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x vessel. points to eye, then to vessel or executes.
object.
defers to landing of aircraft, Landing motion with open hand: Execute.
generally used in conjunction with 1. Pats head. Alternate signal - Lower gear.
mother signal: 2. Points to another aircraft.
I. I am landing
2. Directs indicated aircraft to land.
I. Join up or break up, as Flashing external lights. 1. Comply.
appropriate 2. Wingman continues approach in
!. On GCA/CCA final: Leader has accordance with standard
runway/ship in sight. operating procedures.
Mngman cross under. Leader raises forearm vertically. Execute.
Section cross under. Leader raises forearm vertically Execute.
and moves arm in pumping
motion.
3efers to CV Case l/Case II
Jattern:
1. Spin whole flight.
!. Indicated aircraft spin.
MR REFUELING
1. Leader gives a two finger turnup 1. Execute
signal. 2. Counting from last aircraft in
2. Turnup signal followed by flight specified number of
number of aircraft to spin. aircraft execute spin.
Extend Drogue Form cone-shape with hand, and Tanker execute.
move hand aft.
RetracDt rogue Form cone-shape with hand, and Tanker execute.
move hand forward.
Secure Turbine One finger turn-up signal followed Tanker execute.
by cut signal.
Figure1 9-14.I n-FlightC ommunication(Ss hee3t of 4)
19-29 ORIGINAL
NAVAIR 0%FUAAD-1
~OORMATION SIGNALS MADE By AIRCRAFT MANEUVER (COMBAT OR FREE CRUISE)
iingle aircraft cross under in Single wing dip Execute.
,irection of wing dip.
;ection cross under. Double wing dip Execute.
:lose up. Series of small zooms Execute.
oin up: join up on me. Porpoise aircraft Expediiejoin-up.
Figure 19-14. In-Flight Communications (Sheet 4 of 4)
ORIGINAL 19-30
NAVAIR Ol-Fl4AAD-1
WING SWEEP 20’
ARIAS IN HU66lN6 POSlllON
ACROSSIH C CHCSTT.H ENS WEPT
OUT IO SIDES, ARMS WELD
SlllAlSll~Jl. _
OVERSWEEP
ARMS. fROM SYRAIGNY OUT
SWEM IN ACROSS RE CHEST
HU66lNE THE SNOULOERS
3 x
DLC CHECK/ LOWER SPOILER
RAISE SPOILERS ARMS EXIENREO HORKONTAL
AOMS CXKNOLD H06lZ0NlAt IIIRECILV AHEAD WAH PALMS
ANDO lllEClll ANEA6N. ANOSP OP SHOWINGD. ROP PALMS FROM
UP FROMW RISTT O SHOWP ALMS. WRIST.
3 a 3 &
WING SWEEP SO’
ARMSF 6OMS TRIIGHOT UTS WEPl
NAli WAY DOWN TO SIOE.
BACKUP MODULE CHECK/
FLIGHT CONTROLS
CYCLE CHECK
PILOT ROTATESC LENCNEOFI ST
IN A HORKONTAPLt ANE.S l6NAt.
MAN REPEATS SIPNAL If ALL
CONIROL SURfACES ARE CtLAR
Of PERSONNEL/EO!4lPMENT.
Nl6HY SIGNALSA RE THE SAME AS 011 Sl6NAtS UCEPY A6 NOTEDf.t ASHLl6HYSO R WANDS
WILL SURSVlYlJYFEO RN ANDA N6 FlN6ERM OVEMENTOSU RIN Nl6Hl OPERATIONS.
CARRIER RIGHTDECK PERSONNELCOLOR CODING
REDW IRTS- ORONANCaEn d CRASNC REW
YELLOW SHIRTS- PRIF LY,P UNt OIRECYORCSA. TAPULT
OFfICERmdA RRESYMENOYF FICER
BLUE SHIRVS- PtANE HANDLERS
mhsn. chock AJonN, C.)
PURPLES WRYS- FUELH ANWIN
GREEN SPRYS- AIRCRAFMI ANITENANCE,
CATAPULCTR EW,ANO
ARlKSYHENl CREW
BROWN WIRTS- PUNE CAPTAINS
WHlYE SHIRTS- MEOICALS, AFETY,
VROU6tESHOOTERS.
AN0 LSO
Figure 19-15. Deck/Ground Handling Signals
W-31 (Reverse Blank) ORIGINAL

NAVAIR 01.F14AAP1
CHAPTER 20
Navigation System
20.1 NAVIGATION SYSTEM
The navigation system (Figure 20- 1) combines inputs
from various on-board sensors with inputs entered by
the crew and provides the following outputs of aircraft
position: velocity, attitude, heading, accelerations, and
angular rates. This information is displayed to the crew
and also used by the weapons system and other aircrag
functions. The system also provides steeringandcontrol
commands for display to the crew as required.
‘Ihe ANIASN-139 inertial navigation set is the primary
navigation sensor. It provides inertial information
to the MCS via a standardd ata bus. As a backup to the
INS, the AN/USN-2(V) SAHRS can provide similar,
but somewhat degraded inertial information. Selection
of SAHRS data is either automatic on failure of the INS
or by operator selection. The MCS processes inertial
data along with information from other navigation aids
to provide smoothed and optimized outputs for display
or for use by other aircraft systems and functions.
The ANAJRC-107 ITIDS provides navigation correction
data for use in updating the navigation system
and velocity data for aligning the INS in flight. When
installed, the JTIDS receiver/transmitter replaces the
AN/ARN-118 tacan. With JTIDS installed, the CIU is
not used to convert the tacan data to a 1553 format; the
　
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