RST 2 19 Tech

Question 1

When operating with normal power sources available, placing the Battery (BAT) Switch to OFF will remove power from:

Answer 1

The battery bus and switched hot battery bus.

Question 2

The Number 1 Generator Drive (DRIVE) light illuminates (amber). This is directly caused by:

Answer 2

IDG low oil pressure

Question 3

During an autopilot ILS approach:

Answer 3

at glideslope capture DC Bus 1 and DC Bus 2 are isolated from each other

Question 4

Illumination (amber) of the Electrical (ELEC) Light in flight indicates:

Answer 4

This light operates only when the aircraft is on the ground.

Question 5

The blue ‘APU GEN OFF BUS’ light will illuminate:

Answer 5

when the APU is at operational speed and is not supplying an AC transfer bus

Question 6

If the aircraft takes off with the APU powering both transfer buses:

Answer 6

The engine generators are automatically connected to their related transfer buses if the APU is shut down

Question 7

Which bus supplies electrical power to the main battery charger?

Answer 7

AC ground service bus 2

Question 8

The TR UNIT light will illuminate (amber) in flight if:

Answer 8

TR1 has failed

Question 9

In addition to Hydraulic System A and B, the rudder can also be powered by the Standby Hydraulic System through the:

Answer 9

Standby Rudder PCU

Question 10

In the event of an elevator control column jam, an override mechanism allows:

Answer 10

The control columns to be physically separated. The column which is free to move will be able to provide elevator control

Question 11

Illumination of the amber AUTO SLAT FAIL light during MASTER CAUTION recall that extinguishes when master caution system is reset indicates:

Answer 11

Failure of a single Stall Management Yaw Damper (SMYD) computer.

Question 12

With loss of hydraulic system B (system A operating normally):

Answer 12

Main and Standby Yaw Dampers are not available.

Question 13

Which statement is true regarding aileron trim?

Answer 13

If the autopilot is engaged the amount of trim is not indicated on the scale.

Question 14

The number of flight spoilers located on each wing are:

Answer 14

4

Question 15

Why are mechanical gates installed on the flap selector unit?

Answer 15

To hinder inadvertent flap lever movement beyond Flaps 1 and Flaps 15 during a go-around

Question 16

If a wheel spin-up signal is not detected on landing and the speed brake is ARMED, the flight spoilers will deploy automatically:

Answer 16

When the Air /Ground system senses ground mode (any gear strut compresses).

Question 17

If the thrust lever(s) are advanced after touchdown:

Answer 17

The AUTO BRAKE DISARM light will illuminate, except during the first 3 seconds after touchdown

Question 18

If a landing is made with RTO selected:

Answer 18

AUTO BRAKE DISARM light illuminates 2 seconds after touchdown

Question 19

Which of these pressures can be indicated by the Hydraulic Brake Pressure Indicator?

Answer 19

Maximum pressure of 3500 psi.

Question 20

Landing autobrake settings may be selected after touchdown:

Answer 20

prior to decelerating through 30 knots of groundspeed

Question 21

When the landing gear Manual Extension Access Door is open:

Answer 21

manual landing gear extension is possible with landing gear lever in any position.

Question 22

What happens if you reject a takeoff with a groundspeed of 100 knots with Autobrakes in RTO?

Answer 22

maximum braking is applied automatically when the forward thrust levers are retarded to idle

Question 23

During alternate brake operation, the following protection is provided:

Answer 23

Skid, locked wheel, touchdown and hydroplane

Question 24

The purpose of the Landing Gear Transfer Unit is to:

Answer 24

automatically use hydraulic system B for gear retraction if No.1 engine is lost and the landing gear lever is positioned up

Question 25

During AUTO LAND at what radio altitude will the flare maneuver start and FLARE engaged is annunciated?

Answer 25

50 feet

Question 26

When the aircraft batteries are the only source of power:

Answer 26

b. The Captain’s inboard and outboard DUs operate until the battery is discharged.

Question 27

On the ground, the TR UNIT Light illuminates (amber) if:

Answer 27

Any TR has failed.

Question 28

Illumination (blue) of a Generator Off Bus (GEN OFF BUS) Light indicates:

Answer 28

the IDG is not supplying power to the related transfer bus

Question 29

The trailing edge flaps are set to position 15. The correct indication on the aft overhead panel for the leading edge devices is (assume for non-Short Field Performance aircraft YC496 through YW097):

Answer 29

all LE devices FULL EXT lights illuminated green

Question 30

The flap/slat electronics unit (FSEU) provides:

Answer 30

c. protection for LE devices if two or more slats on one wing move from the commanded position

Question 31

The red landing gear indication lights are illuminated under which of the following conditions?

Answer 31

Landing gear is in disagreement with LANDING GEAR lever position OR the landing gear is not down and locked (with either or both thrust levers retarded to idle, and below 800 feet AGL).

Question 32

If the nose gear steering lockout pin is not installed for pushback or towing:

Answer 32

System A hydraulic pumps must be switched off.

Question 33

Which statement is true?

Answer 33

rudder pedal steering is deactivated as the nose gear strut extends

Question 34

What airspeed must be considered with a wheel well fire situation?

Answer 34

Extend limit speed of 270k/.82M maximum.