RNP APCH procedures for BEJAIA Soummam-Abane Ramdane RWY26

Transcription

1 RNP APCH procedures for BEJAIA Soummam-Abane Ramdane RWY26 NAME POSITION DATE SIGNATURE Drafted by Fabrizio LOVINO Flight Procedure Designer/Airspace Design Department 18/11/2015 SIGNED Verified by Paolo MEZZACAPO Angelo CERASARI Airspace Design Department Airspace Design Department 04/12/2015 SIGNED 04/12/2015 SIGNED Approved by Giuseppe SCALA Head of Airspace Design Department 9/12/2015 SIGNED GNSS approach procedures for Bejaia Airport RWY26 Pag. 1

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3 Change Log Version Data Description Ref. Paragraphs Ref. Pages Note /10/2015 Draft Version All All /11/2015 Final Version All All GNSS approach procedures for Bejaia Airport RWY26 Pag. 3

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5 Summary 1 Acronyms and Definitions Reference Documents Data Artificial Obstacles Terrain Raster Working Methods ATS Geography Waypoints Procedure Segments TAAs Initial Approach Holding Initial Approach Segment Right Initial Approach Segment Central Initial Approach Segment Left Initial Approach Segment Intermediate Approach Segment Final Segment Final Segment LNAV APV BARO-VNAV SBAS APV I Missed Approach Segment Straight Missed Approach Segment Straight Missed Approach Segment LNAV Straight Missed Approach Segment BARO-VNAV Straight Missed Approach Segment SBAS APV I Turning Missed Approach Segment Turning Missed Approach Segment (AE708-AE709) LNAV Turning Missed Approach Segment (AE708-AE709) BARO-VNAV Turning Missed Approach Segment (AE708-AE709) SBAS APV I Turning Missed Approach Segment (AE709-AE711) LNAV Turning Missed Approach Segment (AE709-AE711) BARO-VNAV Turning Missed Approach Segment (AE709-AE711) SBAS APV I Turning Missed Approach Segment (AE711-AE701) Holding Missed Approach VSS SBAS FAS DATA BLOCK Procedures Overview Minima Table GNSS approach procedures for Bejaia Airport RWY26 Pag. 5

6 Table of figures Figure 1 TAA AE701 visual filter 3000FT Figure 2 TAA AE702 visual filter 4000FT Figure 3 TAA AE702 Subsector visual filter 5000FT Figure 4 TAA AE703 visual filter 5000FT Figure 5 Initial Approach Holding MHA5500FT Figure 6 Initial Approach Holding Altitude 14000FT Figure 7 Right Initial Approach Segment (AE701-AE706) Figure 8 Central Initial Approach Segment (AE702-AE706) Figure 9 Left Initial Approach Segment (AE703-AE704-AE706) Figure 10 Intermediate Approach Segment LNAV (AE706-AE707) Figure 11 Intermediate Approach Segment SBAS (AE706-AE707) Figure 12 Final Approach Segment LNAV (AE707-AE708) Figure 13 Final Approach Segment, FAS & Ground Plane BARO-VNAV Figure 14 OAS SBAS APV I Figure 15 Straight Missed Approach Segment LNAV Figure 16 Straight Missed Approach Segment BARO-VNAV Figure 17 Straight Missed Approach Segment SBAS APV I Figure 18 Turning Missed Approach Segment LNAV (AE708-AE709) visual filter 1500FT Figure 19 Turning Missed Approach Segment BARO-VNAV (AE708-AE709) visual filter 1000FT Figure 20 Turning Missed Approach Segment SBAS APV I (AE708-AE709) Figure 21 Turning Missed Approach Segment LNAV (AE709-AE711) visual filter 1641FT Figure 22 Turning Missed Approach Segment BARO-VNAV (AE709-AE711) visual filter 1641FT Figure 23 Turning Missed Approach segment SBAS APV I (AE709-AE711) visual filter 1641FT Figure 24 Turning Missed Approach segment (AE711-AE701) Figure 25 VSS RWY Figure 26 NGA EGM96 Ellipsoidal height THR Figure 27 UNAVCO Ellipsoidal height THR Figure 28 LNAV RWY26 Overview Figure 29 BARO-VNAV RWY26 Overview Figure 30 SBAS APV I RWY26 Overview GNSS approach procedures for Bejaia Airport RWY26 Pag. 6

