787 Progressive Functions 2020 (Automatic Features)

ZNode Audio Series 787 Progressive Functions A production of Z-Man Audio Series 2020, 787 Progressive Functions, taxi out engine start. Engine start plus 3 minutes, all demand pumps stop running, take off. Take off thrust set, all hydraulic demand pumps start to run. 30 knots, manual rudder trim inputs are zeroed, 40 knots, flight control lockout is disengaged if it was engaged. 50 knots, HUD ground deceleration scale is shown if deceleration is sensed, if not previously pushed, toga switches are inhibited until 400 feet. 60 knots, flight control system attempts to maintain 0 yard, 65 knots, engine fail warning in the PFD HUD, primary flight display HUD becomes available indicated airspeed. Toga reference line is shown on HUD 75 knots, anti-ice actions, anti-ice detection begins, an automatic win, wing, anti-ice is available indicated air 80 knots. Intriguing system actions, caution lights, sounds, and eye-cast advisory message inhibit begins, indicated airspeed, new predictive wind shear system caution alert inhibit begins, indicated airspeed, entry door handles lock to prevent door opening during flight. Pushing toga switches disarms LNAV and VNAV. With flight director switches off, the flight director will still engage if toga switches are pushed, indicated airspeed. 35 knots, RTO actions, RTO auto break is armed, speed break lever will move to up if thrust levers are closed. 100 knots, new predictive wind shear system warning inhibit begins, indicated airspeed. V1 minus 6 knots, indicated airspeed, engine fail warning inhibited, engine thrust eye-cast amber caution message becomes available instead. Note, this message is shown for either of the following two. The thrust is more than the commanded thrust. The thrust is less than the commanded thrust, displayed above 6 knots prior to V1. If the engine is producing higher or lower thrust than what is commanded and is not correcting, replaces the engine failure alert system, red engine fail on primary flight display from 6 knots before V1. The engine, indication thrust command arc becomes filled amber. V1, new eye-cast warning lights bell siren inhibit begins. Initial climb out, weight off wheels, elapsed flight time timer start at 50 feet, new predictive wind shear system warning inhibit ends, HUD flight director guidance queue appears, LNAV engages if armed, pushing toga switches removes any derate and puts roll mode back to toga. Caution lights sounds eye-cast advisory message and eye-cast communication alert inhibited ends. Redder trim indication blank when gear up for 10 seconds or 60 seconds after liftoe. 400 feet, VNAV engages if armed, pushing toga switches removes any derate and puts both roll and pitch mode back to toga. Caution lights sounds eye-cast advisory message and eye-cast communication alert inhibited ends or 20 seconds after liftoe whichever occurs first. New predictive wind shear system caution inhibited ends, new eye-cast warning lights bell siren inhibit ends for 25 seconds after liftoe. 600 feet, T-cast TA inhibited ends, 800 feet, status queue inhibited ends or 30 seconds after liftoe if that occurs first, 1,100 feet, T-cast RA inhibited ends, 1200 feet, T-cast descend RA inhibited ends, predictive wind shear system, system stops issuing new cautions and warnings, 2000 feet, center demand pump stops, first flap retraction speed error tape is displayed, flaps up, left and right demand pumps stop, climb 10 minutes after takeoff ILS auto tune inhibited ends, a note about derated thrust climb, two fixed climb thrust derates climb 1 and climb 2 can be selected on the thrust limit page, the percentage of derate is 5% for climb 1, 15% for climb 2, the derated climb thrust is maintained until reaching 10,000 feet where the thrust then increases linearly to an altitude to achieve climb thrust by 30,000 feet, in cruise the thrust reference defaults to climb. Additionally, use of an assumed temperature reduced thrust takeoff or takeoff derate affects automatic selection of the climb derate, if the takeoff derate percentage fixed derate plus assumed temperature method is less than 5% than climb is selected, or greater than or equal to 5% and less than 15%, then climb 1 is selected, or greater than or equal to 15%, then climb 2 is selected, 30,000 feet, general electric engines ice crystal anti-ice function ICA becomes available, cruise 20 minutes into cruise above 25,000 feet, humidification system operates when humid switch is on, and until one to one and a half hours prior to landing, halfway or 400 nautical miles to destination landing altitude on the primary flight, or