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4. Banner crew then utuolIs leader forward, down
angle deck and parallel to catapult track to prevent
entanglement and kinks. The forward end of
leader is brought back and laid on deck near the
aircraft’s right main landing gear. Forward end of
leader has Mk 8 Mod 0 target release ring attached
to it.
5. Upon clearance from catapult officer, banner
crewmember crawls underneath aircraft with
leader in hand just aft of right ventral tin. He then
attaches Mk 8 Mod 0 target release ring to banner
tow adapter. Upon appropriate signals from the
flight deck director, the pilot lowers hook to assure
proper detachment of target release ring and then
raises the hook. The banner crewmember will then
reattach target release ring.
6. After hookup, the banner crewmember exits from
beneath aircraft at same place he entered. He then
walks toward island and gives thumbs up signal to
catapult officer. The banner, towline, and leader
are now ready for launch.
9.3.3 Flight Procedures. Flight tests have demonstrated
no significant degradation of aircraft performancea
nd handling characteristicsw hent owing a banner.
Angle ofbank should be limited to 30” or less
to preclude contact between the tow cable
and afterburner nozzle.
ORIGINAL
Note
Depending on the airspeed of the tow aircraft,
the banner will normally hang 200 to
400 feet below the tow aircraft’s altitude.
Refer to Chapter 4 for banner towing restrictions.
9.3.3.1 Takeoff. Normal takeoffproceduresi.n cluding
rotation speeds and techniques, are suitable for takeoff
with the banner.
Takeoff ground roll with banner can be
estimated by adding a factor of 10 percent
to basic aircraft takeoff performance. If
aircraft lift-off will not occur prior to
crossing the long-field arresting gear, the
gear must be removed to preclude the banner
being tom off.
If the crosswind component is in excess
of 10 knots, the takeoff roll should be
made on the upwind side of the runway to
prevent the banner from striking the runway
lights on the downwind side of the
runway.
Note
Adequatec learancee xists to prevent contact
betweent he tow cable and speedbrakesd uring
ground operation. If takeoff is aborted,
basic emergency procedures are applicable.
The tow cable will be releasedw hen the tailhook
is lowered.
After liftoff, continue rotation to 15’ (maximum of
209, while raising the landing gear. Do not exceed 17
units AOA. Climb out at 180 to 200 KIAS until the flaps
are up, then continue climb at 200 to 220 KIAS.
Note
l Avoid use of afterburner to prevent damage
to tow cable.
l Tow airspeedsin excesso f 220 KIAS will
result in excessive banner fraying.
For shipboard operations, after lift-off, rotate to 15”
(20” maximum) not to exceed 17 units AOA while raising
the gear and flaps. Prior clearance must be received
t?om the tower for an unrestricted climb. Maintain heading
until the banner is well clear of ship. Climb out at
NAVAIR Ol-Fl4AAD-1
180 to 200 KIAS until flaps are up, then continue to
climb out at 200 to 220 KIAS.
Note
The maximum aircraft gross weight for a
shipboard banner launch is 67,000 pounds.
9.3.3.2 Cruise/Pattern. No specialpilottechniques
are required when towing a banner. En route cruising
speedso f 180t o 220 KIAS will provide adequatee nergy
for mild maneuvering while minimizing banner fray If
a low-pattern airspeed is desired, extend flaps/slats if
necessaryt o maintain AOA at or below 12 units. The
tow aircraft must call all turns to allow the chase aircraft
to position itself on the outside of the turn.
If the banner is shot off or falls off in flight, the
remaining cable should be dropped in the gunnery area
or in a confirmed clear area. After the cable is released,
a chase aircraft should join to verify that the cable has
been dropped.
[pi&-I
Without the banner, any remaining cable will
flail unpredictably. The chase should approach
the tow aircraft from abeam, avoiding
a cone-shapeda rea defined by the tow’s 4-
to S-o’clock positions.
9.3.3.3 Descent. Airspeeds of 160 to 220 KIAS
should be used for descent. Flaps and slats may be utilized
to increase the rate of descent as desired.
Speedbrakess hould not be used while towing
since limited clearance exists between
the cable and speedbrakesd uring extension
and retraction in flight.
9.3.3.4 Banner Drop. The tow aircraft should extend
its flaps and reduce airspeed (140 to 160 KIAS, 12
　
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