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8 1 Acronyms and Definitions AIP APV ARP ATT Baro-VNAV CTA DA DB DH ENR FAF/P FPDAM FTA HA HG IAF IAS IF KK KT LNAV LNAV/VNAV LPV MA MAF Aeronautical Information Publication Approach Procedure with Vertical guidance Aerodrome Reference Point Along Track Tolerance Barometric vertical navigation (Baro-VNAV) is a navigation system that presents to the pilot computed vertical guidance referenced to a specified vertical path angle (VPA), nominally 3. The computer-resolved vertical guidance is based on barometric altitude and is specified as a VPA from reference datum height(rdh) Control Area Decision Altitude Data Base Decision Height Enroute Final Approach Fix/Point Flight Procedure Design and Airspace Manager Fix Tolerance Area Height of equivalent approach obstacle Height Gain Initial Approach Fix Indicated Air Speed Intermediate Fix Earliest TP tolerance. It is a main reference to evaluate a missed approach obstacle in the turn area, when a turn at a given fix is defined. Knots Lateral Navigation: The minima line on the chart for RNP Approaches without vertical guidance The minima line based on Baro-VNAV system performances that can be used by aircraft approved according to AMC or equivalent. LNAV/VNAV minima can also be used by SBAS capable aircraft Localizer Performance with Vertical Guidance: the minima-line based on SBAS performances that can be used by aircraft approved according to AMC or equivalent Missed Approach Missed Approach Fix GNSS approach procedures for Bejaia Airport RWY26 Pag. 8

9 MAHF MAPt MEA MHA MHL MOC MSD NA NM OAS OCA/H PBN PT RA RDH RNAV RNP RWY SBAS SDF SOC TAA THR TIA TP TRD VNAV VPA VSS WPT Z Eq Missed Approach Holding Fix Missed Approach Point Minimum En-Route Altitude Minimum Holding Altitude Minimum Holding Level Minimum Obstacle Clearance Minimum Stabilization Distance Nominal Altitude Nautical Miles Obstacle Assessment Surface Obstacle Clearance Altitude/Height Performance-Based Navigation. The PBN concept specifies Navigation Specifications in terms of navigation system performance accuracy, integrity and continuity along with the functionality required onboard an aircraft for the proposed operations Path & Terminator Required Altitude Reference Datum Height (for APV or Precision Approaches) Area Navigation Required Navigation Performance Runway Space Based Augmentation System Step Down Fix Start Of Climb Terminal Arrival Altitude Threshold Turn Initiation Area. It is a main reference to evaluate a missed approach obstacle in the turn area, when a turn at a given altitude is defined. Turning Point Track Distance Vertical Navigation Vertical Path Angle Visual Segment Surface Waypoint Equivalent Obstacle (for missed approach obstacle) GNSS approach procedures for Bejaia Airport RWY26 Pag. 9

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11 2 Reference Documents ICAO Annex 4 Aeronautical Charts ICAO Annex 11 Air Traffic Services ICAO Annex 15 Aeronautical Information Service DOC ICAO 8168 vol. II Construction of visual and Instrument Flight Procedure DOC ICAO 8697 Aeronautical Chart Manual DOC ICAO 9613/AN/937 Performance-based Navigation (PBN) DOC ICAO 9906-AN/472 The Quality Assurance Manual for Flight Procedure Design Volume 1 Flight Procedure Design Quality Assurance System ICAO DOC 4444 Air Traffic Management - Procedures for Air Navigation Services (PANS-ATM) GNSS approach procedures for Bejaia Airport RWY26 Pag. 11

12 3 Data 3.1 Artificial Obstacles The artificial obstacles were made available by Algerian Authorities in an excel file containing artificial obstacles in the around area of Bejaia. Other artificial obstacles have been detected from AIP Algerie as published in ENR Terrain The following terrain data provided by Algerian Authorities have been used: INCA (SPACING 9M) format.grd, reference system UTM31-WGS84; INCA (SPACING 9M) format.bt, reference system UTM31-WGS84; Contour lines (25M Equidistance) format.dgn reference system UTM31-WGS84. Where the above datum were not available, the following terrain data have been used: DEM Aster GDEM (SPACING 30M) format.grd, reference system UTM31-WGS84; DEM Aster GDEM (SPACING 30M) format.bt, geographic reference system (Latitude/Longitude)/WGS84; 3.3 Raster The following raster data, dating back to the 1993/1994, were used only as an additional check on existing obstacles. Cartography Joint Operations Graphics series Air scale 250K : ED ALGER-ALGERIA-NJ_31-15; ED BAJAIA-ALGERIA-NJ_ GNSS approach procedures for Bejaia Airport RWY26 Pag. 12

