| IATA/ICAO CODE: |
CMN/GMMN |
| CITY: |
Casablanca |
| COUNTRY: |
Morocco |
AIRPORT CONTACT
No changes reported by the airport in 2011
Verify information below with the airport
| Name: |
El Hamdani Jilali |
Alaoui Abdellah |
Title:
|
Airport Director |
Director of Operations |
| Airport: |
Casablanca - Mohammed V International
Airport |
Address:
|
Office National Des Aeroports
Aeroport Casablanca/Mohammed V
B.P. 52 Casablanca/Nouasser 20240
Morocco |
| Phone: |
+212 5 22 53 9040 |
|
| Fax: |
+212 5 22 53 90 51 |
Email:
|
|
| Airport Web Site: www.onda.ma/onda/fr |
ELEVATION: 656 ft.
| RUNWAY
INFORMATION |
| Orientation |
Length (m) |
Displaced
Threshold (m) |
Glide Slope(deg) |
Width (m) |
| 17L/35R |
3720 |
- |
- |
45 |
| 17R/35L |
3720 |
- |
- |
45 |
NOISE ABATEMENT PROCEDURES
See AIP Maroc for details.
1. Aircraft use restrictions
Turbojet aeroplanes are to comply with the climb procedures shown below:
- Maintain the speed V2 +10 (or that which allows aircraft attitude, depending on the type of aircraft) up to 3000 ft with flaps set in the take-off configuration.
- Maintain the take-off power until 1500 ft, then reduce climbing power until 3000 ft.
2. Aerodrome use restrictions
a) Use restrictions by night:
For take-off from 2300 – 0600 UTC and with a tailwind component less than or equal to 7 Kts, the RWY 17L or 17R is to be used.
If for operational reasons RWY 17L or 17R cannot be used, upon pilot request, at engine start up, an other QFU may be attributed with additional delays.
b) Engine test
Engine test shall not be done except in areas assigned by the Control Tower and after authorization of this one.
c) Conditions of RWY use
- Take-off
From 0600 to 2300 and with a tailwind component less than or equal to 7 Kts, RWY 35R must be used. If for operational limitation reasons RWY 35R or35L cannot be used, upon pilot request, at engine start up, an other QFU may be attributed with additional delays.
- Landing
- RWY 35 R or 35L must be used until a tailwind component less than or equal to 7 Kts.
- when the landing is only possible on RWY 17R or 17L, 2 cases shall be considered:
1st case: ceiling more or equal than 1500 ft/ ground and the visibility more than or equal to 5000m.
Instrument procedure of RWY 35R or 35L is used followed by a right down-wind for RWY 17L or 17R.
2nd case: ceiling less than 1500 ft/ground.
The instrument procedure of RWY 17L or 17R is used.
|
CONTINUOUS DESCENT ARRIVAL
(CDA) - NONE
AIRPORT CURFEWS - NONE
PREFERENTIAL RUNWAYS - NONE
OPERATING QUOTA - NONE
ENGINE RUN-UP RESTRICTIONS
| Engine test runs may not be conducted in areas other than those
assigned by ATC and only with ATC persmission. |
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 - NONE
CHAPTER 2 RESTRICTIONS - UNKNOWN
CHAPTER 2 PHASEOUT - UNKNOWN
CHAPTER 3 RESTRICTIONS - NONE
|