(SAL) 25.6 Aeroplane Flight Manual
ED Decision 2013/010/R
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]
For steep approach landings, the Aeroplane Flight Manual must include landing distance data, weight/altitude/temperature limits, and specific procedures. It should state limitations, including one-engine-inoperative approach restrictions, and clarify that performance data doesn't constitute operational approval. Headwind/crosswind limits, glide slope angle, screen height, and height loss during go-around must also be provided.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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