Engines

Question 1

What component regulates the engine to keep it within operating parameters?

Answer 1

The dual channel electronic engine control (EEC).

Question 2

Thrust reverser operation is available below _____ radio altitude or when the air/ground sensor is in the _____ mode.

Answer 2

10 feet/ground

Question 3

A green “Rev” light above N1 on the upper display indicates that the ____.

Answer 3

thrust reverser is deployed

Question 4

Each engine is equipped with _____ ignitors.

Answer 4

2

Question 5

What are the methods of inflight restarting?

Answer 5

Windmill and crossbleed

Question 6

The Fuel Used readout is displayed ____.

Answer 6

when the Fuel Flow Switch is moved to Used or Reset

Question 7

The amber ENGINE CONTROL light functions on the ground below ____ KIAS prior to takeoff, or approximately _____ seconds after touchdown.

Answer 7

80/30

Question 8

How can you tell if the EECs are in the normal mode?

Answer 8

The white ON is in view.

Question 9

The indication of a properly deployed thrust reverser after landing is a/an ____

Answer 9

green REV

Question 10

How is an EGT exceedance displayed after engine shutdown?

Answer 10

A red box

Question 11

The EEC selects approach idle ____.

Answer 11

inflight when the flaps are in landing configuration or engine anti-ice is turned on for either engine

Question 12

The EGT digital readout and EGT round dial indications are red, indicating what?

Answer 12

You have exceeded maximum EGT limits

Question 13

The EEC provides ____ protection in the normal mode.

Answer 13

N1 & N2

Question 14

The EEC will abort the engine start on the ground for ____.

Answer 14

a wet start
or
an impending hot start
(hot and wet!)

Question 15

You will see an ENG FAIL alert ____.

Answer 15

when N2 drops below 50% and the start lever is in IDLE

Question 16

The approximate engine starter cutout speed and the indication of engine starter cutout is ____.

Answer 16

56% N2, Engine Start Switch moves to AUTO and START VALVE OPEN light extinguishes

Question 17

The engine thrust reversers are operated ____.

Answer 17

The engine thrust reversers are operated ____.

Question 18

The cockpit indications of a thrust reverser malfunction are a Master Caution

Answer 18

ENG System Annunciator light, and REVERSER light

Question 19

If a wet start is detected, the EEC aborts the start ____ seconds after the start lever is moved to IDLE.

Answer 19

15

Question 20

Is it possible to use a reverser after landing with just the REVERSER light on?

Answer 20

YES

Question 21

Engine maximum and minimum limits are displayed in ____.

Answer 21

Red

Question 22

The ____ position provides ignition to selected igniter(s) when the engine is running and flaps are not UP.

Answer 22

AUTO