Quiz 2 Review CRJ-700 Systems Flashcards
Primary Flight Controls
Rudder, Elevator, Multifunction Spoilerions, Ailerons
A controlling surface on an aircraft’s tail that regulates yaw. Located on the vertical stabilizer of the aircraft.
Rudder
A rear horizontal stabilizer located on an aircrafts tail that controls up and down or pitching motion of the aircraft nose.
Elevator
Ailerons
Located on the trailing edge of the wiLocated on the trailing edge of the wing to provide roll controlng to provide roll control
Multifunction Spoilerons
Small hinged plates on the top portion of wings. Operates the down going wing only to assist ailerons in roll, and control at lower speeds
3 Systems
The CRJ-700 has 3 Hydraulic systems
2 pumps
The CRJ-700 has 2 pumps per hydraulic system (6 total pumps)
3 sources of AC Electrical power
IDG, ADG, APU
ADG
Air Driven Generator- Emergency source of AC electrical power
IDG
Integrated Drive Generator- Primary source of electrical power
APU
Auxiliary Power Unit- A small engine installed in the tail of an aircraft. Two primary functions are to provide bleed air for engine start and back up the IDG’s. It is also used to provide electrical power and air conditioning while the aircraft is on the ground.
Max Landing Weight:
67,000 lbs
Max Zero Fuel Weight:
62,300 lbs
MEL
Minimum Equipment List. A list that details which equipment must be functioning properly in order for the aircraft to be permitted to fly and which equipment may be inoperative for a specified period of time.
Altitude Restriction and No icing conditions- MEL
MEL restrictions that are generally associated with the Bleed Air System
Altitude Restrictions- MEL
MEL restrictions that are generally associated with the Air-conditioning Pack System