Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 3961

6. MLS/RNAV procedures may require the Level 3 and 4 integrity, continuity of service and MTBO objectives of the elevation, DME/P and, if used, back azimuth to be equivalent to the approach azimuth equipment. ATT G-59 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I P EAMB E SECTO SI NA S TO SCAN TIME S OT PA SE TIME O SCAN TIME S OT O ND ADIATED TEST ( O P SE) NE T P EAMB E A IM T NCTIONS ON O T-O -CO E A E INDICATION (P SE(S)) ECEI E E E ENCE TIME CODE CA IE AC ISITION PE IOD Figure G-1. Angle function organization 23/11/06 ATT G-60 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications A A A A A A t m Figure G-2. Angle scan timing parameters ATT G-61 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I ms A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A e g 3 0 A ms otes en ac a imut is ro ided asic data ord must e transmitted only in t is osition ata ords may e transmitted in any o en time eriods e total time duration of se uence 1 lus se uence must not exceed 13 ms Figure G-3A. Transmission sequence pair which provides for all MLS angle guidance functions 23/11/06 ATT G-62 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications ms A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A A otes 1 ata ords may e transmitted in any o en time eriods en ac a imut is ro ided asic data ord must e transmitted only in t is osition e total time duration of se uence 1 lus se uence must not exceed 13 ms Figure G-3B. Transmission sequence pair which provides for the MLS high rate approach azimuth angle guidance function ATT G-63 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I 1 ms = 1 ms A Figure G-3C. Complete multiplex transmission cycle showing open time periods available for data words Figure G-4. Scanning conventions for azimuth guidance functions APP OAC A IM T ANTENNA O SCAN APP OAC A IM T IDANCE AN E N A BAC A IM T IDANCE AN E - (MA IM M) TAA (MA IM M) AA T (MA IM M) BA T - (MA IM M) BA O SCAN TO SCAN BAC A IM T ANTENNA APP OAC DI ECTION T TO SCAN 23/11/06 ATT G-64 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications A A A A A A A A 000 m 0 000 ft m 00 m 000 ft m m A A A A A A A A A A A 1 0 ormally 0 Note. The above represents the coverage sector originating at the phase centre of the installed antenna. A ot to scale A A Figure G-5A. Approach azimuth region coverage ATT G-65 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I ot to scale A 90 m 300 ft A 3 m A A A 000 m 0 000 ft A 00 m 000 ft 00 m 000 ft A A A A A m ft A A A A A A Note. The above represents the minimum proportional guidance sector re uired, irrespective of e uipment location or orientation. A A A Figure G-5B. Azimuth runway region coverage and minimum operational coverage region 23/11/06 ATT G-66 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications A A A 00 m 000 ft m ft A A A A 3 000 m 10 000 ft 0 9 m 10 A A ot to scale m 1 0 ft A A A A m 1 0 ft m 10 A A A A A A Figure G-6. Back azimuth region coverage ATT G-67 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I NE ATI E IMITS O SCAN POSITI E IMITS O SCAN IDT O P OPO TIONA IDANCE SECTO IDT O P OPO TIONA IDANCE SECTO POSITI E IMITS O SCAN NE ATI E IMITS O SCAN O SCAN TIME S OT O SCAN TIME S OT TO SCAN TIME S OT TO SCAN TIME S OT MIDSCAN POINT MIDSCAN POINT APP OAC A IM T BAC A IM T - I T C EA ANCE P SES - E T C EA ANCE P SES SCANNIN BEAM P SES Figure G-7. Clearance pulse conventions for azimuth functions 23/11/06 ATT G-68 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications SB and clearance in-phase SB and clearance out-of-phase Clearance first Clearance first Clearance last Clearance last TIME E E ENCED TO C EA ANCE P SE ED E ( s) P IDEO AMP IT DE (dB) 0 s P 0 s P 5 s P 5 s P 10 s P 10 s P -10 -20 -30 -10 -20 -30 -10 -20 -30 -200 -100 -200 -100 Figure G-8. Examples of received video waveforms in SB/clearance transition region for switching times of 0 5 and 10 microseconds ATT G-69 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I