| IATA/ICAO CODE: |
LGG/EBLG |
| CITY: |
Grâce-Hollogne |
| COUNTRY: |
Belgium |
AIRPORT CONTACT
No changes reported by the airport in 2008
Verify information below with the airport.
| Name: |
|
| Title: |
Airport Authority |
| Airport: |
Liège Airport |
Address:
|
Ministere wallon de l'Equipment et des
Transports
Direction de l'aeroport de Liege
B - 4460 Grâce-Hollogne
Belgium |
| Phone: |
+32 4 234 84 07 |
| Fax: |
+32 4 234 84 08 (Airport Authority) |
| Email: |
liegeairport@sab.be |
| Airport Web Site:
www.liegeairport.com |
ELEVATION: 659 ft
|
RUNWAY INFORMATION
|
| Orientation |
Length (m)
|
Displaced
Threshold (m)
|
Glide Slope(deg)
|
Width (m)
|
| 23L/05R |
3287
|
5R(237 m)
|
3
|
45
|
| 23R/05L |
2340
|
-
|
3
|
45
|
Displaced THR 05R: 236 m
RWY 05L / 23R is a secondary RWY available for operational needs
in VMC and CAT. I but also usable as TWY (designation TWY B) - double
lighting according to the use.
Runway 23L is available for CAT. III operations
Main Runway 05R/23L extended to 3700(m) - completion due 2004 |
NOISE ABATEMENT
PROCEDURES
a. General
Noise abatement take-off and climb procedures are applicable for
whatever runway-in-use and for SID's.
b. Climb gradient :
In order to minimize noise disturbance and to clear obstacles in
the departure area, aircraft shall maintain a net climb gradient
of not less than 5.8 % until passing 3600 ft QNH. |
| c. Turbo-jet powered aircraft
|
- From take-off to 2100 ft QNH :
|
* take-off power;
* take-off flaps
* climb to V2 + 10 or 20 kt or as limited by body angle |
| - At 2100 ft QNH : |
* reduce thrust to not less than climb thrust |
| - From 2100 ft QNH to 3600 ft QNH: |
* climb at V2 + 10 or 20 kt. |
- At 3600 ft QNH :
|
* accelerate smoothly to the en-route
climb speed with flaps retraction. |
| Propeller aircraft |
- From take-off to 1600 ft QNH :
|
* take-off power;
* climb at a maximum gradient compatible with safety;
* speed not less than single engine climb speed nor higher than
best rate of climb speed |
- At 1600 ft QNH :
|
* reduce power to the normal operating
power if this power has been used for showing compliance with the
noise certification requirements or to the maximum climb power. |
|
- From 1600 ft QNH to 3600 ft QNH:
|
* climb at the maximum gradient with reduced
power, maintaining constant speed |
- Above 3600 ft QNH :
|
* accelerate smoothly to the en-route
climb speed. |
| Use of reverse thrust : the reverse thrust
should be kept to a minimum compatible with the safety of the aircraft. |
AIRPORT CURFEWS
| See Chapter 2 and Chapter 3 restrictions below. |
PREFERENTIAL RUNWAYS
OPERATING QUOTA
| The maximum number of movements/hour is 20. |
ENGINE RUN-UP RESTRICTIONS
| Full power engine test runs are prohibited from 2100-0900 local
time. |
APU OPERATING RESTRICTIONS - NONE
NOISE BUDGET RESTRICTIONS - NONE
NOISE SURCHARGE
Note: The information shown below for Chapter
2 airplanes is for historical purposes only as landing and takeoff is
forbidden.
| Landing Charge |
Basis: MTOW |
| Liege |
EUR 5.49 per tonne |
| Chapter 2 Aircraft |
|
|
Between 2300 and 0700
|
50% Surcharge |
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
FLIGHT
TRACK MONITORING SYSTEM -
NONE
NOISE LEVEL LIMITS
| The principle of the repression against noise pollution generated
by the airline traffic is into force by the Walloon Region decree
dated 2001, 08 June.
Noise level limits by area, based on Noise Exposition Map, and
are :
| AREA |
LAeq (1s) MAX |
| B |
87 dBA |
|
C
|
82 dBA |
|
D
|
77 dBA |
Penalties will are 200 to 7500 EUR / offense.
Rules, limits and penalties table are published in the Walloon
Region decree dated 2004, 29 January.
|
CHAPTER 2 RESTRICTIONS
| 1.3 Recertificated Civil Subsonic Jet
Aircraft*
Recertificated civil subsonic jet aircraft are banned from 2200
to 0600 UTC. However, their operation authorized during this period
until 1 July 2002 provided those aircraft have been operated before
the Nov. 8, 2000 decree, entered into force.
* Recertificated civil subsonic jet aircraft are aircraft that
were initially certificated to Chapter 2 or equivalent standards
or initially not noise certificated but have been modified to
meet Chapter 3 standards either directly through technical measures
or indirectly through operational restrictions. Airplanes which
initially could only be dual certificated to the standards of
Chapter 3 by means of weight restrictions, have to be considered
as re certificated airplanes. Airplanes that have been modified
to meet Chapter 3 standards by being completely re-engine with
engines having a by- pass ration of three or more are not to be
considered re certificated airplanes.
There are exceptions to this regulation for operations related
to missions in case of disasters or for the purpose of medical
assistance, military missions, flights on which there is immediate
danger to the life or health of persons as well as animals and
flights diverted to the airport for meteorological reasons.
Exceptionally and on explicit justified request, the Minister
of Transport may authorize a take-off or landing of an aircraft
that is banned by virtue of para above.
|
CHAPTER 2 PHASEOUT
CHAPTER 3 RESTRICTIONS
| 1.3 Recertificated Civil Subsonic Jet
Aircraft*
Recertificated civil subsonic jet aircraft are banned from 2200
to 0600 UTC. However, their operation authorized during this period
until 1 July 2002 provided those aircraft have been operated before
the Nov. 8, 2000 decree, entered into force.
* Recertificated civil subsonic jet aircraft are aircraft that
were initially certificated to Chapter 2 or equivalent standards
or initially not noise certificated but have been modified to
meet Chapter 3 standards either directly through technical measures
or indirectly through operational restrictions. Airplanes which
initially could only be dual certificated to the standards of
Chapter 3 by means of weight restrictions, have to be considered
as re certificated airplanes. Airplanes that have been modified
to meet Chapter 3 standards by being completely re-engine with
engines having a by- pass ration of three or more are not to be
considered re certificated airplanes.
There are exceptions to this regulation for operations related
to missions in case of disasters or for the purpose of medical
assistance, military missions, flights on which there is immediate
danger to the life or health of persons as well as animals and
flights diverted to the airport for meteorological reasons.
Exceptionally and on explicit justified request, the Minister
of Transport may authorize a take-off or landing of an aircraft
that is banned by virtue of para above. |
|