Incident Overview

Date: Thursday 11 May 2023
Aircraft Type: Hawker 900XP
Owner/operator: Angkasa Super Services
Registration Number: PK-LRU
Location: Maleo Airport (MOH) – ÿ Indonesia
Phase of Flight: Landing
Status: Substantial
Casualties: Fatalities: 0 / Occupants: 8
Component Affected: Main Landing Gear StrutMain Landing Gear Strut
Category: Accident
A Hawker 900XP, PK-LRU experienced a runway excursion after landing on runway 23 at Maleo/Morowali Airport (MOH). The aircraft stopped approximately 200 meters past the end of the runway due to upslope terrain across a perimeter road. The aircraft sustained substantial damage during the landing. No injuries occurred. The latest wind report was 060 degrees at 5 knots, influencing the calculated landing distance and VREF.A Hawker 900XP, PK-LRU experienced a runway excursion after landing on runway 23 at Maleo/Morowali Airport (MOH). The aircraft stopped approximately 200 meters past the end of the runway due to upslope terrain across a perimeter road. The aircraft sustained substantial damage during the landing. No injuries occurred. The latest wind report was 060 degrees at 5 knots, influencing the calculated landing distance and VREF.

Description

A Hawker 900XP, PK-LRU, suffered a runway excursion after landing on runway 23 at Maleo/Morowali Airport (MOH). The aircraft came to a stop about 200 m past the end of the runway, on upsloping terrain across a perimeter road. The Hawker suffered substantial damage. There were no injuries. During the descent towards MOH, the latest wind report given was 060 degrees at 5 knots. Based on these wind conditions, the FMS calculated the required landing distance as 4519 feet for the predicted landing weight and flaps 45 configuration. The FMS also calculated the VREF was 125 knots. Runway length was 4920 feet. About 14:59 the aircraft touched down on runway 23. During the landing roll, the crew felt that the aircraft tilted to the right. Both pilots recalled that this might be same as several occurrences before that were caused by the right main landing gear strut being depleted. The PF used steering wheel to control the aircraft direction as advised by the PM. While controlling the aircraft direction, the PF applied brake pedals and pulled the thrust reverser levers but the thrust reverser levers would not deploy. Both pilots attempted to decelerate the aircraft by applying the brakes, but the aircraft failed stop on the runway and overran.

Source of Information

https://www.antaranews.com/berita/3534033/pesawat-tergelincir-di-bandara-morowali-angkut-empat-penumpang?mibextid=Zxz2cZhttps://www.antaranews.com/berita/3534033/pesawat-tergelincir-di-bandara-morowali-angkut-empat-penumpang?mibextid=Zxz2cZ

Primary Cause

Depleted main landing gear strut caused by previous occurrences during right main landing gear strut depletion.Depleted main landing gear strut caused by previous occurrences during right main landing gear strut depletion.

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