| IATA/ICAO CODE: |
HAJ/EDDV |
| CITY: |
Hannover |
| COUNTRY: |
Germany |
AIRPORT CONTACT
Information updated by the airport 4/2008
| Name: |
Dr. Raoul Hille |
Michael Büsing |
| Title: |
Chief Executive Officer |
Airport Operations |
| Airport: |
Hannover Airport |
Hannover Airport |
Address:
|
Flughafen Hannover
Langenhagen GmbH
Postfach 42 02 80
30662 Hannover
Germany
|
Flughafen Hannover
Langenhagen GmbH
Postfach 42 02 80
30662 Hannover
Germany |
| Phone: |
+49 5 119 77 1919 |
+49 5 119 77 1388 |
| Fax: |
+49 5 119 77 1917 |
+49 5 119 77 1774 |
| Email: |
r.hille@hannover-airport.de |
m.buesing@hannover-airport.de |
| Airport Web Site: www.hannover-airport.de |
ELEVATION: 183 ft.
|
RUNWAY INFORMATION
|
| Orientation |
Length (ft)
|
Displaced
Threshold (ft)
|
Glide Slope(deg)
|
Width (ft)
|
| 09L/27R |
12467
|
984/984
|
09L/3
27R/2.9
|
148
|
| 09R/27L |
7677
|
-
|
09R/3
27L/3
|
148
|
| 09C/27C |
2559
|
196/558
|
-
|
75 (max 5.7 t MTOW)
|
NOISE ABATEMENT PROCEDURES
See AIP Germany ENR 1.5 for details of noise abatement
procedures.
Departures Chapter
2 Aircraft licensed in
accordance with ICAO Annex 16, Chapter 2:
Operation within the European Union is not permitted since April
1, 2002
Chapter 3
For aircraft licensed in accordance with ICAO Annex 16,
Chapter 3 as well as B737-200 as far as the noise levels for takeoff
pursuant to ICAO Annex 16, Chapter 3 have provably been reached
by supplementary equipment: |
Takeoff to 1500 feet AGL |
Takeoff power
Takeoff flaps
Climb at V2 + 10 KT (or as limited by body angle). |
At 1500 feet AGL |
Reduce power to not less than climb power.
Normal speed and flap retraction schedules to enroute climb |
Reverse Thrust
Reverse thrust other than idle thrust shall only be used to
an extent necessary for safety reasons. |
Arrivals
Pilots should arrange their flight so as to leave the initial approach
fix at a speed which permits operation of the aircraft in clean
configuration. This speed should be maintained until reaching a
distance of approximately 12 NM from touchdown. For this portion
of the approach, an indicated airspeed of 210 kt +/- 10 kt is recommended
unless a higher airspeed is required for performance reasons.
The subsequent portion of the approach up to a point shortly prior
to the Outer Marker should be flown at an airspeed of 160 kt +/-
10 kt using an intermediate flap setting as appropriate for the
type of aircraft concerned with the landing gear retracted. This
phase will normally include the transition from level flight to
descent on the glide path which should be intercepted at a height
of not lower than 2000 ft above touchdown zone elevation.
Landing configuration should be established shortly prior to or
over the Outer Marker, i.e. at this time the landing gear should
be extended, the flaps set for landing and the aircraft stabilized
at a safe approach speed. Reverse Thrust
Reverse thrust other than idle thrust shall only be used to an extent
necessary for safety reasons.
Reverse Thrust
Between 2000-0500 (1900-0400) reverse thrust other than idle
thrust shall only be used to an extent necessary for safety reasons.
Fuel -Saving and Noise-Reducing ILS Approach Procedures (based on
Nfl 1-78/96)
1. General
For the purpose of fuel-saving and noise abatement during approach,
the following procedure is announced. It may be requested by the
pilot or offered by the controller. It can be performed only in
connection with an ILS approach.
2. Procedure
2.1 Aircraft will be guided by Approach Control by means of radar
vectoring and will be cleared for a continuous descent to the
intermediate approach level in such a way that after reaching
this intermediate approach level on the localizer course, about
one NM will be left for intercepting the glide path in level flight.
This intermediate approach segment will serve to reduce speed.
It is assumed that the continuous descent will be performed at
a rate of 300 ft/NM (descent angle approx.3) down to the cleared
level.
If for specific reasons (e.g. separation, airspace structure,
obstacles), levels above the intermediate approach level have
to be assigned first, these restrictions will be lifted early
enough to allow a continuous descent at a rate of 300 ft/NM.
Details about the distance from touchdown will be transmitted
to the pilot together with the clearance for descent and usually
at 20, 15 and 10 NM from touchdown. This should enable the pilot
to correct the rate of descent as required.
2.2 In case of traffic situations allowing no CDA (e.g. approaches
of aircraft with different performance data), pilots will be informed
by the notice NO CDA POSSIBLE. In this case, approaches must be
conducted according to previous procedures.
