General Navigation - ATPL Exam & ATPL Question Bank

Inertial Reference System sensors include:	4 Answers
During the initial alignment of an inertial navigation system (INS) the equipment:	4 Answers
The alignment time, at mid-latitudes, for an Inertial Reference System using laser ring gyros is approximately:	4 Answers
The full alignment of the stable platform of an Inertial Navigation System:	4 Answers
Which of the following lists the order of available selections on the Mode Selector switches of a 737-400 Inertial Reference System?	4 Answers
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?	4 Answers
Given: True Heading = 090° TAS = 200 kt W/V = 220° / 30 kt. Calculate the GS?	4 Answers
Given: TAS = 485 kt, HDG (T) = 168°, W/V = 130/75kt. Calculate the Track (°T) and GS?	4 Answers
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:	4 Answers
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?	4 Answers

General Navigation - ATPL - Airline Transport Pilot license