Crj 200/700/900 Aircraft Limitations

Front 1

Maximum 90 degree crosswind for takeoff and landing?

Back 1

27kts

Front 2

Maximum 90 degree crosswind for landing from a cat 2 approach?

Back 2

15kts

Front 3

Maximum headwind for landing from a cat 2 approach?

Back 3

16kts

Front 4

Maximum tailwind for takeoff and landing?

Back 4

10kts

Front 5

Maximum Operating Altitude in the 200?

Back 5

36,000ft

Front 6

Maximum Operating Altitude 700/900

Back 6

41,000ft

Front 7

Maximum Taxi/Ramp Weight 701

Back 7

75,250 lbs

Front 8

Maximum Taxi and Ramp Weight 900

Back 8

85,000 lbs

Front 9

Maximum Takeoff Weight 701

Back 9

75,000 lbs

Front 10

Maximum Takeoff Weight 900

Back 10

84,500 lbs

Front 11

Maximum Landing Weight 701

Back 11

67,000 lbs

Front 12

Maximum Landing Weight 900

Back 12

75,100 lbs

Front 13

Maximum Zero Fuel Weight 701

Back 13

62,300 lbs

Front 14

Maximum Zero Fuel Weight 900

Back 14

70,750 lbs

Front 15

Turbulence Penetration Speed

Back 15

280 KIAS/.75M whichever is lower

Front 16

Max Gear Extension Speed

Back 16

220 KIAS

Front 17

Maximum Gear Extended Speed

Back 17

220 KIAS

Front 18

Maximum Gear Retraction Speed

Back 18

200 KIAS

Front 19

Maximum Speed for Windshield Wiper Operation

Back 19

220 KIAS

Front 20

Flaps 1 speed 701/900

Back 20

230 KIAS

Front 21

Flaps 8 Speed

Back 21

230 KIAS

Front 22

Flaps 20 Speed

Back 22

220 KIAS

Front 23

Flaps 30 Speed

Back 23

185 KIAS

Front 24

Flaps 45 Speed

Back 24

170 KIAS

Front 25

During Taxi or Takeoff when would you only activate Cowl Anti-Ice?

Back 25

Ground contamination or visible moisture with an OAT 10°c or below.

Front 26

During Takeoff when would you activate both Wing and Cowl Anti-Ice systems?

Back 26

With ground contamination or visible moisture with an OAT 5°c or below.

Front 27

In flight what conditions would require the use of only Cowl Anti-Ice?

Back 27

Visible moisture from TAT 10°c to SAT -40°c and an airspeed greater than or equal to 230 KIAS.

Front 28

In flight what conditions would require the use of both Wing and Cowl Anti-Ice systems?

Back 28

Visible moisture from TAT 10°c to SAT -40°c and an airspeed less than 230 KIAS.

Front 29

If the Ice Annunciation illuminates what is the response?

Back 29

Wing and Cowl Anti-Ice systems on.

Front 30

What does a red engine EICAS message signify?

Back 30

Maximum and minimum limitations.

Front 31

What does an Amber engine EICAS message indicate?

Back 31

Caution range

Front 32

What does a green engine EICAS message indicate?

Back 32

Normal operating range.

Front 33

When are there no limitations on applying TOGA thrust due to wind direction?

Back 33

Wind within 30° of the nose, or more than 30° with a wind speed less than 5 kts

Front 34

When may you only apply 75% N1 before brake release on takeoff?

Back 34

Wind more than 30° off the nose between 5 kts and 30 kts.

Front 35

When may you only apply idle/taxi thrust before brake release on takeoff?

Back 35

Wind more than 30° off the nose with a windspeed greater than 30 kts.

Front 36

Engine start crank limits first start.

Back 36

90 seconds on 10 off. 7/9

60 seconds on 10 off. 2

Front 37

Engine start crank limits second start.

Back 37

90 seconds on then 10 seconds off. 7/9

60 seconds on then 10 seconds off. 2

Front 38

Engine start crank limits third and subsequent starts.

Back 38

90 seconds on 5 minutes off 7/9

60 seconds on 5 minutes off 2

Front 39

Minimum oil pressure for takeoff

Back 39

45 psi

Front 40

Max fuel imbalance for takeoff 701/900

Back 40

300 lbs

Front 41

Max fuel imbalance all phases other than takeoff 701/900

Back 41

800 lbs

Front 42

Maximum fuel quantity in pounds 701/900

Back 42

19,594 lbs

Front 43

What must the ITT be below for all ground starts?

Back 43

120°c

Front 44

Bleed air extraction for air conditioning from the APU is not permitted

Back 44

At or above 25,000 ft

Front 45

Which engines may be started using the APU as the bleed source?

Back 45

Each engine may be started using the APU

Front 46

What is the APU starter motor duty cycle?

Back 46

No more than 3 starts/start attempts in 1 hour with 2 minutes between each cranking attempt.

Front 47

If the APU door is not closed, or the position is unknown what precautions must be taken?

Back 47

Airspeed limited to 220 KIAS (300 KIAS in the 200), or the APU must remain in operation.

Front 48

What is ground contamination?

Back 48

Runways, ramps, or taxiways with surface snow, ice, slush, or standing water.

Front 49

What is visible moisture?

Back 49

Visible moisture or precipitation in any form (including fog with vis 1sm or less) is present in flight or below 400 ft agl for takeoff.