13 4 Working Methods This chapter reports assumptions and criteria followed to design the instrument approach procedures detailed in this document. 1) The flight procedures segments are designed in true degrees. As the magnetic variation for DAAE airport is equal to 0 E (see AIP/AD2 DAAE-1), these values do not need to be converted in magnetic ones, for publication purposes. 2) Procedure design has been carried out in accordance with ICAO PANS-OPS DOC 8168 Vol. II Construction of Visual and Instrument Flight Procedures. The software used for the design is compliant with ICAO PANS OPS DOC Where it was not possible to apply the regulation, clear explanations have been provided. 3) The development of the study described in this report includes the construction of all procedures elements involved in the Initial, Intermediate, Final and Missed Approach segments. Specifically, FIX/Waypoint (IAF, IF, FAF, MAPt, SOC, Missed Approach Turning Point, Missed Approach additional fixes, Missed Approach Holding Fix and their FTAs), Initial, Intermediate, Final and MA tracks and their respective protection areas. The RNP APCH Navigation Specification is applied for all procedures segments from Initial Approach Segment to the Final Missed Approach Segment (as prescribed by ICAO DOC 8168 and ICAO DOC PBN Manual). The RNAV holding patterns have been designed considering navigation specifications not requiring RNAV systems with holding functionality and RNAV1 specification. 4) Determination of Minimum Stabilization Distances and Minimum segment length have been assessed according to the provisions of ICAO Doc 8168, Part III, sec. 2, ch. 1, par. 1.4 (Minimum Stabilization Distance) and 1.5 (Determination of the minimum length of an RNAV segment limited by at least one waypoint which is not a turning point). GNSS approach procedures for Bejaia Airport RWY26 Pag. 13

14 5) For Minima calculation, the following criteria have been applied: a. MOC reduction in secondary protection areas for Initial, Intermediate, Final and MA segments; b. As indicated by Algerian Authorities, vegetation of 50FT have been considered in order to safeguard minima calculation (except for VSS surface analysis); c. Procedure design is limited up to cat C aircraft, according the indication received from Algerian Authorities. GNSS approach procedures for Bejaia Airport RWY26 Pag. 14

15 5 ATS Geography ATS Geography data reported in this section, considered as significant input to the procedures design activity, were provided by the Algerian Authorities and made available through the AIP Algeria (ENR2/5). Airport Information Airport Name BEJAIA/Soummam-Abane Ramdane ICAO Identifier DAAE A/D Elevation 6M ARP Latitude 36:42:43N ARP Longitude 005:04:10E Magnetic Variation 0 E (2005) Aircraft Categories A B C Threshold Information Threshold Latitude Longitude Elevation (M) (DD:MM:SS.SS DDD: MM:SS.SS ) THR26 36:42:48.69N - 005:04:59.48E 3 THR08 36:42:37.53N - 005:03:23.68E 6 GNSS approach procedures for Bejaia Airport RWY26 Pag. 15

16 6 Waypoints ROLE IDENT Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) IAF (Right) AE701 36:54: N 005:18: E IAF (Central) AE702 36:46: N 005:32: E IAF (Left) AE703 36:34: N 005:22: E SDF (Left Initial Segment) AE704 36:40: N 005:21: E IF AE706 36:44: N 005:20: E FAF AE707 36:43: N 005:14: E MAPt (LNAV only) AE708 36:43: N 005:06: E MAF AE709 36:45: N 004:59: E MAF AE711 36:52: N 004:59: E MAHF AE701 36:54: N 005:18: E GNSS approach procedures for Bejaia Airport RWY26 Pag. 16

