B767-400 LOD Nav Display

• -autopilot disengage bar
• -control wheel autopilot disengage switch

-autothrottle has disconnected

-push either control column autopilot disengage switch

• -Autothrottle has disconnected
• -push either autothrottle disconnect switch

-MCDU is dsplaying an operationally significant message in the scratch pad.

(pushing the MCDU CLR key will get rid of the message and advisory)

at the top of the PFD beneath the bank pointer

SPD- autothrottles are controlling thrust to maintain speed selected in the IAS/Mach window, or if VNAV is engaged, the speed as programmed by the FMC.

IDLE- autothrottle reduced to flight idle

THR HOLD- thrust levers remain in existing positions or where manually placed.

N1- autothrottle controlling to the slected N1 reference thrust

FLCH- thrust to max of the selected mode reference thrust during climb, and to a mim thrust during descent

GA- max referenced thrust to maintain a climb rate of at least 2000 fpm. (if both flight directors and the autopilot are off, autothrottle controls to go-around ref thrust subject to flap and VMA limit speeds)

• LNAV -(armed) LNAV in white is armed to activate when parameters are met
• (active) LNAV in green activates when in position to turn onto the active route leg. immediate activation within 2 1/2 miles of active leg

HDG- HDG SEL - airplane turns to or maintains heading selected in MCP window.

• LOC - (armed) AFDS captures the localizer when within range and within 120 degrees of course
• (active) AFDS follows the localizer course

B/CRS (armed)AFDS is armed to capture and track inbound on the backcourse of localizer after the localizer capture

(active) AFDS tracks the inbound on backcoure of localizer

• TO -ON the ground, TO annunciates by selecting either F/D switch ON when the both flight directors are OFF
• TO roll and pitch guidance become active at lift-off

GA - After the reference thrust limit changes from taeoff to climb, GA arms wenever flaps are out of up or glideslope capture