A A ot to scale A A A A A A A A A A A A Figure G-9. Scanning conventions for approach elevation function 23/11/06 ATT G-70 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications A A A A A A A A A A 3 m A A A A 00 m 000 ft 000 m 0 000 ft A A A A A Note. The above represents the coverage sector originating at the phase centre of the installed antenna. ot to scale A A A A A A A A Figure G-10A. Elevation approach region coverage ATT G-71 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I m 10 ft A 1 0 m 00 ft A A A A A A A A A A A Note. The above represents the minimum proportional guidance sector re uired, irrespective of e uipment location or orientation. A A 00 m 000 ft m ft m 0 ft m 0 ft A 3 m A A A 10 (Minimum) APP OAC DI ECTION A A ot to scale Figure G-10B. Elevation minimum operational coverage 23/11/06 ATT G-72 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications A A A A A A d 1 d d Z1 Z1 Z0 Z0 Z Z Z 0 3 orner fre uencies adians sec uidance function A roac a imut A roac ele ation ecei er out ut filter at follo ing filter ontrol motion noise filter Z1 = Z ] n Z Z n Zn Z ] = 1 = 0 Z Z n A at follo ing error at follo ing error filter Z0 ontrol motion noise ontrol motion noise filter Z1 - ecei er out ut filter Z ecei er a angle estimates A solute osition reference Figure G-11. Filter configurations and corner frequencies ATT G-73 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I E O TIME O TP T O P E O CMN I TE T1 T2 T4 T3 T = S IDIN INDO Notes: = Error specification T = egion to be evaluated T T T = Time intervals that error exceeds specifications. or the ground e uipment to be acceptable in this region, the follo ing ine uality should be true:  à (T T T ) T 0.05 à   Figure G-12. MLS measurement methodology 23/11/06 ATT G-74 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications datum oint res old of t e rimary run ay Figure G-13. MLS/RNAV way-point coordinate system ATT G-75 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I Figure G-14. Definition of curved segments 23/11/06 ATT G-76 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications P3 P3 P2 P4 P2 P1 P1 ASE -1-A SEMO -1-C Missed approach A SO-6-D P3 P2 P1 P1 P2 un ay un ay un ay NE SO-1-B Figure G-15. Diagram of sample MLS/RNAV procedures ATT G-77 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I Beam centre 0dB -3dB -10dB 0.5 B 0.5 B 0.76 B 0.76 B 0.96 B 0.96 B B = Beam idth Figure G-16. Far field dynamic signal-in-space 23/11/06 ATT G-78 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications Signal in space considerations Is collocation ith I S glide path antenna re uired Section 4.1.1.2 Siting elevation antenna bet een the glide path antenna and run ay Section 4.1.1.3 Siting elevation antenna at a greater offset than the glide path antenna Section 4.1.1.4 Alternatives Determine elevation antenna setback 4.1.1.2.1-4.1.1.2.3 Determine resnel zone migration region 4.1.1.2.4 Are obstacle re uirements satisfied 4.1.1.2.5 Are obstacle re uirements satisfied 4.1.1.3.3 Is lateral pattern penetration acceptable 4.1.1.3.2 Ad ust elevation setback as re uired 4.1.1.3.1 Are critical areas acceptable 4.1.1.2.6 Are critical areas acceptable 4.1.1.2.6 Alternatives 4.1.1.4 Is monitor site acceptable 4.1.1.2.7 Is monitor site acceptable 4.1.1.2.7 un ay threshold Site elevation antenna Site elevation antenna NO NO NO NO NO NO NO NO ES ES ES ES ES ES ES ES lide path antenna Figure G-17. Elevation/glide path logic flow diagram ATT G-79 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I ESNE ONE MI ATION E ION N A OS min. IDE PAT ANTENNA T PICA 1 0 m (590 ft) ACCEPTAB E E E ATION ANTENNA E ION Figure G-18. Elevation antenna regions for collocation with ILS (3 minimum glide path) 23/11/06 ATT G-80 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications OS E SB P AN IE P O I E IE PC A D SB = A D - PC tan Q Figure G-19. Elevation siting parameters ATT G-81 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I 23/11/06 ATT G-82 Figure G-20. Azimuth/localizer logic flow diagram Signal in space consideration ILS collocation W/ILS localizer required? Verify collocation criteria, section 4.2 Is an approach lighting system present? Section 4.1.2.2 Azimuth ahead of ILS localizer Section 4.1.2.4 Integrated azimuth/ localizer Section 4.1.2.3 Azimuth behind localizer Is azimuth-localizer spacing acceptable? 