17 7 Procedure Segments 7.1 TAAs Segment Data TAA Right TAA AE701 Central TAA AE702 Left TAA AE703 Reference Point IF (AE706) Subsector Subsector Subsector TAA AE701 (Right) AE702 (Central) AE702 (Subsector) AE703 (Left) OBST. Orographic + Vegetation CONTROLLING OBSTACLE Latitude Longitude TAA Elev. MOC Minima DD:MM:SS.SSSS Altitude DDD: MM:SS.SSSS 36:44: N 004:51: E :38: N 005:41: E :30: N 005:28: E :30: N 005:28: E Remarks Considering the published transition altitude of 2010M (6594FT) and barometric excursion of 1500FT: TAA AE702 subsector: 7700FT FT = FL95 TAA AE703: 7700FT FT = FL95 GNSS approach procedures for Bejaia Airport RWY26 Pag. 17

18 Figure 1 TAA AE701 visual filter 3000FT Figure 2 TAA AE702 visual filter 4000FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 18

19 Figure 3 TAA AE702 Subsector visual filter 5000FT Figure 4 TAA AE703 visual filter 5000FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 19

20 7.2 Initial Approach Holding Segment Data Holding Point MHA Inbound Track ( ) IAS (KT) Time (sec) AE Turn Direction Entry Sectors RNAV Specification MAX Holding Altitude RIGHT ALL RNAV Type RNAV without holding functionality CONTROLLING OBSTACLE Latitude Longitude Calculated Minimum OBST. (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) Elev. MOC Minima Holding Altitude Remarks Holding protection areas develop entirely over the sea. MHA 5500FT has been considered in order to ensure the standard gradient 2.5% in the missed approach segment and to use the same holding pattern for both Initial and Missed Approach phase. Figure 5 Initial Approach Holding MHA5500FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 20

21 Segment Data Holding Point Altitude Inbound Track ( ) IAS (KT) Time (sec) AE Turn Direction Entry Sectors RNAV Specification Type RIGHT ALL RNAV 1 RNAV without holding functionality OBST. Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) CONTROLLING OBSTACLE Elev. MOC Calculated Minima Holding Altitude Orographic 36:46: N Vegetation 005:05: E (5th ring) Remarks The table above refers to an altitude of 14000FT. No restrictions for greater holding altitude. Figure 6 Initial Approach Holding Altitude 14000FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 21

22 7.3 Initial Approach Segment Right Initial Approach Segment Segment Data START POINT END POINT Length (NM) Descent Gradient Course (000 ) AE701 (5500FT) AE (TRD 9.3) -3.7% 172 CONTROLLING OBSTACLE OBST. Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) Elev. MOC Calculated Minima AE706 Altitude Remarks Right Initial Approach protection areas develop entirely over the sea IAS MAX 210KT during AE706 turn According to DOC 8168 Part III Section 2, Ch. 3, 3.2.3/4, descent gradient is based on the shortest possible TRD In order to ensure a descent gradient, for the left initial approach segment, within the maximum prescribed by DOC 8168 Part I Section 4, Ch and equal to 8%, AE706 (IF) has been considered at 3400FT Figure 7 Right Initial Approach Segment (AE701-AE706) GNSS approach procedures for Bejaia Airport RWY26 Pag. 22

23 7.3.2 Central Initial Approach Segment Segment Data START POINT END POINT Length (NM) Descent Gradient Course (000 ) AE702 (6100FT) AE % 262 CONTROLLING OBSTACLE OBST. Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) Elev. MOC Calculated Minima AE706 Altitude Orographic 36:43: N Vegetation 005:33: E (secondary) Remarks In order to ensure a descent gradient, for the left initial approach segment, within the maximum prescribed by DOC 8168 Part I Section 4, Ch and equal to 8%, AE706 (IF) has been considered at 3400FT Figure 8 Central Initial Approach Segment (AE702-AE706) GNSS approach procedures for Bejaia Airport RWY26 Pag. 23

