: Standardized procedures are often customized to fit an airline’s specific safety philosophy or cockpit culture.
: The 787 is a "more-electric" aircraft. Understanding the Variable Frequency Starter Generators (VFSGs) and the Common Core System (CCS) is foundational to every other system.
The manual details the 787's unique sideslip elimination logic, which automatically applies rudder commands during an engine failure, drastically reducing pilot workload during critical phases of flight.
The ECL automatically senses when a step has been completed. For example, if the checklist requires the pilot to place the left fuel control switch to CUTOFF, the system registers the switch state change and automatically checks off the item with a green checkmark. 787 fcom exclusive
If you need further details on specific , please tell me:
4. Non-Normal Checklist (NNC) Philosophy and ECL Integration
Instead of using pneumatic air from the APU to start engines, the FCOM details the use of high-voltage AC electricity. : Standardized procedures are often customized to fit
To give you a concrete sense of the kind of detail you'll find, here are a few specific examples from the official 787 FCOM.
The manual is built to seamlessly complement the Engine Indicating and Crew Alerting System (EICAS). Every non-normal checklist in the FCOM correlates directly to electronic checklists (ECL) on the multi-function displays (MFDs).
The defining characteristic found in the 787 FCOM is the shift from bleed-air systems to electrical power. In traditional aircraft, hot air is bled from the engines to power air conditioning and anti-ice systems. The 787 FCOM describes a radical departure: Electric Cabin Air: The manual details the 787's unique sideslip elimination
It utilizes a multi-tier information structure, separating immediate operational needs from deep technical background data.
The network can generate up to 1.4. Megawatts (MW) of electrical power, enough to supply a small community. Nitrogen Generation & Anti-Ice Systems
The 787 has no hydraulic backup for the primary flight controls. Instead, they are powered by localized electric actuators.