Incident Overview

Date: Saturday 3 January 2004
Aircraft Type: Boeing 737-3Q8
Owner/operator: Flash Airlines
Registration Number: SU-ZCF
Location: 15 km S off Sharm el Sheikh – ÿ Egypt
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 148 / Occupants: 148
Component Affected: Aircraft Control System (Specifically Autopilot and Throttle Control).Aircraft Control System (Specifically Autopilot and Throttle Control).
Investigating Agency: ECAAECAA
Category: Accident
A Flash Airlines Boeing 737-300 crashed into the sea off Sharm el Sheikh, resulting in the loss of all 148 passengers and crew. The flight departed from Red Sea resort Sharm el-Sheikh for Paris-CDG with an intermediate stop in Cairo. Initial conditions were favorable with perfect weather ? excellent visibility (17 degrees C), a light breeze (17 knots). The flight was cleared for a procedural left turn to intercept the 306 radial, and the captain initiated an autopilot switch. The captain then requested heading select, and the autopilot was switched off. The captain then requested a right bank turn, and the copilot issued a warning about the increasing bank angle. The aircraft reached a maximum altitude of 5460 feet with a 40-degree bank, and the copilot stated ‘Overbank’. The aircraft then increased speed, leading to a maximum bank angle of 111 degrees right, resulting in a pitch attitude of 43 degrees nose down and an altitude of 3470 feet. The observer on the flight deck reported a retard power command, and the aircraft experienced a nose-down recovery, but the speed increased, causing an overspeed warning. The aircraft struck the water at a speed of 416 kts, with a 3.9 G load, resulting in a 24-degree right bank and a depth of approximately 900 meters. The investigation concluded that while the crew attempted recovery, the gravity upset ? a combination of attitude, altitude, and speed ? was insufficient to achieve a successful recovery.A Flash Airlines Boeing 737-300 crashed into the sea off Sharm el Sheikh, resulting in the loss of all 148 passengers and crew. The flight departed from Red Sea resort Sharm el-Sheikh for Paris-CDG with an intermediate stop in Cairo. Initial conditions were favorable with perfect weather ? excellent visibility (17 degrees C), a light breeze (17 knots). The flight was cleared for a procedural left turn to intercept the 306 radial, and the captain initiated an autopilot switch. The captain then requested heading select, and the autopilot was switched off. The captain then requested a right bank turn, and the copilot issued a warning about the increasing bank angle. The aircraft reached a maximum altitude of 5460 feet with a 40-degree bank, and the copilot stated ‘Overbank’. The aircraft then increased speed, leading to a maximum bank angle of 111 degrees right, resulting in a pitch attitude of 43 degrees nose down and an altitude of 3470 feet. The observer on the flight deck reported a retard power command, and the aircraft experienced a nose-down recovery, but the speed increased, causing an overspeed warning. The aircraft struck the water at a speed of 416 kts, with a 3.9 G load, resulting in a 24-degree right bank and a depth of approximately 900 meters. The investigation concluded that while the crew attempted recovery, the gravity upset ? a combination of attitude, altitude, and speed ? was insufficient to achieve a successful recovery.

Description

Flash Airlines flight 604, a Boeing 737-300, crashed into the sea off Sharm el Sheikh following a loss of control, killing all 148 occupants Weather was perfect (excellent visibility, 17 degrees C and a light breeze) when Flash Air flight 604 departed the Red Sea resort of Sharm el Sheikh for a flight to Paris-CDG with an intermediate stop at Cairo. On board were 135, mostly French, holidaymakers who were heading home. At 04:38 the flight was cleared to taxi to runway 22R for departure. After takeoff, at 04:42, the plane climbed and maneuvered for a procedural left turn to intercept the 306 radial from the Sharm el-Sheikh VOR station. When the autopilot was engaged the captain made an exclamation and the autopilot was immediately switched off again. The captain then requested Heading Select to be engaged. The plane then began to bank to the right. The copilot then warned the captain a few times about the fact that the bank angle was increasing. At a bank angle of 40 degrees to the right the captain stated “OK come out”. The ailerons returned briefly to neutral before additional aileron movements commanded an increase in the right bank. The aircraft had reached a maximum altitude of 5460 feet with a 50 degrees bank when the copilot stated: “Overbank”. Repeating himself as the bank angle kept increasing. The maximum bank angle recorded was 111 degrees right. Pitch attitude at that time was 43 degrees nose down and altitude was 3470 feet. The observer on the flight deck, a trainee copilot, called “Retard power, retard power, retard power”. Both throttles were moved to idle and the airplane gently seemed to recover from the nose-down, right bank attitude. Speed however increased, causing an overspeed warning. At 04:45 the airplane struck the surface of the water in a 24 degrees right bank, 24 degrees nose-down, at a speed of 416 kts and with a 3,9 G load. The wreckage sank to a depth of approx. 900 metres. CONCLUSION: “No conclusive evidence could be found from the findings gathered through this investigation to determine the 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 upset condition with regards to attitude, altitude and speed made this attempt insufficient to achieve a successful recovery.”

Source of Information

http://www.skybrary.aero/index.php/B733,_vicinity_Sharm_El-Sheikh_Egypt,_2004http://www.skybrary.aero/index.php/B733,_vicinity_Sharm_El-Sheikh_Egypt,_2004

Primary Cause

The primary cause appears to be a combination of factors related to the pilot’s actions and the aircraft’s response to unexpected conditions. The initial right bank turn, combined with the increasing bank angle, created a dangerous situation. The pilot’s attempts to recover were inadequate given the severity of the situation, resulting in the aircraft’s uncontrolled descent and impact.The primary cause appears to be a combination of factors related to the pilot’s actions and the aircraft’s response to unexpected conditions. The initial right bank turn, combined with the increasing bank angle, created a dangerous situation. The pilot’s attempts to recover were inadequate given the severity of the situation, resulting in the aircraft’s uncontrolled descent and impact.

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