24 7.3.3 Left Initial Approach Segment Segment Data START POINT END POINT Length (NM) Descent Gradient Course (000 ) AE703 (7700FT) AE (TRD 9.3) -7.6% 352 CONTROLLING OBSTACLE (AE703 AE704) OBST. Orographic + Vegetation OBST. Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) Elev. MOC Calculated Minima AE704 Altitude 36:35: N 005:22: E CONTROLLING OBSTACLE (AE704 AE706) Latitude Longitude Calculated (DD:MM:SS.SSSS Elev. MOC Minima DDD: MM:SS.SSSS ) AE706 Altitude Remarks Initial Approach protection areas from AE704 to AE706 develop entirely over the sea IAS MAX 210KT during AE706 turn According to DOC 8168 Part III Section 2, Ch. 3, 3.2.3/4, descent gradient is based on the shortest possible TRD In order to ensure a descent gradient within the maximum prescribed by DOC 8168 Part I Section 4, Ch and equal to 8%, AE706 (IF) has been considered at 3400FT Figure 9 Left Initial Approach Segment (AE703-AE704-AE706) GNSS approach procedures for Bejaia Airport RWY26 Pag. 24

25 7.4 Intermediate Approach Segment Segment Data START POINT END POINT Length (NM) Descent Gradient Course (000 ) AE706 AE % 262 CONTROLLING OBSTACLE OBST. Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) Elev. MOC Calculated Minima AE707 Altitude Remarks Intermediate Approach protection areas develop entirely over the sea According to DOC 8168 Part III Section 2, Ch. 3, 3.2.3/4, descent gradient is based on the shortest possible TRD 1.5NM flat prior to the FAF has been taken into account for intermediate descent gradient computation. Figure 10 Intermediate Approach Segment LNAV (AE706-AE707) GNSS approach procedures for Bejaia Airport RWY26 Pag. 25

26 Figure 11 Intermediate Approach Segment SBAS (AE706-AE707) GNSS approach procedures for Bejaia Airport RWY26 Pag. 26

27 7.5 Final Segment Segment Data START POINT END POINT Length (NM) Descent Gradient Course (000 ) AE707 THR % (-3 ) Final Segment LNAV CONTROLLING OBSTACLE OBST. Latitude Longitude Calculated OCA(H) LNAV (DD:MM:SS.SSSS Elev. MOC Altitude DDD: MM:SS.SSSS ) Remarks Due to MAPt (AE708) placed at 1.5NM from THR26, the Final Approach protection areas LNAV develop entirely over the sea Figure 12 Final Approach Segment LNAV (AE707-AE708) GNSS approach procedures for Bejaia Airport RWY26 Pag. 27

28 7.5.2 APV BARO-VNAV OBST. Orographic + Vegetation Latitude Longitude (DD:MM:SS.SSSS - DDD: MM:SS.SSSS ) 36:41: N 005:05: E CONTROLLING OBSTACLE Elev. CAT HL 543 A B C 0 (margin of the side surface) 0 (margin of the side surface) 0 (margin of the side surface) OCA(H) VNAV 543(533) 543(533) 543(533) Remarks Specify minimum VNAV temperature: -10 C Temperature correction: 66.37M Min. effective VPA: 2.73 Hi: 75M Xfas: 0.86NM αfas: 2.71 Xz CAT C: -1100M Xz CAT A/B): -900M According to DOC 8168 Part III Section 3, Chapter 4, the APV OAS ends at the missed approach turning fix (SOC LNAV). FAS develops entirely over the sea Ground Plane develops largely over the sea, indeed, orographic controlling obstacle has been detected only on the margin of the side surface Figure 13 Final Approach Segment, FAS & Ground Plane BARO-VNAV GNSS approach procedures for Bejaia Airport RWY26 Pag. 28

29 7.5.3 SBAS APV I OBST. Orographic + Vegetation Latitude Longitude DD:MM:SS.SSSS DDD:MM:SS.SSSS 36:43: N 005:01: E CONTROLLING OBSTACLE Elev Equivalent Elevation CAT Height Loss OCA(H) VNAV 764 A (884) 764 B (896) 764 C (904) Remarks The report below refers to CAT C aircraft and the controlling obstacle computed already takes into account vegetation of 50FT. Figure 14 OAS SBAS APV I GNSS approach procedures for Bejaia Airport RWY26 Pag. 29

