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Posted

Mahendra Aerospace website only lists GA8 and GA10. GA18 gone byebye.

 

 

  • Caution 1
Posted
Mahendra Aerospace website only lists GA8 and GA10. GA18 gone byebye.

Sadly, the GA18 guru's were let go in one of there mass sackings. No one is even qualified to fly the demo machine now and it is gathering dust in the hanger last I heard.

 

 

Posted

The only mention is on the Service page, and refers to Nomad, not GA18.

 

 

Posted
The only mention is on the Service page, and refers to Nomad, not GA18.

Yer I heard they brought the "Nomad" from Boeing along with a massive parts inventory and part of the deal is they have to support all current nomads that are flying across the world.

 

 

Posted
was the demo a n24?

N24A, purchased from Air Safari's New Zealand in 2011, Ex ZK-NMC now registered VH-XGZ

 

 

Posted

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History of VH-XGZ from http://nzcivair.blogspot.com.au/2011/09/exported-gaf-n24a-nomad-zk-nmc.html?m=1

 

It was first registered to the Department of Health Northern Territory Medical Service (Flying Doctor is easier to say) of Darwin on 03-11-1977 as VH-DHP.

 

In September of 1987 it went to Skywest Aviation Pty Ltd of Cloverdale, West Australia and then was noted parked up at Darwin until listed to Kelvin Stark of Auckland on 17-12-1996.

 

It arrived in NZ in December of 1996 and joined the Air Safaris & Services (NZ) Ltd fleet at Tekapo from 05-05-1997 as ZK-NMC.

 

image.jpeg.c7121e2cd1c8a9f9110e50a10ef7cc37.jpeg

 

 

Posted

I have the video that did on air safaris. it was well done. they also seem to enjoy there nomad aircraft.

 

 

  • 2 weeks later...
  • 3 weeks later...
Posted
Gday Mike.

Ah.. Pilks.. Hello again.. by the way I am pretty sure I know the cause of the N24 stick force anomaly.. after I left GAF I was going over all the details.. with the crash I kept going back to the aerodynamic model.. and in the end a simple diagram of prop vorticity in a turn gave the answer..

(N24 stretched fuse) + (2 x same prop rotation) + (higher power) + (critical up elevator) = fuselage power induced vortex = differential tailplane incidence = half tailplane stall or some level of separation = sudden reduction in stick force.

 

What do think..

 

 

Posted

what model was the one that crashed when being test flown from the factory?

 

 

Posted
what model was the one that crashed when being test flown from the factory?

Had to be N24 because as far as I can recall the N22 did not have the problem..

 

 

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