Front 50

Do not hold in icing conditions with...

Back 50

Slats/flaps extended

Front 51

When must a tactile check be performed?

Back 51

OAT 10°c or less

Bulk fuel 0°c or less

Atmospheric conditions conducive for frost

Ice and frost may continue to adhere to wing surfaces even at temps above 10°c

Front 52

Max itt of thrust lever from shut-off to idle?

Back 52

120°c or less

Front 53

After starting the engines do not exceed...

Back 53

75% N1 for 2 minutes or until engine indicators are in the green, whichever is longer.

Front 54

Operate all engines at or near idle for...

Back 54

2 minutes prior to shutdown

Front 55

Min oil pressure for takeoff?

Back 55

45 PSI

Front 56

When must continuous Ignition be used?

Back 56

Takeoff/landing on contaminated runway

Takeoff with crosswind >15kts

Flight through moderate or heavier intensity rain

Flight through moderate or greater turbulence

Flight in vicinity of thunderstorm

Front 57

Maximum single pack altitude 701

Back 57

31,000ft

Front 58

Max altitude single pack 900

Back 58

25,000ft

Front 59

Minimum autopilot engagement altitude under normal circumstances?

Back 59

600ft

Front 60

Minimum auto pilot engagement altitude on a non precision and precision approach respectively?

Back 60

400 ft / 80 ft

Front 61

What auto pilot mode is prohibited during approach?

Back 61

Speed

Front 62

Maximum slats/flaps extension altitude?

Back 62

15,000ft

Front 63

Enroute use of slats/flaps

Back 63

Is prohibited

Front 64

Minimum altitude for flight spoiler deployment?

Back 64

1,000ft agl

Front 65

Minimum speed for flight spoilers?

Back 65

Ref +17kts

Front 66

Minimum brake cooling time after a RTO

Back 66

15 minutes and all BTMS must indicate green and not be increasing

Front 67

Max time for taxi light operation while stationary?

Back 67

No longer than 10 minutes

Front 68

Draw the RVSM required equipment list.

Back 68

Front 69

How much fuel may be in the center tank during Takeoff?

Back 69

500 lbs unless there is at least 4,400 lbs in each wing tank.

Front 70

Maximum runway slope

Back 70

2% takeoff or landing

Front 71

Max temp for takeoff

Back 71

ISA +35

Front 72

Minimum temperature

Back 72

-40°c

Front 73

Max windshield failed non parked speed

Back 73

250 KIAS

Front 74

Tire Limit Ground Speed

Back 74

700/200-182kts 900-195kts

Front 75

Max cruise Mach in RVSM airspace

Back 75

.82 mach

Front 76

Max altitude to start the APU?

Back 76

37,000ft

Front 77

Max APU running altitude

Back 77

41,000ft

Front 78

Permissible AC electric load

Back 78

40 kVA

Front 79

Max load on each TRU

Back 79

120 amps

Front 80

Max itt for a 200/700/900 ground start.

Back 80

120°c

Front 81

What conditions would be considered cold soaked?

Back 81

-30°c or below for more than 8 hours

Front 82

What are the cold soak starting procedures?

Back 82

Motor engines for 60 seconds and verify fan rotation.

Thrust reversers must be actuated until stow and deploy cycles are 2 seconds or less.

Front 83

Max continuous oil temperature

Back 83

155°c

Front 84

Dry motor cycle limits

Back 84

First: 90 seconds on 5 minutes off

Second and subsequent: 30 seconds on 5 minutes off

Front 85

When would you not use FLEX takeoff?

Back 85

Anti-skid inop

Contaminated runway

Airplane has been de-iced

Wing or Cowl Anti-Ice in use

Any windshear/downdraft warnings

Engine cannot create full thrust

When a departure calls for full thrust

Front 86

Engine fuel temp must be at least what temperature for takeoff?

Back 86

5°c

Front 87

Contaminated runway landing is prohibited when

Back 87

Standing water more than .75 inches

Slush or wet snow is more than .88 inches

Dry snow more than 3.75 inches

Front 88

Max pressure altitude for takeoff and landing

Back 88

8,000ft

Front 89

Maneuvering limit load factors

Back 89

Flaps up: -1 to 2.5

Flaps down: 0 to 2

Front 90

Max pressure differential during ground ops?

Back 90

.1psi

Front 91

Max pressure differential at touchdown?

Back 91

1.0psi

Front 92

Do not exceed what cabin Altitude when In manual mode?

Back 92

-1,500ft

Front 93

Max altitude to use APU to start the engines?

Back 93

21,000ft

Front 94

What time limit is applied to the usage of normal takeoff power and maximum power?

Back 94

Limited to 5 minutes

Front 95

APR power usage single engine is limited to

Back 95

10 minutes

Front 96

APR power is prohibited

Back 96

Above 7,500ft

Front 97

Max itt for airstart

Back 97

90°

Front 98

In flight starter cranking limits

Back 98

2 minutes on 10 seconds off

Then 1 minute on 5 minutes off

Front 99

After deploying thrust reversers

Back 99

Do not attempt a go around

Front 100

Turning radius of 700

Back 100

75ft

Front 101

Min fuel per wing tank for a go around

Back 101

600lbs 7/9

450lbs 2

Front 102

Cat 2 approaches not allowed when braking action is less than

Back 102

Fair