Localization
Title Page ID Reason
OP-020 PROTECTIONS 7/14 1 Text modified to highlight that the FCPC computes the energy level.
OP-030
autopilot/flight director 1/14 1 Additional information concerning the minimum height for other approaches. The second item of the list is added: the DA for straight in LNAV/VNAV approach.
OP-030
AUTOTHRUST (A/THR) 3/14 2 Text modified for improved technical understanding and for clarification.
OP-040
use of summaries 7/10 1 Text modified to introduce the new LDG DIST and Vapp computation methods.
OP-040
use of summaries 7/10 2 Sequence modified to introduce the new LDG DIST and Vapp computation methods.
SUMMARY OF HIGHLIGHTS
Intentionally left blank
OPERATIONAL PHILOSOPHY
INTRODUCTION
INTRODUCTION
Applicable to: ALL
The Airbus cockpit is designed to achieve pilot operational needs throughout the aircraft operating environment, while ensuring maximum commonality within the Fly by Wire family. The cockpit design objectives are driven by three criteria:
? Reinforce the safety of flight
? Improve efficiency of flight
? Answer pilot requirements in a continuously changing environment
Airbus operational rules result from the design concept, more particularly from the following systems:
? The Fly by wire system with its control laws and protections, commanded through the side stick,
? An integrated Auto Flight System comprising:
‐ The FMS interfaced through the MCDU
‐ The AP/FD interfaced through the FCU,
‐ The A/THR interfaced through the non back driven thrust levers,
‐ The FMA, providing Guidance targets and Information, to monitor the AFS
? A set of Display units (DU) providing information and parameters required by the crew ‐ To operate and to navigate the aircraft (the EFIS)
‐ To communicate (the DCDU)
‐ To manage the aircraft systems (the ECAM)
‐ FMA interface to provide Guidance targets and information to monitor the AFS/FD
? A Forward Facing Cockpit Layout with "Lights out" or "Dark Cockpit" concept assisting the crew to properly control the various aircraft systems.
The operational rules applicable to these specific features are given in the other sections of this chapter.
OPERATIONAL GOLDEN RULES
Applicable to: ALL
1. The aircraft can be flown like any other aircraft
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