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Jeddah Approach [OEJN_X_APP]

This section details all the necessary Standard Operating Procedures for Approach Operations in King Abdulaziz International Airport (OEJN)


1. General Provisions

Jeddah Approach Control (APP/FIN) is tasked with handling the arrival and departure of aircraft at King Abdulaziz International Airport within the Terminal Manevouring Area (TMA). Their responsibility includes maintaining adequate spacing and order to ensure safe and efficient operations.


2. Airspace

The Jeddah Terminal Manevouring Area (TMA) is an airspace classified as Class C that reaches up to FL195. This airspace encompasses the entirety of Jeddah city and the adjacent mountainous region within a 60 nautical mile radius.

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Figure 1.1 - Jeddah TMA

2.1 Aerodromes Covered

The Jeddah TMA comprises King Abdulaziz International Airport (OEJN) and King Faisal Naval Base (OEJF).

King Faisal Naval Base (OEJF) is a controlled naval airbase that features an Aerodrome Traffic Zone (ATZ) surrounding the airport's vicinity.

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Figure 1.2 - King Faisal ATZ

2.2 Airspace Sectorization

2.2.1 Lateral View

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Figure 1.3 - Jeddah TMA Sectorization - Lateral View

2.2.2 Vertical View

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Figure 2.3 - Jeddah TMA Sectorization - Vertical View

2.3 Surrounding Airspace

2.3.1 Lateral View

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Figure 2.3 - Surrounding Airspaces - Lateral view

2.3.2 Vertical View

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Figure 2.3 - Surrounding Airspaces - Vertical view

2.4 Restricted Airspace

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Figure 1.4 - Restricted Areas

2.4.1 Prohibited Areas

A prohibited area is a designated area above a country's land or territorial waters where aircraft flight is completely prohibited at all times under any circumstances.

Identification & NameVertical LimitsRemarks
OEP01 MAKKAHSFC - UNLPermanent. Makkah.

Table 1.1 - Prohibited Areas in the Jeddah TMA

2.4.2 Restricted Areas

Restricted airspace is a designated area above a state's land or territorial waters where aircraft flights are regulated based on specific conditions. Civil aircraft can fly in this airspace only if certain requirements are met, such as specified times, meteorological conditions, or special permissions.

Identification & NameVertical LimitsRemarks
OER18B JEDDAHSFC - 1000FT AGLPermanent.
OER18A JEDDAHSFC - 1000FT AGLPermanent.
OER11 JEDDAHSFC - 5000FT AMSLPermanent.
OER12 JEDDAHSFC - 5000FT AMSLPermanent.

Table 1.2 - Restricted Areas in the Jeddah TMA

2.4.3 Areas of Danger

A danger area is a specified area where activities posing a risk to aircraft flight may occur at certain times. This term is used when the potential danger does not warrant the airspace being classified as restricted or prohibited. By designating a danger area, operators and pilots are cautioned to assess the risks and take responsibility for ensuring the safety of their aircraft.

Identification & NameVertical LimitsRemarks
OED14B OEJNSFC - 1500FT AMSLMilitary. VFR helicopter operation.
OED14A OEJNSFC - 1500FT AMSLMilitary. VFR helicopter operation.
OED105 OEJNSFC - 1800FT AMSLFiring. Permanent

Table 1.2 - Areas of Danger in the Jeddah TMA

2.5 Minimum Radar Vectoring Altitude (MRVA)

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Figure 1.8 - Minimum Radar Vectoring Altitudes

2.6 Transitional Layer

The transitional layer in the Jeddah TMA is between 13000ft and FL150.


3. ATS Positions

The following are the ATS Positions relevant to this document. They will be subsequently denoted by their stated abbreviations.

Radio CallsignLogon CallsignAbbreviationFrequency
Jeddah TowerOEJN_1_TWRAIR 1118.200
Jeddah TowerOEJN_2_TWRAIR 2118.500
Jeddah ApproachOEJN_APPAPP 1124.000
Jeddah Final EastOEJN_FE_APPFIN E123.800
Jeddah Final WestOEJN_FW_APPFIN W124.675
Jeddah Final Monitor ControlOEJN_FMC_APPFMC 1125.850
Jeddah Terminal ControlOEJN_1_CTRCTR 1125.450
Jeddah Terminal ControlOEJN_2_CTRCTR 2119.100
Jeddah ControlOEJD_1_CTRACC 1126.500
Jeddah ControlOEJD_1_CTRACC 2133.900

Table 1.3 - ATS Positions


4. Designated Areas of Responsiblity (DAOR)

4.1 34s DDRO/SDRO Configuration

In any 34 Configuration, APP 1 covers the two parts of the TMA, while APF E handles the 34 FIN SEC East and APF W manages the 34 FIN SEC West.

