The height at which approach is aborted when the runway is not in sight is called as?(a) Decision height(b) Approach altitude(c) Clearance altitude(d) Landing altitudeThis question was addressed to me by my school teacher while I was bunking the class.I'd like to ask this question from Phases of Flight topic in section Introduction & Navigation Equations of Avionics

The height at which approach is aborted when the runway is not in sigh

1.	The height at which approach is aborted when the runway is not in sight is called as?(a) Decision height(b) Approach altitude(c) Clearance altitude(d) Landing altitudeThis question was addressed to me by my school teacher while I was bunking the class.I'd like to ask this question from Phases of Flight topic in section Introduction & Navigation Equations of Avionics
Answer» The correct choice is (a) DECISION HEIGHT Easiest explanation: Decision altitude is the altitude above the runway at which the APPROACH must be aborted if the runway is not sight. Decision height PUBLISHED for each runway at each airport.

Discussion

No Comment Found

Related InterviewSolutions

What is TDOP?(a) Time Dilution of pseudorange(b) Time Dilution of position(c) Time Dilution of pressure(d) Time Distortion of positionThis question was posed to me by my school principal while I was bunking the class.This intriguing question comes from Navigation Equations topic in chapter Introduction & Navigation Equations of Avionics
________ related ranging errors to the dispersion in measured position?(a) GEOP(b) GDCP(c) GDOP(d) APEGI have been asked this question during an online interview.I'd like to ask this question from Navigation Equations in division Introduction & Navigation Equations of Avionics
The angle of arrival, relative to the airframe, of a radio signal from an external transmitter is called _________(a) Bearing(b) Heading(c) Phase(d) Approach angleI had been asked this question during an online exam.Question is taken from Navigation Equations in chapter Introduction & Navigation Equations of Avionics
What is the technique of calculating position from measurements of velocity called?(a) Dead reckoning(b) Doppler radar(c) Secondary surveillance(d) Celestial navigationThe question was posed to me in class test.The origin of the question is Navigation Equations topic in portion Introduction & Navigation Equations of Avionics
Geocentric spherical coordinates are used for short range dead reckoning navigation.(a) True(b) FalseI have been asked this question during an interview for a job.Question is taken from Navigation Equations in section Introduction & Navigation Equations of Avionics
Which coordinate system is used in satellite based radio navigation?(a) Earth centered, Earth fixed(b) Earth centered inertial(c) Geodetic spherical coordinates(d) Geodetic wander azimuthI had been asked this question in an interview for job.This interesting question is from Navigation Equations topic in chapter Introduction & Navigation Equations of Avionics
Which of the following is false with respect to Earth centered inertial coordinate system?(a) Accuracy is 10^-5/hr(b) Newton’s laws are not valid(c) Angular coordinates of stars are conventionally tabulated in ECI(d) Used in mechanizing inertial navigatorsI got this question during an online interview.This intriguing question comes from Navigation Equations in division Introduction & Navigation Equations of Avionics
Which one of the following is not an input utilized by the aircraft navigation system?(a) Sonar(b) Radio aids(c) Dead reckoning data(d) Celestial measurementsI have been asked this question by my school teacher while I was bunking the class.The origin of the question is Navigation Equations in chapter Introduction & Navigation Equations of Avionics
What is the angle between the normal to the reference ellipsoid and the equatorial plane at a point called?(a) Geodetic angle(b) Correction factor(c) Geodetic latitude(d) Earth angleI have been asked this question by my school teacher while I was bunking the class.The doubt is from Navigation Equations topic in section Introduction & Navigation Equations of Avionics
The navigation equations are used by the on-board computer to calculate position velocity and altitude.(a) True(b) FalseI have been asked this question in quiz.This key question is from Navigation Equations in portion Introduction & Navigation Equations of Avionics

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment