of the Final Report made by the US as a participant in the Investigation was that"

“The only scenario identified by the investigative team that explained the accident sequence of events and was supported by the available evidence was a scenario indicating that the Captain experienced spatial disorientation, which resulted in his making inadvertent actions that caused the accident. The remaining scenarios and possible causes were not consistent with the evidence and did not explain the sequence of events identified by the investigative team.”

To which the response of the MCA, as the body with responsibility for the conduct and findings of the Investigation was that:

“With regard to the statement that there was supporting evidence that the captain experienced spatial disorientation is inaccurate to say the least. The investigation team studied this scenario extensively, numerous conflicting evidences appeared leading to the MCA adopting the position that no conclusive evidence could be found to explain this accident.”

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