A rotorcraft including a safety apparatus comprising: at least one detachable safety bar, fastener, or loop that is attached to the rotorcraft in an area or surface between a windshield of the rotorcraft and a tail boom of the rotorcraft and is connectable to a user safety device to provide fall protection from the area or surface, wherein: the at least one detachable safety bar is attached to one or more sides of the rotorcraft at hard points (176a-c; 184; 186a-c; 248a-c) that are within or outside a body of the rotorcraft , and wherein the at least one detachable safety bar is at least one of vertical, horizontal, or diagonal orientation to the ground and provides an anchor point for a user safety device, or the at least one detachable safety bar or loop is attached on a grip or a flapping stop of a main rotor of the rotorcraft , or within or about a firewall between one or more engines and the rotorcraft , or the at least one detachable safety bar, fastener, or loop is attached to a rotor, or the at least one detachable safety bar, fastener, or loop is attached to one or more hard points (176a-c; 184; 186a-c; 248a-c) on the one or more engines or to a yoke of the rotorcraft . at least one detachable safety bar, fastener, or loop that is attached to the rotorcraft in an area or surface between a windshield of the rotorcraft and a tail boom of the rotorcraft and is connectable to a user safety device to provide fall protection from the area or surface, wherein: the at least one detachable safety bar is attached to one or more sides of the rotorcraft at hard points (176a-c; 184; 186a-c; 248a-c) that are within or outside a body of the rotorcraft , and wherein the at least one detachable safety bar is at least one of vertical, horizontal, or diagonal orientation to the ground and provides an anchor point for a user safety device, or the at least one detachable safety bar or loop is attached on a grip or a flapping stop of a main rotor of the rotorcraft , or within or about a firewall between one or more engines and the rotorcraft , or the at least one detachable safety bar, fastener, or loop is attached to a rotor, or the at least one detachable safety bar, fastener, or loop is attached to one or more hard points (176a-c; 184; 186a-c; 248a-c) on the one or more engines or to a yoke of the rotorcraft . the at least one detachable safety bar is attached to one or more sides of the rotorcraft at hard points (176a-c; 184; 186a-c; 248a-c) that are within or outside a body of the rotorcraft , and wherein the at least one detachable safety bar is at least one of vertical, horizontal, or diagonal orientation to the ground and provides an anchor point for a user safety device, or the at least one detachable safety bar or loop is attached on a grip or a flapping stop of a main rotor of the rotorcraft , or within or about a firewall between one or more engines and the rotorcraft , or the at least one detachable safety bar, fastener, or loop is attached to a rotor, or the at least one detachable safety bar, fastener, or loop is attached to one or more hard points (176a-c; 184; 186a-c; 248a-c) on the one or more engines or to a yoke of the rotorcraft . <EOS>