Incident Overview

Date: Friday 1 June 2007
Aircraft Type: Gulfstream G-V
Owner/operator: G5 Executive
Registration Number: HB-IMJ
Location: Zrich-Kloten Airport (ZRH) – ÿ Switzerland
Phase of Flight: Landing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 9
Component Affected: Nose landing gearNose landing gear
Investigating Agency: BFU Switz.BFU Switz.
Category: Accident
A Gulfstream V aircraft experienced a forced landing due to a structural failure of the nose landing gear. Four mounting screws on the end cover of the nose gear actuator door tore, preventing extension of the landing gear. This resulted in a low pass over runway 14, leading to a failure of the alternate landing procedure and subsequent forced landing.A Gulfstream V aircraft experienced a forced landing due to a structural failure of the nose landing gear. Four mounting screws on the end cover of the nose gear actuator door tore, preventing extension of the landing gear. This resulted in a low pass over runway 14, leading to a failure of the alternate landing procedure and subsequent forced landing.

Description

The Gulfstream V was conducting an ILS approach to runway 14 at Zrich-Kloten Airport, Switzerland when the crew noticed that the nose landing gear failed to extend. After retracting the undercarriage again, there was a drop in pressure of the left hand hydraulic system. A second approach was flown and again the nose landing gear failed to extend. A low pass over runway 14 so the condition of the nose gear could be observed from the ground. The alternate procedure to get gear down failed, as did g-load manoeuvres. At 22:53 a forced landing was carried out with the nose gear retracted. Causes The accident is attributable to the fact that all four mounting screws of the end cover (gland) of the shuttle valve of the nose gear actuator door had torn, breaking the cover plate. As a result, the nose landing gear could not be extended. have contributed to the accident: – Failure of the emergency system due to a leak, which was caused by the severed end cap of the shuttle valve – Unsuitable and insufficient tightened fixing screws on the end cap of the shuttle valve – Low material thickness of closure lid

Primary Cause

Tearing of four mounting screws on the end cover of the nose gear actuator door.Tearing of four mounting screws on the end cover of the nose gear actuator door.

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