This is my first post. I have lurked here off and on for the last year. I finally decided to buy the Preview Plans for the 9A and they arrived earlier this week.
While pouring over the Weight and Balance section, I came up with a question about the data presented on Page 14-12.
That page addresses calculating the nose wheel weight based on gross weight and CG. The example given at the bottom of the page results in a nose wheel weight of 362 lbs. using a 100 lb. pilot, 216 lbs. of fuel, no passenger and no baggage. Furthermore, the horizontal line indicating the 362 lb nose wheel weight solution is shown below the hatched area with its lower boundary value of 325 lbs.
In the notes to the right of the example and on page 14-3, in the boxed data, it states that the maximum allowable nose wheel weight is 325 lbs. Is there an error in the maximum allowable nose wheel weight? It doesn?t seem reasonable that with only a really skinny pilot and full fuel, that one could exceed the maximum nose wheel weight allowance.
Also in doing some math, I calculate that in that same example, the nose wheel weight is 339 lbs not 362 lbs. I admit my calculations could be faulty however they still result in exceeding the stated maximum.
Does anyone have any insight into this. Is it possible that this data was reproduced for the 9A from a previous model or is there some other explanation?
Bob Paulsen
While pouring over the Weight and Balance section, I came up with a question about the data presented on Page 14-12.
That page addresses calculating the nose wheel weight based on gross weight and CG. The example given at the bottom of the page results in a nose wheel weight of 362 lbs. using a 100 lb. pilot, 216 lbs. of fuel, no passenger and no baggage. Furthermore, the horizontal line indicating the 362 lb nose wheel weight solution is shown below the hatched area with its lower boundary value of 325 lbs.
In the notes to the right of the example and on page 14-3, in the boxed data, it states that the maximum allowable nose wheel weight is 325 lbs. Is there an error in the maximum allowable nose wheel weight? It doesn?t seem reasonable that with only a really skinny pilot and full fuel, that one could exceed the maximum nose wheel weight allowance.
Also in doing some math, I calculate that in that same example, the nose wheel weight is 339 lbs not 362 lbs. I admit my calculations could be faulty however they still result in exceeding the stated maximum.
Does anyone have any insight into this. Is it possible that this data was reproduced for the 9A from a previous model or is there some other explanation?
Bob Paulsen