Jump to content

Jabiru7252

Members
  • Posts

    1,155
  • Joined

  • Last visited

  • Days Won

    3

Posts posted by Jabiru7252

  1. I do not think spin training or spiral dives (did both as a PPL student) are required in LSA training. We used to do fully developed spins in the Tomahawk. Spin long enough for the instructor to point out airspeed, rate of descent, impact point etc. Thank God we don't do that anymore, I'd lose my lunch in my rompers pretty quick these days...

  2. 1 hour ago, anjum_jabiru said:

    Hi everyone

     

    I was just doing a desktop comparison between the Jabiru J160 and J170. One of the things that got my attention was the difference in stall speeds between the 2 aircrafts. The clean stall speed of J160 is 55KCAS (58KIAS), whereas that of the J170 is 45 KCAS. A difference of 10 knots!!

     

    Just wondering if this raises any eyebrows or is it a cause for concern, as it appears to have a very low threshold or safety margin, before it can enter a stall or spin, especially if one happens to do a steep turn and if the speed was to bleed off rapidly and unintentionally. 

     

    I would like to know of any real life experience or any thoughts on this high stall speed in a J160?

    Where did that info come from? It's wrong! When I learnt to fly the Jabs it was in a J160 and my speed on late final was around 60kts. I think you'll find 45kts clean and 40kts with full flaps. (10 minutes later....) I downloaded the POH for the J160D and it does state what you said. That's very strange, I'd be tempted to contact Jabiru.

    • Helpful 1
  3. My halogen light causes no interference - why would it? The strobe doesn't either though some can. The strobe electronics fried not long after I bought my plane so I replaced with a cheap unit from Dick Smiths. (A burglar alarm unit). Cost $40 as opposed to $350. Been working great for the last 10 years.

    • Informative 1
  4. On 05/12/2020 at 11:20 AM, old man emu said:

    Leaving out changes to power settings, we move the elevator to induce pitch changes and the rudder to induce yaw changes. But how do these moveable surfaces at the rear of fixed surfaces produce the forces necessary to change pitch and yaw angles? Are these devices increasing Drag, or increasing aerodynamic Lift?

    A simple way to describe what's going on. The airflow pushes on the deflected surface (elevator/aileron etc.) and the reactionary force pushes the surface in the opposite direction of deflection. For every action there is an equal and opposite reaction. The downward pointing arrow is a vector representing the deflection force and the drag. 

    foobar.png

×
×
  • Create New...