4.1.2.2.1 Is obstacle clearance above localizer satisfied? 4.1.2.4.1.1 Is spacing and AZ height acceptable? 4.1.2.3.1 AZ blockage by ILS monitor pole? 4.1.2.3.2 Are obstacle requirements satisfied W/DME? 4.1.2.2.2 Determine localizer height above AZ 4.1.2.4.1.2 AZ blockage by ILS monitor pole? 4.1.2.4.3 Are obstacle requirements satisfied W/DME? 4.1.2.2.2 Are critical areas acceptable? 4.1.2.2.3 Is monitor site acceptable? 4.1.2.2.4 Are critical areas acceptable? 4.1.2.2.3 Are obstacle requirements satisfied? 4.1.2.2.2 Are critical areas acceptable? 4.1.2.2.3 Is monitor site acceptable? 4.1.2.2.4 Site azimuth antenna if a monitor site can be found 4.1.2.2.4 Are obstacle requirements satisfied W/OUT DME? Site antenna or consider options Runway stop end Localizer array For offset azimuth siting considerations see section 4.1.2.5 Adjust phase centre height as required Adjust phase centre height as required Are obstacle requirements satisfied W/OUT DME? Site antenna or consider options Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No No No No No No No No No No No No No No No No No No 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications ront and back course case 9m 6m 3m 3m ³ 3m 30m 30m ocalizer array determined by obstacle clearance criteria 3m 6m 9m ront course case STOP END O SET A IM T SITIN A EA 1: ecommended siting positions (Directly abeam) A EA 2: No measurable effects on ocalizer front course A EA 3: Measurable degradation to ocalizer front course signal or Azimuth signals Sho s additional re uirement hen ocalizer back course is utilized nacceptable degradation to ocalizer signal in these areas A IM T OCATIONS O ND MO NTED INTE ATED E E ATED ( /o OC Back course) E E ATED ( or /o OC Back course) : SEE E END ON T E E T CENTE INE O SET Figure G-21. Azimuth antenna regions for collocation with ILS ATT G-83 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I (MA IM M A E) N D OCA I E A IM T ANTENNA P ASE CENT E N A OC = 2.5m D 0.6 D DECISION EI T =3 1 D 0.06D - D = - OC (D, , and are in metres) N Figure G-22. Azimuth phase centre height requirement when siting an azimuth antenna behind an ILS localizer 23/11/06 ATT G-84 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications 10 m (33 ft) 10 m (33 ft) Sensitive area N A CENT E INE light path deviation allo ance (0.2 ) To field monitor pole as re uired Azimuth antenna C ITICA A EA TO N A STOP END See Table -12A P AN IE P O I E IE N A MEAS ED O I ONTA OM A IM T ANTENNA MEAS ED E TICA OM BOTTOM O A IM T ANTENNAAPE T E B = BEAM IDT m (ft) m (ft) m (ft) 30 (100) 1.1 (3.5) 5.7 (1 .6) 75 (250) 2.7 ( .7) 10.5 (34.3) 150 (500) 5.3 (17.5) 17.1 (56.2) 225 (750) 7.5 (24.5) 23.2 (76.0) 300 (1 000) .6 (2 .3) 2 .9 (94. ) here: = 0.035 200m = 2 0.06  200m = tan 3 3 0.06 4.6 m (15 ft) Azimuth antenna As re uired to protect field monitor 200 m (656 ft) 1.7 BW A E O a b and 1.7 BW 2 x Fresnel zone radius 3 x Fresnel zone radius 2° 3° Figure G-23. Typical azimuth critical and sensitive areas ATT G-85 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I 75 m (250 ft) N A E E ATION ANTENNA 10 m (33 ft) 10 m (33 ft) TO IE D MONITO AS E I ED (See Table belo ) B-747 B-727 B-727 B-747 320 m (1 050 ft) 170 m (560 ft) 1 0 m (600 ft) 3 5 m (1 260 ft) 400 m (1 310 ft) 250 m ( 20 ft) 300 m (990 ft) 565 m (1 60 ft) C EAN SITE COMP E SITE P AN IE P O I E IE T IS O ME E ISTS ON E E APP OAC P OCED ES O M TIP E E E ATION AN ES A E APP O ED E E ATION ANTENNA AS E I ED TO P OTECT IE D MONITO MINIM M IDE PAT MA IM M E E ATION AN E O IC AN APP O ED APP OAC P OCED E E ISTS 1.7 B 1.7 B MA P MIN P ( 1.0 )  I T PAT DE IATION A O ANCE (0.2 ) BEAM IDT 1.0 1.5 