New Thunder Gull owner...its official!!
Posted: Tue Jun 18, 2013 10:41 pm
Well, I am now the proud owner of a Thunder Gull "F"! I posted pics in a new album entitled "Folding Thunder Gull - new purchase"
Here are the stats/specs
91 hours TTAE, 41 hours since 447 "rebuild" in 2005. Pull start, inverted 447 , points and single carb
Specs from an old ad for this plane
folding wing, 27.5' wingspan
wing area 128 sq ft
length 18.5'
width folded 7' 8"
64" IVO 3 blade prop
rate of climb 1100 FPM
stall speed 27 MPH
Take off dist. 80'
Landing distance 80'
Glide ratio 12-1
VNE 105 MPH
YLF +6 -4
I hope Mark will chime in and see if this is matches his figures. Lower VNE than the modern gulls...If correct, maybe folding wing related, maybe overall design related?
Stall speed seems a bit optimistic as well since it has no flaps, just full length ailerons. Of course, it does have that big wing...
Some additional differences between the "F" and the "J"
non aerodynamic tail with elevators instead of stabilators
no in cockpit trim
struts (of course)
no flaps
Those are what I have noticed so far. Again, maybe Mark can enlighten us further...
Will be taking lessons in a two seat Flightstar in the next few weeks. Brushing up on the ground school and book work as well. I will be more than happy to answer any questions you may have.
And any suggestions for a new flyer would be very welcome!
Thanks for the group!!
Bob
Here are the stats/specs
91 hours TTAE, 41 hours since 447 "rebuild" in 2005. Pull start, inverted 447 , points and single carb
Specs from an old ad for this plane
folding wing, 27.5' wingspan
wing area 128 sq ft
length 18.5'
width folded 7' 8"
64" IVO 3 blade prop
rate of climb 1100 FPM
stall speed 27 MPH
Take off dist. 80'
Landing distance 80'
Glide ratio 12-1
VNE 105 MPH
YLF +6 -4
I hope Mark will chime in and see if this is matches his figures. Lower VNE than the modern gulls...If correct, maybe folding wing related, maybe overall design related?
Stall speed seems a bit optimistic as well since it has no flaps, just full length ailerons. Of course, it does have that big wing...
Some additional differences between the "F" and the "J"
non aerodynamic tail with elevators instead of stabilators
no in cockpit trim
struts (of course)
no flaps
Those are what I have noticed so far. Again, maybe Mark can enlighten us further...
Will be taking lessons in a two seat Flightstar in the next few weeks. Brushing up on the ground school and book work as well. I will be more than happy to answer any questions you may have.
And any suggestions for a new flyer would be very welcome!
Thanks for the group!!
Bob