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hose and drogue without causing further damage than to
make another approach. If the initial approach position
is correctly in line with the drogue, the chance of hooking
the hose is diminished as the need for last-minute
corrections is minimized. After executing a missed approach,
analyze previous misalignment problems and
apply positive correctionst o preclude a hazardoust endency
to blindly stab at the drogue.
9.1.3.3 Contact. When the receiver probe engages
the basket, it will seat itself into the drogue coupling and
a slight ripple will be evident in the refueling hose. The
tanker’s drogue and hose must be pushed forward 3 to 5
feet by the receiver probe before fuel transfer can be
ORIGINAL 9-2
effected. This advanced position is evident by the tanker’s
amber ready light going out and the green fuel transfer
light coming on. While plugged in, merely fly a close
tail-chase formation on the tanker. Although this tuckedin
condition restricts the tanker’s maneuverability, gradual
changesin volving heading,a ltitude, antior airspeed
may be made. The precise flying imposed on both the
tanker and receiver pilots requires a lot of“heads down”
time, yet a sharp lookout doctrine must be maintained.
This is the receiver RIO’s primary responsibility.
9.1.3.4 Disengagement. Disengagement from a
successful contact is accomplished by reducing power
and backing out at a 3- to S-knot separation rate. Care
should be taken to maintain the same relative alignment
on the tanker as upon engagement.T he receiver probe
will separate from the drogue coupling when the hose
reaches full extension.
When clear of the drogue:
1. REFUEL PROBE switch - RET.
2. Probe transition light - Check Out.
3. AIR SOURCE pushbutton - BOTH ENG.
4. Wing-sweep switch - AUTO.
Resume normal flight operations.
9.2 FORMATION FLIGHT
The following formation descriptions are recommended
guidelines for F-14 multiplane positioning.
pii-1
Parade formation IFR/VFR and loose cruise
flight shall not be performed with the flight
lead utilizing autopilot ground-track destination
steering because of the midair collision
potential associated with inadvertent waypoint
steering selection and rapid aircraft
AOB changes.
9.2.1 Parade Formation. The basic parade position
is either left or right echelon, or a combination of
both, as in fingertip three-plane formation. The parade
formation is used primarily for multiplane maneuvering
at night, in IMC, or during entry into or exit from an
airport traffic area.
Wing sweep: 20”
Configuration: Clean or dirty.
1. Line ofbearing is determined by placing the upper
leading edge of the lead aircraft’s intake on the
explosive seat warning triangle below the RIO
cockpit.
2. Wingtip separation is determined by a position on
the bearing line where the leading edges ofthe lead
aircraft’s ventral tins are aligned.
3. Stepdown is determined by aligning the lead’s opposite
engine nacelle just under the near engine
nacelle.
This positioning should provide the wingman with
approximately 5 feet of wingtip separation and 10 feet
of stepdown.
9.2.2 Break Formation. The basic break formation
is either left or right echelon, or a combination of both
as in a fingertip three-plane formation. This formation
is used primarily for multiplane entry into the overhead
break pattern.
Wing sweep: 68”
Configuration: Clean.
1. Line ofbearing is determinedby placing the upper
leading edge of the lead aircraft’s intake on the
explosive seat warning triangle below the RIO
cockpit.
2. Wingtip separation is determined by a position on
the bearing line where approximately 1 foot of the
forward edge of the lead’s opposite ventral tin
shows in front of the near ventral tin.
3. Stepdown is determined by aligning the lead’s opposite
engine nacelle just under the near engine
nacelle.
This position should provide the wingman with approximately
15 feet ofwingtip separation and 10 feet of
stepdown.
9.2.3 Diamond Four-Plane Formation. The diamond
is the basic four-plane formation used for entry
into the overhead break or for aerial fly-bys.
Wing sweep: 68’
Configuration: Clean.
Right and left echelon (dash-2 and dash-3, respectively)
NAVAIR 0%F14AAD-1
1. Line ofbearing is determined by placing the upper
leading edge of the lead aircratt’s intake on the
pilot’s helmet.
2. Wingtip separationis determinedb y a position on
　
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