Another DA / DH question?
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Another DA / DH question?
There are several answers to this question from 2011 onwards so fear they are outdated.
Is my understanding correct as of 2015?
1) during a non-precision approach we only use a DA based on baro. The fact that the aircraft, during a go-around, may continue to descend another 50 feet during the transition to climb remains LEGAL. (MDA is no longer to be used)??
2) during an ILS all decisions to go round (at minimums) are based on radio altimeter?? Is baro used during final stages of ILS, other than gross error checks?
Thanks
Is my understanding correct as of 2015?
1) during a non-precision approach we only use a DA based on baro. The fact that the aircraft, during a go-around, may continue to descend another 50 feet during the transition to climb remains LEGAL. (MDA is no longer to be used)??
2) during an ILS all decisions to go round (at minimums) are based on radio altimeter?? Is baro used during final stages of ILS, other than gross error checks?
Thanks
If you're referring to NPAs flown using the CDFA technique, then an allowance must be included when calculating a DA from the published MDA.
If an NPA is flown using a notional GS, but without the CDFA technique, then it will invariably be above the GS at MDA as power must be applied to level at MDA.
However, if an NPA is flown using a free-descent technique at the maximum descent gradient assumed by procedure design (where permitted), then the aircraft can be levelled at MDA until either landing criteria are achieved or the MAP is reached.
So for large CAT aircraft, the CDFA technique is now normal SOP, as it then means that only one basic SOP is required for non-LVP ops. Whereas for light GA aircraft, either the notional GS or the free-descent technique to MDA may well be preferable.
Those who use the stupid term 'duck and drive' probably have no idea that the maximum free-descent gradient assumed by procedure design is only 25% steeper than the normal notional GS....
If an NPA is flown using a notional GS, but without the CDFA technique, then it will invariably be above the GS at MDA as power must be applied to level at MDA.
However, if an NPA is flown using a free-descent technique at the maximum descent gradient assumed by procedure design (where permitted), then the aircraft can be levelled at MDA until either landing criteria are achieved or the MAP is reached.
So for large CAT aircraft, the CDFA technique is now normal SOP, as it then means that only one basic SOP is required for non-LVP ops. Whereas for light GA aircraft, either the notional GS or the free-descent technique to MDA may well be preferable.
Those who use the stupid term 'duck and drive' probably have no idea that the maximum free-descent gradient assumed by procedure design is only 25% steeper than the normal notional GS....
Last edited by BEagle; 30th Mar 2015 at 16:57.