used for the center of the |
of a three degree glide path , |
pilot ’ s mass , we can deduce : |
our G450 pilot ’ s eyes will be |
263 ’ behind the aim point , | |
We ’ ll call that an even 40 |
which means the wheels |
feet . |
will be 303 ’ behind the aim |
Further research leads us |
point . In other words , if |
to a Gulfstream Eye Wheel |
you are aiming for the five |
Height Paper which tells |
hundred foot markers and |
us the pilot ’ s eyes will be |
don ’ t flare , you wheels will |
between 10.4 and 10.8 feet |
just barely make the runway . |
off the ground , depending on |
Add a gust of wind or just |
weight and center of gravity . |
a little deviation from glide |
We ’ ll use 10.5 feet . |
path , you may not reach the |
runway at all . What about | |
Photo : G450 eye wheel |
aircraft with flatter deck |
height , from Tom ’ s notes . |
angles ? The Challenger 604 , |
The Gulfstream Eye Wheel |
for example , has 0 ° approach |
Height Paper tells us our |
deck angle . To isolate only |
eyes will be 13.8 ’ off the |
the deck angle factor , we |
runway when the wheels |
will use G450 dimensions to |
touch on landing , which is |
explore the impact of deck |
what we needed for this |
angle on look down angle . |
exercise . The process to | |
find the deck angle of the | |
Issue January | www . mdnvirtual . org | MDN || 7 |