Figure G-24. Typical elevation critical and sensitive areas/volume 23/11/06 ATT G-86 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications C ITICA A EA SENSITI E A EA, B-727 (STATIONA AI C A T P O IBITED) SENSITI E A EA, B-747 (STATIONA AI C A T P O IBITED) See plan vie of igure -23 for monitor and near-field protection See Table -12 B 300 m Note. Profile vie is sho n in igure -23. APP OAC T AC Figure G-25. Typical azimuth critical and sensitive areas for offset azimuth installation ATT G-87 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I A 3° A See 4.3.7.2.2 N A 1.7 B flight path deviation allo ance (0.2 ) D (MAP) 300 m (1 000 ft) B = Beam idth Not to scale See 4.3.7.2.1 C ITICA A EA SENSITI E A EA Figure G-26. Typical azimuth critical and sensitive areas/volume for the computed centre line procedure 23/11/06 ATT G-88 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications 3° STANDA D ST AI T-IN APP OAC C ITICA A EA O -CENT E INE C ITICA A EA E I EMENT SENSITI E A EA B = Beam idth Sensitive area un ay stop end Azimuth antenna Azimuth antenna See Table -13 1.73 1.7 B 1.7 B 1.73 Taxi ay See plan vie on igure -23 for monitor and near-field protection P O I E IE P AN IE Plan vie of approach light path deviation allo ance (0.2 ) Minimum height surface applies to this region only Proportional coverage limit Protected by centreline Critical and sensitive areas ( igure -23) N A Minimum height surface Not to scale Figure G-27. Typical extension of azimuth critical and sensitive areas for segmented and curved approaches ATT G-89 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I SEE I E -24 N A E E ATION ANTENNA TA I A SE O E E ATION IDANCE BE INS E E APP OAC 2D, 3D APP OAC O P O I E IE : T E C ITICA A EA E TENDS BE O T E NOMINA T AC B AN AN E O 1.7 B P S AN A O ANCE O I T PAT DE IATIONS. 10 m (33 ft) C ITICA A EA : 3.0 CENT E INE APP OAC C ITICA A EA E TENSION E I ED TO ENS E E E ATION SI NA A IT IN T E SECTO S SED O SE MENTED AND C ED APP OAC P OCED ES. APP OAC . Figure G-28. Typical extension of the elevation critical area for segmented and curved approach procedures 23/11/06 ATT G-90 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications 120 m (400 ft) Elevation antenna DME/N transponder (if DME/P not available) Collocated approach azimuth antenna and DME/P transponder AAz antenna offset un ay centre line AAz to elevation distance Figure G-29. Ground equipment geometry for computed centre line approaches ATT G-91 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I 2 500 2 000 1 500 1 000 -500 -1 000 -1 500 -2 000 -2 500 Azimuth antenna offset distance (metres) -500 Azimuth to elevation distance (metres) M S datum point -5 000 -4 500 -4 000 -3 500 -3 000 -2 500 -2 000 -1 500 -1 000 Figure G-30. Permissible azimuth antenna offsets for computed centre line approaches with DME/P (Standard 1) ranging 23/11/06 ATT G-92 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications -50 -100 -150 -200 -250 -500 -0 Azimuth antenna offset distance (metres) Azimuth to elevation distance (metres) M S datum point -4 500 -4 000 -5 000 -3 500 -3 000 -2 500 -2 000 -1 500 -1 000 Figure G-31. Permissible azimuth antenna offsets for computed centre line approaches with DME/N ranging ATT G-93 23/11/06 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I Secondary run ay Primary run ay Approach azimuth and DME/P 120 m (400 ft) Elevation 300 m (1 000 ft) Threshold stagger (-) un ay spacing (-) Approach direction Note. The position sho n for the elevation antenna is defined by typical values that are used to compute the data sho n in igure -33. Figure G-32. Runway and equipment geometry for computed centre line approaches to parallel secondary runways 23/11/06 ATT G-94 2007/70/II. szám Attac ment G Annex 10 — Aeronautical Communications 2 000 1 600 1 200 -400 - 00 -1 200 -1 600 -2 000 -400 - 00 Threshold stagger (metres) un ay spacing (metres) Azimuth to elevation distance = 3 000 m A Notes:

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