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F LW Forwa rd Loo ki ng Wi n ds h ear Radar
F M Freque ncy Modula t ion
F M A Fl ight Mode An nunc ia tor
F M C ( 1 ) Fl ight Director Con trol (FD)
( 2 ) Fl ight Ma n age ment Com p u ter (FMC S )
F M C F Fl ight Ma n age ment Com p u ter Funct ion
F M C S Fl ight Ma n age ment Com p u ter Syste m
F M C W Freque nc y - Modula ted Con t i nu o us Wave
F M E A Fa i l u re Mode and Effects An a lys i s
F M F Fl ight Ma n age ment Funct ion
F M P Fl ight Mode Pa n e l
F M S Fl ight Ma n age ment Syste m
F M U Fuel Me teri ng Un i t
F / O ( 1 ) Fi r st Officer
( 2 ) Fuel/Oil Cooler
F O C ( 1 ) Fuel/Oil Cooler
( 2 ) Full Opera t ional Capa bi l i ty
F O G Fi ber Optic Gyro
F O Q A Fl ight Opera t ions Quality Ass u ra nce
F PA ( 1 ) Fl ight Pa th Ang le
( 2 ) Focal Plane Array
FPAC Fl ight Pa th Acce lera t ion
FP C Fl ight Profi le Com pa ra tor
FP G A Fie ld Progra m m a ble Ga te Array
FP M Feet Per Minu te
F P V Fl ight Pa th Vector
F Q I S Fuel Quantity In dic a t i ng Syste m
F Q P U Fuel Quantity Processor Un i t
4 0
4 3
G GT F M G ro un d - G ro und Traffic Flow Ma n age me n t
G G R G ro un d - G ro und Ro u ter
G G S G lo bal Pos i t ion i ng System Gro und Sta t ion
G H G ro und Ha n dl i ng
G H z G igah ertz (bi l l ion hertz )
G I G roup Id e n t i fier
G I B GN SS In tegri ty Broa d c a st
G I C GN SS In tegri ty Channel
G I C B G ro un d - In i t ia ted Com m - B
G I G O Ga r bage - In Ga r bage - O u t
G I H O G ro und In i t ia ted Ha n d off
G L ( 1 ) G ro und Loc a t ion (ACA RS / AFE PS )
( 2 ) G roup Le ng th
G l i d e p a t h The approach pa th used by an airc raft du ri ng an
i n strument la n di ng or the port ion of the glid es lo pe
that inter sects the loc a l izer.The glid e pa th does not
provide guid a nce com ple te ly to a to uch d own point
on the runway.
G l i d e s l o p e The vert ical guid a nce port ion of an ILS syste m .
GLN S G PS Landi ng and Naviga t ion Syste m
GLN U G PS Landi ng and Naviga t ion Un i t
G LO N A S S G lo bal Naviga t ion Sa te l l i te Syste m
GLS ( 1 ) G PS Landi ng Syste m
( 2 ) Gun Layi ng Syste m
G L U G PS L a n di ng Un i t
G M Guid a nce Ma teria l
G M C G ro und Move ment Con trol
G M T G ree nwich Mean Ti me. GM T is a un iver sal time
sc a le ba sed upon the mean ang le of ro ta t ion of th e
ea rth about its axis in re la t ion to the sun . It is
refere nced to the pri me meridian that pa sses th ro ug h
G ree nwich , Eng la n d.
G M U G lo bal Ne twork Arch i tect u re
F W D Forwa rd
F W S Fl ight Wa rn i ng Syste m
F Y D S Fl ight Director / Yaw Da m per Syste m
G A ( 1 ) Ge n eral Avia t ion
( 2 ) Go Aro un d
G A A S Ga l i um Ar se n id e
G AC S Ge n e t ic ATN Com mun ic a t ions Service
G A I T G ro un d - ba sed Augme n ta t ion and In tegri ty
G A M A Ge n eral Avia t ion Ma nu fact u rers Assoc ia t ion
G AT M G lo bal Air Traffic Ma n age me n t
G B S T G ro un d - Ba sed Softwa re Tool
G b y t e G iga byte (bi l lon bytes )
G C A S G ro und Col l i s ion Avoid a nce Syste m
G C B Ge n era tor Circuit Breaker
G C C G ro und Cluster Con trol ler (ACA RS )
G C S G ro und Clutter Suppress ion
G C U Ge n era tor Con trol Un i t
G DLP G ro und Da ta Link Processor
G D O P Geome tric Dilution Of Prec i s ion .A term referri ng to
error introduced in a GPS calcula t ion due to th e
pos i t ion i ng of the sa te l l i tes and the rece iver.
G D P G ro und De lay Progra m
G E N Ge n era tor
G E O Geosta t ion a ry Earth Orbi t
G E S G ro und Earth Sta t ion
G F E Government Fu rn i s h ed Equi pme n t
G F I Ge n eral Format Id e n t i fier
G F S K Gauss ian Freque ncy Shift Keyi ng
G G ( 1 ) G ra p h ics Ge n era tor
( 2 ) G ro un d - G ro un d
4 2
4 5
Gray Code S pec ial bi n a ry code used to transmit altitude data
be tween fra m i ng pul ses of a tra n s pon d er re ply. A
c yc l ic code havi ng only one digit ch a nge at a time.
Used in Mode C to transmit airc raft ba rome tric
a l t i t u d e. A l so kn own as Gilham cod e.
G r o u n d A ra dio wave that travels along the ea rth’s surface.
Wa v e
G R P Geogra p h ic Refere nce Poi n t
G S ( 1 ) G l id es lo pe
( 2 ) G ro und Speed
G / S G l id es lo pe
G S C G ro und Sta t ion Con trol ler (ACA RS )
G S E G ro und Support Equi pme n t
G S I F G ro und Sta t ion Inform a t ion Fra me
G S M G lo bal Systems Mo bi le
G S M S G ro und Sta t ionMa n age ment Syste m
　
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