CRJ-200 Study Guide

Question 1

Max Ramp Weight

Answer 1

53,250 lbs

Question 2

Max T/O Weight

Answer 2

53,000 lbs

Question 3

Max T/O OAT

Answer 3

ISA +35C

Question 4

Max X/Wind

Answer 4

27 Kts

Question 5

MMO

Answer 5

.85

Question 6

Max Alt

Answer 6

37,000’

Question 7

The CRJ-200 is a:

Answer 7

Twin engine, 50 seat regional jet

Question 8

Normal Crew:

Answer 8

CA, FO, and FA …an additional jump seat is located on the flight deck

Question 9

Passenger boarding is accomplished:

Answer 9

through the main cabin door via a jet bridge or the integral door stairs. The door stairs have a limitation of 4 people or 1000 lbs at any one time.

Question 10

Emergency egress is possible through:

Answer 10

The main cabin door, galley service door, two overwing emergency exits, and a cockpit escape hatch

Question 11

Powerplant:

Answer 11

2 General Electric CF34-3B1 High Bypass Turbofan Engines each producing 8,729 lbs of thrust under normal operations and 9,220 lbs with Automatic Performance Reserve active

Question 12

Total fuel capacity:

Answer 12

14,518 pounds of Jet A can be carried in 2 wing (4,760 each), and 1 center fuel tank (4,998 lbs).

Question 13

Fuel is transferred automatically from the center tank to the wing tanks

Answer 13

Via 2 motive flow transfer ejector pumps.

Question 14

Each wing tank transfers fuel to the respective engine’s

Answer 14

Collector tanks via scavenge ejector pumps (1 per side)

Question 15

Fuel is sent to each engine from the

Answer 15

Collector tanks to each engine via the main ejector pumps (1 per side)

Question 16

Supply motive flow for the fuel system:

Answer 16

2 fuel boost pumps and engine driven pumps

Question 17

Refueling is accomplished through a

Answer 17

Single point pressure refuel port or overwing fuel caps

Question 18

Provisions to jettison fuel inflight?

Answer 18

No

Question 19

Electrical System:

Answer 19

115 Volt AC, 28 Volt DC System.

6 AC buses & 10 DC buses

Question 20

Power can be provided by:

Answer 20

2 engine driven generators
1 APU Generator 
2 24 Volt batteries 
1 emergency Air Driven Generator (ADG)
Ground Power

Question 21

Convert AC to DC power:

Answer 21

5 Transformer Rectifier Units (TRUs) Each TRU has a max load of 100 amps.

Question 22

The ADG:

Answer 22

Automatically or manually deployed following a power loss and supplies emergency power to the AC and DC essential buses as well as hydraulic pump 3B. Maximum output of the ADG is 15 KVA

Question 23

Flight Controls:

Answer 23

Hydraulically powered elevators, ailerons, spoilerons, and rudder provide aircraft control.

Each flight control surface is powered by more than one hydraulic system for redundancy.

Question 24

Flaps are:

Answer 24

Electrically operated with detents at 0, 8, 20, 30, and 45 degrees

Question 25

Takeoffs are accomplished with

Landings are normally accomplished with

Answer 25

Flaps 8 or 20

Flaps 45

Question 26

Flight spoilers

Answer 26

Available to aid in descent management and are usable to 1000’ AGL.

Question 27

Immediate Action Checklist Memory Item

L (R) REV UNLOCKED Msg:

Answer 27

(1) Affected thrust lever………………………CONFIRM & IDLE
(2) Affected THRUST REVERSER,
EMER STOW………………………………………………SELECT
Refer to QRH POWERPLANT Section

Question 28

Immediate Action Checklist Memory Item

Smoke or Fumes Removal Procedure or
Smoke / Fire / Fumes Procedure

Answer 28

(1) Oxygen masks / smoke goggles…………………….ON, 100%
(2) Crew and cabin communication…………………..ESTABLISH
Refer to QRH SMOKE - FIRE Section