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Figure 1.6 - DOAR 34 Configuration

4.2 16s DDRO/SDRO Configuration

In any 16 Configuration, APP 1 covers the two sections of the TMA as usual, APF E is responsible for the 16 FIN SEC East and APF W is responsible for the 16 FIN SEC West.

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Figure 1.6 - DOAR 16 Configuration

4.3 Standard Connection Hierarchy

Controllers must log in the following order to maintain realizm and follow SOPs:

  • APP 1 [OEJN_APP]
  • APF E [OEJN_FE_APP]
  • APF W [OEJN_FW_APP]
  • FMC 1 [OEJN_FMC_APP]

This hierarchy of connection must always be followed unless ATS staff explictly permit you to do otherwise.


5. General Separation Minimas

5.1 Surveillance-Based Separation

Unless specified in 6.1.6.1, aircraft flying within the Jeddah TMA must maintain a horizontal separation of at least 3 nautical miles. If this distance cannot be achieved, a minimum vertical separation of 1000 feet should be maintained.

Controllers are required to give suitable speed and altitude directives, along with control over the aircraft's lateral path, to guarantee the necessary separation standards are upheld.

5.2 Wake Turbulence Separation

The correct Wake Turbulence Separation (WTS) minimum must always be enforced between aircraft operating below 6000 feet in the following situations:

  • When an aircraft is flying directly behind another at the same altitude or less than 1000 feet below.
  • If both aircraft are utilizing the same runway, except as specified in 6.1.6.1.
  • When an aircraft is crossing behind another aircraft at the same altitude or less than 1000 feet below.

6. Procedures

The below procedures are considered as standard and no coordination is required to employ them, except where explicitly required.

caution

Should a situation arise that does not match any of the below cases, coordinate an arrangement with the affected agencies

6.1 Arrival Procedures

6.1.1 STAR Allocation

STARs are issued by CTR 1/2, or if unavailable, issued by ACC 1/2. The Center always assigns the preferred STARs, typically RNAV STARs with a PTM (Point to Merge) when feasible.

Runways, approaches, and transitions are issued by the approach controller. If the approach controller desires an alternative assignment, they should coordinate this through VCCS with the appropriate enroute controller.

6.1.1.1 Preferred STARs 34s Configuration
Entry PointVEMEMMISAMNOMDAMOVULBOSUTEGMEG
Preferred Arrival (34R)VEMEM2NMISAM2NNOMDA2NMOVUL2NBOSUT2NEGMEG2N
Preferred Arrival (34L)VEMEM2LMISAM2LNOMDA2LMOVUL2LBOSUT2LEGMEG2L

Table 1.6 - Preferred STARs 34s Configuration

6.1.1.2 Preferred STARs 16s Configuration
Entry PointVEMEMMISAMNOMDAMOVULBOSUTEGMEG
Preferred Arrival (16R)VEMEM2RMISAM2RNOMDA2RMOVUL2RBOSUT2REGMEG2R
Preferred Arrival (16L)VEMEM2SMISAM2SNOMDA2SMOVUL2SBOSUT2SEGMEG2S

Table 1.7 - Preferred STARs 16s Configuration

6.1.2 Approach and Runway Assignment

Upon initial contact with an aircraft, the aircraft should be assigned the arrival runway and the expected approach type.

APP 1: “SVA449, JEDDAH APPROACH, EXPECT ILS APPROACH RUNWAY 34R, INFORMATION F, [FURTHER INSTRUCTIONS]”

tip

If the pilot has correctly noted the ATIS information during their initial contact, the controller is not required to reiterate it.

6.1.2.1 Instrument Approach

In general, the ILS approach is the favored approach type. Nevertheless, aircraft may be instructed to perform a visual approach based on the conditions specified in 6.1.2.2.

RNAV approaches are accessible but should only be utilized if requested by the pilot or due to circumstances like ILS unavailability.

6.1.2.2 Visual Approach

Visual approaches can be initiated by the Approach (APP) controller or requested by the pilot. When a pilot agrees to a visual approach, they are confirming their ability to maintain safe terrain clearance visually and accept responsibility for ensuring a safe landing interval behind the preceding aircraft.

APP can initiate a visual approach under the following conditions:

  • The Pilot concurs.
  • Pilot reports sighting the preceding aircraft and agrees to maintain their own separation.
  • A caution about potential wake turbulence has been issued where necessary.

If the minimum wake turbulence separation cannot be upheld, controllers may propose a visual approach to enable pilots to maintain visual or wake turbulence separation from preceding traffic.

Be careful!!

An aircraft conducting a visual approach cannot participate in simultaneous independent parallel approaches. During BUSY Independent Parallel Approaches (Mode 1) Operations, visual approaches are discouraged.

6.1.2.3 Change of Approach Type/Runway

Controllers should not initiate a change of approach type or runway within 30 nautical miles of touchdown. However, pilots are allowed to request a change of approach type or runway at any point.

