The NG 'slippery runway' figures do assume max reverse thrust, ...Boeing Landing Distance Advisory Data in the QRH includes reversers for Manual and Autobrakes. This statement is made on the last slide of the Boeing presentation Airplane Deceleration on Slippery Runways – What You Should Know. (http://uk.geocities.com/
[email protected]/alf5071h.htm)
This is an extremely valuable presentation explaining the peculiarities of the Boeing landing distance data.
The presentation must be read very carefully – two different uses of Mu, Certified (factored) data vs Advisory (unfactored) data, each obtained in different ways (slides 9-11). Take care with the use engineering language relating to deceleration capability (a 'value' which pilots are not aware of).
Of particular interest, note the interchange of deceleration capability between reverse and autobrake, such that in certain low friction conditions braking could be reduced as reverse meets the need for the demanded (autobrake) retardation, yet in similar conditions, brakes and reverse may not be sufficient to meet the required deceleration at all (slides 28-30).
A conclusion as a non 737 operator could be that autobrake should not be used on contaminated runways; this is hidden in the small print in the advisory data on slides 12–13 (FAA 737 FCOM).
Thus it would also appear prudent to hold thrust reverse in reserve for any misjudgment of conditions or miscalculation of the scheduled landing distance (possible contributing factors in recent accidents).
Another consideration could be that whilst JAR/CS 25.125 appears to allow the use of reverse it has to be reliable (the difference between models), perhaps an issue arising from the Midway accident; thus the NG comes into line with older variants.
CS 25.125
(3) Means other than wheel brakes may be used if that means –
(i) Is safe and reliable;
(ii) Is used so that consistent results can be expected in service; and
(iii) Is such that exceptional skill is not required to control the aeroplane.
(f) If any device is used that depends on the operation of any engine, and if the landing distance would be noticeably increased when a landing is made with that engine inoperative, the landing distance must be determined with that engine inoperative unless the use of compensating means will result in a landing distance not more than that with each engine operating.
Overall, any change that improves safety in landing operations should be welcome – just review the large number of incidents and accidents reported this year.