30 7.6 Missed Approach Segment Missed approach description: Proceed on TR262 climbing to 5500FT. At AE708 (MAPt for LNAV only) turn right (IAS MAX 160KT) on TR 297 bound to AE709, then turn right on TR001 bound to AE711, then turn right (IAS MAX 230KT)on TR082 bound to AE701 to join AE701 holding pattern Straight Missed Approach Segment Straight Missed Approach Segment LNAV Segment Data START POINT END POINT Length (NM) Climb Gradient Course (000 ) AE708 (MAPt) SOC 1.1 0% 262 CONTROLLING OBSTACLE OBST. Orographic + Vegetation Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) 36:41: N 005:05: E Elev. 543 MOC 0 (margin of secondary area) Calculated Altitude OCA(H) LNAV (533) Remarks Seeing that the missed approach segment foresees an as soon as practicable turn on MAPt (AE708), the straight missed approach protection areas is based on the MAPt SOC segment only, which develops largely over the sea. Orographic obstacle has been detected only on the margin of the secondary protection area Figure 15 Straight Missed Approach Segment LNAV GNSS approach procedures for Bejaia Airport RWY26 Pag. 30

31 Straight Missed Approach Segment BARO-VNAV Segment Data START POINT END POINT Length (NM) Climb Gradient Course (000 ) SOC AE % 262 CONTROLLING OBSTACLE OBST. Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) Elev. MOC Calculated Altitude OCA(H) VNAV Remarks The Missed Approach Surface (which starts at the origin of the Z surface, xz CAT C= -1100m, xz CAT B = -900m) does not exist as the missed approach segment foresees an as soon as practicable turn. According to DOC 8168 Part III Section 3, Chapter 4, the APV OAS ends at the missed approach turning fix and the LNAV missed approach criteria has to be applied after the end of the APV OAS. Therefore, only the Ground plane and FAS could have been evaluated, see APV BARO-VNAV. SOC altitude for each aircraft category has been evaluated considering the highest maximum VPA 3.5 allowed. Figure 16 Straight Missed Approach Segment BARO-VNAV GNSS approach procedures for Bejaia Airport RWY26 Pag. 31

32 Straight Missed Approach Segment SBAS APV I Segment Data START POINT END POINT Length (NM) Climb Gradient Course (000 ) SOC AE % 262 CONTROLLING OBSTACLE OBST. Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) Elev. MOC Calculated Altitude OCA(H) LPV Remarks Straight Missed Approach segment, protected by the APV OAS segment, develops entirely over the sea. Figure 17 Straight Missed Approach Segment SBAS APV I GNSS approach procedures for Bejaia Airport RWY26 Pag. 32

33 7.6.2 Turning Missed Approach Segment Turning Missed Approach Segment (AE708-AE709) LNAV Segment Data START END POINT Length (NM) Climb Gradient Course (000 ) POINT AE708 AE % 295 Turn Parameters Turning WP Turn Type Turn Direction Path & Terminator AE708 Fly-over Right DF Initial Altitude IAS (KT) Bank Angle ( ) Turn Angle ( ) Turn Gradient (%) 1400 (SOC) OBST. Orographic + Vegetation Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) 36:43: N 005:01: E CONTROLLING OBSTACLE Elev. MOC Remarks d0 (shortest distance from obstacle to line K-K ) = 3.1NM HG = d0 * MA gradient = 3.1NM * = 470FT RA = Controlling Obstacle + MOC = 1691FT + 164FT=1855FT NA = SOC + HG = 1400FT + 470FT = 1870FT Clearance from obst. OCA(H) LNAV (1390) Figure 18 Turning Missed Approach Segment LNAV (AE708-AE709) visual filter 1500FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 33

34 Turning Missed Approach Segment (AE708-AE709) BARO-VNAV Segment Data START END POINT Length (NM) Climb Gradient Course (000 ) POINT AE708 AE % 295 Turn Parameters Turning WP Turn Type Turn Direction Path & Terminator AE708 Fly-over Right DF Initial Altitude IAS (KT) Bank Angle ( ) Turn Angle ( ) Turn Gradient (%) AE OBST. Orographic + Vegetation Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) 36:43: N 005:01: E CONTROLLING OBSTACLE Elev. MOC CAT Clearance from obst. OCA(H) VNAV A (1260) B (1290) C (1320) Remarks The computation below refers to CAT C aircraft only: SOC altitude for each aircraft category has been evaluated considering the highest maximum VPA 3.5 allowed. dz (horizontal distance from SOC to the earliest TP) = 0.3NM d0 (shortest distance from obstacle to line K-K ) = 5NM HG1 = dz * MA gradient = 0.3NM * 151.9FT/NM = 45.6FT HG2 = d0 * MA gradient = 5NM * 151.9FT/NM = 759.5FT RA = Controlling Obstacle + MOC = 1691FT + 164FT=1855FT NA = SOC altitude + HG1 + HG2 = FT FT = FT Latest SOC for all aircraft category is coincident with the earliest (AE708) TP line. Figure 19 Turning Missed Approach Segment BARO-VNAV (AE708-AE709) visual filter 1000FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 34

