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B. MultiScan Initialization Process
C. Left/Right Receiver-Transmitter Selection
D. Predictive Windshear Operation
E. Display Annunciations
F. Mode Controls
G. Test Procedures
H. Windshear Detection Features
I. Summary (Test Option)
V. MultiScan Manual Mode Operation
A. Manual Mode Selection
1. Airbus Control Panel
2. Boeing Control Panel
B. Ground Clutter Suppression Controls (Inoperative during Manual Mode)
C. Tilt Control Settings
1. Low Altitude Tilt
2. Takeoff Tilt
3. Descent Tilt
4. Mid-Altitude Tilt
5. High Altitude Tilt
D. Overscan Prevention Techniques
E. Summary (Test Option)
TCDS.A.014 Page 1/9
Is sue 02, 06 Febru ary 200 8
European Aviation Safety Agency
EASA
TYPE-CERTIFICATE
DATA SHEET
AIRBUS A300-600ST
Manufacturer:
AIRBUS
1 Rond-point Maurice Bellonte
31707 BLAGNAC - FRANCE
For model: A300F4-608ST
Issue 2, 06 February 2008
List of effective Pages:
Page 1 2 3 4 5 6 7 8 9
Issue 2 1 2 2 2 2 1 1 2
TCDS.A.014 Page 2/9
Is sue 02, 06 Febru ary 200 8
TABLE OF CONTENT
I. General......................................................................................................................................... 4
1. Aeroplane ........................................................................................................................... 4
II. Certification Basis ...................................................................................................................... 4
1. Reference Proposal Date for EASA Restricted TypeCertification ...................................... 4
2. French DGAC Special Certification Dates.......................................................................... 4
3. EASA Certification Basis .................................................................................................... 4
4. Special Conditions.............................................................................................................. 5
5. Equivalent Safety Findings ................................................................................................. 5
6. Environmental Standards ...................................................................................................5
III. Technical Characteristics and Operational Limitations......................................................... 5
1. Type Design Definition ....................................................................................................... 5
2. Maximum Certified Weights................................................................................................ 6
3. Centre of Gravity Range..................................................................................................... 6
4. Limit Speeds (Indicated Airspeed – IAS – unless stated otherwise) .................................. 6
5. Engines limitations.............................................................................................................. 6
6. Auxiliary power unit (APU).................................................................................................. 7
7. Fuel Tank Capacity (0.8 kg/litre)......................................................................................... 7
8. Fuel.................................................................................................................................... 7
9. Hydraulics.......................................................................................................................... 8
10. Tyres.................................................................................................................................. 8
11. Minimum Flight Crew.......................................................................................................... 8
12. Maximum number of occupants ......................................................................................... 8
13. Maximum Authorized Altitude............................................................................................. 8
14. Cargo compartment loading ............................................................................................... 8
15. Other Limitations ................................................................................................................ 8
16. Environmental Flight Envelope........................................................................................... 8
17. All Weather Capabilities ..................................................................................................... 8
18. Equipment .......................................................................................................................... 9
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