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Cargo smoke
. 5,24 : Observe tail strike pitch limit.
. 7, 26 : Emphasize use of reversers (interlock mechanism) Landing phase: observe tail strike pitch limit at 400 feet AGL. AURAL WARNING “PITCH, PITCH” triggered > 8.1°. EMPHASIZE PNF monitoring. Do not chase PAPI Guidance below 200 feet AGL, note auto call out 70,60 feet. Be aware of higher approach speed and higher inertia but no handling difference. Emphasize stabilized approach.
. INIT TAKE OFF: MTOW: 342 T ZFW: 235 T ZFWCG: 32% Fuel: 107 t Speed V1: 145 kt VR: 159 kt V2: 173kt Conf 3 TOGA
. 11, 30: Use maximum weight parameters to justify Jettison after engine failure. ON GROUND: Rudder is used conventionnally to maintain the A/C on runway cen-terline. At VR, rotate the A/C smoothly, at a slower rate than with all engines operating, to an initial attitude of 12.5°. SRS orders should then be followed and may demand a lower pitch attitude to acquire or maintain V2. -Shortly after light off, the LATERAL NORMAL LAW commands some rudder surface deflection to minimize the side slip (there is no feedback of this command to the pedals). Thus, the lateral behavior of the A/C is safe. The pilot will have to adjust conventionnally the rudder pedals to center the Beta tar-get and trim accordingly the rudder trim. The use of the AP is STRONGLY recommended.
. 13 : Set Max Gross Weight Point out : Green dot is higher than VFE conf 1. Therefore apply VFE next procedure. Extend flaps until final configuration for demonstration. Return to Green dot and clean the aircraft after demonstration. Restore slats failure.
. 18 : Demonstrate VLS increasing to VMCL-2.
. 39 : Order a go around reaching Commit altitude.
