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E C S R Right Envi ronme n tal Con trol System Card
E C U ( 1 ) E ICAS Con trol Un i t
( 2 ) Electron ic Con trol Un i t
( 3 ) E xternal Com pe n sa t ion Un i t
E D E ICA SD i s play
E / D En d - of - Desce n t
E DA Electron ic Des ign Au tom a t ion
E DAC E rror De tect ion and Correct ion
( used interch a ngea bly wi th EDC )
E D C E rror De tect ion and Correct ion
3 2 3 3
3 5
E O M End Of Message
E OT End Of Text
E P E xternal Power
E P C E xternal Power Con tactor
E P C S Engine Pro p ul s ion Con trol Syste m
E- P I R E P S Electron ic Pilot Re ports
E- P l a n e The E- Plane is the plane of an antenna that con ta i n s
the electric fie ld.The pri nc i pal E- Plane also con ta i n s
the di rect ion of maxi mum ra dia t ion .
E P L D Electric a l ly Progra m m a ble Logic Device
E P P Enh a nced Pa ra l lel Port
E P R Engine Press u re Ratio
E P R O M E ra sa ble Progra m m a ble ROM
E P S Electrical Power Syste m
E Q U I P E qui pme n t
E q u i v a l e n t E quiva lent Ai r s peed is a di rect mea s u re of th e
Airspeed i nc om press i ble freestream of dyn a m ic press u re.
( E A S ) It is CAS corrected for com press i bi l i ty effects.
ER PDU E cho Re ply Pro toc ol Da ta Un i t
E R A E u ro pean Regional Ai rl i n es Assoc ia t ion
E R B Engi n eeri ng Review Boa rd
E R D End Ro u t i ng Dom a i n
E R D I En Ro u te Domain Infra struct u re
E R E E xternal Roll Extrus ion
E R P Eye Refere nce Poi n t
ERP PDU E cho Re ply Pro toc ol Da ta Un i t
ERQ PDU E cho Request Pro toc ol Da ta Un i t
E R U Engine Re lay Un i t
E S End Syste m
E I A Electron ic In dustries Assoc ia t ion
E I C A S Engine In dic a t ion and Crew A lert Syste m
E I C A S C Engine In dic a t ion and Crew A lert System Con trol s
E I P I E xte n d ed In i t ial Pro toc ol Id e n t i fier
E I R P E a rth Inc ident Radia ted Power
E I S ( 1 ) Electron ic In strument Syste m
( 2 ) Engine In dic a t ion Syste m
E I S A E xte n d ed In dustry Sta n d a rd Arch i tect u re
E I U E FIS / E ICAS In terface Un i t
E L / F C G Electron ic Log book and Fault Correct ion Guid e
E L B / I S E Electron ic Log book In - Service Eva l u a t ion
E L C E m i t ter Coupled Logic
E L E C Electric a l
E L M E xte n d ed Le ng th Message
E L M S Electrical Load Ma n age ment Syste m
ELS Electron ic Libra ry System
E LT E merge ncy Loc a tor Tra n s m i t ter
E M Ele ment Ma n ager
E M C ( 1 ) Electrom agn e t ic Com pa t i bi l i ty
( 2 ) En terta i nment Mul t i plexer Con trol ler
E M E R E merge nc y
E M I Electro - Magn e t ic In terfere nce
E M S ( 1 ) E merge ncy Medical Services
( 2 ) Engine Ma n age ment Syste m
E N G Engi n e
E N O C Engi n eeri ng Ne twor k O pera t ions Center
E N Q En qui re
E / O Engi n e - O u t
E O D End Of Day
3 4
3 7
E U R E u ro pea n
E U R AT N E u ro pean AT N
E U R E T E u ro pean Tra n s port
E u r o c a e E u ro pean Orga n iz a t ion for Civil Avia t ion Electron ic s.
A regula tory age ncy for avion ics cert i fic a t ion in
E u ro pe.
E U R O-C O N T R O L E u ro pean Orga n iz a t ion for the Safe ty of Ai r
Naviga t ion Opera t ion s
E V E a rn ed Va l ue
E V M E rror Vector Magn i t u d e
E V S Enh a nced Vi s ion Syste m
E X E C E xecu t ive
F Fah re nh e i t
FA Final A p proach
FA A ( 1 ) Fed eral Avia t ion Adm i n i stra t ion (U. S.)
( 2 ) Fed eral Avia t ion Au th ori ty
FA ATC FA A Tech n ical Center (U. S.)
FAC Fl ight Augme n ta t ion Com p u ter
FA D E C Full Au th ori ty Digi tal Electron ic Con trol
FA F Final A p proach Fi x
FA I Fi r st Art ic le In s pect ion
Fan Marke r A m a r ker beac on used to provide id e n t i fic a t ion
of pos i t ions along airways. S ta n d a rd fan marker
produces an elliptic a l - s h a ped pa t tern .A sec ond
type produces a dum b be l l - s h a ped pa t tern .
FA N S Fu t u re Air Naviga t ion Syste m
FA R ( 1 ) Fed eral Acqui s i t ion Regula t ion
( 2 ) Fed eral Avia t ion Regula t ion
FA S T Final A p proach Spac i ng Tool
FAT Factory Acce p ta nce Test
F B L Fly - By - L ig h t
E S A E u ro pean Space Age nc y
E S A S ( 1 ) Electron ic Situation Awa re n ess Syste m
( 2 ) Enh a nced Situational Awa re n ess Syste m
E-S c a n Electron ic Sc a n n i ng
E S D Electrosta t ic Disch a rge
E S D S Electrosta t ic Se n s i t ive Devices. A l so kn own as ESSD.
E S H End System He l lo
E S I D Engine and System In dic a t ion Display
　
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