35 Turning Missed Approach Segment (AE708-AE709) SBAS APV I Segment Data START END POINT Length (NM) Climb Gradient Course (000 ) POINT AE708 AE % 295 Turn Parameters Turning WP Turn Type Turn Direction Path & Terminator AE708 Fly-over Right DF Initial Altitude IAS (KT) Bank Angle ( ) Turn Angle ( ) Turn Gradient (%) AE OBST. Orographic + Vegetation Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) 36:43: N 005:01: E CONTROLLING OBSTACLE Elev. MOC CAT Clearance from obst. Remarks The computation below refers to CAT C aircraft only: dz (horizontal distance from SOC to the earliest TP) = 0.98NM d0 (shortest distance from obstacle to line K-K ) = 4.5NM HG1 = dz * MA gradient = 0.98NM * 151.9FT/NM = 149FT HG2 = d0 * MA gradient = 4.5NM * 151.9FT/NM = 683FT RA = Controlling Obstacle + MOC = 1691FT + 164FT=1855FT NA = SOC altitude + HG1 + HG2 = FT + 149FT + 683FT = FT OCA(H) LPV A (1150) B (1160) C (1170) Figure 20 Turning Missed Approach Segment SBAS APV I (AE708-AE709) GNSS approach procedures for Bejaia Airport RWY26 Pag. 35

36 7.6.3 Turning Missed Approach Segment (AE709-AE711) LNAV Segment Data START END POINT Length (NM) Climb Gradient Course (000 ) POINT AE709 AE % 001 Turn Parameters Turning WP Turn Type Turn Direction Path & Terminator AE709 Fly-by Right TF Initial Altitude IAS (KT) Bank Angle ( ) Turn Angle ( ) Turn Gradient (%) AE OBST. Orographic + Vegetation Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) 36:46: N 004:57: E CONTROLLING OBSTACLE Elev. MOC Remarks d0 (shortest distance from obstacle to line K-K ) = 6.5NM HG = d0 * MA gradient = 6.5NM * 151.9FT/NM = 987FT RA = Controlling Obstacle + MOC = 1855FT + 164FT = 2019FT NA = SOC altitude + HG = 1400FT + 987FT = 2387FT Clearance from obst. OCA(H) LPV (1390) Figure 21 Turning Missed Approach Segment LNAV (AE709-AE711) visual filter 1641FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 36

37 7.6.4 Turning Missed Approach Segment (AE709-AE711) BARO-VNAV Segment Data START END POINT Length (NM) Climb Gradient Course (000 ) POINT AE709 AE % 001 Turn Parameters Turning WP Turn Type Turn Direction Path & Terminator AE709 Fly-by Right TF Initial Altitude IAS (KT) Bank Angle ( ) Turn Angle ( ) Turn Gradient (%) OBST. Orographic + Vegetation Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) 36:46: N 004:57: E CONTROLLING OBSTACLE Elev. MOC CAT Remarks The computation below refers to CAT C aircraft only: d0 (shortest distance from obstacle to line K-K ) = 8.4NM HG = d0 * MA gradient = 8.4NM * 151.9FT/NM = 1276FT RA = Controlling Obstacle + MOC = 1855FT + 164FT=2019FT NA = line K-K altitude + HG = FT FT = FT Clearance from Obst. OCA(H) LPV A (1260) B (1290) C (1320) Figure 22 Turning Missed Approach Segment BARO-VNAV (AE709-AE711) visual filter 1641FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 37

