MOC VTOL.2270(a) and (c) Emergency landing conditions: General considerations

• n/a found in: Small Category VCA (Revision 0) SC-VTOL (Oct 2024)

MOC VTOL.2270(a) and (c) Emergency landing conditions: General considerations n/a This MOC provides a set of general design conditions that, when used in their entirety, are accepted to ensure adequate protection of occupants against injuries that would prevent egress in an emergency landing. (a) CS 27.561(a) Amdt. 6 is accepted as a means of compliance. (b) CS 27.561(b) Amdt. 6 is accepted as a means of compliance with the addition under subparagraph (3)(ii) of a 18 g ultimate inertial load factor in the forward direction for CTOL aircraft. (c) CS 27.561(c) Amdt. 6 is accepted as a means of compliance replacing “rotors, transmissions and engines” by “lift/thrust units, transmissions and energy storage systems”. (d) CS 27.561(d) Amdt. 6 is accepted as a means of compliance replacing “fuel tanks” by “energy storage systems”. (e) For CTOL, CS 23.561(d) Amdt. 4 is accepted as a means of compliance.