F-14D 飞行手册 Flight Manual 2(141)

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canopy releases.
Try to determine the direction of the wind at the
surface using white caps, smoke from the wreckage, or
known surface winds in the vicinity. Nom that surface
winds may be quite different from those at altitude.
When nearing the surface, steer into the wind and assume
the proper body position for landing:
1. Feet together, knees slightly bent, toes pointed
slightly downward.
2. Eyes on the horizon.
3. Grasp canopy risers and tuck elbows in prior to
water entry.
NAVAIR Ol-Fl4MD-1
4. On water entry, release the canopy manually. The the end of the lanyard securely to the gated helo hoist
SEWARS releasesw ill operatet he canopyr elease ring on the harness,t hen ensuret hat the oxygen hose is
fittings on saltwater entry as a backup. disconnected from the kit lid and release the laphelt
16.3.6 Raft Boarding
quick-releasefi ttings, releasingt he kit lid. Bring the raft
around for entry from the small end (stem); grasp the
Note
stem, and forcibly push under LPA waist lobes. Using
the boarding handles, pull into the raft and turn into a
l If the life& has not inflated automat- comfortable, balanced, seated position. Locate the
ically, pull on the red operatingh andleo n dropline and retrieve the survival package.
the dropline to inflate.
l If the survival package has not been deployed
before water entry, first pull the
yellow deployment handle then the red
operating handle. Do not attempt to retrieve the kit lid. Any
attempt to do so could capsize the raft.
When clear ofthe canopy, retrieve the rat? by locating
the dropline and pulling the raft to you. The raft retaining Close the canopy and orally inflate the canopy and
lanyard is in a pocket next to the CO2 cylinder. Attach floor. An integral baler is provided to bale the raft as
necessary.
16-9 (Reverse Blank)

NAVAIR 0%F14AAD-1
PART VI
All-Weather Operations
chapter 17 - Instnlment Procedures
Chapter IS-Extreme Weather
85 (ReverseB lat& ORIGINAL

NAVAIR Ol-F14AAD-1
CHAPTER 17
Instrument Procedures
17.1 AUTOMATIC CARRIER LANDING
SYSTEM
ACLS approachesa pply to properly configured aircraft
utilizing carrier or shore-based AN/SPN-10 or
AN/SPN-42 ACLS radar facilities. Three primary
modes of operation and two submodes are available.
1. Mode I approach automatically controlled to
touchdown
2. Mode IA approach automatically controlled to a
minimum of 200 feet and one-half mile; manual
control remainder of approach
3. Mode II approach manually controlled using
ANBPN-41 or AN/SPN-42 vertical display indicator
and/or heads-up display presentation for
glideslope and lineup information
4. Mode III approach manually controlled using
only CCA-controller-supplied information
5. Flight director approach manually controlled using
HUD flight director presentation derived from
AN/SPN42/46 information and navigation system
data for glidepath intercept and following.
17.1.1 Mode I. Mode 1 provides a fully automatic,
hands-off landing capability, called automatic carrier
landing or all-weather landing. The landing radar system
(AlVSPN-42) tracks the aircraft and compares its
position with the desired position. The aircraft position
is corrected to fly the desired glidepath by commands
t?om the naval tactical data system using the radar computer.
These commands are transmitted over the UHP
data link to the aircraft, where the automatic flight control
systeme xecutest he pitch and bank commands. Additional
ramp input commands tailored to each specific
ship or field are applied at the proper time to assist the
aircraft through the burble. In addition to control of the
aircraft, discrete words and glideslope error signals are
transmitted for cockpit displays to show the pilot where
his aircraft is in relation to the desired glideslope. Independent
glideslope error signals from the AlWSPN-41
instrument landing system may also be displayed. The
pilot may take control at any time and continue the
landing via Mode II.
17.12 Mode II. The control of the aircraft remains
with the pilot along the entire glideslope to touchdown.
Glideslope error signals are transmitted to the aircraft
for cockpit displays from the ANBPN-41 or the
AN/SPN-42. The pilot flies the aircmtl to null the error
and to keep the vertical and lateral crosshairs centered.
During a Mode II T approach, the final controller provides
a Mode III-type talkdown to assist the pilot in
flying his needles or for controller tmining.
17.1.3 Mode Ill. The pilot flies the aircraft in response
　
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