38 7.6.5 Turning Missed Approach Segment (AE709-AE711) SBAS APV I Segment Data START END POINT Length (NM) Climb Gradient Course (000 ) POINT AE709 AE % 001 Turn Parameters Turning WP Turn Type Turn Direction Path & Terminator AE709 Fly-by Right TF Initial Altitude IAS (KT) Bank Angle ( ) Turn Angle ( ) Turn Gradient (%) AE OBST. Orographic + Vegetation Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) 36:46: N 004:57: E CONTROLLING OBSTACLE Elev. MOC CAT Remarks The computation below refers to CAT C aircraft only: d0 (shortest distance from obstacle to line K-K ) = 7.9NM HG = d0 * MA gradient = 7.9NM * 151.9FT/NM = 1200FT RA = Controlling Obstacle + MOC = 1855FT + 164FT=2019FT NA = line K-K altitude + HG = 1178FT FT = 2378FT Clearance from Obst. OCA(H) LPV A (1150) B (1160) C (1170) Figure 23 Turning Missed Approach segment SBAS APV I (AE709-AE711) visual filter 1641FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 38

39 7.6.6 Turning Missed Approach Segment (AE711-AE701) Segment Data START END POINT Length (NM) Climb Gradient Course (000 ) POINT AE711 AE % 082 Turn Parameters Turning WP Turn Type Turn Direction Path & Terminator AE711 Fly-by Right TF Initial Altitude IAS (KT) Bank Angle ( ) Turn Angle ( ) Turn Gradient (%) OBST. Latitude Longitude (DD:MM:SS.SSSS DDD: MM:SS.SSSS ) CONTROLLING OBSTACLE Elev. MOC Clearance from obst. AE701 Altitude Remarks Turning Missed Approach protection areas (AE711-AE701) develops entirely over the sea. Figure 24 Turning Missed Approach segment (AE711-AE701) 7.7 Holding Missed Approach See par. 7.2 Initial Approach Holding. GNSS approach procedures for Bejaia Airport RWY26 Pag. 39

40 7.8 VSS Figure 25 VSS RWY26 The Visual Segment Surfaces associated to the Straight-in approach procedures and procedures with localizer look-alike lateral guidance (APV I) are not penetrated since developing entirely over the sea. GNSS approach procedures for Bejaia Airport RWY26 Pag. 40

41 8 SBAS FAS DATA BLOCK FPAP = RWY End for Approach RWY26 = THR08 Actually on the AIP-Algerie is not published the Geoid Undulation or the Ellipsoidal height of the THR08 (RWY End for RWY26). For the calculation of the FAS Data Block the up above missing data has been calculated by the NGA EGM96 Geoid Calculator and cross checked with the value obtained with the UNAVCO Geoid Height Calculator. Ellipsoidal height THR08 = 44.7M Figure 26 NGA EGM96 Ellipsoidal height THR08 Figure 27 UNAVCO Ellipsoidal height THR08 GNSS approach procedures for Bejaia Airport RWY26 Pag. 41

42 9 Procedures Overview Figure 28 LNAV RWY26 Overview GNSS approach procedures for Bejaia Airport RWY26 Pag. 42

43 Figure 29 BARO-VNAV RWY26 Overview GNSS approach procedures for Bejaia Airport RWY26 Pag. 43

44 Figure 30 SBAS APV I RWY26 Overview GNSS approach procedures for Bejaia Airport RWY26 Pag. 44

45 10 Minima Table Segment WPT Minima Right TAA AE701 AE FT Initial Approach Holding AE FT Central TAA AE FT AE702 Central TAA AE702 Subsector 7700FT Left TAA AE703 AE FT Right Initial Segment (AE701 AE706) 3400FT AE706 Central Initial Segment (AE702 AE706) 3400FT Left Initial Segment (AE703 AE704) AE704 (SDF) 4100FT Left Initial Segment (AE704 AE706) AE FT Intermediate Segment (AE706 AE707) AE FT Final Segment (AE707 AE708) AE708 (MAPt LNAV only) 1400FT OCA(H) A B C LNAV 1400(1390) LNAV/VNAV 1270(1260) 1300(1290) 1330(1320) LPV 1160(1150) 1170(1160) 1180(1170) Segment WPT Minima Turning Missed Approach Segment (AE708 AE701) AE FT GNSS approach procedures for Bejaia Airport RWY26 Pag. 45

46 Intentionally Blank GNSS approach procedures for Bejaia Airport RWY26 Pag. 46