Beware!

In Jeddah, Standard Terminal Arrival Routes (STARs) are specific to each runway, meaning a single STAR CANNOT be utilized for multiple runways. If a runway change is required, the current STAR must be canceled, and radar vectors provided instead. This practice is strongly discouraged to maintain operational efficiency and safety.

6.1.3 Point To Merge System

The Point to Merge System (PTM) is engineered to operate effectively under heavy traffic conditions without the need for radar vectoring. It is built around a specific P-RNAV route framework that includes a merge point and pre-defined, equidistant sequencing legs from that merge point.

Why is it so important?

Jeddah relies entirely on this system to manage traffic sequencing onto the downwind leg, which is relatively short in the area. As a result, the system is heavily utilized to ensure that aircraft are properly sequenced before reaching the downwind.

Substitution

If using a STAR with a PTM is not practical/possible, we resort to holding patterns, transitions, or vectors for sequencing.

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Figure 1.9 - Point To Merge

6.1.3.1 PTM Rules

The Point Merge System is structured symmetrically, with uniform rules that facilitate the calculation and separation of traffic. The key principles are as follows:

  • Each waypoint in the sequencing is equidistant from the merge point;
  • The distances between the fixes on the sequencing legs are the same;
  • Overlapping PTMs with two arrival flows have altitude restrictions that ensure a vertical separation of at least 1,000 feet to maintain the minimum separation requirements

These principles ease the calculation and sequencing for the controller.

6.1.4 Descent Profile

When giving descend instructions, the approach controller must mention weather the pilot must descend via the star or descend unrestricted for the first altitude.

If you want to descend via the STAR:

Controller: SVA123, Descend via the STAR, FL170

If you want to descend unrestricted:

Controller: SVA123, Descend unrestricted, FL170

Change of Profile

If you would like to chenge the descend from via the STAR you can use the phrasesolgy below:

Controller: SVA123, Continue descend, unrestricted, FL150

6.1.4.1 Initial Segment of the STAR
6.1.4.1.1 34 Configuration - Right Downwind (34R)
ArrivalDescend ProcedureAdditional Notes
VEMEM2NCTR 2: FL190 by VEMEM
APP 1: FL170 on the sequencing leg
APP 1: FL150
APP 1: Leaving IMDAP, 13000ft
APP 1: 9000ft by OBTUG
APP 1: 7000ft by PUSPO, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
FL160 can be given as appropriate in the PTM.
MOVUL2NCTR 1: FL190 by MOVUL
APP 1: FL170 on the sequencing leg
APP 1: 13000ft by GINKU
APP 1: Leaving GINKU, 7000ft by PUSPO, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
MISAM2NCTR 2: FL170/FL150 by MISAM
APP 1: FL150 on the sequencing leg
APP 1: Leaving IMDAP, 13000ft
APP 1: 9000ft by OBTUG
APP 1: 7000ft by PUSPO, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
NOMDA2NCTR 1: FL190 by NOMDA
APP 1: FL170 on the sequencing leg
APP 1: FL150
APP 1: Leaving NIVGO, 13000ft
APP 1: 9000ft by OBTUG
APP 1: 7000ft by PUSPO, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
EGMEG2NCTR 1: FL170/FL190 by EGMEG
APP 1: FL170
APP 1: Leaving ULULU, 10000ft
APP 1: Leaving JN917, 8000ft
APP 1: 7000ft, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
BOSUT2NCTR 1: 13000ft by BOSUT
APP 1: 10000ft
APP 1: 6000ft, Handoff to APF E
Further with APF E. Refer to Section 6.1.4.2.
ULULU2NxIMLER1NCTR 1: 13000ft by BOSUT
APP: Clearance for ULULU2N via IMLER1N.
APP 1: 13000ft by ULULU
APP 1: Leaving ULULU, 10000ft
APP 1: 8000ft
APP 1: Leaving JN920, 7000ft, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
IMLER1N Transition
Holds over ULULU as necessary for sequencing.

Table 2.9 - Descent Profile - Right Downwind (34R)

6.1.4.1.2 34 Configuration - Left Downwind (34L)
ArrivalDescend ProcedureAdditional Notes
VEMEM2LCTR 2: FL190 by VEMEM
APP 1: FL170
APP 1: Leaving RABEP, FL150
APP 1: Leaving IMDAP, 11000ft
APP 1: 11000ft by OBTUG
APP 1: Leaving OBTUG, 7000ft
APP 1: Past Midfield and clear of the DEPs, 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
FL160 can be given as appropriate in the PTM.
MOVUL2LCTR 1: FL190 by MOVUL
APP 1: FL170
APP 1: FL150
APP 1: 10000ft by GINKU
APP 1: 8000ft
APP 1: 6000ft, Handoff to APF W by TOTNU



