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The number of electrical fuses of a particular rating required to be carried in an aircraft is
- 5 amp or less 3, off 5 amp or more 10 off.
- 3% of each rating or 10, whichever is the greater.
- 10% of each rating or 3, whichever is the greater.
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The input is 115V and is applied across the 300 turn portion of the autotransformer shown. What is the output?

- 115V
- 28V
- 460V
Could someone clarify this?
Intense or loud noise may lead to
- vertigo.
- fatigue.
- fitness.
Quite unlikely...
Before an aircraft reaches critical mach
- the nose pitches up because the CP moves Forward.
- the aircraft buffets because the CP moves to the shock wave.
- the nose pitches down because the CP moves rear.
why CP moves rear?
Excessive wear on both sides of the control cable pulley groove is evidence of
- pulley misalignment.
- excessive cable tension.
- cable misalignment.
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