RST 2 19 Tech Flashcards
When operating with normal power sources available, placing the Battery (BAT) Switch to OFF will remove power from:
The battery bus and switched hot battery bus.
The Number 1 Generator Drive (DRIVE) light illuminates (amber). This is directly caused by:
IDG low oil pressure
During an autopilot ILS approach:
at glideslope capture DC Bus 1 and DC Bus 2 are isolated from each other
Illumination (amber) of the Electrical (ELEC) Light in flight indicates:
This light operates only when the aircraft is on the ground.
The blue ‘APU GEN OFF BUS’ light will illuminate:
when the APU is at operational speed and is not supplying an AC transfer bus
If the aircraft takes off with the APU powering both transfer buses:
The engine generators are automatically connected to their related transfer buses if the APU is shut down
Which bus supplies electrical power to the main battery charger?
AC ground service bus 2
The TR UNIT light will illuminate (amber) in flight if:
TR1 has failed
In addition to Hydraulic System A and B, the rudder can also be powered by the Standby Hydraulic System through the:
Standby Rudder PCU
In the event of an elevator control column jam, an override mechanism allows:
The control columns to be physically separated. The column which is free to move will be able to provide elevator control
Illumination of the amber AUTO SLAT FAIL light during MASTER CAUTION recall that extinguishes when master caution system is reset indicates:
Failure of a single Stall Management Yaw Damper (SMYD) computer.
With loss of hydraulic system B (system A operating normally):
Main and Standby Yaw Dampers are not available.
Which statement is true regarding aileron trim?
If the autopilot is engaged the amount of trim is not indicated on the scale.
The number of flight spoilers located on each wing are:
4
Why are mechanical gates installed on the flap selector unit?
To hinder inadvertent flap lever movement beyond Flaps 1 and Flaps 15 during a go-around
If a wheel spin-up signal is not detected on landing and the speed brake is ARMED, the flight spoilers will deploy automatically:
When the Air /Ground system senses ground mode (any gear strut compresses).
If the thrust lever(s) are advanced after touchdown:
The AUTO BRAKE DISARM light will illuminate, except during the first 3 seconds after touchdown
If a landing is made with RTO selected:
AUTO BRAKE DISARM light illuminates 2 seconds after touchdown
Which of these pressures can be indicated by the Hydraulic Brake Pressure Indicator?
Maximum pressure of 3500 psi.
Landing autobrake settings may be selected after touchdown:
prior to decelerating through 30 knots of groundspeed
When the landing gear Manual Extension Access Door is open:
manual landing gear extension is possible with landing gear lever in any position.
What happens if you reject a takeoff with a groundspeed of 100 knots with Autobrakes in RTO?
maximum braking is applied automatically when the forward thrust levers are retarded to idle
During alternate brake operation, the following protection is provided:
Skid, locked wheel, touchdown and hydroplane
The purpose of the Landing Gear Transfer Unit is to:
automatically use hydraulic system B for gear retraction if No.1 engine is lost and the landing gear lever is positioned up
