| IATA/ICAO CODE: |
SVO/UUEE |
| CITY: |
Moscow |
| COUNTRY: |
Russian Federation |
AIRPORT CONTACT
No changes reported by the airport in 2011
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: |
+7 495 737 53 91 |
|
| Email: |
aviationmarketing@svo.aero |
|
| Airport Web Site:
www.sheremetyevo-airport.ru |
ELEVATION: 630 ft.
|
RUNWAY INFORMATION
|
| Orientation |
Length (m)
|
Displaced
Threshold (m)
|
Glide Slope(deg)
|
Width (m)
|
| 07L/25R |
3550
|
-
|
-
|
60
|
| 07R/25L |
3700
|
-
|
-
|
60
|
NOISE ABATEMENT PROCEDURES
See AIP Russia for details.
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. General provisions
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 Runway 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:
- Runway 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 Runway 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 Runway 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 Reverse thrust power (with the exception of reverse idle thrust) shall be used only for safety reasons.
3. Runway 07L/R noise abatement approach procedures.
3.1 The noise abatement approach procedures are as follows: by the moment of reaching by aircraft the distance of 25.0 km from RWY threshold the crew must conduct the flight at (900) m AAL maintaining IAS 390 km/h and flight direction enabling to intercept ILS LOC coverage area providing approach-to-land on RWY 07L/R.
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 ILS LOC at a distance of 14 km from RWY 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 RWY threshold.
3.4 After this limit the speed shall be maintained as per the Aeroplane Flight Manual.
|
CONTINUOUS DESCENT ARRIVAL
(CDA) - NONE
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. |
|