Sheremetyevo Airport

IATA/ICAO CODE: SVO/UUEE
CITY: Moscow
COUNTRY: Russian Federation

AIRPORT CONTACT

No changes reported by the airport in 2009
Verify information below with the airport.
Name: Mikhail M Vasilenko Vladimir A Buryak
Title:
Airport Director Director of Operations
Airport: Sheremetyevo Airport  
Address:


Sheremetyevo Airport
141400 Moscow
Khimky Town
Russia
Phone:
+7 495 232 65 65, +7 495 578 91 01,
+7 495 578 01 08
+7 495 578 38 00
Fax: +7 495 578 01 08  
Email: aviationmarketing@svo.aero  
Airport Web Site: www.sheremetyevo-airport.ru/

ELEVATION: 630 ft.
RUNWAY INFORMATION
Orientation
Length (ft)
Displaced
Threshold (ft)
Glide Slope(deg)
Width (ft)
07L/25R
11647
-
-
262
07R/25L
12149
-
-
197

NOISE ABATEMENT PROCEDURES

Noise abatement procedures are divided into two parts:

1. Noise abatement procedures during take-off and climbing phase.
2. Noise abatement procedures during approach phase.

Noise Abatement Procedures During Take-off and Climbing Phase:

1.1 Noise abatement procedures during take-off and climbing phase shall be executed by crews of all aircraft.

1.2 Noise abatement procedures shall not be executed at the expense of reduction of flight safety.

1.3 Noise abatement procedures shall not be executed in case of one of the aircraft engines failure during take-off phase

1.4 RWY 07L/R are noise preferential, and shall be used to the maximum possible degree.

2. Restrictions.
2.1 Take-off of aircraft with tail-wind component up to 5 m/sec is allowed under the following conditions:

- RWY is dry or damp;
- friction coefficient is 0.5 or more;
- cross-wind component is not more than 5 m/sec.

2.2 During take-off from RWY 25L/R on take-off heading and maximum possible climb gradient aircraft shall proceed to D 2.1 km DME MR 114.6 then immediate right turn onto assigned heading. It is strictly prohibited to reduce the track of 340°MAG until intersecting QDM 227° Ivanovskoye NDB UM 405 or reaching D 6.0 km DME MR 114.6 unless it is required for further flight safety.

2.3 During take-off from RWY 07L/R on take-off heading and maximum possible climb gradient aircraft shall proceed to distance of 7.2 km DME MR 114.6, then immediate left turn onto track 045°MAG.

2.4 The changing of flight course of the aircraft after take-off is permitted only after reaching flight height of (120) m above aerodrome level.

2.5 Turn of aircraft at flight height from (120) m to (300) m above aerodrome level shall be executed with a bank not exceeding 15°, from height (300) m to (900) m – 20°.

2.6 Turn of aircraft at flight height of (900) m AAL shall be executed with 25° bank or with angular rate of turn 3°/sec.

2.7 The minimum indicated air speed during steady shall not be less than V2+20 km/h (10 kt) or less than that prescribed in the Aeroplane Flight Manual if it has greater value.

2.8 The maintaining of the minimum indicated air speed of climb is not required if it brings to exceeding the maximum permissible angle of attack.

2.9 The reduction of engines power shall not be applied until:

- the established standard power mode enables with maximum certified take-off mass to maintain the established climb gradient of not less than 4% at a speed specified above in para 2.8 and 2.9;

- take-off flight path provides overflying of all obstacles located under flight path with sufficient clearance both when all engines are operating normally and also taking into account possible engine failure and time period necessary for the rest engines to develop full power.

2.10 “AIR-GROUND” communication shall be reduced to absolute minimum during initial departure phase.

3. Noise abatement procedures during climbing phase.
The crews of aircraft shall apply two noise abatement procedures during climbing phase:

- noise abatement departure procedure near the aerodrome (NADP 1);
- noise abatement departure procedure far from the aerodrome (NADP 2).

The pilot-in-command may use any of them for reaching necessary effect (ICAO Doc 8168, Volume I, Part V, Chapter 3)

Noise Abatement Procedures During Approach Phase
1. General provisions.

1.1 Noise abatement procedures during approach phase shall be executed by crews of all aircraft.

1.2 If special meteorological conditions, such as considerable wind speed, cumulo-nimbus clouds and etc. are present in arrival and approach sectors, ATS unit may at its own discretion or by a pilot-in-command's request deviate from the provisions of par. 2.1 given below if it deemed necessary for safety reasons.

1.3 RWY 25L/R are noise preferential, and shall be used to the maximum possible degree.

1.4 The crews of aircraft shall maintain the prescribed STAR routes, and in case of deviation – join the assigned track immediately.

