General Navigation - Quiz ATPL - Airline Transport Pilot license

The principle of 'Schuler Tuning' as applied to the operation of Inertial Navigation Systems/ Inertial Reference Systems is applicable to:	4 Answers
What additional information is required to be input to an Inertial Navigation System (INS) in order to obtain an W/V readout?	4 Answers
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

General Navigation - ATPL - Airline Transport Pilot license