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

R N R Rece ive Not Rea dy
R N T P R a dio Nav Tun i ng Pa n e l
R O ( 1 ) R a dio O pera tor
( 2 ) Roll Out
R OA Rec ogn ized Opera t i ng Age nc y
R O B Right Outboa rd
R O C ( 1 ) R a te Of Climb
( 2 ) R a te of Opera t ional Capa bi l i ty
R O D R a te Of Desce n t
R O M ( 1 ) Read Only Me m ory
( 2 ) Ro ugh Ord er of Magn i t u d e
R O N Remain Over Nig h t
R OT H R Re loc a ta ble Over- T h e - Horizon Radar
R P Ro u t i ng Pro toc ol
8 4
R P I R a pid Process Im prove me n t
R P M Revol u t ions Per Minu te
R P OA Rec ogn ized Priva te Opera t ion Age ncy (CC ITT )
R R Rece iver Rea dy
R R I Ro u ter Refere nce Im ple me n ta t ion
R S D P Re l ia ble Seque nc i ng De l ivery Confi rm a t ion Pro toc ol
R S N Regional Subnetwor k
R S P ( 1 ) Requi red Surve i l la nce Perform a nce
( 2 ) Rever s ion Se lect Pa n e l
R S S I Rece ived Signal Stre ng th In dic a tor
R T ( 1 ) R a dio Te lec om mun ic a t ion
( 2 ) Rece iver- Tra n s m i t ter (R/T). A l so referred to as a
tra n sce iver. ( See T / R )
R TA ( 1 ) Rece iver- Tra n s m i t ter An te n n a
( 2 ) Requi red Ti me of Arriva l
R TC Rea l - Ti me Clock
R TC A R a dio Tech n ical Com m i ss ion for Aeron au t ic s
R TCA DO- 1 6 0 RTCA Document 160, Envi ronme n tal Con di t ions and
Test Procedu res for Ai r borne Equi pme n t , Iss ued
12 / 04 / 89
R TCA DO- 1 7 8 RTCA Document 178, Softwa re Con s id era t ions in
Ai r borne Systems and Equi pment Cert i fic a t ion ,
i ss ued 03 / 22 / 85
R T E Ro u te
R T F R a dio te le p h ony
R T I Rea l - Ti me In terroga te
R T M R a dio Tra n s m i ss ion Module
R T P Re l ia bi l i ty Test Pla n
R TO Re jected Takeoff
R TO S Rea l - Ti me Opera t i ng Syste m
R T P R a dio Tun i ng Pa n e l
86 87
R T R Re m o te Tra n s m i t ter Rece iver Site
R T S Request To Se n d
R T T I R un - Ti me Type Id e n t i fic a t ion
R T U R a dio Tun i ng Un i t
R U R ack Un i t
R u n w a y The act of inadverte n tly cross i ng the runway holdi ng
I n c u r s i o n point wi thout ATC clea ra nce.
R V D T Ro ta ry Vol tage Differe n t ial Tra n sducer
R V R R unway Visual Range
R V S M Reduced Vert ical Se pa ra t ion Minimum
R / W Rea d / Wri te
R W R unway
R W M Rea d -Wri te Me m ory.Ame m ory in wh ich each cell is
se lected by applyi ng appro pria te electrical inp u t
s ign a l s, and the stored data may be eith er se n sed at
the appro pria te output terminal or ch a nges in
res pon se to oth er electrical input sign a l s.
R x Rece iver
R Z Re t u rn to Zero
S So u th
S 0 Segment O
S 1 Segment 1
S A ( 1 ) Se lect ive Ava i la bi l i ty
( 2 ) S i t u a t ion Awa re n ess
S A A Service Access Area
S A A R U Sec on d a ry Attitude Air Da ta Refere nce Un i t
S A E Soc ie ty of Au tom o t ive Engi n eer s
S A I System Arch i tect u re and In terface
S A M A Small Ai rc raft Ma nu fact u rers Assoc ia t ion
S A P Service Access Poi n ts
S A R Sea rch and Rescue
S A R P S S ta n d a rds And Rec om me n d ed Pract ices
S A S ( 1 ) S ta bi l i ty Augme n ta t ion Syste m
( 2 ) S ta t ion Ad dress Se t
S AT ( 1 ) S ta t ic Air Te m pera t u re is the to tal air te m pera t u re
c orrected for the Mach effect . Inc rea ses in
a i r s peed cause pro be te m pera t u re to ri se
prese n t i ng erron eo us inform a t ion . SAT is th e
o u ts ide air te m pera t u re if the airc raft could be
bro ught to a stop before mea s u ri ng te m pera t u res.
( 2 ) System Acce p ta nce Test
S ATC O M Sa te l l i te Com mun ic a t ion s
S AT N AV Sa te l l i te Naviga t ion
S B Service Bul le t i n
S B C S i ng le Boa rd Com p u ter
S B D Sch e m a t ic Block Diagra m
S B E S i ng le Bit Error
S / C S tep Climb
S C S pec ial Com m i t tee
SCAT S pec ial Category
S C D ( 1 ) S pec i fic a t ion Con trol Drawi ng
( 2 ) System Category Diagra m
S C D U Sa te l l i te Con trol Da ta Un i t
SCI D Softwa re Configu ra t ion In d ex Drawi ng
SCI U R a dio A l t i me ter In dic a tor
S C M Softwa re Configu ra t ion Ma n age ment
SCP C S i ng le Carrier Per Channel
SCS S i ng le Channel Simplex .A c om mun ic a t ion system th a t
uses simplex .
S C S I Small Com p u ter System In terface
S C U ( 1 ) S ignal Con di t ion i ng Un i t
( 2 ) S ignal Conver s ion Un i t
8 9
S E U ( 1 ) S i ng le Event Upse t
( 2 ) Seat Electron ics Un i t
S F D F S u bsystem Fault De tect ion Funct ion
S F E S u p pl ier Fu rn i s h ed Equi pme n t
　
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