(SAL) 25.6 Aeroplane Flight Manual

For steep approach landing, the AFM shall include the following:

(a)The steep approach landing distance determined in accordance with paragraph (SAL) 25.3 of this Appendix for the selected screen height and aeroplane configuration. The landing distance data may additionally include correction factors for runway slope and temperature other than standard, within the operational limits of the aeroplane, and may provide the required landing field length including the appropriate factors for operational variations prescribed in the relevant operating regulation.

(b)The more limiting of the landing weight, altitude and temperature (WAT) limits derived in accordance with:

(1)CS 25.119, and

(2)The one-engine-inoperative approach climb requirement of paragraph (SAL) 25.4 of this Appendix.

(c)Appropriate limitations and detailed normal, non-normal, and emergency procedures. Where an aeroplane is not approved for deliberate one-engine-inoperative steep approach landings, this limitation shall be stated.

(d)A statement that the presentation of the steep approach limitations, procedures, and performance reflects the capability of the aeroplane to perform steep approach landings but that it does not constitute operational approval.

(e)A statement of headwind and crosswind limitations if they are different from those for non-steep approaches. The tailwind limitation is 5 knots unless test evidence shows that more than 5 knots is acceptable.

(f)The reference steep approach glide slope angle and the screen height used for determination of the landing distance.

(g)The height loss during a go-around from the all-engines-operating steep landing approach to the approach climb configuration with one engine made inoperative, determined in accordance with (SAL) 25.5(g).

[Amdt No: 25/13]