12.106.2(b) datum;
Status : - -
12.106.2(c) moment (including units used);
Status : - -
12.106.2(d) centre of gravity (C of G);
Status : - -
12.106.2(e) longitudinal C of G range and associated limits;
Status : - -
12.106.2(f) station;
Status : - -
12.106.2(g) basic aircraft empty weight (standard empty weight);
Status : - -
12.106.2(h) zero fuel weight (ZFW);
Status : - -
12.106.2(i) gross weight (AUW);
Status : - -
12.106.2(j) maximum certified take-off weight (MCTOW).
Status : - -
* * * Weight and Loading * * *
Status : - -
12.108 Weight and Loading
Status : - -
12.108.2 Given a basic aircraft load sheet/data, demonstrate the ability to:
Status : - -
12.108.2(a) calculate the C of G position;
Status : - -
12.108.2(b) use a typical loading graph to determine C of G position;
Status : - -
12.108.2(c) use index units.
Status : - -
* * * Centre of Gravity (C of G) * * *
Status : - -
12.110 Centre of Gravity (C of G)
Status : - -
12.110.2 State the reasons for operating an aircraft within the C of G limits.
Status : - -
12.110.4 State the effect on the stability and control of an aircraft if flown with the C of Gat the:
Status : - -
12.110.4(b) aft limit.
Status : - -
12.110.4(a) forward limit;
Status : - -