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Compared with the flap down configuration the maximum angle of attack for the flaps up configuration is
- smaller.
- larger.
- unchanged.
diaandrita asking:
Could please anyone explain this question?
A restrictor in the landing gear hydraulic retraction and lowering system is positioned in the
- landing gear down line.
- return line from the landing gear selector.
- landing gear up line.
diaandrita asking:
Why? i though it will be positioned in the lowering line to damping landing gear extention due to aerodynamics loads.
log 100/2 =
- 1
- log 98
- log 200
gav_18s asking:
how do you work this out?
60 mm expressed as a percentage of 3 meters is
- 0.5%.
- 1.8%.
- 2%.
gav_18s asking:
How do you work this out?
Choose the correct statement
- sec^2 * x + tan^2 * x = 1
- cosec^2 * x - cot^2 * x = 1
- cos^2 * x - sin^2 * x = 1
gav_18s asking:
Can anyone explain this?