continually monitor this circuit to receive any messages from aircraft
out of VHF range and pas necessary messages to the aircraft. The 'F
air -to~zround circuit may e used by the Senior Controller for coordination or by the Controller on scope five if the sammler element (CASSIDY
excee’s VHF range). Positions one and six will be received from the A0C
and positions two through five will be given to the AOC. Positions will
be viven using the aircraft call sign, position and tise aircraft reaches
the position (PENTER 1 position two at zero six one. five), The operator
receivinz the positions from the AOC will write the positon information
on a slip of paper and zive it to the Status Controller (P:"'TER 1 nosition
tuo at zero six one five). The Status Controller will provide the monitor teller with the same information for positions to be told to the AOC,
PLOTTER NUMBER ONE:
Plotter Number One will receive positions on
‘PEWTER 1, 2 and 3, HARDTI@ 1, and VIKING aircraft from teller for scopes
two, three and seven, The Teller will vive aircraft call sizn, »earing
and range, (PEUTER 1, zero nine zero at forty). Arrows will be used to
plot the position of aircraft with the point of the arrow designating the
position of aircraft. Aircraft arriving and departing miscion nositions
will have three arrows showing flight path._ Upon plottinz fourth arrow,
number 1 will %e removed. ( “08.2 “17.3 7-4 >) Aircraft upon reaching assimmed mission position will be plotted wit" only one arrow, the
last plotted position. The time will be placed by each arrow in minutes.
The teller will normally give a position on each aircraft each three
minutes, although in case an aircraft is in an emergency, a nosition and
time will be plotted each minute. Aircraft in emergency will take prior4
ity over other aircraft plots to insure constant plotting vith three
arrovs to depict aircraft heading and positioh. After H-hour, the communications of Teller #1 will be used by Teller at scone six *o provide
.plots on TIGER aircraft, from position two until taken over by the Con-~
trolier on scope five anproaching nositions three and on TIGSR aircraft
released by scope five to scone six after departing vosition four for
position five.
PLOTIOR NUMER TWO: Plotter Number Two will receive positions on
ELATNE 1, ELATNE 2, CASSIDY, STABLE, WILSON and TIGER from Teller on
scopes four (4), five (5) and six (6), The Teller will give aircraft
call sign, bearing and range (ELAINE 2, 180 at 10), arrows will be
used to plot the position of aircraft with the point of the arro designating the position of aircraft. aircraft arriviny and departing
mission position will have three arrovs showing flight path and upon
plotting the fourth, arrow number one (1) will be removed. ( = be? a7 >
- $43).
Aircraft upon reaching miasion station will be plotted leaving
only one (1) arrow. The last plotted position. The time vill *e
placed by each arrow in minu’es. The Teller will normall~ give a nosition on each aircraft each three minutes. In case of an aircraft emergency, a position and tite will be nlotted each minute. Aircraft in
emergency will take priority over other aircraft plots to insure cons-
tant plotting with three arrows to depict aircraft heading position
and time.
EFFECTS STATUS CLERK: The Effects Status Cler: will enter the time
eaca aircraft reacies positions one through six ‘n the appropriate srace
as received from the status controller and tellers over his direct circuit.
The Teller will state aircraft call sim, position and tine (PS/TER 2
position one 0705).
The onl~ entry made by the Status Clerk will be the
time in the a propriate position onposite aircraft call] sign.
Positions
- one and six will be told to the Effects S-atus Clerk by the Status Suner-
visor, Positions two through five for PEWTER One, Two and Three, HARD-~
TI:iz, and VIKING aircraft will be received from the Teller for scones Two,
Three and Seven, The Teller on scopes Four and Six will give position ™
Two through Five for ELAINE One and Two respectively.
TASK GROUP 7.4
OPRS ORDGR NO. 1-54
ANNEX T, APNDX 2
T2-2