Incident Overview

Date: Tuesday 2 January 1990
Aircraft Type: CASA/Nurtanio NC-212 Aviocar 200
Owner/operator: Pelita Air Service
Registration Number: PK-PCM
Location: Banten Bay, Java Sea – ÿ Indonesia
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 9 / Occupants: 16
Component Affected: Second engineSecond engine
Category: Accident
A Pelita Air Service C-212 passenger plane crashed in the northern part of Banten Bay, Indonesia, resulting in the deaths of nine passengers and seven survivors. The aircraft experienced a loss of power on the second engine, leading to a gradual descent and a ditching.A Pelita Air Service C-212 passenger plane crashed in the northern part of Banten Bay, Indonesia, resulting in the deaths of nine passengers and seven survivors. The aircraft experienced a loss of power on the second engine, leading to a gradual descent and a ditching.

Description

A Pelita Air Service C-212 Aviocar ditched in the sea between Palembang and Jakarta, Indonesia, killing 9 occupants; 7 survived the accident. The Aviocar passenger plane of Pelita Air Service was en route between Palembang and Jakarta, Indonesia, when the no. 2 engine failed. Altitude could not be maintained and the airplane began a gradual descent over sea. All luggage and two ground fire extinguishers were thrown overboard, but the descent was not arrested. Eventually a ditching became inevitable. The airplane came down in the northern part of Banten Bay, approx 90 km WNW from Jakarta. It is understood that the takeoff weight on departure from Palembang was 18,192 lb, which was over the 16,160 lb maximum takeoff weight. The weight of two ground fire extinguishers and a GPU which were carried on board as cargo were probably underestimated.

Source of Information

https://news.google.com/newspapers?id=S6RUAAAAIBAJ&sjid=iZADAAAAIBAJ&dq=indonesia%20plane&pg=3901%2C625300https://news.google.com/newspapers?id=S6RUAAAAIBAJ&sjid=iZADAAAAIBAJ&dq=indonesia%20plane&pg=3901%2C625300

Primary Cause

Loss of engine power on the second engine during descent.Loss of engine power on the second engine during descent.

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