3. Noise Abatement
On approaches in accordance with the CDA, pilots are expected
to continue using the approach techniques recommended for noise
abatement in the vicinity of airports.
4. The CDA Procedure may be used at the following airports:
Stuttgart - RWY 25 (Zwischenanflughohe/intermediate approach altitude
3500)
Nurnbert - RWY 10 (Zwischenanflughohe/intermediate approach altitude
4000)
RWY 28 (Zwischenanflughohe/intermediate approach altitude 4000)
Hamburg - RWY 23 (Zwischenanflughohe/intermediate approach altitude
3000)
RWY 05 (Zwischenanflughohe/intermediate approach altitude 3000)
RWY 15 (Zwischenanflughohe/intermediate approach altitude 3000)
Hannover - RWY 27L (Zwischenanflughohe/intermediate approach altitude
2000)
RWY 27R (Zwischenanflughohe/intermediate approach altitude 2000)
RWY 09L (Zwischenanflughohe/intermediate approach altitude 2000)
Munich - RWY 26L/R (Zwischenanflughohe/intermediate approach altitude
5000)
RWY 08L/R (Zwischenanflughohe/intermediate approach altitude 5000)
|
AIRPORT CURFEWS
| Local flying Restrictions
1. Between 2100 and 0500 (19 00 and 0400) flight operations exceeding
the noise levels pursuant to ICAO Annex 16, Volume 1 Chapter 3
are not permitted.
2. Between 2200 and 0500 (2100 and 0400) the following flights
and aircraft only are permitted:
2.1 Take-offs and landings of turbo-jet aircraft not exceeding
the noise levels pursuant to ICAO Annex 16 Volume 1 Chapter
3 and which are marked in the Attachment below which is part
of this regulation and shall be amended
|
| Attachment to
2.1 |
| All jet-propelled aircraft up to a MTOW of 25000kg
not exceeding the noise found in Annex 16 Chapter 3 pursuant to
ICAO as well as the following airplane types: |
| A300(all versions) |
B727-100 (3 tay engines) |
BAe146(all versions)AVRO-RJ-series |
| A310(all versions) |
B737-300/400/500/600/700/800 |
Fokker 100/70 |
| A320(all versions) |
B757(all versions) |
Gulfstream IV |
| A340(all versions) |
B767(all versions) |
L1011(all versions,only take-offs) |
| A319 |
B777 |
DC8-70 |
| A321 |
B747-400
Canadair RJ
Dash 8-400 |
DC10-30 and all versions of MD80 ( landings only)
DC 10 ( only take-offs ) |
A330
A340
B717 |
MD80(all versions, landings only) |
MD11(all versions)
MD90
Tupolev 204 |
Note: The times stated in brackets are applicable
during legal summer time.
Newly invented types of aircraft may be treated as listed in this
attachment as long as no other decision is made. |
PREFERENTIAL RUNWAYS
During night-hours 09L/27R
Between 2100 (2000) and 0500 (0400), take-offs and landings by aircraft
listed below may generally only be performed on the northern Runway
( 09L/27R). Exceptions to this regulation are permitted based on
compelling air traffic control reasons, meteorological reasons or
flight operational reasons. |
| Propeller aircraft with a MTOW of more than 5,7 t |
B737-200 |
MD DC10
MD DC 8-70 series |
| A300 (all versions) |
B757-300 |
MD11
MD80-series |
| A310 (all versions) |
B767 (all versions) |
MD90 |
| A330 |
B777 |
Tupolev 154 |
| A340 |
B747-400 |
Tupolev 204 |
| B727-100 re- engined with 3 tay engines |
L1011 |
|
OPERATING QUOTA - NONE
ENGINE RUN-UP RESTRICTIONS
| Run-up of jet engines other than idle run-ups are not permitted
between 2100-0500 (local time) out side the noise reduction shelter.
