曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

the bearing line where the trailing edges ofthe lead
aircraft’s ventral tins are aligned. At this position,
the trailing edge of the exhaust nozzles should
appear in line to the RIO.
3. Stepdown is determined by allowing approximately
6 inches of the lead’s opposite engine nacelle
to show below the near engine nacelle.
This position should provide the wingman with approximately
12 feet of wingtip separationa nd 12 feeto f
stepdown.
Slot (dash+
1. Line of bearing is determined by lining up on the
lead aircraft’s centerline.
2. Approximately 20 feet of nose-to-tail separation
can be established by placing the wingman’s canopy
bow on the lead aircraft’s exhaust nozzles.
3. Approximately 25 feet of stepdown should be
used. This position may be cross-referencedb y
placing the upper leading edge of dash-2’s ordash-
3’s intake on the pilot’s helmet.
9.2.4 Cruise Formation. Cruise is thebasic formation
used for multiplane transit to or from an operating
area where increased maneuverability is desired.
Wing sweep: 20”
Configuration: Clean.
1. Line ofbearing is determined by placing the upper
leading edge of the lead aircraft’s intake on the
RIO’s canopy bow.
2. A second line of bearing is determined by placing
the lead aircraft’s wingtip light on the forward
upper UHF antenna.
3. Wingtip separation is determined by allowing approximately
1 foot of the lead’s opposite exhaust
nozzle to show behind the near exhaust nozzle.
This position should provide the wingman with approximately
64 feet of wingtip separationa nd 10f eet of
nose-to-tail separation.
9-3 ORIGINAL
NAVAIR 01.Fl4AAD-1
9.2.5 Aircraft Lighting During Night Formation
Flight. The lead aircraft anticollision lights will normally
be off during night formation flight in parade.
However, the possibility exists that the wing aircraft can
inadvertently stray into a position aft of the normal
bearing where only a single white tail light on lead is
visible. In this position, serious misjudgment of separation
and closure.r ate can occur. To prevent this, lead
aircraft anticollision lights should be on when the wing
aircraft is not in normal parade and mission requirements
permit.
9.3 BANNER TOWING
9.3.1 Ground Procedures. The following procedures
are provided for guidance. Local course roles may
dictate modification of these steps:
1. When tower clearance onto the duty runway has
been received, tow aircraft taxis to position as directed
by tow ho&up crew. Tow pilot holds this
position until releasedb y tow hookup crew. Escort
pilot maintains position on taxiway at approach
end of runway.
2. When signaled to do so by tow hookup crew, tow
pilot proceeds to taxi down runway.
3. Upon receipt ofvisual taxi signal from tow hookup
crew to slow down, escort pilot relays this signal
to tow pilot via UHF radio.
4. Upon receipt ofvisual taxi signal from tow hookup
crew to stop, escort pilot relays this signal to tow
pilot via UHF radio.
5. Upon receipt of signal from tow hookup crew that
tow hookup is complete, escort pilot requests tow
pilot to take up slack.
6. TOW pilot proceeds to taxi down the runway.
7. When banner moves forward onto runway, escort
pilot transmits, “Tow aircraft hold, good banner,”
and taxis onto runway abeam banner for takeoff.
8. When ready, tow pilot transmits, “Tower, Lizard
616 for banner takeoff, escort to follow banner.”
9. After banner becomes airborne, escort pilot commences
takeoff roll.
9.3.2 Shipboard Procedures. The following procedures
are provided for guidance. Local rules may dictate
modification of these steps:
1. When clearance has been received, tow aircraft
taxis to the catapult shuttle in use as directed by
flight deck personnel.T ow pilot holds this position
until released by catapult director.
2. When signaled to do so, banner crew lays banner
on flight deck 45 feet starboard of waist catapult
centerline and 10 feet aft of unit horizontal stabi-
Iator, with banner bar perpendicular to the catapult
centerline.
3. Banner crew sequentially positions nylon towline
bundle lengthwise and parallel to catapult track in
position in front of banner. Nylon towline, with
prepared end facing banner buckle, is attached to
banner using swivel and connecting link. Steel cable
leader (75 feet of 3/16-inch diameter) is attached
to forward end of nylon towline bundle
using connecting link.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：F-14D 飛行手冊 Flight Manual 2(45)