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8.0 CONCLUSIONS/RECOMMENDATIONS--------------------------------------------------25
8.1 Conclusions---------------------------------------------------------------------------------------------------------------------26
8.2 Recommendations--------------------------------------------------------------------------------------------------------------27
Revision 14.0 3
Appendix A Effects Of Additional Thrust On Windshear Recovery---------------------------28
Evaluation of Engine Effects on Takeoff Performance in Windshear using the A320
Simulator----------------------------------------------------------------------------------------------28
I. Overview----------------------------------------------------------------------------------------------------------------------------29
II. Equipment Description----------------------------------------------------------------------------------------------------------29
III. Data Acquisition-----------------------------------------------------------------------------------------------------------------29
IV. Findings / Results --------------------------------------------------------------------------------------------------------------29
V. Conclusions / Recommendations--------------------------------------------------------------------------------------------30
Evaluation of Engine Effects on Takeoff Performance in Windshear in the B-777----32
I. Overview----------------------------------------------------------------------------------------------------------------------------33
II. Equipment Description----------------------------------------------------------------------------------------------------------33
III. Data Acquisition-----------------------------------------------------------------------------------------------------------------33
IV. Findings / Results --------------------------------------------------------------------------------------------------------------33
V. Conclusions / Recommendations--------------------------------------------------------------------------------------------34
Evaluation of Engine Effects on Windshear Recoveries in the B-777 --------------------35
I. Overview----------------------------------------------------------------------------------------------------------------------------35
II. Equipment Description----------------------------------------------------------------------------------------------------------35
III. Data Acquisition-----------------------------------------------------------------------------------------------------------------35
IV. Findings / Results --------------------------------------------------------------------------------------------------------------35
V. Conclusions / Recommendations--------------------------------------------------------------------------------------------36
Appendix B Flight Test Results Of The Controlled Flight Into Terrain Avoidance
Maneuver In Fly-By-Wire Transports----------------------------------------------------------------37
I. Abstract-----------------------------------------------------------------------------------------------------------------------------37
II. Introduction ------------------------------------------------------------------------------------------------------------------------37
A. Purpose of Flight Test-------------------------------------------------------------------------------------------------------37
B. Ground Proximity Warning Systems -----------------------------------------------------------------------------------38
C. CFIT Escape Maneuvers----------------------------------------------------------------------------------------------------38
1. AIRCRAFT WITH CONVENTIONAL FLIGHT CONTROLS --------------------------------------------38
2. FBW AIRCRAFT WITH ÒHARDÓ PROTECTION FEATURES ----------------------------------------39
3. FBW AIRCRAFT WITH ÒSOFTÓ PROTECTION FEATURES-----------------------------------------39
III. Test Plan--------------------------------------------------------------------------------------------------------------------------40
A. Test Articles/Locations------------------------------------------------------------------------------------------------------40
1. Airbus A-330-200----------------------------------------------------------------------------------------------------------40
2. Boeing B-777-300 ---------------------------------------------------------------------------------------------------------41
B. Maneuvers/Test Points------------------------------------------------------------------------------------------------------41
C. Test Methods ------------------------------------------------------------------------------------------------------------------42
IV. Discussion of Results ----------------------------------------------------------------------------------------------------------42
　
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