AS 410 CHAPTER 4 AIRCRAFT SYSTEMS & LIMITATIONS QUESTIONS
WITH VERIFIED ANSWERS
Correct 51
Incorrect 00
1 of 51
Definition
3 sources: System A, B, and Standby
standby can be activated if A or B fail
Give this one a try later!
Autobrake System Hydraulic Standby System
Fuel System General Hydraulics General
Don't know?
2 of 51
Definition
,is automatically controlled by opening and closing The main and
forward outflow valves through AC or DC motors
Pressurized areas include: Cockpit, Cabin, electrical equipment
compartment, and forward and aft cargo compartments
Two safety relief valves limit max differential pressure
A negative pressure relief door prevents atmospheric pressure from
exceeding internal cabin pressure
Max differential pressure is limited to 8.65psi
Give this one a try later!
Spoiler Systems info Engine Anti-Ice
Pressurization Landing Gear
Don't know?
3 of 51
Definition
Air conditions the cockpit and cabin
Heats cargo compartments, cool electronics, and supplies air for
pressurization
Air supplied from bleed air that is cooled by AC packs
Give this one a try later!
, Bleed Air General Hydraulics General
Air conditioning General Describe General APU Info
Don't know?
4 of 51
Definition
Main tank 1 monitors fuel temperature with a sensor
Fuel is heated by a fuel/oil heat exchanger for each engine
Give this one a try later!
Fuel Temperature Nose Wheel Steering
Fueling and Defueling Ice and rain protection
Don't know?
5 of 51
Term
How many pounds of thrust does each engine produce?
, Give this one a try later!
135,000lbs 37,000ft
10,000ft 20,000lbs
Don't know?
6 of 51
Term
What is max landing weight?
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116,000lbs 106,500lbs
135,000lbs 1000lbs
Don't know?
7 of 51
Term
What is the capacity of each fuel tank on the aircraft?
WITH VERIFIED ANSWERS
Correct 51
Incorrect 00
1 of 51
Definition
3 sources: System A, B, and Standby
standby can be activated if A or B fail
Give this one a try later!
Autobrake System Hydraulic Standby System
Fuel System General Hydraulics General
Don't know?
2 of 51
Definition
,is automatically controlled by opening and closing The main and
forward outflow valves through AC or DC motors
Pressurized areas include: Cockpit, Cabin, electrical equipment
compartment, and forward and aft cargo compartments
Two safety relief valves limit max differential pressure
A negative pressure relief door prevents atmospheric pressure from
exceeding internal cabin pressure
Max differential pressure is limited to 8.65psi
Give this one a try later!
Spoiler Systems info Engine Anti-Ice
Pressurization Landing Gear
Don't know?
3 of 51
Definition
Air conditions the cockpit and cabin
Heats cargo compartments, cool electronics, and supplies air for
pressurization
Air supplied from bleed air that is cooled by AC packs
Give this one a try later!
, Bleed Air General Hydraulics General
Air conditioning General Describe General APU Info
Don't know?
4 of 51
Definition
Main tank 1 monitors fuel temperature with a sensor
Fuel is heated by a fuel/oil heat exchanger for each engine
Give this one a try later!
Fuel Temperature Nose Wheel Steering
Fueling and Defueling Ice and rain protection
Don't know?
5 of 51
Term
How many pounds of thrust does each engine produce?
, Give this one a try later!
135,000lbs 37,000ft
10,000ft 20,000lbs
Don't know?
6 of 51
Term
What is max landing weight?
Give this one a try later!
116,000lbs 106,500lbs
135,000lbs 1000lbs
Don't know?
7 of 51
Term
What is the capacity of each fuel tank on the aircraft?