PDF, altitude tape changes from departure runway to destination run, 150 nautical miles from destination or 50 nautical miles from touch top of descent or FMC in descent, ILS GLS MPS approach reference data appears on primary flight display, ILS GLS auto-tunes, descent, 28,500 feet, general electric engines ice crystal anti-ice function ICA terminates, approach 25 nautical miles from mist approach point, final approach course pointer is shown on the primary flight display, aircraft positions 60 degrees within final approach course, glide path pointer is shown on primary flight display, max 6,000 feet above field, aircraft position within 60 degrees and track 90 degrees to final approach course, 2500 feet, radio altitude shows on primary flight display and HUD, rising runway symbol is shown on primary flight display, 2300 feet, predictive wind shear system starts to scan 2000 feet, center demand pump starts to run, wind gear is down also, 1500 feet, reactive wind shear warning enabled, 1450 feet, T-CAS increase descent RA inhibits begin, 1200 feet, predictive wind shear system enabled for warnings and cautions, 1000 feet, T-CAS descent RA inhibits begins, T-CAS RA inhibits begins, ND changes from traffic to TA only, left and right demand pumps start to run if not already started by gear selected 800 feet, config gear warning, red if thrust levers closed and gear not down, and I cast communication message inhibits begins, status queue inhibits begins, speed brake extended caution enabled, note about config gear warning, a landing gear is not down and locked and one of these occurs below 800 feet, radio altitude and a thrust lever is at idle, or the flaps are in a landing position, note about speed brake extended, amber caution message, the speed brakes are extended and at the same time one or more of the following occurs, the radio altitude is between 1500 and 800 feet, correction 15 feet and 800 feet, the flat lever is in a landing setting, thrust lever is not at idle, this message is one of three caution messages that are not inhibited below alert height on an auto land, the other two are amber autopilot, amber auto throttle disconnect, further this caution message should not be confused with the oral time critical warning that occurs during rollout on landing or a rejected takeoff when the speed brake has not deployed, that message is not on the i-cast but rather on the primary flight display and HUD accompanied by the master warning light and the oral speed brake, speed brake 400 feet, tcaste a voice alert inhibits begins. New, predictive wind shear caution alert inhibit begins. HUD Flight Path Acceleration Symbol is removed if decreasing performance wind shear is to 300 feet, HUD runway edge lines are shown if in decluttered mode. Land 2 or land 3 displayed and 200 feet, master caution light beeper inhibited for all messages except for amber autopilot, amber auto throttle disconnect, amber speed brake extended, rising runway symbol moves toward the airplane symbol. At 70 feet, HUD glide slope reference line is removed. At 60 feet, HUD runway edge lines are removed. At 50 feet, new predictive wind shear system warning alert inhibit begins. HUD Flight Director Guidance Q disappears. Standing, new predictive wind shear system warning alert inhibit ends, 80 knots, new predictive wind shear system caution alert inhibit ends indicated airspeed, 75 knots, eye cast communication message inhibit ends indicated airspeed status Q inhibit ends or begins rather indicated airspeed, master caution light beeper inhibit ends indicated airspeed. At 70 knots, entry door flight locks are unlocked. 60 knots, center demand pump normally stops. 40 knots, left and right demand pumps normally stop if reversers are stowed. Rutter and stab trim indication is shown on eye cast. 30 seconds after weight applied on wheels, elapsed flight time timer stops. At 25 knots, HUD ground deceleration scale is removed. If a go around is initiated. At 50 feet, elnab engages manual flight. 200 feet elnab engages automatic flight. 600 feet, t cast TA voice alert inhibit ends, 800 feet master caution light beeper inhibit ends. 900 feet t cast RA inhibit ends, 1200 feet t cast descend RA inhibit ends, 1600 feet t cast increase descent RA inhibit ends. Thank you for listening to the Znotes audio series audio and production editors note. This audio content is compiled and read by a 25 year airline pilot, qualified on the 787 since 2015. A certified advanced ground instructor, retired military standards pilot, instructor pilot, instrument evaluator for both rotor and fixed wing aircraft. Thank you again for listening to Zman audio notes.