Crash-aerien 06 AUG 1976 d'un GAF Nomad N.24 [VH-SUZ] - Avalon Airport, VIC (AVV)
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Statuts:Accident investigation report completed and information captured
Date:vendredi 6 aot 1976
Type/Sous-type:Silhouette image of generic NOMA model; specific model in this crash may look slightly different
GAF Nomad N.24
Compagnie:Government Aircraft Factories - GAF
Immatriculation: [VH-SUZ]
Numéro de série: 10
Année de Fabrication: 1975
Heures de vol:139
Moteurs: 2 Allison 250-B17B
Equipage:victimes: 2 / à bord: 3
Passagers:victimes: 0 / à bord: 0
Total:victimes: 2 / à bord: 3
Dégats de l'appareil: Détruit
Conséquences: Written off (damaged beyond repair)
Lieu de l'accident:Avalon Airport, VIC (AVV) (   Australie)
Élévation des lieux de l'accident: 11 m (36 feet) amsl
Phase de vol: En montée initiale (ICL)
Aéroport de départ:Avalon Airport, VIC (AVV/YMAV), Australie
Aéroport de destination:Avalon Airport, VIC (AVV/YMAV), Australie
Numéro de vol: 128
During the certification process, the GAF N24 Nomad encountered problems with longitudinal stability at the 20° flap setting. In the opinion of the Chief Test Pilot, the stick force gradient was unacceptable at the 20° flap setting.
While the longitudinal stability problem may not have affected Australian certification of the N24, it was considered important to solve the problem for a developed version of the aircraft. Accordingly, the Government Aircraft Factories (GAF) made and flight tested a series of modifications to the tailplane.
Before the accident flight the full-span trim tabs were fitted with 50 mm T strips.
The purpose of the flight on which the accident occurred was to examine the effect of these tailplane modifications on the longitudinal stability of the aircraft in the 20 degree flap configuration required for the N24A model. It was intended that, after take-off, the aircraft would proceed to a designated flight test area where, at a safe altitude, the tests would be carried out. The aircraft was not to be flown at a speed in excess of 120 knots equivalent airspeed (EAS).
At 10:51 hours the pilot of the aircraft, using his personal radio callsign GAF ONE, contacted Avalon Tower by radio and advised that he had received the current aerodrome terminal information and was taxiing. The aircraft then taxied to the east-west grass strip.
At 10:58 hours Avalon Tower advised the aircraft of the local weather and that there were aircraft reports of extensive cloud and build-ups to the south-west moving in a north-easterly direction. The pilot acknowledged this information. At 11:00 hours the aircraft notified that it was ready for take-off and the controller advised that there would be a short delay, which was due to other traffic landing on the runway. At 11:00:23 hours the Nomad was cleared for take-off and an unrestricted climb.
The aircraft took off into the west from the grass strip and, immediately it became airborne, the pilot applied a series of 'push-pull' control inputs to the tailplane after which the aircraft commenced its initial climb. The aircraft climbed straight ahead in a normal manner and reached a height of about 950 feet when over or just past the runway. At this point three witnesses on the ground observed the trailing edge of the aircraft's tailplane fluttering and he saw a dark object fall from the aircraft to the ground. At about this time the aerodrome controller, located in the control tower some 1250 metres south-east of the aircraft, saw it adopt a steep nose-down attitude and asked whether operations were normal. The pilot replied 'negative', and the aerodrome controller then initiated emergency procedures and the crash alarm was sounded.
The aircraft then turned left onto a southerly heading while still descending, and may have maintained this heading briefly before continuing to turn left onto an easterly heading. Just prior to contact with the ground, the left wing and the nose dropped, and after impact the aircraft rotated through 120 degrees in the horizontal plane and skidded rearwards for a distance of some 70 metre before coming to rest.
For the flight on which the accident occurred the aircraft carried the trade-plate registration VH-SUZ.

Probable Cause:

CAUSE: "The cause of the accident was that the simplified design criterion which was used to justify freedom from flutter during the flight testing of various tailplane modifications was not valid for a design which included tab trailing edge T strips."

Accident investigation:

Investigating agency: ASIB
Status: Investigation completed
Duration: 1 years
Accident number: jan-77
Download report: Final report

» The Sydney Morning Herald - Aug 19, 1976


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Les informations ci-dessus ne représentent pas l'opinion de la 'Flight Safety Foundation' ou de 'Aviation Safety Network' sur les causes de l'accident. Ces informations prélimimaires sont basées sur les faits tel qu'ils sont connus à ce jour.
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