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P i lot rece ives inform a t ion from airfie ld and adjusts his
a l t i me ter acc ordi ng ly and it will read zero altitude at
to uch d own on the runway.
Q M Q u a l i ty Ma n age me n t
Q M P Q u a l i ty Ma n age ment Pla n
Q N E The me th od of se t t i ng the altime ter to the sta n d a rd
a tm os p h ere datum -29.92 inch es of mercu ry
( 1,013.25 m b ).This se t t i ng is used in the Un i ted Sta tes
a i r s pace by all airc raft above FL 180.
Q N H The more com m on me th od of se t t i ng the altime ter to
c om pe n sa te for ch a nges in ba rome tric press u re. P i lo t
rece ives inform a t ion from airfie ld, a d j usts his
a l t i me ter acc ordi ng ly and the altime ter will rea d
a i rfie ld eleva t ion at to uch d own .
Q O P Q u a l i ty Opera t i ng Procedu res
Q o S Q u a l i ty of Service
Q R H Q uick Refere nce Ha n dboo k
Q T Y Q u a n t i ty
Q UA D Q u a dra n t
Quadrantral E rror in the re la t ive bea ri ng caused by the di stort ion
E r r o r of the rece ived ra dio signal (RF fie lds) by th e
struct u re of the airc raft .
R ( 1 ) Rig h t
( 2 ) Ro u te Tun ed NAVAID
R A ( 1 ) Resol u t ion Advi sory (ge n era ted by TCA S )
( 2 ) R a dio A l t i me ter
( 3 ) Ro u t i ng Area
8 0
8 3
R E L Re la t ive
R E Q ( 1 ) Request
( 2 ) Requi red / Requi re me n t
R E R Res idual Error Rate
Resolution A di s play indic a t ion given to the pi lot rec om me n di ng
A d v i s o r y a maneuver to inc rea se vert ical se pa ra t ion re la t ive to
an intru di ng airc raft .A resol u t ion advi sory is also
c la ss i fied as correct ive or preve n t ive.
R E S T R Restrict ion
R E S Y N C I N G Resynch ron izi ng
R E T ( 1 ) R a pid Exit Ta xi way
( 2 ) Re l ia bi l i ty Eva l u a t ion Test
R E U Re m o te Electron ics Un i t
R F R a dio Freque nc y. A ge n eral term for the ra nge of
freque nc ies above 150 kHz, to the infra - red region
( 1012 Hz).
R F C Request for Com me n ts
R F I ( 1 ) R a dio Freque ncy In terfere nce
( 2 ) Request For Inform a t ion
R F P Request For Pro posa l
R F T P Request For Tech n ical Pro posa l
R F U R a dio Freque ncy Un i t
R G B Red / G ree n / Bl ue
R G C S P Review of the Ge n eral Concept of Se pa ra t ion Pa n e l
R H R a dio Ha n dler
R H O Res pon se on Ha n d off
R H S M Reduced Horizon tal Se pa ra t ion M i n i m a
R I B ( 1 ) Right Inboa rd
( 2 ) Ro u t i ng Inform a t ion Ba se
R I P Ro u t i ng Inform a t ion Pro toc ol
R I S C Reduced In struct ion Set Com p u ter
R I U R a dio In terface Un i t
R C C Re m o te Charge Converter
R C E R a dio Con trol Equi pme n t
R C L R a dio Com mun ic a t ions Link
R C O Re m o te Com mun ic a t ions Outle t
R C P ( 1 ) R a dio Con trol Pa n e l
( 2 ) Requi red Com mun ic a t ions Perform a nce
R C R Ro u t i ng and Circuit Restora l
R C V R Rece iver
R C U Re m o te Con trol Un i t
R & D Resea rch and Deve lo pme n t
R d R-Channel used for data
R DA R A Regional Domest ic Air Ro u te Area
R D C Ro u t i ng Domain Confed era t ion
R D F Ro u t i ng Domain Form a t
R D I Ro u t i ng Domain Id e n t i fier
R D M I R a dio Dista nce Magn e t ic In dic a tor
R D P Radar Da ta Process i ng (syste m )
R D R R a d a r
R D S S R a dio De term i n a t ion Sa te l l i te Service
R D U Rece iver / Dec od er Un i t
R DV Requi re me n ts Deve lo pment and Va l id a t ion
R DV S R a pid De ployment Voice Swi tch
R E C A P Re l ia bi l i ty Eva l u a t ion and Correct ive Act ion Progra m
R E F Refere nce
R E F L Reflect ion
Re f l e c t i v i t y This is a mea s u re ment of the abi l i ty of a ta rget to
Factor (Z) reflect the energy from a radar bea m .
Re l a t i v e The bea ri ng of a gro und sta t ion re la t ive to th e
B e a r i n g di rect ion the airc raft nose poi n ts, or the di rect ion of
an airc raft to or from an NDB.
8 2
8 5
RJ Regional Je t
R L E Res pon se on Link Esta bl i s hme n t
R L P Ri ng Laser Gyro
R L S ( 1 ) Re l ia ble Link So u rce
( 2 ) Re m o te Light Se n sor
R LY Re lay
R & M Re l ia bi l i ty and Ma i n ta i n a bi l i ty
R M & A Re l ia bi l i ty Ma i n ta i n a bi l i ty and Ava i la bi l i ty
R M I R a dio Magn e t ic In dic a tor
R M M S RM Ma n age ment Syste m
R M P ( 1 ) R a dio Ma n age ment Pa n e l
( 2 ) Re m o te Ma i n te n a nce Pa n e l
R- N AV Area Naviga t ion
R N G R a nge
R N G A R a nge Arc
R N P Requi red Naviga t ion Perform a nce
　
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