Abstract: A removable aerial application system and a method of installing the removable aerial application system in an aircraft such as a helicopter. In one embodiment, a removable aerial application system for an aircraft comprises: a tank insertable into a cabin of the aircraft; a first delivery conduit and a second delivery conduit, the first and second delivery conduits being in communication with the tank and extending aftward beneath a fuselage of the aircraft, a first auger within the first delivery conduit and a second auger within the second delivery conduit; a collector assembly defining a chamber, each of the first and second delivery conduits being in communication with the chamber; a distribution system coupled to the collector assembly; and a hydraulic system in mechanical communication with each of the first and second augers.

Abstract: A removable aerial application system and a method of installing the removable aerial application system in an aircraft such as a helicopter. In one embodiment, a removable aerial application system for an aircraft comprises: a tank insertable into a cabin of the aircraft; a first delivery conduit and a second delivery conduit, the first and second delivery conduits being in communication with the tank and extending aftward beneath a fuselage of the aircraft, a first auger within the first delivery conduit and a second auger within the second delivery conduit; a collector assembly defining a chamber, each of the first and second delivery conduits being in communication with the chamber; a distribution system coupled to the collector assembly; and a hydraulic system in mechanical communication with each of the first and second augers.

Abstract: A removable aerial application system and a method of installing the removable aerial application system in an aircraft such as a helicopter. In one embodiment, a removable aerial application system for an aircraft comprises: a tank insertable into a cabin of the aircraft; a first delivery conduit and a second delivery conduit, the first and second delivery conduits being in communication with the tank and extending aftward beneath a fuselage of the aircraft, a first auger within the first delivery conduit and a second auger within the second delivery conduit; a collector assembly defining a chamber, each of the first and second delivery conduits being in communication with the chamber; a distribution system coupled to the collector assembly; and a hydraulic system in mechanical communication with each of the first and second augers.

Abstract: A swing-away rack for mounting a spare tire to a substantially vertical surface of a motor vehicle. A spare tire holder is mounted on a vertical support member which is pivotally mounted on a hinge. The hinge enables the support member and the spare tire to be swung sufficiently downwardly and backwardly to avoid the swinging arc of an adjacent door mounted on the motor vehicle, thus enabling access to the door. A latch maintains the support member in its normal, vertical orientation. The latch comprises a thin resilient bar which is disposed adjacent and parallel to the support member. The latch has an opening which cooperates with a projecting member secured to the vertical support member. When this projecting member penetrates the opening, the support member is constrained against lowering. When the latch is resiliently drawn away from the support member, the projecting member is released from the opening, and the support member may be lowered.