Casualties unknown

2011-12-24: Boeing 737-200 (PK-CJD) — Sriwijaya Air — Sultan Mahmud Badaruddin II Airport, Palembang, ID

Sultan Mahmud Badaruddin II Airport, Palembang, ID

On December 24, 2011, a Boeing 737-200 (registration PK-CJD) operated by Sriwijaya Air was involved in an aviation accident near Sultan Mahmud Badaruddin II Airport, Palembang, ID. This summary draws on records from the Indonesian National Transportation Safety Committee (KNKT); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Indonesian National Transportation Safety Committee (KNKT)Primary reportUpdated 1785107694Data APIEditorial standards
Boeing 737-200
Photo: San Diego Air & Space Museum Archives / Public domain, via Wikimedia Commons

On 24 December 2011, a Sriwijaya Air Boeing 737-200 (PK-CJD) experienced a hydraulic hose failure and overran the runway at Sultan Mahmud Badarudin II Airport, Palembang, Indonesia. The flight was scheduled from Pekanbaru to Jakarta with 134 persons aboard.

History of the Flight

On 24 December 2011, a Boeing 737-200 aircraft registered PK-CJD, operated by PT. Sriwijaya Air, was performing scheduled passenger flight SJ 041 from Sultan Syarif Kasim II Airport, Pekanbaru, to Soekarno-Hatta International Airport, Jakarta. The aircraft carried 134 persons: 2 pilots, 4 cabin crew, and 128 passengers (114 adults and 4 children).

Hydraulic System Failure

During the flight, a hydraulic hose installed on the right main landing gear (RH MLG) burst. The burst occurred at the middle section of the hose, as documented in the investigation. The failure led to a loss of hydraulic fluid, affecting the aircraft's hydraulic systems.

Runway Overrun

The aircraft subsequently landed at Sultan Mahmud Badarudin II Airport, Palembang. During landing, it overran the runway and came to a stop in the overrun area (area 11). The aircraft sustained damage, and the investigation documented the final position of the aircraft.

Investigation Findings

The National Transportation Safety Committee (NTSC) conducted the investigation. Tests on the failed hydraulic hose (part number AE2464163E0192) revealed that the wire mesh had fractured due to fatigue and static tensile overload. The fracture characteristics indicated initial fatigue cracks, followed by static rupture. The investigation also examined the hydraulic system, flight data, and maintenance actions. The NTSC's conclusions identified contributing factors, which are detailed in the final report.