CRJ 200 Limitations.

Question 0

Maximum ramp weight

Answer 0

53,250 lbs

Question 1

Kinds of operations

Answer 1

Transport category
Day and Night
VFR and IFR
Flight into icing conditions

Question 2

Maximum take off weight

Answer 2

53,000 lbs

Question 3

Maximum landing weight

Answer 3

47,000 lbs

Question 4

Maximum zero fuel weight

Answer 4

44,000 lbs

Question 5

Maximum take off and landing pressure altitude

Answer 5

10,000’

Question 6

Maximum operating altitude

Answer 6

41,000’

Question 7

Max take off and landing air temp

Answer 7

iSA +35

Question 8

Minimum take off and landing air temp

Answer 8

-40c / -40f

Question 9

cowl anti ice -Ground

Answer 9

On: OAT <= +10 & Visible moisture. Visibility <=1sm

On: Contaminated surfaces

Question 10

Cowl anti-ice in flight

Answer 10

On: TAT <= 10c and visible moisture except SAT <=-40c

On: when ICE annunciation illuminates by the ice detection system

Question 11

Wing anti-ice ground

Answer 11

On: OAT <=5c and visible moisture. Visibility < 1sm

Contaminated runway

When type II or IV fluid has been applied-just prior to applying take off thrust

Question 12

Wing anti-ice. Flight

Answer 12

On: ice annunciation illuminates by the ice detection system

When in icing conditions and airspeed is <=230 KIAS

Question 13

Super cooled large droplets (SLD) icing

Answer 13

Continued flight operations prohibited, identified by side window icing.

Question 14

It asks off permitted with frost

Answer 14

Upper surface of fuselage (see surface features)

Underside of cold soaked wing (1/8 in max)

Question 15

Runway slope

Answer 15

+- 2%

Question 16

Max tailwind component

Answer 16

10 Kts

Question 17

Minimum flight crew

Answer 17

1 pilot, 1 co-pilot

Question 18

Cargo limits

Answer 18

Flight within 60 minutes if cargo is in cargo compartment

Question 19

Ozone limits.

Answer 19

25 ppm, sea level equivalent at any time above FL320

.01 ppm equivalent time weighed average during any 3 hour interval above FL270

Sea level equivalent = 25c / 760 mm Mercury

Question 20

Engines

Answer 20

General Electric CF34-3B1

Question 21

N1 % RPM

Answer 21

98.6, O-98.5

Question 22

N2 % RPM.

Answer 22

99.3, 0-99.2

Question 23

Oil Temp. C

Answer 23

163 max
150-162 caution
-40 - 149 Normal

Question 24

Oil Pressure

Answer 24

0-25 Red 115-156 Caution 26-115 normal

Question 25

Airplane Cold Soak

Answer 25

> 8 hours at <(-30c, -22f) Before start, motor engines for 60 sec and verify fan rotation Actuate Thrust Reversers until deploy and stow cycles are less than 5 seconds

Question 26

Use of continuous ignition

Answer 26

Take off and landing on contaminated runway Rain > moderate Turbulence > moderate In the vicinity of thunderstorms Take off with high crosswinds

Question 27

Starter limitations

Answer 27

Starts 1&2, 60 seconds on, followed by 10 seconds off Starts 3 +, 60 seconds on, followed by 5 minutes off

Question 28

ITT Starting limits

Answer 28

At initiation of thrust lever movement from shut off to idle: ITT must be 120c or less for ground starts ITT must be less than 90 c for air starts