Further with APF W. Refer to Section 6.1.4.2.
MISAM2LCTR 2: FL170/FL150 by MISAM
APP 1: FL150 on the sequencing leg
APP 1: 13000ft
APP 1: 11000ft by OBTUG
APP 1: Leaving OBTUG, 7000ft
APP 1: Past Midfield and clear of the DEPs, 6000ft, Handoff to APF W


Further with APF W. Refer to Section 6.1.4.2.
NOMDA2LCTR 1: FL190 by NOMDA
APP 1: FL170
APP 1: Leaving JN789, FL150
APP 1: Leaving NIVGO, 13000ft
APP 1: 10000ft by GINKU
APP 1: 8000ft
APP 1: 6000ft, Handoff to APF W by TOTNU

Further with APF W. Refer to Section 6.1.4.2.
EGMEG2LCTR 1: FL150 by EGMEG
APP 1: 13000ft
APP 1: 11000ft
APP 1: 8000ft
APP 1: 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
ULULU2LxTADMA1LCTR 1: FL150 by EGMEG
APP 1: Clearance for ULULU2L via TADMA1L transition.
APP 1: 13000ft
APP 1: 11000ft
APP 1: 6000ft by ULULU
APP 1: Overhead ULULU, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
TADMA1L Transition
Holds over ULULU as necessary for sequencing
If the traffic will be entering the holding, descend to the MHA (10000)
BOSUT2LCTR 1: 13000ft by BOSUT
APP 1: 8000ft
APP 1: 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
ULULU2LxTAPSU1LCTR 1: 13000ft by BOSUT
APP 1: Clearance for ULULU2L via TAPSU1L transition.
APP 1: 11000ft
APP 1: Passing REXED, 6000ft
APP 1: Overhead ULULU, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
TAPSU1L Transition
Holds over ULULU as necessary for sequencing
If the traffic will be entering the holding, descend to the MHA (10000)

Table 3.0 - Descent Profile - Left Downwind (34L)

6.1.4.1.3 16 Configuration - Left Downwind (16L)
ArrivalDescend ProcedureAdditional Notes
VEMEM2SCTR 2: FL150 by VEMEM
APP 1: 13000ft
APP 1: 10000ft by IMDAP
APP 1: Leaving IMDAP, 6000ft, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
MOVUL2SCTR 2: FL150 by MOVUL
APP 1: 13000ft
APP 1: 11000ft/7000ft
APP 1: 5000ft, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
MISAM2SCTR 2: 13000ft by MISAM
APP 1: 11000ft on the sequencing leg
APP 1: 10000ft by IMDAP
APP 1: Leaving IMDAP, 6000ft, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
NOMDA2SCTR 1: FL150 by NOMDA
APP 1: 13000ft on the sequencing leg
APP 1: 11000ft
APP 1: 6000ft, Handoff to APF E by NABGI

Further with APF E. Refer to Section 6.1.4.2.
EGMEG2SCTR 1: FL150 by EGMEG
APP 1: 13000ft
APP 1: 12000ft
APP 1: 9000ft
APP 1: 7000ft
APP 1: Past Midfield/Clear of DEPs 6000ft, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
BOSUT2SCTR 1: FL190
APP 1: FL160
APP 1: FL150
APP 1: 11000ft
APP 1: 8000ft till ITOMA
APP 1: 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
ULULU2SxIMLER1SCTR 1: FL190 at BOSUT
APP 1: Clearance for ULULU2S Via IMLER1S Transition
APP 1: FL160
APP 1: 12000ft
APP 1: 9000ft
APP 1: 7000ft
APP 1: Past MIdfield/Clear of DEPS, 6000ft, Handoff to APF E

Further with APF E. Refer to Section 6.1.4.2.
IMLER1L Transition
Cleared for the BOSUT2S by CTR
Holds over ULULU as necessary for sequencing
If the traffic will be entering the holding, descend to the MHA (9000)

Table 3.1 - Descent Profile - Left Downwind (16L)

6.1.4.1.4 16 Configuration - Right Downwind (16R)
ArrivalDescend ProcedureAdditional Notes
VEMEM2RCTR 2: FL150 by VEMEM
APP 1: 13000ft on the sequencing leg
APP 1: 10000ft by IMDAP
APP 1: 8000ft
APP 1: 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
MOVUL2RCTR 2: FL150 by MOVUL
APP 1: 13000ft
APP 1: 11000ft/6000ft
APP 1: 4000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
MISAM2RCTR 2: 13000ft by MISAM
APP 1: 11000ft on the sequencing leg
APP 1: 10000ft by IMDAP
APP 1: 8000ft
APP 1: 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
NOMDA2RCTR 1: FL150 by NOMDA
APP 1: 13000ft on the sequencing leg
APP 1: 11000ft
APP 1: 6000ft, Handoff to APF W by NABGI

