A rotorcraft including a safety apparatus (120a, 120b, 130, 140, 160a, 160b, 170, 180, 190, 200, 210, 220, 230, 240) 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 (178, 188, 224) between one or more engines (152a, 152b) 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 (152a, 152b) 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 (178, 188, 224) between one or more engines (152a, 152b) 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 (152a, 152b) 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 (178, 188, 224) between one or more engines (152a, 152b) 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 (152a, 152b) or to a yoke of the rotorcraft.