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EN ATPL General Navigation Questions in English
Practise General Navigation
What are the main navigation sensors in a conventional ring-laser-gyro-based strapdown inertial reference system?
For a conventional, stand-alone INS during ground alignment, which statement about an incorrectly entered starting position is correct?
For the conventional INS/IRS ground-alignment process described in the EASA theoretical-knowledge syllabus, what is the approximate full-alignment time at mid latitudes?
For a conventional, unaided civil-aircraft INS whose full navigation alignment uses a stationary ground procedure, full alignment of the stable platform:
Which of the following lists the order of available selections on the Mode Selector switches of a 737-400 Inertial Reference System?
Which of the following statements concerning the aircraft positions indicated on a triple fit Inertial Navigation System (INS)/ Inertial Reference System (IRS) on the CDU is correct?
Given: True Heading = 090° TAS = 200 kt W/V = 220° / 30 kt. Calculate the GS?
Given: TAS = 485 kt, HDG (T) = 168°, W/V = 130/75kt. Calculate the Track (°T) and GS?
For a distance of 1860 NM between Q and R, a ground speed 'out' of 385 kt, a ground speed 'back' of 465 kt and an endurance of 8 HR (excluding reserves) the distance from Q to the point of safe return (PSR) is:
Given: Distance A to B is 360 NM. Wind component A - B is -15 kt, Wind component B - A is +15 kt, TAS is 180 kt. What is the distance from the equal-time-point to B?
