Quiz 2 Review CRJ-700 Systems

Question 1

Primary Flight Controls

Answer 1

Rudder, Elevator, Multifunction Spoilerions, Ailerons

Question 2

A controlling surface on an aircraft’s tail that regulates yaw. Located on the vertical stabilizer of the aircraft.

Answer 2

Rudder

Question 3

A rear horizontal stabilizer located on an aircrafts tail that controls up and down or pitching motion of the aircraft nose.

Answer 3

Elevator

Question 4

Ailerons

Answer 4

Located on the trailing edge of the wiLocated on the trailing edge of the wing to provide roll controlng to provide roll control

Question 5

Multifunction Spoilerons

Answer 5

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

Question 6

3 Systems

Answer 6

The CRJ-700 has 3 Hydraulic systems

Question 7

2 pumps

Answer 7

The CRJ-700 has 2 pumps per hydraulic system (6 total pumps)

Question 8

3 sources of AC Electrical power

Answer 8

IDG, ADG, APU

Question 9

ADG

Answer 9

Air Driven Generator- Emergency source of AC electrical power

Question 10

IDG

Answer 10

Integrated Drive Generator- Primary source of electrical power

Question 11

APU

Answer 11

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.

Question 12

Max Landing Weight:

Answer 12

67,000 lbs

Question 13

Max Zero Fuel Weight:

Answer 13

62,300 lbs

Question 14

MEL

Answer 14

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.

Question 15

Altitude Restriction and No icing conditions- MEL

Answer 15

MEL restrictions that are generally associated with the Bleed Air System

Question 16

Altitude Restrictions- MEL

Answer 16

MEL restrictions that are generally associated with the Air-conditioning Pack System

Question 17

Hazardous weather Restriction- MEL

Answer 17

MEL restrictions that are generally associated with the Weather Radar

Question 18

APU Constantly Running, Altitude Restriction- MEL

Answer 18

MEL restrictions that are generally associated with the Integrated Drive Generator

Question 19

Areas of the CRJ-700 that are anti-iced using bleed air from the engines

Answer 19

Engine Cowls, Leading edges of wings

Question 20

Areas of the CRJ-700 that are anti-iced electronically

Answer 20

Windshields, Pitot and Static ports

Question 21

Aircraft performance is planned

Answer 21

One engine inoperable

Question 22

Stages of the engine that are used for bleed air

Answer 22

6th and 10th

Question 23

V1 speed

Answer 23

Takeoff Decision Speed

Question 24

V2 speed

Answer 24

TAKEOFF SAFETY SPEED (THE
PLANE WILL CONTINUÉ TO
CLIMB WITH ONE ENGINE INOP)

Question 25

VR speed

Answer 25

ROTATION SPEED (THE NOSE WHEEL COMES OF THE GROUND)

Question 26

Method 1 drift down

Answer 26

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.

Question 27

Method 2 drift down

Answer 27

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

Question 28

Engine cowl

Answer 28

A removable covering placed over and around an airplane`s engine

Question 29

3B Pump

Answer 29

Emergency Backup Pump

Question 30

EGPWS

Answer 30

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.

Question 31

TCAS

Answer 31

Traffic Collision Avoidance System- an aircraft collision avoidance system designed to reduce the incidence of mid-air collisions between aircraft

Question 32

FMS

Answer 32

Flight Management System

Question 33

Maximum Takeoff weight CRJ

Answer 33

75,000 lbs

Question 34

WHAT IS THE AVERAGE SPEED WE PLAN WHEN ESTIMATING FUEL FOR WEIGHT AND BALANCE?

Answer 34

400 kts

Question 35

IN WHAT MONTHS DO WE USE WINTER PASSENGER WEIGHTS?

Answer 35

November 1-April 30

Question 36

WHATDOES CDL STAND FOR?

Answer 36

CONFIGURATION DEVIATION LIST

Question 37

WHAT IS A CONFIGURATION DEVIATION LIST?

Answer 37

A LIST OF THINGS OUTSIDE THE AIRCRAFT THAT MAY BE INOPERATIVE ANDIHE FLIGHT CAN STILLCONTINUE

Question 38

WHAT ARE THE 3 PRIMARY FUNCTIONS OF THE APU?

Answer 38

TO PROVIDE BLEEDÅiR FOR ENGINE START, BACK UP THE IDC'S, PROVIDE AIR CONDITIONING AND ELECTRICAL POWER WHILE THE AIRCRAFT IS E ROUND

Question 39

AIRCRAFT PERFORMANCE IS PLANNED BY THE DISPATCHER BASED ON WHAT BEING INOP?

Answer 39

ONE ENGINE

Question 40

ACARS

Answer 40

Aircraft Communications Addressing and Reporting System. It's a digital datalink system that transmits short messages between aircraft and ground stations