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-   -   Hughes/MD 500 (https://www.pprune.org/rotorheads/386804-hughes-md-500-a.html)

Shawn Coyle 26th Aug 2012 00:26

Not sure which blades, but definitely not the Van Horn ones as they're not on the market yet.

500 Fan 25th Aug 2013 22:07

G-BIOA on BBC2 now doing a little sling-load/glider launch work for James May.

500 Fan.

Hughes500 26th Aug 2013 20:58

Highest I have ever flown a helicopter agl that is !!!!

Hedski 28th Aug 2013 21:11

Looked nice. Digressing slightly how did the R44 fly that far over water with pax and no floats single engine?

Hughes500 29th Aug 2013 16:36

Can do what you want single engine if there are no fare paying pax !

500e 14th Aug 2014 11:28

Playing with more things on a string & James then H500

Hughes500 14th Aug 2014 16:28

Well it was satisfying dropping a Lada from 500ft for Mr May, made a large dent in the grass, was sweating a bit as it landed very close to the runway !

catseye 14th Aug 2014 22:33

hughes 500,

thought they would have at least wanted a Volkswagon......:=

Hot and Hi 2nd Apr 2016 18:08

VNE differences between 250-C20B and C20R/2 engine
 
Could somebody explain why the VNE is differs between the two engines, for the same type?

For example, at >2,500 lbs, 30 deg C OAT, and a pressure ALT of 6,000' the VNE for the 500D equipped with a B engine is 103 KTS. With the (more powerful) R/2 engine it is 96 KTS.

On the 500E the respective VNE's are: 102 KTS (B engine) vs 96 KTS (R/2 engine).

(Source: VNE placards from the MD Rotorcraft Flights Manuals: 500D revision 9; 500E revision 14)

mfriskel 2nd Apr 2016 19:12

It could be a number of things.
1. Different test pilot getting the test points for a very subjective test point.
2. Different rotor blades, possibly a difference in abraision strips from C20B testing to C20R2 testing.
3. A less smooth track on the acft that set the C20R2 test points.
4. Rougher air when they flew the C20R2 test points.




Originally Posted by Hot and Hi (Post 9331277)
Could somebody explain why the VNE is differs between the two engines, for the same type?

For example, at >2,500 lbs, 30 deg C OAT, and a pressure ALT of 6,000' the VNE for the 500D equipped with a B engine is 103 KTS. With the (more powerful) R/2 engine it is 96 KTS.

On the 500E the respective VNE's are: 102 KTS (B engine) vs 96 KTS (R/2 engine).

(Source: VNE placards from the MD Rotorcraft Flights Manuals: 500D revision 9; 500E revision 14)


AnFI 3rd Apr 2016 16:48

You would expect lower Vne with more power.

Other way to do it would be a reduced Vne above a certain power.
Many helicopters do that.

Hot and Hi 21st May 2022 07:43

High skid conversion
 
Converting a low skid 500E to high skid, is that feasible? What parts are needed?

rudestuff 21st May 2022 08:21


Originally Posted by Hot and Hi (Post 11233133)
Converting a low skid 500E to high skid, is that feasible? What parts are needed?

Probably skids?

md 600 driver 21st May 2022 09:32

The e and the d have both different speed regardless of engine if I remember correctly the d is faster due to the different body shape

Flyting 2nd Mar 2023 13:23

Hi All
I´m looking for options for pods and/or baskets for a 520


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