Further with APF W. Refer to Section 6.1.4.2.
EGMEG2RCTR 1: FL150 by EGMEG
APP 1: 13000ft
APP 1: 8000ft
APP 1: Past Midfield/Clear of DEPs 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
BOSUT2RCTR 1: FL190
APP 1: FL150
APP 1: 11000ft
APP 1: 8000ft till GEVUS
APP 1: 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
ULULU2RxIMLER1RCTR 1: FL190 at BOSUT
APP 1: Clearance for ULULU2R Via IMLER1R Transition
APP 1: FL160
APP 1: 12000ft
APP 1: 8000ft
APP 1: Past Midfield/Clear of DEPS, 6000ft, Handoff to APF W

Further with APF W. Refer to Section 6.1.4.2.
IMLER1R Transition
Cleared for the BOSUT2R by CTR
Holds over ULULU as necessary for sequencing
If the traffic will be entering the holding, descend to the MHA (9000) or as appropriate

Table 3.1.1 - Descent Profile - Right Downwind (16R)

6.1.4.2 Final Segment of the STAR

The Downwind till final of the star is defined as the final segment. This part of the star is with the appropriate APF Controller.

Do note

The final segment of the STAR descend profile is really variable depending on the sequence's leg, the amount of traffic, and much more. Use this as the standard profile but adjust as appriorpraite ensuring separation requirmenets are met

6.2.4.2.1 34s Configuration - Downwind - Suggested Descents
LegDescent ProfileMandatory Altitudes
Right Downwind (34R)Generally ODD (7000ft, 5000ft)For ILS Z 34R (Vectors), maintain a minimum altitude of 5000ft on the downwind, typically assigned at ITOMA, to avoid the MRVA of 4200 when canceling the STAR for vectors. For ILS Y (IAF ITOMA), descend to 3000ft at ITOMA.
Left Downwind (34L)Generally EVEN (8000ft, 6000ft, 4000ft)N/A

Table 3.2 - 34s Configuration - Suggested Descents

do note

This may be adjusted to accommodate more traffic during high traffic operations.

6.2.4.2.2 16s Configuration - Downwind - Suggested Descents
LegDescent ProfileMandatory Altitudes
Right Downwind (16R)Generally EVEN (8000ft, 6000ft, 4000ft)Nil.
Left Downwind (16L)Generally ODD (7000ft, 5000ft)Nil.

Table 3.3 - 16s Configuration - Suggested Descents

do note

This may be adjusted to accommodate more traffic during high traffic operations.

6.1.5 Lateral Profile

6.1.5.1 Standard Shortcuts'

When provided by APP 1, direct routings/shortcuts for arrivals in any configuration should only lead to a merge point when employing a point-to-merge system, or to one of the downwind fixes for sequencing in coordination with the respective APF controller.

6.1.5.2 Sequencing/Horizontal Separation

Traffic entering the downwind should be separated horizontally by a minimum of 7nm.

6.1.6 Speed Control

Aircraft should ideally be provided with speeds according to section 5.1 to ensure separation. If necessary for maintaining distance between aircraft, speeds within the appropriate range can be utilized, ensuring that maximum or minimum speeds for each segment are not exceeded.

To ease the workload of controllers, aircraft may be directed to adhere to the specified speeds on the STAR.

Example: “SVA499, MAINTAIN STAR SPEEDS”

Arrival segmentRecommend/Published SpeedSpeed Range
TMA Entry250280-230
On the Point to Merge250/230250-220
Approaching Downwind220;this must be enforced before handing off traffic to APF230-220
On Downwind210230-190
Turning Base/Base190200-180
10NM from Touchdown170-190160-190
4NM from Touchdown160160

Table 3.6 - Speed Control

It is advised to adhere to recommended speeds from the downwind leg onward to avoid affecting turn radius and rate, potentially leading to a localizer overshoot. Consistent speeds also give controllers more time to manage aircraft on the downwind leg effectively.

For aircraft on a straight-in approach from the initial STAR fix, speed control is unnecessary until the aircraft aligns with the final approach course, or if needed for separation purposes. However, it is advisable to instruct traffic to maintain a maximum speed of 190 knots at 10 nautical miles from the landing threshold to ensure approach stabilization criteria are met.

In the TMA, higher speeds may be allowed if the aircraft does not anticipate turns exceeding a 30-degree course change in any arrival segment, and if the traffic volume and controller workload permit such speeds.

