General Navigation - Quiz ATPL - Exam test Airline Transport Pilot license

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 ktW/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
An aircraft at FL370 is required to commence descent when 100 NM from a DME facility and to cross the station at FL120. If the mean GS during the descent is 396 kt, the minimum rate of descent required is approximately:	4 Answers
In a Flight Management System (FMS), control Display Units (CDUs) are used pre-flight to	4 Answers
The term drift refers to the wander of the axis of a gyro in:	4 Answers
The purpose of the TAS input, from the air data computer, to the Inertial Navigation System is for:	4 Answers

ATPL - Airline Transport Pilot license - General Navigation