Question 29

N2 RPM limits for starts

Answer 29

N2 must be less than 55%

Question 30

Starter limits for motoring engine

Answer 30

Start 1: 90 seconds on, 5 minutes off Starts 2+: 30 seconds on, 5 minutes off

Question 31

Fuel capacity

Answer 31

``` Total = 14,518 Wings = 9520 Center = 4998 ```

Question 32

Minimum go-around fuel

Answer 32

450 lbs per wing, 10 nose up pitch max

Question 33

Max fuel imbalance in-flight

Answer 33

800 lbs

Question 34

APU type

Answer 34

Garrett GTPC-36-150RJ

Question 35

APU max RPM

Answer 35

107%

Question 36

APU maximum Temp

Answer 36

743c-974c

Question 37

APU Minimum Start Temp

Answer 37

-40c / -40 f

Question 38

APU maximum generator load

Answer 38

30 kVA

Question 39

APU altitude limits

Answer 39

Max Alt= FL370 Starting=FL300 Pneumatics=15,000'

Question 40

Vmo/Mmo

Answer 40

335kias / 0.85m

Question 41

Vt (turbulence)

Answer 41

280kias / 0.75m

Question 42

Max ADG operating speed

Answer 42

Dry ADG type, no limit

Question 43

Max windshield wiper

Answer 43

220 KIAS

Question 44

Maximum RVSM airspeed

Answer 44

O.83m

Question 45

Minimum airspeed

Answer 45

Vss (stick shaker)

Question 46

Vfe flaps 8

Answer 46

200 KIAS

Question 47

Vfe flaps 20

Answer 47

200 KIAS

Question 48

Vfe flaps 30

Answer 48

185 KIAS

Question 49

Vfe flaps 45

Answer 49

170 KIAS

Question 50

Flaps use prohibited

Answer 50

Enroute .flights with flaps extended at altitudes above 15,000'

Question 51

Vlo / Vle

Answer 51

250 KIAS

Question 52

Vlo ret

Answer 52

200 KIAS

Question 53

Max tire speed

Answer 53

182 Kts ground speed

Question 54

Max relief differential

Answer 54

+8.7 psi

Question 55

Min relief differential

Answer 55

-.5 psi

Question 56

Max taxi / takeoff / landing differential

Answer 56

+.1 psi

Question 57

Autopilot minimum use height

Answer 57

Take off = 600' NPA= 400' PA=80'

Question 58

Max generator load 0-FL350

Answer 58

Engine / APU generator = 30kVA

Question 59

Max generator load 35,001'-37,000'

Answer 59

Engine=25kVA | APU=30kVA

Question 60

Max generator load 37,001' and above

Answer 60

Engine only = 25kVA

Question 61

Max load, each TRU in flight

Answer 61

100 amps

Question 62

Max ground time, DC power only

Answer 62

5 minutes

Question 63

Use of spoilers prohibited

Answer 63

< 300' agl Less than approach speed +17 Kts

Question 64

Stall protection system switches

Answer 64

On for all phases of flight

Question 65

Fuel Balance for take off

Answer 65

Center tank > 500 lbs and wing tanks < 4400 lbs Or Minimum wing tank cannot be less than 2200 lbs and ZFW reduced by the amount of center fuel tank fuel over 500 lb limit And CG compliance

Question 66

Max fuel imbalance

Answer 66

Less than 800 lbs

Question 67

Min engine fuel temp

Answer 67

5c

Question 68

Min bulk fuel temp for takeoff

Answer 68

Jet a <=-30c Jet A1 <=-37c

Question 69

Powered Xfeed and gravity Xfeed for takeoff

Answer 69

Off

Question 70

Starter assist re-light. Bleed >60 psi | SFC to 15,000'

Answer 70

Sfc to 15,000': speed: Vref to Vmo N2: 0-55%

Question 71

Starter assist relight Bleed >60psi | 15,000' to 21,000'

Answer 71

Speed: 180 KIAS to Vmo N2: 0-55%

Question 72

Windmilling relight SFC to 15,000'

Answer 72

Speed: 300 KIAS to Vmo / Mmo N2: 9-55%

Question 73

Windmilling relight 15,000' to 21,000'

Answer 73

Speed: 300 KIAS to Vmo / Mmo N2: 12 to 55%

Question 74

Minimum flight weight

Answer 74

30,000 lbs

Question 75

Minimum BOW

Answer 75

25,480 lbs

Question 76

Minimum pavement for 180 turn

Answer 76

75'

Question 77

Dimensions

Answer 77

H=21' L= 88' W= 69'8"

Question 78

What doors are not on EICAS

Answer 78

Crew Hatch and Aft Equipment Hatch

Question 79

Max weight on door

Answer 79

1000 lbs (4 pax)

Question 80

Door EICAS colors

Answer 80

Cabin. Red, open. Amber, handle not latched, Green, closed All other Green closed, Amber open

Question 81

Engines and thrust

Answer 81

GE CF34 3B1 8729 normal 9220 APR

Question 82

APU functions

Answer 82

Primary is electric | Secondary is pneumatic

Question 83

Green line on Airspeed Tape

Answer 83

1.26 Vs

Question 84

Alignment times for AHRS

Answer 84

70 seconds Mag mode 10 minutes DG mode

Question 85

Deck utter criteria

Answer 85

Pitch 30 / -20 | Roll more than 65

Question 86

CRT and AVIONICS Cooling

Answer 86

Fan 1 flight Fan 2 ground Vented overboard with door open Underfloor door closed

Question 87

Function of Data Concentrator Unit

Answer 87

To collect data from A/C systems, processes and information and relays it to proper component display

Question 88

What audio warnings are not disabled with DCU Disable switch

Answer 88

EGPWS AND TCAS

Question 89

What happens if ED 1 fails

Answer 89

Automatically switches to ED2

Question 90

What items can be boxed on EICAS

Answer 90

White and Amber can be boxed Red and green cannot

Question 91

What does step button on EICAS Control do

Answer 91

Allows a sequential step thru all synoptic pages

Question 92

How does info get to FDR

Answer 92

EICAS sends alt, as, position, hug, acceleration and radio communication to the FDR

Question 93

Turning on the beacon or strobes or WOW senses airborne

Answer 93

What activates the FDR