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AIRCRAFT POSITION AWARENESS AND OPERATIONAL CONSEQUENCES............................................... 4/8
SI-040 ZFW - ZFCG ENTRY ERRORS
general.................................................................................................................................................................1/4
technical background.......................................................................................................................................... 1/4
entry error and operational consequences...........................................................................................................2/4
operational recommendations.............................................................................................................................4/4
SI-050 CENTRE OF GRAVITY
PREFACE..........................................................................................................................................................1/10
MECHANICAL ASSUMPTIONS........................................................................................................................1/10
INFLUENCE OF THE CENTER OF GRAVITY ON THE AIRCRAFT PERFORMANCE.................................... 1/10
Influence of the CG on the Structure and Handling Characteristics...................................................................3/10
THE CG AND TRIM POSITION....................................................................................................................... 9/10
SI-060 TCAS
TECHNICAL BACKGROUND............................................................................................................................. 1/4
OPERATIONAL RECOMMENDATION.................................................................................................................2/4
A330/A340 FLIGHT CREW TRAINING MANUAL
SUPPLEMENTARY INFORMATION
PRELIMINARY PAGES
TABLE OF CONTENTS
A330/A340 FLEET SI-PLP-TOC P 2/2
FCTM 17 JUN 09
SI-070 USE OF RADAR
GENERAL .......................................................................................................................................................... 1/6
FUNCTIONS........................................................................................................................................................1/6
OPERATIONAL RECOMMENDATIONS FOR WEATHER DETECTION.............................................................4/6
OTHER OPERATIONNAL RECOMMENDATION.................................................................................................5/6
A330/A340 FLIGHT CREW TRAINING MANUAL
SUPPLEMENTARY INFORMATION
PRELIMINARY PAGES
SUMMARY OF HIGHLIGHTS
A330/A340 FLEET SI-PLP-SOH P 1/2
FCTM 17 JUN 09
Localization
Title
Page ID Reason
SI-060
TECHNICAL BACKGROUND
1/4 1 To update the aural warning :"TRAFFIC TRAFFIC"
A330/A340 FLIGHT CREW TRAINING MANUAL
SUPPLEMENTARY INFORMATION
PRELIMINARY PAGES
SUMMARY OF HIGHLIGHTS
Intentionally left blank
A330/A340 FLEET SI-PLP-SOH P 2/2
FCTM 17 JUN 09
A330/A340 FLIGHT CREW TRAINING MANUAL
SUPPLEMENTARY INFORMATION
ADVERSE WEATHER
A330/A340 FLEET SI-010 P 1/16
FCTM 17 JUN 09
GENERAL
Applicable to: ALL
Adverse weather operations take into account the following aspects:
• Cold weather operations and icing conditions
• Turbulence
• Windshear
• Volcanic ash.
COLD WEATHER OPERATIONS AND ICING CONDITIONS
Applicable to: ALL
PREFACE
Aircraft performance is certified on the basis of a clean wing. Ice accretion affects wing
performance. When the wing is clean, the airflow smoothly follows the shape of the wing. When
the wing is covered with ice, the airflow separates from the wing when the Angle-Of-Attack (AOA)
increases. Therefore, the maximum lift-coefficient is reduced. As a result, the aircraft may stall at a
lower AOA, and the drag may increase.
The flight crew must keep in mind that the wing temperature of the aircraft may be significantly
lower than 0 °C, after a flight at high altitude and low temperature, even if the Outside Air
Temperature (OAT) is higher than 0 °C. In such cases, humidity or rain will cause ice accretion on
the upper wing, and light frost under the wing. (Only 3 mm of frost on the under side of the wing
tank area is acceptable.)
EXTERIOR INSPECTION
When icing conditions on ground are encountered, and/or when ice accretion is suspected, the
Captain should determine, on the basis of the exterior inspection, whether the aircraft requires
ground deicing/anti-icing treatment. This visual inspection must take into account all vital parts of
the aircraft, and must be performed from locations that offer a clear view of these parts.
　
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