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211

Thereare        over wing emergency exits on theB737.

1

2

3

4

4

212

 

The over wing emergency exits lock when_____. Select the most correct answer.

a. 3 of the 4 entry/service doors areclosed

b. either engine isrunning

c. the airplane air/ground logic indicates that the airplane is in the air or both throttles areadvanced

d. all of the above

d. all of the above

213

Thereare        56 person raft(s) installed in the ceiling of theaircraft.

1

2

3

4

4

214

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

a. N1 andN2

b. The dual channel electronic engine control(EEC).

c. Flight Management Computer(FMC)

d. N1, N2, andEGT

b. The dual channel electronic engine control(EEC).

215

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

a. 5feet/ground

b. 10feet/air

c. 10feet/ground

d. 5feet/air

c. 10feet/ground

216

A green "Rev" light above N1 on the upper display indicates that the_____

A. reverser sleeve has not moved from stowedposition

B. thrust reverser is in transit

C. thrust reverser is deployed

D. auto stow circuitry has activated

C. thrust reverser is deployed

217

Each engine is equipped with _____ igniters

1

2

3

emergency

2

218

What are the methods of inflightrestarting?

Windmill and air

Windmill and crossbleed

Air andcrossbleed

APU and ExternalAir

Windmill and crossbleed

219

220

The Fuel Used readoutisdisplayed_____

a. when the Fuel Flow Switch is moved to Used or Reset

b. at brake release just prior topushback

c. upon touchdown through the ground sensingswitch

d. automatically whenever the airplane isrefueled

a. when the Fuel Flow Switch is moved to Used or Reset

221

The amber ENGINE CONTROL light functions on thegroundbelow        KIAS prior to takeoff, or approximately      seconds aftertouchdown.

a. 70/20

b. 50/5

c.   80/30

d.   60/10

c.   80/30

222

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

The amber OFF is inview.

The white OFF is inview.

The amber ON is inview.

The white ON is in view

The white ON is in view

223

The indication of a properly deployed thrust reverser after landingisa/an      displayed aboveN1.

amberREV

greenREV

whiteREV

blueREV

greenREV

224

How is an EGT exceedance displayed after engineshutdown?

An amberbox

Flashing whitebox

A redbox

Flashing reddisplay

A redbox

225

The EEC selects approach idle       .

a. when the engine start switches are moved to FLIGHT position

b. automatically below 18,000feet

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

d. when N1 and N2 fall below presetlimits

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

226

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

a. MAX go around thrust has been selected.

b. MAX continuous thrust EGT has been selected.

c. Start limit has been exceeded.

d. MAX takeoff thrust has beenselected.

c. Start limit has been exceeded.

227

TheEECprovides        protection in the normalmode.

a. EGT only

b. N1 andEGT

c. N1, N2, andN3

d. N1 andN2

d. N1 andN2

228

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

a. a wet start

b. no oil pressure

c. an EGT start limit exceedance

d. either A or C above

d. either A or C above

229

You will see an ENG FAIL alert_____

a. in flight with the start lever in CLOSED

b. when the applicable start selector switch faults

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

d. on the ground only - it is notdispatchable

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

230

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

a. 56% N2, Engine Start Switch moves to AUTO and START VALVE OPEN lightextinguishes

b. 50% N2 and starter trips to OFF position

c. 60% N2 and the starter trips toOFF

d. 57% N2 and ENGINE FAIL lightextinguishes

a. 56% N2, Engine Start Switch moves to AUTO and START VALVE OPEN lightextinguishes

231

The engine thrust reversers are operated       .

a. pneumatically

b. mechanically

c. electrically

d. hydraulically

d. hydraulically

232

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

a. a bell, and severeyaw

b. a horn, and an auto-restow light

c. severe yaw, and an auto-restow light

d. ENG System Annunciator light, and REVERSER light

d. ENG System Annunciator light, and REVERSER light

233

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

5

10

15

20

 

 

 

15

234

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

a. Yes

b. Only if the standby rudder system powers thereversers

c. In REVERSE IDLEonly

d. No

a. Yes

235

Engine maximum and minimum limits aredisplayedin        .

a. red

b. amber when RESET is pressed

c. white text numbers

d. blue

red

236

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

a. GRD

b. AUTO

c. OFF

d. FLT

b. AUTO

237

In stabilized cruise flight, the EEC automatically displays the light to the right, which indicates that the #1 EEC is inthe__mode.

Normal

Hard Alternate

Soft Alternate

Backup

Soft Alternate

238

In this mode, what parameters is the EEC using to control the # 1engine?

a. The atmospheric condition sensed when the engine wasstarted.

b. Preprogrammed data.

c. The atmospheric data from the altitude set in the pressurization FLT AL Twindow.

d. The last valid flight conditions that the EEC sensed before it went into the Soft Alternatemode.

d. The last valid flight conditions that the EEC sensed before it went into the Soft Alternatemode.

239

What protection is the EEC providing the #1 engine in thismode?

a. Low oil pressure red linelimits

b. Exceeding EGT redlinelimits

c. Exceeding N1, N2 redline limits

d. Exceeding engine vibration limits

c. Exceeding N1, N2 redline limits

240

This light at right indicates that the #1 EEC isinthe        mode.

Hard Alternate

Soft Alternate

Normal

Backup

Hard Alternate