Status:	Definitief
Datum:	28 JUN 2002
Tijd:	ca. 18:00
Type:	Saab 340B
Luchtvaartmaatschappij:	Hazelton Airlines
Registratie:	VH-OLM
Constructienummer:	340B-205
Bouwjaar:	1990
Aantal vlieguren:	28793
Motoren:	2 General Electric CT7-9B
Bemanning:	slachtoffers: 0 / inzittenden: 3
Passagiers:	slachtoffers: 0 / inzittenden: 29
Totaal:	slachtoffers: 0 / inzittenden: 32
Schade:	Geen
Plaats:	7 km (4.4 mijl) ESE of Bathurst, NSW (Australië)
Fase:	Nadering (APR)
Soort vlucht:	Binnenlandse lijnvlucht
Vliegveld van vertrek:	Sydney-Kingsford Smith International Airport, NSW (SYD/YSSY), Australië
Vliegveld van aankomst:	Bathurst-Raglan Airport, NSW (BHS/YBTH), Australië
Vluchtnummer:	185

Beschrijving:
The Saab was approaching Bathurst's runway 17 with gear down and flaps at 20 degrees. At a radio altitude of 1,266 feet above ground level and a speed of 133 knots the captain commanded the autopilot to roll the aircraft to the right to begin tracking downwind for runway 17. It attained 28 degrees right roll after 7 seconds. Approximately 1 second later, the aircraft commenced an uncommanded roll to the left at a recorded airspeed of 114 knots and a nose-up pitch of 8 degrees. The aircraft rapidly rolled to the left reaching 109 degrees left bank within 4 seconds, before pitching 27 degrees nose down 3 seconds later. During the recovery the aircraft rolled back through wings level to 56 degrees right wing low. The aircraft descended approximately 1,080 feet in 16 seconds, and the minimum radio altitude recorded was 114 feet/35m above ground level. The aircraft's aerodynamic stall warning systems of stick shaker, audible alarm, visual warnings and stick pusher, did not activate.

SIGNIFICANT FACTORS:
1. Although provided with visual cues (windshield wiper), the flight crew did not detect airframe or wing ice during the descent and therefore did not take measures to remove the ice.
2. The flight crew left the power setting unchanged at 17 per cent after levelling out when 50 per cent-60 per cent would have been appropriate given the aircraft configuration and environmental conditions.
3. The flight crew allowed the aircraft’s speed to slow below a safe speed.
4. The stall warning system did not activate prior to the stall.
5. The aircraft was not fitted with the Canadian stall warning system modification. If this had been fitted and activated, it would have alerted the flight crew and provided them with between 3-4 seconds warning of the impending stall.
6. The SOP did not require activation of the de-ice boots in known icing conditions as per the manufacturer documentation.
7. The SOP allowed for the use of the autopilot during icing conditions which masked tactile cues regarding the increasing nose up attitude.

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