B777 - Part 5

Airborne vibration indications have limiting values that must not be exceeded.

Low oil quantity cannot automatically display the secondary engine display.

The APU battery powers the electric start motor, the inlet door and the fuel valve.

On the ground, the APU can be started with no pumps operating.

Fire bottle 1 is discharged or the pressure is low (aisle stand lights indicate discharge).

An overheat condition exists in the right engine.

The APU shuts down automatically and the fire bottle discharges automatically.

Push the fire override switch, then pull the fire switch.

Fire detection for this engine is no longer available.

APU fire detection is no longer available.

Two rapid dump bottles discharge into the forward cargo compartment.

There is no built-in fire extinguishing system for the wheel well.

An aural warning activates and a light illuminates outside the lavatory if smoke is detected.

Fire detection for the aft cargo compartment is not available.

Fire detection for the forward cargo compartment is not available.

The APU fire bottle has discharged.

The EICAS caution message "FIRE CARGO (FWD or AFT)" is displayed.

The WHEEL WELL FIRE light illuminates.

The EICAS caution message "FIRE APU" is displayed.

The EICAS advisory message "DET FIRE APU" is displayed if there is an APU fire.

The Autopilot and envelope protection features are NOT available.

Flaperons

Ailerons, flaperons and spoilers

Primary flight computers (PFCs)

Left and right stick shakers.

Use of alternate pitch trim levers reduces the column forces below the minimum maneuvering speed.

Activating the stabilizer trim switches on the control wheel disengages the autopilot.

Control wheel pitch trim switches

Nose gear pressure sensor disagrees with the FMC calculation.

Ailerons, flaperons and spoilers

Normal

The extension of speedbrakes in the landing configuration is prohibited.

Speedbrakes are extended, and landing flaps are selected or RA is between 15 and 800 feet.

The flap position indicator is located on the PFD.

The message is displayed when the flap drive mechanism has failed.

Autopilot, automatic speedbrakes and envelope protection

Ability to control initial effects of an engine failure with control wheel only.

During airspeed changes only.

The green band and the pointer are not displayed.

The levers move the stabilizer directly in all modes.

The system is in the direct mode.

Arm ALT FLAPS ARM switch. Select ALT FLAPS selector to EXT

All spoilers remain usable.

Flight control system is operating in the secondary mode.

When one engine differs by 10 percent or more from the other engine.

Roll control assisted by asymmetric spoilers.

8 degrees

Both stabilizer cutout switches are in the CUTOUT position.

A total of 14 spoiler panels.