6.1.7 Final Approach Sequencing

6.1.7.1 Standard Vectors
RunwayBase LegIntercepting Vector
34L070010 (340-010)
34R250310 (340 - 310)
16L250190 (160-190)
16R070130 (160-130)

Table 3.4 - Standard Vectors

6.1.7.2 Platform Altitudes
RunwayPlatform Altitude
34L2700
34R2100
16L1700
16R2700

Table 3.5 - Platform Altitudes

6.1.8 Independent Parallel Approaches (Mode 1)

Independent Parallel Approaches (Mode 1) involves the simultaneous use of parallel instrument runways without requiring radar separation between aircraft utilizing adjacent ILS systems. This operational method is highly efficient and facilitates high traffic volume.

In independent parallel approaches, significant attention is placed on the altitude levels at which the glide path or vertical path is intercepted (referred to as "high side" and "low side"), and the necessity to adhere to these levels until the aircraft is established on both the final approach course and glide path.

6.1.8.1 Separation Requirements

A vertical separation of 1000 feet or 5nm horizontally must be maintained between aircraft until:

  • The aircraft is aligned with the Localizer/Inbound Course, and
  • Enters the Normal Operating Zone (NOZ).
tip

Following the High/Low Side procedure and descending aircraft to the corresponding High/Low Side Altitudes as outlined in section 6.1.8.2.1 automatically ensures this separation.

Once these conditions are met and the aircraft is within 10 nautical miles, diagonal or vertical separation is no longer necessary

6.1.8.2 High/Low Side

A set of parallel approaches includes a designated "high side" and "low side" for vectoring purposes, ensuring vertical separation until aircraft are aligned with their respective parallel ILS localizer courses.

The low side altitude should be chosen so that the aircraft becomes aligned with the ILS localizer course well in advance of intercepting the ILS glide path. The high side altitude should be maintained at least 300 meters (1,000 feet) above the low side altitude until 18 kilometers (10 nautical miles) from the threshold.

To achieve this, aircraft should be descended to the appropriate high or low side altitude specified in section 6.1.8.2.1.

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Figure 2.0 - High/Low Side

6.1.8.2.1 High/Low Side Altitudes

The altitudes for the "high side" and "low side" must be assigned to aircraft before or at the time of the base instruction.

APF: SVA123, Descend 3000ft, Turn Right Heading 070, Base Leg

DO NOTE!! VERY IMPORTANT

Aircraft can always maintain or ascend to the high side altitude as this action only enhances vertical separation. HOWEVER, for the low side altitude, aircraft must already be descending or positioned at the lower altitude before initiating the base turn to guarantee that separation does not decrease below 1000 feet.

ApproachSideAltitude
ILS 34RHigh4000ft
ILS 34LLow3000ft
ILS 16RHigh3000ft
ILS 16LLow2000ft

Table 3.7 - High/Low Side Altitudes

6.1.8.3 Radar Vectoring

When vectoring aircraft to intercept the ILS localizer course, the final vector must allow the aircraft to approach the localizer course or final approach track at an angle not exceeding 30 degrees, as per standard vectors outlined in section 6.1.5.1.

Additionally, there should be a minimum of 1.0NM of straight and level flight before intercepting the ILS localizer course. The vectors should ensure that the aircraft is aligned with the ILS localizer course or MLS final approach track in level flight for at least 2NM before intercepting the ILS glide path.

Traffic MUST be cleared on the localizer initially, then cleared to descend via the glide after entering the NOZ and on the correct localizer course.

This indicates that aircraft must be established on the localizers no later than:

ApproachAltitudeEstablished on the LOC Before
ILS 34R4000ft (High Side)14NM
ILS 34L3000ft (Low Side)11NM
ILS 16R3000ft (High Side)11NM
ILS 16L2000ft (Low Side)8NM

Table 3.8 - High/Low Side Altitudes

6.1.8.4 Non Transgression Zone (NTZ)

Since radar separation is not provided between traffic on adjacent extended runway centre lines in Mode 1 approaches, there must be an established means of determining when an aircraft deviates too far from the ILS localizer course or the MLS final approach track. This is achieved through the concept of the NTZ.

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Figure 4.1 - NTZ/NOZ

6.1.8.4.1 Normal Operating Zone (NOZ)

The Normal Operating Zone, illustrated in Figure 4.1, is the designated region near the localizer where an aircraft is considered secure and on its approach path. To enable independent parallel approaches, aircraft must remain within the NOZ.


