Aircraft General, Emergency Equipment, & Doors Flashcards
Which is true concerning an open cockpit window?
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.
The suction cup securing system must be attached in the designated securing location and must comply with which of the following requirements?
Both statements are true
What is the main cargo door maximum wind gust with the door open?
60 kts
Indicator light brightness can be manually set to dim or bright or the system automatically will override the dim position and illuminates the indicator lights full bright for the following conditions?
Loss of equipment cooling air flow (recirculation fan in operative on the B757), as detected in the flight deck or in the forward E/E compartment.
The B757/B767 Aircraft have which two types of push button switches?
Alternate action and momentary action
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?
250 kts
What is the power source for emergency lights?
- The standby DC bus
- The Hot Battery Bus
- A battery pack which is charged by aircraft electrical power (if powered) when the emergency lights switch is in the off or armed position.
A battery pack which is charged by aircraft electrical power (if powered) when the emergency lights switch is in the off or armed position.
The main cargo horn switch (N362UP - N364UP) is continuously armed. The horn can be activated manually by pressing the switch. The horn in the cargo compartment will automatically activate:
- The horn will not automatically activate and requires crew action.
- if the cargo fire switch is pushed or if the cabin altitude warning occurs.
- The horn will automatically activate if both smoke detector loops detect smoke in the main cargo compartment.
• if the cargo fire switch is pushed or if the cabin altitude warning occurs.
Automatic activation of PRM emergency exit lights occurs:
- during a PRM smoke event, aircraft depressurization or in the event of a power loss
- when any cargo fire detector detect smoke or if the aircraft decompression occurs
- when a cargo fire is detected, if aircraft decompression occurs, or in the event of a power loss
• during a PRM smoke event, aircraft depressurization or in the event of a power loss
(757) what indicates to the crew that the main deck cargo access door is not closed and locked?
- The access doors light
- The cargo doors light
- A red pen extending on the flight deck side of the rigid barrier
• A red pen extending on the flight deck side of the rigid barrier
To halo on fire extinguishers are located on the flight deck. If a fire extinguisher is to be discharged in the flight deck area:
- all flight crew members must wear oxygen mask and use 100% oxygen with emergency selected
- immediately descend to 10,000 feet or minimum safe altitude (which ever is higher)
- hold the extinguisher nozzle as close as possible to the base of the flames as possible to ensure thorough coverage
• all flight crew members must wear oxygen mask and use 100% oxygen with emergency selected
(767) what actuate the main cargo door?
- The center hydraulic system
- Electric system – ground handling Bus
- The left hydraulic system
• Electric system – ground handling Bus
Which flight deck window can be open from the outside?
- either the left-hand window adjacent to the captain or the right hand window adjacent to the first officer
- The left-hand window adjacent to the captain
- The right hand window adjacent to the first officer
• The right hand window adjacent to the first officer
What does the EMER lights EICAS message indicate?
- The emergency light switch is not in the arm position
- The emergency lights have been activated
- The emergency light battery pack voltage is low
• The emergency light switch is not in the armed position
