曝光台 注意防骗
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? Arrange medical assistance after landing giving many details about the condition of the affected crewmember
Second phase
? Prepare the approach and read the checklist earlier than usual
? Request radar vectoring and prefer a long approach to reduce workload
? Perform the landing from the fit pilot usual seat.
SUPPLEMENTARY
INFORMATION
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SUPPLEMENTARY INFORMATION
PRELIMINARY PAGES
TABLE OF CONTENTS
SI-PLP. PRELIMINARY PAGES
TABLE OF CONTENTS 1/2
SUMMARY OF HIGHLIGHTS 1/2
SI-010. ADVERSE WEATHER
general 1/16
cold weather operations and icing conditions 1/16
turbulence 8/16
windshear 10/16
volcanic ash 14/16
SI-020. FLYING REFERENCE
GENERAL 1/4
THE ATTITUDE 1/4
THE FLIGHT PATH VECTOR 1/4
GO AROUND 4/4
SI-030. NAVIGATION ACCURACY
GENERAL 1/8
COMPUTATION OF THE AIRCRAFT POSITION 1/8
USE OF FMS 3/8
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
TABLE OF CONTENTS
SI-070. USE OF RADAR
GENERAL 1/4
FUNCTIONS 1/4
OPERATIONAL RECOMMENDATIONS FOR WEATHER DETECTION 3/4
OTHER OPERATIONNAL RECOMMENDATION 4/4
SUMMARY OF HIGHLIGHTS
Localization
Title Page ID Reason
SI-060
TECHNICAL BACKGROUND 1/4 1 To update the aural warning :"TRAFFIC TRAFFIC"
SUMMARY OF HIGHLIGHTS
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SUPPLEMENTARY INFORMATION
ADVERSE WEATHER
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.
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