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Re: X-Air Ultralight Aircraft Re: Indicated airspeed problem


 

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what aircraft you have?xair or falcon ?
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during initial flight testing aircraft is actually flown to Vd which is over the Vne but that is for design approval purposes,
Vne speed is set during loading calculations, i.e. all the loads applied to the airframe are based on this speed,? there are safety factors built in but this is where Vne comes from and cannot be changed without further load testing (not flight testing)
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----- Original Message -----
Sent: Friday, July 27, 2018 1:03 PM
Subject: Re: X-Air Ultralight Aircraft Re: Indicated airspeed problem

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? VNE is 85 knots or 98 mph, however during the original testing of type in England, the aircraft was flown over VNE? to 95 knots or 109 mph.

Not that I would recommend flying at 95 knots, the original test pilot had a BRS parachute fitted, something the BMAA? won’t let me fit without retesting the whole aircraft.

Regards,

Jon

John you mention 95knots its 95mph (83kn)
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----- Original Message -----
From: mailto:avia1or01@... [X-Air_Ultralight_Aircraft]
To: X-Air_Ultralight_Aircraft@...
Sent: Friday, July 27, 2018 9:25 AM
Subject: X-Air Ultralight Aircraft Re: Indicated airspeed problem
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This is all well and good, however if the aircraft has been changed since it was built it could be that the MAAN figures used by the BMMA are incorrect and they could potentially be asking members to fly their aircraft significantly over VNE.
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I solved the problems with my own aircraft and got my permit. I took advice from various experts and then flew the VNE test again.
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Before re-flying the the VNE test, I made a rough calibration myself to check that I was not doing anything dangerous. I simply flew level at full throttle into wind and then full throttle down wind and observed the GPS speed and IAS.
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The GPS speed was approximately in line with my expectations and so I did the test. I actually did the VNE test twice, again into and down wind. ( there was little wind on that day ) During the test I kept an eye on the GPS speed and ensured that it never at any time exceeded 95 knots.
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Which is 10 knots faster than VNE and also the maximum speed achieved by the test pilot during certification of the the aircraft. By coincidence, my particular aircraft was the prototype used in the original testing and so I know it has flown at 95 knots previously.
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I am very concerned that other owners may be persuaded to fly their aircraft at dangerous speeds and I have heard stories of X airs being pushed to a near vertical dive to achieve the required indicated airspeed.
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To me that suggests they may well have been flying too fast. Mine achieved VNE with a steep dive on full throttle, it was not vertical or anything near it. I simply opened the throttle fully and when maximum level speed was achieved, I pushed the nose down and allowed the aircraft to accelerate to VNE.
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Aside from the these particular concerns, more generally I don’t see the point of any test where the only two possible outcomes are either a pass or a fatal accident.
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Regards,
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Jon

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