|
|
SiteMap
|
You are here: home->pvt_plt->H317->5.3.7.0.8.A.1
3708
(Refer to figure 41.) Determine the approximate ground roll distance required for takeoff.
| OAT |
90 °F |
| Pressure altitude |
2,000 ft |
| Takeoff weight |
2,500 lb |
| Headwind component |
20 kts |
| * | A) 650 feet. |
| | B) 850 feet. |
| | C) 1,000 feet. |
|
Anonymous says: |
17 Sep 2008 |
The explanation should read: The wording of the question is misleading. As currently stated with the word 'category' being singular, the answer would be [B] because the listed classes are all in one category. If the question were stated "... which are categories of aircraft?" the correct answer would be [A] because these are all separate categories of aircraft.
|
|
|
|
|
|