Asa Crj-200 Limitations V2

Front 1

Maximum takeoff weight

Back 1

53,000lbs

Front 2

Maximum ramp weight

Back 2

53,250lbs

Front 3

Maximum landing weight

Back 3

47,000lbs

Front 4

Maximum zero fuel weight

Back 4

44,000lbs

Front 5

Cargo compartment is limited to _______ lbs.

Back 5

3,500lbs

Front 6

Maximum airport pressure altitude for takeoff and landing?

Back 6

10,000ft

Front 7

Maximum Operating Altitude

Back 7

41,000ft

Front 8

Maximum ambient air temperature for takeoff and landing?

Back 8

ISA+35C

Front 9

Minimum ambient temperature approved for takeoff?

Back 9

M40C

Front 10

Cowl Anti-ice Must be on ...

1) Temperature and Condition

2) Temperature and Environment

Back 10

1) When OAT is +10C or less with any visible moisture

2) When OAT is +10C or less and operating on a contaminated runway.

Front 11

What two anti-ice devices must be on in Super-Cooled Large Droplet Icing conditions?

Back 11

1) Wing Anti-Ice

2) Cowl Anti-Ice

Front 12

Wing Anti-Ice must be on when:
-Flight Operations
1) _________
2) _________

Back 12

1) When Ice is annunciated by the ice detection system

2) In icing conditions and airspeed is below 230kts

Front 13

Wing Anti-Ice must be on when:
-Ground Operations
1) ________
2) ________
3) ________

Back 13

1) Must be on for takeoff when OAT is 5C or less and visible moisture
2) Must be on for takeoff when OAT is 5C or less and on contaminated runway.
3) When Type II or Type IV anti-icing has been applied

Front 14

Maximum approved runway slope for takeoff and landing?

Uphill: ___%
Downhill: ___%

Back 14

+2% Uphill

-2% Downhill

Front 15

Maximum Tailwind Component

Back 15

10kts

Front 16

Minimum Flight crew?

Back 16

1 Pilot
1 Co-Pilot

Front 17

EICAS Color meanings?

1) Red
2) Amber
3) Green

Back 17

1) Maximum and Minimum limitations
2) Caution Range
3) Normal Operating Range

Front 18

Associated conditions for movement from Shut off to Idle

1) ITT for ground
2) ITT for air

Back 18

1) ITT Ground: 120C or less for all ground starts

2) ITT Air: 90C or less for all air starts

Front 19

APU Bleed Air Limitations

Condition: Air Conditioning
Limitation: _____________

Back 19

No Bleed air extraction above 15,000ft.

Front 20

APU Bleed Air Limitations

Condition: Engine Start During Flight
Limitation: __________

Back 20

Not permitted for Single Engine Operations. Permitted for Double Engine failure conditions, limited to 13,000ft and below.

Front 21

APU Bleed Air Limitations

Condition: Engine Start During Ground
Limitation: ________ (and Key N2 setting?)

Back 21

No Limitation. May be used, but engines' thrust must not exceed 70% N2.

Front 22

How much delay should be observed between APU cranking attempts?

Back 22

Two (2) Minutes

Front 23

APU Starting

Min Temp for start? ____C

Back 23

M40C

Front 24

APU Starting

Start Cycles

Max time ON for all attempts?

Back 24

30 Seconds

Front 25

APU Starting

Start Cycles

Min time OFF for attempts Two (2) and Four (4)?

Back 25

Attempt 2: 20 Minutes Off

Attempt 4: 40 Minutes Off

Front 26

APU

1) Max RPM: ___%

2) Max EGT: ___C

Back 26

1) 107%

2) 743C

Front 27

APU Cranking

How long of a delay should be observed between cranking attempts to allow for cooling of starter and start contactor and for APU drainage?

Back 27

Two (2) Minutes

Front 28

Engine Start

The starter must not be used if indicated N2 RPM exceeds ___%.

Back 28

55%

Front 29

Engine Start Cranking Limits

Start attempts one, two, three and any subsequent attempts have a max time ON of ________.

Back 29

One (1) Minute

Front 30

Engine Start Cranking Limits

Start attempts one and two have a max time on of one (1) minute, followed by ________ seconds off.

Back 30

10 Seconds

Front 31

Engine Start Cranking Limits

Start attempts three and any subsequent attempts have a max time on of one (1) minute, follow by ________ minutes off.

Back 31

5 Minutes

Front 32

Dry Motoring Cycle

Start 1 has a max time on of (1)_____ followed by (2)______ off.

Back 32

1) 90 Seconds On
2) Five (5) Minutes off

Front 33

Dry Motoring Cycle

Starts 2 and any subsequent starts have a max time on of (1)______ followed by (2)_____ off.

Back 33

1) 30 Seconds On
2) Five (5) Minutes off

Front 34

When must Continuous Engine Ignition be used?

Five (5) Items

Back 34

1) Takeoff on contaminated runway
2) Takeoffs with high crosswinds
3) Moderate or greater rain
4) Moderate or greater turb
5) Flight in the vicinity of thunderstorms

Front 35

For the following conditions:

First flight of the day, cold soak at less than M30C for more than 8 hours

Engines must be motored for (1)_______ seconds and rotation must be (2)________.

Back 35

1) 60 Seconds
2) verified

Front 36

In a cold soak at M30C or less for more than eight (8) hours, thurst reversers must be actuated until the deploy and stow cycles are less than ____ seconds.

Back 36

Five (5) seconds

Front 37

Engines must be running for (1)______ minutes prior to (2)_______.

Back 37

1) Two (2) Minutes
2) Takeoff

Front 38

Engines should be operated at (1)_______ for (2)_____ minutes prior to shutdown.

