Airplane General, Emergency Equipment and Doors

Question 1

The MAIN CARGO HORN switch (N362UP through N364UP) is continuously armed.
The horn can be activated manually by pressing the switch. The horn in the cargo
compartment will AUTOMATICALLY activate:

Answer 1

If the Cargo Fire switch is pushed or if the Cabin Altitude

warning occurs

Question 2

(767) What actuates the Main Cargo Door?

Answer 2

Electrical System ‐ Ground Handling Bus

Question 3

What does the EMER LIGHTS EICAS message indicate?

Answer 3

The emergency lights switch is not in the ARMED position

Question 4

Two Halon fire extinguishers are located on the flight deck. If a fire extinguisher is to
be discharged in the flight deck area:

Answer 4

All flight crewmembers must wear oxygen masks and use

100% Oxygen with EMERGENCY selected

Question 5

Automatic activation of PRM emergency exit lights occurs:

Answer 5

During a PRM smoke event, aircraft decompression or in

the event of a power loss

Question 6

What is the power source for emergency lights?

Answer 6

A battery pack which is charged by aircraft electrical
power (if powered) when the Emergency Lights switch is
in the OFF or ARMED position

Question 7

(757) What indicates to the crew that the main deck cargo access door is not closed
and locked?

Answer 7

A red pin extending on the flight deck side of the rigid

barrier

Question 8

Which flight deck window can be opened from the outside?

Answer 8

The right‐hand window adjacent to the first officer

Question 9

Which is true concerning an open cockpit window?

Answer 9

If the Captain's or First Officer's #2 window opened
during flight (including takeoff roll above 80 knots), the
aircraft will continue to fly safely

Question 10

The B757/767 aircraft have which two types of push button switches?

Answer 10

Alternate action and momentary action

Question 11

Indicator light brightness can be manually set to DIM or BRT or the system
automatically will override the DIM position and illuminates the indicator lights full
bright for the following conditions?

Answer 11

Loss of equipment cooling air flow (recirculation fan
inoperative on the B757), as detected in the flight deck
or in the forward E/E compartment

Question 12

What is the main cargo door maximum wind gust with the door open (structural
consideration)?

Answer 12

60 kts

Question 13

Because the force required to move the crank increases with airspeed, it may not be
possible to open or close the window at speeds above?

Answer 13

250 kts

Question 14

The Suction Cup Securing System (SCSS) must be attached in the designated securing
location and must comply with which of the following requirements?

Answer 14

Both statements are true