Investigation number
AO-2009-044
Occurrence date
Location
74 km NE of Perth Airport
State
Western Australia
Report release date
Report status
Final
Investigation level
Systemic
Investigation type
Occurrence Investigation
Investigation status
Completed
Aviation occurrence category
Landing gear/indication
Occurrence class
Serious Incident
Highest injury level
None

On 16 July 2009 the pilot of a Beechcraft King Air C90 aircraft, registered VH-TAM, departed Perth Airport on a flight to Wiluna, Western Australia with one passenger on board.

Sometime after becoming established at flight level (FL) 210, the pilot became affected by hypoxia, which resulted in him becoming fixated on the 'distance-to-run' figures on the aircraft's Global Positioning System equipment display and incorrectly interpreting those figures as the aircraft's 'groundspeed'. That confusion resulted in the pilot interpreting the lower-than-expected figures as a significant headwind and in him descending the aircraft to escape the winds. Once established at FL150 for a significant period of time, he realised that that he had been affected by hypoxia. The pilot descended further before landing at his destination.

The investigation identified problems with the aircraft's left landing gear squat switch that prevented the aircraft from pressurising in flight. In addition, the cabin altitude warning system was non‑operational due to the incorrect connection of the switch wiring during previous maintenance.

Following this occurrence, the aircraft manufacturer changed the aircraft type's maintenance manuals and documentation and the Civil Aviation Safety Authority (CASA) issued a letter to owners and operators of Australian-registered pressurised aircraft that proposed mandating the fitment of aural cabin pressure warning systems in those aircraft. As a result of that industry consultation, CASA determined that a uniquely Australian installation requirement could not be justified.

Notwithstanding, as a result of the ongoing risk of serious incidents and fatal accidents in which the occupants of single-pilot, turbine‑powered, pressurised aircraft have been affected by, or have succumbed to unrecognised hypoxia in an unpressurised cabin, the Australian Transport Safety Bureau has issued a safety advisory notice. That notice encourages all operators of such aircraft to consider the installation of an aural cabin altitude pressure warning system that operates separately to their aircraft's visual warning system.

Aircraft Details
Manufacturer
Beech Aircraft Corp
Model
90
Registration
VH-TAM
Serial number
LJ-919
Operation type
Charter
Sector
Turboprop
Departure point
Perth, WA
Destination
Wiluna, WA
Damage
Nil
Recommendations
Approval Date
Organisation
All operators of single-pilot, turbine-powered, pressurised aircraft
Output Number
Published Date Time
Recommendation type
Status
Body

The Australian Transport Safety Bureau encourages all operators
of single-pilot, turbine-powered, pressurised aircraft to consider
the installation of an aural cabin altitude pressure warning system
that operates separately to their aircraft's visual warning
system.

Mode
Date released