Components. Locations and descriptions of major
components are as follows (figure 1-2):
CARRYING CASE (1). Holds the rope, rope snaphook
and governor assembly. Is provided with a hook and
pile press-fit waist loop and leg strap.
GOVERNOR ASSEMBLY (2). Consists of the governor,
Constructed of aluminum. ' Has five cylindrical rungs.
PERSONNEL HARNESS (3). Made from nylon
webbing. Fits around wearers waist and legs. Primarily
used In self-lowering.
ROPE (4). Made from double braided nylon 150 ft long
and 3/8 In diameter. Feeds from carrying case.
ROPE SNAPHOOK (5). Constructed of steel. Provides
attachment to either cargo or aircraft anchor point.
AIRCRAFT FLOOR ANCHORING DEVICE TIEDOWN
ASSEMBLY (6). Consists of a main web loop with six
snap fasteners. Between the snap fasteners are six D-