Day 13 - Miscellaneous Systems

Question 1

What components are located on the accessory gearbox

Answer 1

DC starter generator, N2 speed sensors, oil pump, hydromechanical metering unit (HMU), hydraulic pump, engine driven fuel pump

Question 2

The maximum thrust loss due to EFC failure could be __

Answer 2

40%

Question 3

When engine shutdown is due to a ______, a loud bang will be audible

Answer 3

Failed turbine rotor shaft

Question 4

T/F - If the engine will not start with the ignition switch in STBY, the manual mode should not be used

Answer 4

TRUE

Question 5

The engines should be manually synchronized within __ before synchronization is used

Answer 5

1.50%

Question 6

At what percent N2 does the starter/generator begin acting as a generator

Answer 6

35 to 40

Question 7

The engine fire extinguishing system uses what type of extinguishing agent

Answer 7

HALON

Question 8

What occurs when an ENG FIRE switchlight is pressed

Answer 8

Respective fuel and hydraulic valves are closed and both extinguisher bottles are armed

Question 9

In the event of a FLAP ASYM annunciator, a __ assymetry is indicated

Answer 9

Main flap

Question 10

Why does the stick shaker actuate twice during the stall warning test

Answer 10

To test the altitude compensator

Question 11

__ on the AOA indicator represents maximum value of lift/drag (L/D Max)

Answer 11

0.6 (actually 0.45 - verify with Dash 1)

Question 12

What are the primary flight controls

Answer 12

Elevator, spoilers, rudder

Question 13

The elevator has a range of __ degrees up and __ degrees down

Answer 13

25, 12

Question 14

Full travel range of the rudder is __ degrees left and right of neutral

Answer 14

30

Question 15

T/F - The rudder boost system is not designed to fully compensate for the loss of thrust in an assymetric condition

Answer 15

TRUE

Question 16

T/F - If a trim system malfunction has occurred it is acceptable to use the failed system if necessary

Answer 16

FALSE

Question 17

T/F - The magnetic compass is unreliable when the windshield heat is set to HIGH

Answer 17

TRUE

Question 18

Can high windshield heat mode be used during takeoff and landing

Answer 18

No

Question 19

With the TCAS set to ABV/BLO the protection window is +/- __ feet

Answer 19

9900

Question 20

A TCAS RA is displayed on the MFD as a symbol.

Answer 20

Red square

Question 21

There are __ emergency lights in the aircraft cabin

Answer 21

4

Question 22

When can the ELT be tested

Answer 22

Within 5 minutes after each hour

Question 23

How long is the BPO good for?

Answer 23

72 hrs unless aircraft was flown

Question 24

Explain Anti Ice/Deice systems tests

Answer 24

(insert explanation)

Question 25

What is the chine on the nose wheel used for?

Answer 25

Direct flow of water and slush away from engines.

Question 26

What should you do if starter does not drop out by 45%

Answer 26

Press the starter disengage button. If yellow start button and white disengage button do not extinguish, cut-off the throttles, battery switch off and turn both master generator switches to EMER.

Question 27

What does it mean when the Fire Bottles blowout disc is missing?

Answer 27

Bottle contents may have been discharged due to ambient temperatures for thermal relief. Consult maintenance

Question 28

Why does the AC BUS shed light come on during the EMER Test on preflight?

Answer 28

Because the No.2 inverter is being powered by the Emergency Bus

Question 29

How do you know if the oil qty indicator is bad or if the qty is low?

Answer 29

If the indicator is bad the light won’t illuminate when pressed to test. If the light tests good but does not light up when the level check switch is pressed then the oil level is low or the system has failed. Visually check dipstick.

Question 30

What are the restrictions for unusual attitudes?

Answer 30

5000 ft AGL, Initiate recoveries above 130 KIAS and below 270 KIAS. Do not exceed 45 deg of bank. Max pitch 25 deg NU and 20 deg ND