2. Restrictions.

2.1 The required noise abatement procedures shall not be observed over the overflown areas in the following cases:

a) if there are ice, slush, water or mud, rubber, oil and etc. on RWY and friction coefficient is 0.4 or less;

b) under meteorological conditions when cloud ceiling is less than 150 m or horizontal visibility is less than 1800 m;

c) when a cross-wind component on RWY (including gusts) exceeds 7 m/sec (15 kt);

d) when a tail-wind component on RWY exceeds 2.5 m/sec (5 kt);

e) when wind shear is forecasted or reported, or it is expected that unfavourable weather conditions (for example, thunderstorms) may influence aircraft approach and landing.

2.2 Directly before final approach excessive rates of descent should be avoided when leaving the holding areas or leaving the assigned altitude.

2.3 The change of configuration and speed of flight connected with noise abatement procedures shall be carried out in accordance with the requirements of the Aeroplane Flight Manual of the given aircraft type.

2.4 During instrument as well as visual approach it is not allowed to fly bellow the ILS glide path angle.

2.5 No noise abatement procedures shall envisage the increasing of indicated air speed of descent.

2.6 A displacement of THR shall not be used as a noise abatement measure.

2.7 Not to distract the crew's attention during the execution of noise abatement procedures, “AIR-GROUND” communication shall be reduced to a minimum.

2.8 Landing of aircraft with a tail-wind component up to 5 m/sec is allowed under the following conditions:

- RWY is dry or damp;
- friction coefficient is 0.5 or more;
- cross-wind component is not more than 5 m/sec.

2.9 Reverse thrust power (with the exception of reverse idle thrust) is used only for safety reasons.

3. RWY 07L/R noise abatement approach procedures.

3.1 The noise abatement approach procedures are the following: by the moment of reaching by aircraft the distance of 25.0 km from threshold the crew shall conduct
the flight at (900) m AAL maintaining IAS 390 km/h and flight direction enabling to intercept ILS LOC operational area providing RWY 07L/R approach-to-land.

3.2 From a distance of 22 km the crew shall reduce IAS from 390 km/h to 340±20 km/h in order to intercept LOC at a distance of 14 km from threshold descending to height (600) m.

3.3 After glide path interception at height (500)m the crew shall continue to reduce IAS in such way that it should be 290 km/h by the moment of reaching (450) m at
a distance of 8 km from threshold.

3.4 After this limit the speed shall be maintained as
per the Aeroplane Flight Manual.

AIRPORT CURFEWS - NONE

PREFERENTIAL RUNWAYS
See Noise Abatement Procedures.

OPERATING QUOTA - NONE

ENGINE RUN-UP RESTRICTIONS

 yes

APU OPERATING RESTRICTIONS - NONE

NOISE BUDGET RESTRICTIONS - NONE

NOISE SURCHARGE - NONE

NOISE MITIGATION/LAND USE PLANNING PROGRAM INFORMATION
Type of Program
Date Implemented
Status
Sound Insulation (Residences and Public Buildings)
-
-
Purchase Assurance for Homeowners Located Within the Airport Noise Contours
-
-
Avigation Easements
-
-
Zoning Laws
-
-
Real Estate/Property Disclosure Laws
-
-
Acquire Land for Noise Compatibility to date
-
-
Population within each noise contour level relative to aircraft operations
-

-

Airport Noise Contour Overlay Maps
-
-
Total Cost of Noise Mitigation Programs to Date
-

-

Source of Noise Mitigation Program Funding for Aircraft Noise
-
-

NOISE MONITORING SYSTEM - NONE

FLIGHT TRACK MONITORING SYSTEM - NONE

NOISE LEVEL LIMITS
City territory adjoining an airport is divided into thee zones:

Zone 1: night noise limited to 80 dBA and day noise to 90 dBA.
Zone 2: all buildings must be sound proofed
Zone 3: all housing construction is banned.

CHAPTER 2 RESTRICTIONS - NONE

CHAPTER 2 PHASEOUT

This airport is located in a country that is an ICAO Contracting State. It is not known if this country adopted the ICAO recommendation (Resolution A28-3) for the phase out of Chapter 2 airplanes.

CHAPTER 3 RESTRICTIONS - NONE

COMMENTS
Annex 16 noise type certification standards were adopted in 1972.

Flight operating procedures have been adopted for each type of plane in the USSR (CIS).

City territory adjoining an airport is divided into thee zones:
Zone 1: night noise limited to 80 dBA and day noise to 90 dBA.
Zone 2: all buildings must be sound proofed
Zone 3: all housing construction is banned.

Effective Jan 1979, fleet acquisitions must meet Annex 16. An ICAO Working Group D questionaire response indicated the USSR (CIS) fleet is in compliance with Annex 16.