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You are here: home->pvt_plt->H928->2.3.2.2.3.A.1
3223
One purpose of the dual ignition system on an aircraft engine is to provide for
| * | A) improved engine performance. |
| | B) uniform heat distribution. |
| | C) balanced cylinder head pressure. |
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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.
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