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
Hazardous weather Restriction- MEL
MEL restrictions that are generally associated with the Weather Radar
APU Constantly Running, Altitude Restriction- MEL
MEL restrictions that are generally associated with the Integrated Drive Generator
Areas of the CRJ-700 that are anti-iced using bleed air from the engines
Engine Cowls, Leading edges of wings
Areas of the CRJ-700 that are anti-iced electronically
Windshields, Pitot and Static ports
Aircraft performance is planned
One engine inoperable
Stages of the engine that are used for bleed air
6th and 10th
V1 speed
Takeoff Decision Speed
V2 speed
TAKEOFF SAFETY SPEED (THE
PLANE WILL CONTINUÉ TO
CLIMB WITH ONE ENGINE INOP)
VR speed
ROTATION SPEED (THE
NOSE WHEEL COMES OF
THE GROUND)
Method 1 drift down
Takeoff at an weight that if an engine failure occurs anywhere from V1 to the destination the aircraft will clear all obstructions 5SM either side of intended route by 1000’ until reaching destination.
Method 2 drift down
Takeoff at a weight that if an engine fails during cruise the aircraft can descend to a suitable alternate. While be able to clear all obstacles by 2000 ft within 5 sm of either side of the intended path to the alternate
Engine cowl
A removable covering placed over and around an airplane`s engine
3B Pump
Emergency Backup Pump
EGPWS
Enhanced Ground Proximity Warning System: a system providing crews with forward warning of the risk of collision with terrain in sufficient time for them to take avoiding action.
TCAS
Traffic Collision Avoidance System- an aircraft collision avoidance system designed to reduce the incidence of mid-air collisions between aircraft
FMS
Flight Management System
Maximum Takeoff weight CRJ
75,000 lbs
WHAT IS THE AVERAGE SPEED WE
PLAN WHEN ESTIMATING FUEL FOR
WEIGHT AND BALANCE?
400 kts
IN WHAT MONTHS
DO WE USE
WINTER
PASSENGER
WEIGHTS?
November 1-April 30
WHATDOES CDL
STAND FOR?
CONFIGURATION
DEVIATION LIST
WHAT IS A
CONFIGURATION
DEVIATION LIST?
A LIST OF THINGS OUTSIDE THE AIRCRAFT
THAT MAY BE INOPERATIVE ANDIHE
FLIGHT CAN STILLCONTINUE
WHAT ARE THE 3 PRIMARY
FUNCTIONS OF THE
APU?
TO PROVIDE BLEEDÅiR FOR ENGINE START, BACK UP THE IDC’S,
PROVIDE AIR CONDITIONING AND ELECTRICAL POWER WHILE
THE AIRCRAFT IS E ROUND
AIRCRAFT PERFORMANCE IS
PLANNED BY THE DISPATCHER
BASED ON WHAT BEING INOP?
ONE ENGINE
ACARS
Aircraft Communications Addressing and Reporting System. It’s a digital datalink system that transmits short messages between aircraft and ground stations