Between 2100-2300 (local time) as well as between 0300-0500 (local
time), runups of jet engines are permitted if required due to safety
reasons shortly before takeoff or after landing or for maintenance
purposes which cannot be postponed. (for more information see AIP
Germany AD2 EDDV 5./ 5.1/ 6. |
APU OPERATING RESTRICTIONS - NONE
NOISE BUDGET RESTRICTIONS - NONE
NOISE SURCHARGE
| 2/2008 IATA Airport and Air Navigation Charges Manual |
Landing Charge
Turbo Jet Powered A/C |
Aircraft over 2 tonnes - MTOW
International and Domestic
|
| Chapter 3 |
|
Included on Bonus List
|
EUR 7.15 per tonne |
|
Not included on Bonus List
|
EUR 16.20 per tonne |
| Night Surcharge (ICAO Annex 16 Chapter
3) |
Per flight (21:00 until 04:49) |
| Noise Category 1 (see attachment below) |
EUR 55.00 |
| Noise Category 2 |
EUR 120.00 |
| Noise Category 3 |
EUR 230.00 |
| Noise Category 4 |
EUR 380.00 |
| Noise Category 5 |
EUR 680.00 |
| Noise Category 6 |
EUR 1330.00 |
| Noise Category 7 |
EUR 2550.00 |
| Night Surcharge (ICAO Annex 16 Chapter
2) |
Per flight (21:00 until 04:49) |
| Noise Category 1 (see attachment below) |
EUR 130.00 |
| Noise Category 2 |
EUR 230.00 |
| Noise Category 3 |
EUR 440.00 |
| Noise Category 4 |
EUR 740.00 |
| Noise Category 5 |
EUR 1350.00 |
| Noise Category 6 |
EUR 2650.00 |
| Noise Category 7 |
EUR 5000.00 |
| Non-Annex 16 Aircraft |
EUR 62.00 per tonne |
|
Bonus List
|
| All types with MTOW below 25 tonnes, plus |
| A300 |
B727-100(3 Tay re-engined) |
DC8-70 |
| A310 |
B737-300 to 800 |
DC10 |
| A320 |
B747-400 |
MD11 |
| A330 |
B757 |
MD90 |
| A340 |
B767 |
Fokker 70/100 |
| A319 |
B777 |
AVRO RJ |
| A321 |
Gulfstream IV/V |
BAe 146 (all versions) |
| The allocation of aircraft into noise categories is
based on the average noise levels measured upon landing and take-off
of the observed aircraft types. Aircraft types not listed will be
classified at the airport's discretion on the basis of noise certificates
presented until satisfactory measurements results are available
to Hanover Airport. |
| Classification
of turbo-jet aircraft licensed according to ICAO Annex 16/3, propeller-driven
aircraft and helicopters |
| Noise Category
1:
LAZ to 69.9 dB(A) |
Noise Category
2:
LAZ 70.0 to 73.9 dB(A) |
Noise Category
3:
LAZ 74.0 to 76.9 dB(A) |
Noise Category
4:
LAZ 77.0 to 79.9 dB(A) |
| All Ch 3 jets with MTOW <34t |
A300 |
A330 |
AN 22 |
| All prop A/C with MTOW <34t |
A310 |
A340 |
BAC 111 hushkit |
| All Helicopters |
B727-100 re-eng. |
AN12 |
MD80-83, MD88 |
| A318, A319, A320 |
B767 |
B727 hushkit |
B747-S |
| B717 |
B737-400 |
DC8-70 Series |
B747-400 |
| B737-300, -500 to 900 |
DC6 |
DC9 hushkit |
DC10 |
| B757 |
IL18, IL 76 re-engined |
IL 96 |
TU154 |
BAe146/Avro RJ
CRJ7 |
TU204 |
MD 87 |
|
| Fokker 70/100 |
YK42/142 |
MD11 |
| Gulfstream IV/V |
A321 |
SC 5 (Shorts Belfast) |
| L188 |
|
C130 (Hercules) |
| C160/ND16 (Transall) |
B777 |
| MD 90 |
|
| |
| Noise Category
5:
LAZ 80.0 to 82.9 dB(A) |
Noise Category
6:
LAZ 83.0 to 85.9 dB(A) |
Noise Category
7:
LAZ 86.0 dB(A) and above |
| B747-100 to 300 |
|
AN124 |
| IL 62 |
| B727 Hushkit |
| |
| Classification
of turbo-jet aircraft licensed according to ICAO Annex 16/2
and turbo-jet aircraft not licensed in accordance with ICAO Annex
16 (military aircraft) |
| Noise Category
1:
LAZ to 69.9 dB(A) |
Noise Category
2:
LAZ 70.0 to 73.9 dB(A) |
Noise Category
3:
LAZ 74.0 to 76.9 dB(A) |
Noise Category
4:
LAZ 77.0 to 79.9 dB(A) |
| |
|
|
All Ch 2 jets with MTOW <34t |
| B747-S |
| DC 9 |
| C17 (Globemaster) |
| Fokker28 |
| Noise Category
5:
LAZ 80.0 to 82.9 dB(A) |
Noise Category
6:
LAZ 83.0 to 85.9 dB(A) |
Noise Category
7:
LAZ 86.0 dB(A)and above |
| B737-200 |
IL 86 |
AN 124 |
| B747-100 to 200 |
BAC 111 |
| IL 62 |
B727 |
| TU 134 |
C5 |
| TU 154 |
E 3 AWACS |
| DC8 (except -70 series) |
VC10 |
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
NOISE LEVEL LIMITS - NONE
CHAPTER 2 RESTRICTIONS
| Chapter 2 airplanes >75,000 lbs are banned from
operating at airports in EU Member States as of April 1, 2002. |
CHAPTER 2 PHASEOUT
|
From April 1, 2002 all civil subsonic jet aeroplanes >75,000
lbs operating at airports in EU Member States must comply with
the standards specified in Part II, Chapter 3, Volume 1 of Annex
16 in accordance with EU Council Directive 92/14/EEC.
|
CHAPTER 3 RESTRICTIONS
| See Airport Curfew Information. |
|