EXTRACTION LINE PANEL 0001 00
NOMENCLATURE CROSS-REFERENCE LIST.
Extraction Line Bag Stow Loop
Extraction Line Panel Tie Strap
Bridle Attaching Loop or Bag Closing Loop
Reinforcement Strap Loop
Section II. EQUIPMENT DESCRIPTION AND DATE
EQUIPMENT CHARACTERISTICS. Universal panel that stows extraction lines and suspension
slings for deployment. One or two panels are required depending upon their application.
CAPABILITIES AND FEATURES
a. Accommodates extraction line and suspension slings.
c. Used with all approved extraction line for C-130, C-141, C-5 and C-17 Aircraft.
d. Various applications.
(1) One panel (half bag) when stowed for low velocity airdrops.
(2) Two panels (full bag) when stowed for low velocity airdrops.
LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (figure 2).
BODY (1). Forms the panel body and is constructed of nylon duck cloth. Strap and closing loops are
stitched to it.
REINFORCEMENT STRAP (2). Three reinforcement straps are used. One is located in the center
and outside on the body, and one each is located 3 ½-inches from each side, on the outside of the
TIE STRAP (3). Three tie straps are used. One is located in the center and inside of the body, and
one each is located 3 ½-inches from each side, on the inside of the body.
STRAP HANDLE (4). Four strap handles are used to carry the panel. Two are located at each side,
on the outside of the body 3 ½-inches from each end.
CLOSING STRAP (5). Two closing straps are used, one at each end of the body on the outside.
CLOSING LOOP (6). Six closing loops are used. Three are located at each side on the outside of the
body. One on each side is located 3 ½-inches from the forward end. One on each side is located 20
½-inches from either end. One on each side is located 4-inches from the aft end.