ED Decision 2022/007/R
The aeroplane flight manual (AFM) shall contain the limitations, procedures and other information pertinent to the operation of the automatic landing system and shall include the following appropriate to the use for which the particular system has been certified:
(a) the approved limits established as a result of consideration of the factors listed in CS AWO.A.ALS.106(a) and CS AWO.A.ALS.106(a);
(b) the approved limits established as a result of consideration of any other factor that the certification has shown to be appropriate;
(c) the normal and abnormal procedures, including airspeeds;
(d) the minimum required equipment;
(e) any additional aeroplane performance limitations (see CS AWO.A.ALS.109);
(f) the type of xLS navigation means (facilities external to the aircraft) and associated limitations (if any) which have been used as the basis for certification (see AMC AWO.A.ALS.113(f)); and
(g) runway or airport conditions, including:
(1) runway elevation;
(2) approach path slope;
(3) touchdown zone slope;
(4) ground profile under the approach path.
[Issue: CS-AWO/2]
AMC AWO.A.ALS.113(f) Aeroplane flight manual
ED Decision 2022/007/R
The aeroplane flight manual (AFM) should define the categories of xLS ground facilities, or space facilities (if applicable), which have been used as the basis for certification. The AFM may also contain a statement on the possible usage of automatic landing on lower categories of xLS ground facilities, or space facilities (if applicable).
[Issue: CS-AWO/2]
CS AWO.A.ALS.114 Wind speed limitations
ED Decision 2022/007/R
Wind speed limitations higher than those established in showing compliance with CS AWO.A.ALS.106 may be specified in the AFM for decision heights (DHs) of 60 m (200 ft) or more, provided that:
(a) it can be shown that reliance may be placed on external visual reference for the detection of unsatisfactory performance; and
(b) the wind speed limits without reliance on external visual reference are not less than 46 km/h (25 kt) head, 28 km/h (15 kt) cross, and 18.5 km/h (10 kt) tail.
[Issue: CS-AWO/2]
CS AWO.A.ALS.115 Approach and automatic landing with an inoperative engine
ED Decision 2022/007/R
If compliance with CS AWO.A.ALS.108 Approach and automatic landing with an inoperative engine (see AMC AWO.A.ALS.108) is established, a statement shall be included in the Non-normal Procedures or equivalent section of the AFM that approach and automatic landing made with an engine inoperative have been satisfactorily demonstrated, together with the conditions under which that demonstration was made.
[Issue: CS-AWO/2]