6.2 Departures Procedures

6.2.1 Climb Profile

6.2.1.1 Climb Procedure - 34 Configuration
DepartureClimb ProcedureAdditional Notes
BOMOX2WAPP: 6000ft till clear of the arrivals/till JN276
APP: Even levels up till FL200
Handoff Passing FL160
MIGDA2WAPP: 6000ft till clear of the arrivals/till JN276
APP: Even levels up till FL200
Handoff Passing FL160
DATAP2WAPP: 6000ft till clear of the arrivals/till JN276
APP: 12000ft till JN510/Clear of NOMDA ARRs
APP: FL160
Handoff Passing 13000ft
If climb to 12000ft was given prior to JN510 and track miles permit, APP may issue even levels till FL200.
EGREP2WAPP: 6000ft till clear of the arrivals/till JN276
APP: 12000ft till JN520/Clear of NOMDA ARRs
APP: FL160
Handoff Passing 13000ft
If climb to 12000ft was given prior to JN520 and track miles permit, APP may issue even levels till FL200.
ISLAM2WAPP: 6000ft till clear of the arrivals/till JN276
APP: 12000ft
Handoff after clear of PTMs
KAROX2WAPP: 6000ft till clear of the arrivals/till JN276
APP: 12000ft till JN610/Clear of NOMDA ARRs
APP: Even levels up till FL200
Handoff Passing FL160
RIBAM2WAPP: 6000ft till clear of the arrivals/till JN276
APP: 8000ft till JN522/Clear of ULULU ARRs
APP: 12000ft till JN521/Clear of ULULU ARRs
APP: Even levels up till FL200
Handoff Passing FL160
EGPOB3VAPP: 6000ft till clear of the arrivals/till JN276
APP: 8000ft till JN522/Clear of ULULU ARRs
APP: 12000ft till JN521/Clear of ULULU ARRs
APP: Even levels up till FL200
Handoff Passing FL160
BOMOX3VAPP: 6000ft till clear of the arrivals/till RIBIL
APP: 12000ft till Clear of NOMDA ARRs
APP: Even levels up till FL200
Handoff Passing FL160
MIGDA3VAPP: 6000ft till clear of the arrivals/till RIBIL
APP: 12000ft till Clear of NOMDA ARRs
APP: Even levels up till FL200
Handoff Passing FL160
DATAP3VAPP: 6000ft till clear of the arrivals/till RIBIL
APP: Even levels up till FL200 (Unrestricted)
Handoff Passing FL160
EGREP3VAPP: 6000ft till clear of the arrivals/till RIBIL
APP: Even levels up till FL200 (Unrestricted)
Handoff Passing FL160
ISLAM3VAPP: 6000ft till clear of the arrivals/till JN236
APP: 12000ft
Handoff after clear of PTMs
KAROX3VAPP: 6000ft till JN236
APP: Even levels up till FL200
Handoff Passing FL160 and clear of ARRs
Traffic must be given the highest altitude (FL200) immediately after JN236 if traffic permits
RIBAM3VAPP: 6000ft till JN236
APP: Even levels up till FL200
Handoff Passing FL160 and clear of ARRs
Traffic must be given the highest altitude (FL200) immediately after JN236 if traffic permits
EGPOB3VAPP: 6000ft till JN236
APP: Even levels up till FL200
Handoff Passing FL160 and clear of ARRs
Traffic must be given the highest altitude (FL200) immediately after JN236 if traffic permits

Table 3.9 - Climb Procedure - 34 Configuration

6.2.2 Lateral Profile

6.2.2.1 Standard Shortcuts

Direct routings can used as appropriate when traffic levels are low.

Do note

THEY MUST NOT BE USED IN HIGH TRAFFIC SCENARIOS.

6.2.2.1.1 Standard Shortcuts - 34s Configuration
DepartureStandard ShortcutsAdditional Notes
BOMOX2WNo direct routings permitted
MIGDA2WNo direct routings permitted
DATAP2WDirect to JN510 if traffic permits
EGREP2WDirect to JN520 if traffic permits
ISLAM2WNo direct routings permitted
KAROX2WFrom JN276/JN254 to NIVBA if above 5000ft and traffic permits
RIBAM2WFrom JN276/JN254 to NIVBA if above 5000ft and traffic permits
EGPOB3WFrom JN276/JN254 to NIVBA if above 5000ft and traffic permits
BOMOX3VNo direct routings permitted
MIGDA3VNo direct routings permitted
DATAP3VNo direct routings permitted
EGREP3VNo direct routings permitted
ISLAM3VNo direct routings permitted
KAROX3VNo direct routings permitted
RIBAM3VNo direct routings permitted
EGPOB3VNo direct routings permitted

Table 5.9 - Standard Shortcuts - 34 Configuration

6.2.2.2 Sequencing/Horizontal Separation

Approach should strive to transfer traffic with a minimum of 8-10 nautical miles in trail, and increasing.

6.2.3 Speed Control

For departing aircraft, speed control can be issued as needed, with a maximum speed of 280 to 300 knots.

Higher Speed

In Class C airspace below 10,000 feet, aircraft are required to maintain speeds of 250 knots or lower. If you wish to grant unrestricted climb and encourage a higher speed, you can communicate the following message:

APP 1: "SVA123, High Speed Approved"

do note

When assigning a speed greater than 250 knots to an aircraft below 10,000 feet in Class C airspace, you do not need to provide a specific "high speed" instruction. Simply state the speed that has been assigned.


