| IATA/ICAO CODE: |
STR/EDDS |
| CITY: |
Stuttgart |
| COUNTRY: |
Germany |
AIRPORT CONTACT
Information updated by the airport 4/2009
Name:
|
Martin Hofmann |
Georg Fundel |
Title:
|
Head of Business Air Cargo |
Director |
| Airport: |
Stuttgart Airport |
Stuttgart Airport |
Address:
|
Flughafen Stuttgart GmbH
Postfach 23 04 61
D-70624
Stuttgart
Germany |
| Phone: |
+ 49 7 11 948 3288 |
|
| Fax: |
+ 49 7 11 9482 2442 |
|
Email:
|
Hofmann@airport-stuttgart.de |
|
| Airport Web Site:
www.flughafen-stuttgart.de |
ELEVATION: 1267 ft.
|
RUNWAY INFORMATION
|
| Orientation |
Length (m)
|
Displaced
Threshold (m)
|
Glide Slope(deg)
|
Width (m)
|
| 07/25 |
3345
|
-
|
-
|
45
|
NOISE ABATEMENT PROCEDURES
See AIP Germany ENT 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 transition to en route climb |
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 other than idle thrust shall
only be used to an extent unavoidable for safety reasons. |
CONTINUOUS DESCENT ARRIVAL
(CDA)
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)
Nurnberg - 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
|
NIGHTTIME OPERATIONS
2.1.1 Take-off and landing
From 2100-0600 LT, civil jet aircraft are not permitted to take-off
or land.
Prop aircraft: 24h/7days, no restrictions
2.1.2 Exceptions
Excepted from the restrictions of 2.1.1 are:
a. take offs of airplanes with a noise certificate according to
Chapter 3
of Annex 16 relating to the ICAO agreement from from 0500 (0400)
until 0600 (0500)LT and from 2000 (2100) until 2200 (2100)
b. landings of airplanes with a noise certificate according to
Chapter 3
of Annex 16 relating to the ICAO agreement from 0500 (0400) until
0600 (0500)LT and from 2100 (2000) until 2230 (2130)
c. landings in the case of delays by airplanes according to 2.2b
if the planned time of arrival is before 2230 (2130) and the delayed
landing is conducted by 2300 (2200)
d. take-offs and landings of airplanes
- in the night airmail service of the Deutsche Post AG however,
only with airplanes in possession of a noise certificate according
to ICAO Annex 16, Chapter 3
- using the airport as an emergency or alternate airport for meteorological,
technical or other safety reasons.
- on a mission in disasters or rendering medical assistance
- conducting flight checks for the unit responsible for air navigation
services.
Deviating from the restrictions in 2.1.1, the approving authority
may grant exceptions in justified individual cases for the airport
or, according to their specifications, for the Aviation Supervision
Office at Stuttgart Airport, if this seems necessary in the public
interest, especially to maintain the safety of air traffic or to
avoid disturbance to air traffic. |
PREFERENTIAL RUNWAYS - NONE
OPERATING QUOTA - NONE
ENGINE RUN-UP RESTRICTIONS:
Test runs and run-ups of engines are generally permitted between
0500 (0400) and 2100 (2200) only.
Test runs and run-ups of jet engines are permitted only after prior
consent and on special instruction by Aviation Supervision Office. |
APU OPERATING RESTRICTIONS - NONE
NOISE BUDGET RESTRICTIONS - NONE
NOISE 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
8 stations, Burell and Kajer
Monitoring used to check mandatory strict adherence to takeoff routing
procedures. Computer controlled system for continuous monitoring,
installed in 1969, measures time that a given threshold level (different
for each station, date, etc.) was exceeded. Stations are symmetrically
located about the axis of the main runway with Station 4 used to
measure the effects of reverse thrust. The previous system was replaced
in 1998. |
FLIGHT
TRACK MONITORING SYSTEM - NONE
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 - NONE
|