1 fatality

2008-08-27: Boeing 737-200 (PK-CJG) — Sriwijaya Air — Jambi, Indonesia

Jambi, IndonesiaLanding (descent or approach)

On August 27, 2008, a Boeing 737-200 (registration PK-CJG) operated by Sriwijaya Air was involved in an aviation accident near Jambi, Indonesia during landing or approach. One person was killed. Investigators recorded the probable cause as: The combination of an excessive touchdown speed and the lack of speed brake deployment prevented effective deceleration following a hydraulic system failure. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781197230Data APIEditorial standards
Aircraft registered PK-CJG
Aircraft registered PK-CJG. Photo: Aeroprints.com / CC BY-SA 3.0, via Wikimedia Commons

A Lion Air flight bound for Jambi overran the runway after a hydraulic failure, resulting in one fatality among farmers working near the airfield.

What happened

On 27 August 2008, a Boeing 737-200, registration PK-CJG, was performing a scheduled flight from Jakarta to Jambi. The aircraft was carrying 124 passengers and 6 crew members. During the descent toward Sultan Thaha Airport, the crew experienced a significant technical failure when the hydraulic system A quantity indicator dropped to zero and a low-pressure warning illuminated while the aircraft was descending through 2500 feet.

Despite the loss of hydraulic pressure, the pilot decided to proceed with the landing on runway 31. During the landing roll, the crew encountered difficulties engaging the thrust reversers and relied on manual braking. The aircraft failed to decelerate sufficiently, drifting from the centerline and exiting the end of the runway. The aircraft came to a rest in a field approximately 6 meters below the runway level.

During the excursion, the aircraft struck three farmers located near the runway perimeter. This impact resulted in one fatality and two serious injuries. Following the stop, the crew attempted emergency ground procedures, but encountered further complications including non-functional radio communications and an inability to shut off engine fuel levers. The aircraft's landing gear and engines detached during the event. While the evacuation was conducted without a formal command from the pilot, all 130 people on board successfully exited the aircraft.

Findings

  • The loss of hydraulic system A occurred at roughly 1,600 feet, providing the crew with enough time to perform a missed approach and evaluate the situation.
  • The aircraft's failure to decelerate was caused by a touchdown speed 27 knots above Vref combined with the failure to deploy speed brakes.

Probable cause

The combination of an excessive touchdown speed and the lack of speed brake deployment prevented effective deceleration following a hydraulic system failure.