6.3 Handoff Procedures

Handoffs should always be made between 2000 and 5000 feet before reaching the assigned altitude.

6.3.2 Arrivals

Entry Point:From:To:Notes
MISAMJeddah Terminal Control East (CTR 2)Jeddah Approach (APP 1)CTR 1 when 2 is offline.
VEMEMJeddah Terminal Control East (CTR 2)Jeddah Approach (APP 1)CTR 1 when 2 is offline.
NOMDAJeddah Terminal Control West (CTR 1)Jeddah Approach (APP 1)
MOVULJeddah Terminal Control West (CTR 1)Jeddah Approach (APP 1)
EGMEGJeddah Terminal Control West (CTR 1)Jeddah Approach (APP 1)
BOSUTJeddah Terminal Control West (CTR 1)Jeddah Approach (APP 1)

Table 4.2 - Handoff Procedure - Arrivals

6.3.3 Departures

Exit Point:From:To:Notes
EGREPJeddah Approach (APP 1)Jeddah Terminal Control East (CTR 2)CTR 1 when 2 is offline.
ISLAMJeddah Approach (APP 1)Jeddah Terminal Control East (CTR 2)CTR 1 when 2 is offline.
BOMOXJeddah Approach (APP 1)Jeddah Terminal Control West (CTR 1)
MIGDAJeddah Approach (APP 1)Jeddah Terminal Control West (CTR 1)
DATAPJeddah Approach (APP 1)Jeddah Terminal Control West (CTR 1)
KAROXJeddah Approach (APP 1)Jeddah Terminal Control West (CTR 1)
RIBAMJeddah Approach (APP 1)Jeddah Terminal Control West (CTR 1)

Table 4.3 - Handoff Procedure - Departures


7. Final Approach Monitering (OEJN_FMC_APP)

The Jeddah Final Monitoring Control (FMC) is responsible for monitoring traffic when the 1000ft vertical separation is reduced.

FMC verifies that when the 1,000 ft vertical separation is decreased:

  • Aircraft do not enter the depicted No Transgression Zone (NTZ).
  • The appropriate minimum longitudinal separation between aircraft on the same ILS localizer course is preserved.

7.1 Termination of Radar Monitering

Radar monitoring should not be terminated until:

  • Visual separation is implemented, ensuring that both radar controllers are informed whenever visual separation is applied; or
  • The aircraft has landed, or in the event of a missed approach, is a minimum of 1.0 NM beyond the departure end of the runway and maintains sufficient separation from any other traffic.
do note

There is no requirement to advise the aircraft that radar monitoring is terminated.

7.2 Infringement of NTZ

When an aircraft is seen deviating from the ILS localizer course towards the No Transgression Zone (NTZ) and remains in the Normal Operating Zone (NOZ), ATC will instruct the aircraft to promptly return to the correct ILS localizer course using the following phraseology:

FMC: “OBSERVING YOU ARE LEFT (or RIGHT) OF THE LOCALIZER (or FINAL APPROACH COURSE), TURN RIGHT (or LEFT) IMMEDIATELY AND REJOIN THE LOCALIZER”

7.2.1 Break-Out Maneuver

When FMC observes an aircraft penetrating or about to penetrate the No Transgression Zone (NTZ), they will first instruct the aircraft on the adjacent ILS localizer course to adjust their course to avoid the deviating aircraft, using the following phraseology:

FMC: “Break-Out Alert, (callsign), turn (Left or Right), Immediately Heading (3 digits), Climb (or descend) to (altitude)”

do note

No heading instruction will be issued when aircraft is below 400 feet.


8. Holding Procedures

There are five primary published holding stacks located within the Jeddah Terminal Maneuvering Area (TMA). These stacks are used for holding arriving aircraft or as part of the missed approach procedures for certain instrument approaches.

use with caution

In the Jeddah Terminal Maneuvering Area (TMA), holdings should be considered the final option for sequencing aircraft. Radar vectors, speed adjustments, direct routing, and using PTM are significantly more efficient methods for managing aircraft traffic flow.

8.1 Holding Stacks in the Jeddah TMA

Holding FixRadial/DMEUse
IMDAPJDW R-053/25DMERNAV STAR RWYs 34C/34L/34R and 16C/16L/16R
IMDAPJDW R-053/25DMEMissed approach holding for RWY34R & RWY34C & RWY16L & RWY16C
ULULUJDW R-208/20DMERNAV STAR RWYs 34C/34L/34R and 16C/16L/16R
ULULUJDW R-208/20DMEMissed approach holding for RWY16R
RADKIJDWR-302/18DMEMissed approach holding for ILS Z or LOC RWY 34L

Table 5.6 - Published Holding Stacks

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Figure 5.6 - Published Holding Stacks