Key N2 setting for cool-down period? (3)

Back 38

1) Idle
2) Two (2) Minutes
3) 80% N2

Front 39

Max Operating Speed for Flaps 8

Back 39

215kts

Front 40

Max Operating Speed for Flaps 20

Back 40

215kts

Front 41

Max operating speed for Flaps 30

Back 41

185kts

Front 42

Max Operating Speed for Flaps 45

Back 42

170kts

Front 43

Max gear extend speed?

Back 43

250kts

Front 44

Max airspeed gear should be retracted?

Back 44

200kts

Front 45

Max airspeed with gear extended?

Back 45

250kts

Front 46

Maximum airspeed for turbulence penetration is (1)____KIAS or (2) ____ Mach, whichever is (3) ______.

Back 46

1) 280
2).75M
3) Lower

Front 47

Minimum Operating Limit Speed:

Intentional speed reduction below the onset of stall warning, as defined by (1) _________ operation, is (2) ________ unless a lower speed is specifically authorized for flight test or training purposes.

Back 47

1) stick shaker
2) prohibited

Front 48

Do not attempt to takeoff or land with wind speeds in excess of (1)____ or a head-wind component that exceeds (2) ____.

Back 48

1) 60kts
2) 55kts

Front 49

Max demonstrated crosswind component for takeoffs and landings

1) Wet/Dry RWY
2) Contaminated RWY with braking action less than good
3) Captain has less than 100 hours PIC

Back 49

1) 27kts
2) 15kts
3) 27kts

Front 50

Reduced thrust can not be used if normal takeoff fan speed is less than ____% N1

Back 50

85%

Front 51

If reduced thrust can be used, the fan speed for the reduced engine thrust must not be lower than ____% N1.

Back 51

85%

Front 52

Flex (Reduced) Thrust must not be used during the following conditions:

1)
2)
3)
4)

Back 52

1) First flight of the day
2) If wing/cowl anti-ice bleeds are in use
3) Contaminated runways
4) Windshear conditions exists or have been forecast

Front 53

What is the maximum fuel imbalance between the left main tank and right main tank?

Back 53

800lbs

Front 54

Takeoff with fuel loads in excess of (1)___lbs in the center tank is permitted unless each wing tank is above (2)______lbs.

Back 54

1) 500lbs
2) 4,400lbs

Front 55

(1)_____lbs is the minimum fuel quantity for a go-around.

Assuming a maximum airplane climb attitude of (2)___ degrees up.

Back 55

1) 450lbs per wing
2) 10 Degrees

Front 56

Autopilot operation is prohibited below (1)_____ft, except for three circumstances.

Back 56

1) 600ft AGL

Front 57

Autopilot may be used below 600ft AGL when performing the following:
1) Visual and Non-Precision Approaches: ____ AGL
2) Precision Approaches: ____ AGL

Back 57

1) 400ft AGL, but not lower than 50ft below the applicable DDA, whichever is higher
2) 80ft AGL, but not lower than 50ft below the applicable DA, whichever is higher.

Front 58

The Bleed Air 10th stage valves must be closed for (1) ________ and (2) _______ if the engine (3) _______ and/or (4) _______ anti-ice systems have been selected on.

Back 58

1) Takeoff
2) Landing
3) Cowl
4) Wing

Front 59

To protect the flight compartment CRT displays, what is the max time on the ground to be using DC Power?

Back 59

5 Minutes

Front 60

A circuit breaker must not be reset or cycled in flight unless doing so is consistent with procedures in what documents?

Back 60

CR2 OM/QRH.

The PIC may deviate from this as needed for safety of flight.

Front 61

En-route use of flaps are __________.

Back 61

Prohibited

Front 62

What is the maximum altitude for flaps extended?

Back 62

15,000ft

Front 63

Flight spoilers must not be deployed when within what airspeed?

Back 63

Approach speed plus 17kts.

Front 64

Flight spoilers must not be extended in flight below an altitude of ______AGL.

Back 64

800ft AGL

Front 65

Flight spoilers must not be extended in flight when wing-flaps are extended beyond ____ degrees.

Back 65

30 Degrees

Front 66

Stall protection switches must _______ ___ for all phases of flight.

Back 66

Remain on

Front 67

Engine operation at or near shaker and pusher settings is predicated on an operable ________________.

Back 67

Auto-ignition system

Front 68

Taxi lights must be switched (1)____ whenever the airplane is stationary more than (2)____ minutes.

Back 68

1) Off
2) Ten (10) minutes

Front 69

Takeoff is prohibited with what three reverser EICAS messages displayed?

Back 69

1) THRUST REVERSER UNLK light
2) REV icon on N1 gauge
3) L or R REV UNLOCKED caution message

Front 70

Below (1)____ kts, reverse thrust must be reduced to (2)____.

Back 70

1) 60
2) Idle

Front 71

During pre-flight check of the thrust reversers with the airplane stationary, reverse thrust must remain at ________ _______.

Back 71

Reverse idle

Front 72

Use of reverse thrust is prohibited during ______ taxi operations. May be used during emergency situations.

Back 72

Normal

Front 73

What is the wait period between a rejected takeoff or a landing stop that triggered a BTMS indication and a future takeoff?

Back 73

15 Minute cool-down period.

Front 74

What exceptions may a pilot not comply with a TCAS RA?

1)
2)

Back 74

1) Aircraft performance is limited such as with an engine failure
2) Conditions are such that it can be seen that there is an obvious error or malfunction in the TCAS.

Front 75

Integrated Standby Instrument

May you use the ISI for backcourse approaches?

Back 75

Never. Backcourse approaches are prohibited when using the ISI.