Quiz 2 Review CRJ-700 Systems Flashcards

1
Q

Primary Flight Controls

A

Rudder, Elevator, Multifunction Spoilerions, Ailerons

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2
Q

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

A

Rudder

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3
Q

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

A

Elevator

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4
Q

Ailerons

A

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

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5
Q

Multifunction Spoilerons

A

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

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6
Q

3 Systems

A

The CRJ-700 has 3 Hydraulic systems

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7
Q

2 pumps

A

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

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8
Q

3 sources of AC Electrical power

A

IDG, ADG, APU

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9
Q

ADG

A

Air Driven Generator- Emergency source of AC electrical power

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10
Q

IDG

A

Integrated Drive Generator- Primary source of electrical power

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11
Q

APU

A

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.

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12
Q

Max Landing Weight:

A

67,000 lbs

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13
Q

Max Zero Fuel Weight:

A

62,300 lbs

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14
Q

MEL

A

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.

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15
Q

Altitude Restriction and No icing conditions- MEL

A

MEL restrictions that are generally associated with the Bleed Air System

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16
Q

Altitude Restrictions- MEL

A

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

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17
Q

Hazardous weather Restriction- MEL

A

MEL restrictions that are generally associated with the Weather Radar

18
Q

APU Constantly Running, Altitude Restriction- MEL

A

MEL restrictions that are generally associated with the Integrated Drive Generator

19
Q

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

A

Engine Cowls, Leading edges of wings

20
Q

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

A

Windshields, Pitot and Static ports

21
Q

Aircraft performance is planned

A

One engine inoperable

22
Q

Stages of the engine that are used for bleed air

A

6th and 10th

23
Q

V1 speed

A

Takeoff Decision Speed

24
Q

V2 speed

A

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

25
Q

VR speed

A

ROTATION SPEED (THE
NOSE WHEEL COMES OF
THE GROUND)

26
Q

Method 1 drift down

A

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.

27
Q

Method 2 drift down

A

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

28
Q

Engine cowl

A

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

29
Q

3B Pump

A

Emergency Backup Pump

30
Q

EGPWS

A

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.

31
Q

TCAS

A

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

32
Q

FMS

A

Flight Management System

33
Q

Maximum Takeoff weight CRJ

A

75,000 lbs

34
Q

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

A

400 kts

35
Q

IN WHAT MONTHS
DO WE USE
WINTER
PASSENGER
WEIGHTS?

A

November 1-April 30

36
Q

WHATDOES CDL
STAND FOR?

A

CONFIGURATION
DEVIATION LIST

37
Q

WHAT IS A
CONFIGURATION
DEVIATION LIST?

A

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

38
Q

WHAT ARE THE 3 PRIMARY
FUNCTIONS OF THE
APU?

A

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

39
Q

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

A

ONE ENGINE

40
Q

ACARS

A

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