Asa Crj-200 Limitations

Front 1

Max. Ramp Weight (MRW)

Back 1

53,250 lbs

Front 2

Max. Takeoff Weight (MTOW)

Back 2

53,000 lbs

Front 3

Max. Landing Weight (MLW)

Back 3

47,000 lbs

Front 4

Max. Zero Fuel Weight (MZFW)

Back 4

44,000 lbs

Front 5

Max. Cargo Capacity

Back 5

3,500 lbs

Front 6

Max. Airport Pres. Alt. for Takeoff/Landing

Back 6

10,000 ft

Front 7

Max Operating Alt.

Back 7

41,000 ft

Front 8

Max Ambient Air Temp for Takeoff/Landing

Back 8

ISA +35°C

Front 9

Min Ambient Temp for Takeoff/Landing

Back 9

-40°C

Front 10

Cowl Anti-Ice (Ground)

Back 10

OAT <= 10°C and vis. moisture (fog with vis. < 1sm, rain, snow, sleet, ice).
OAT <= 10°C and surface snow, ice, standing water, or slush.

Front 11

Cowl Anti-Ice (Air)

Back 11

TAT <= 10°C and vis. moisture, except < -40°C

MUST be ON:
In icing conditions
ICE annunciation

Front 12

Wing Anti-Ice (Ground)

Back 12

On for Takeoff when TAT <= 5°C and vis. moisture
On for Takeoff when TAT <= 5°C and runway contaminated with surface snow, slush, or standing water.
When type 2 or 4 fluid applied to wing, ON just prior to thrust applied for takeoff.

Front 13

Wing Anti-Ice (Air)

Back 13

TAT <= 10°C and vis. moisture

MUST be ON:
ICE annunciation, or
Icing conditions and airspeed < 230 KIAS

Front 14

Super-Cooled Large Droplet Icing

Back 14

Continued Ops Prohibited.
SLD indicated by ice accretion on flight compartment side windows.
Wing and Cowl anti-ice must be ON.
Leave icing conditions immediately when side window icing occurs.

Front 15

Cold Weather Ops (General)

Back 15

Takeoff prohibited with frost, ice, snow, or slush adhering to critical surfaces.

Front 16

Cold Weather Ops (Tactile Check)

Back 16

Tactile Check required when OAT <= 5°C or wing fuel temp <= 0°C and:
Vis. moisture, or
Water on wing, or
Difference between dew point and OAT is 3°C or less, or
Atmospheric conditions conducive to frost formation.

Front 17

Runway Slopes

Back 17

+/- 2%

Front 18

Max. Tailwind for Takeoff/Landing

Back 18

10 kts

Front 19

Min. Flight Crew

Back 19

1 pilot, 1 copilot

Front 20

Color Logic

Back 20

RED - Max/Min limitations
AMBER - Caution Range
GREEN - Normal Op Range

Front 21

Airplane Cold Soak

Back 21

Before first flight of day, and aircraft is cold soaked for more than 8 hours,

engines motored for 60 seconds and fan rotation verified before start initiated.

Thrust reversers must be actuated until deploy/stow cycles are < 5 seconds.

Front 22

Continuous Engine Ignition (Must be on when (2 Takeoffs, 2 others)

Back 22

Must be used:
Takeoff/landing on contaminated rwy.
Takeoff with crosswind comp. > 10 kts.
Mod. or heavier rain or turbulence.
In vicinity of thunderstorms.

Engine ops at or near shaker predicated on operable auto-ignition system.

Front 23

Starter Cranking Limits (Ground/Air) (Regular/ITT limits/Dry Motoring)

Back 23

Starter not used if N2 exceeds 55%.

1st - Max 1 min. - 10 seconds off
2nd - Max 1 min. - 10 seconds off
3+ - Max 1 min. - 5 min. off


Thrust lever SHUT-OFF to IDLE:
Ground ITT 120°C or less
Air ITT 90°C or less


Dry Motoring

Thrust levers SHUT-OFF

1st - 90 sec. - 5 min. off
2+ - 30 sec. - 5 min. off

Front 24

Reduced Thrust (N1 speeds, when not to be used)

Back 24

APR always used.
Cannot be used if normal takeoff fan speed < 85% N1
Cannot be used if reduced fan speed < 85% N1

Cannot be used:
First flight of the day for aircraft.
Wing/Cowl Anti-ice on.
Contaminated runways (Standing water, snow, slush or ice).
Warnings of windshear/downdrafts forecast.

Can be used on wet runway with wet runway performance data.

Front 25

Max. Fuel Imbalance (L/R)

Back 25

800 lbs

Front 26

Fuel - Max. Center for Takeoff

Back 26

500 lbs with less than 4,400 lbs in each wing

Front 27

Fuel - Go Around Fuel Requirement

Back 27

450 lbs with airplane level, assuming max 10° nose up.

Front 28

APU Start Cycle (On Batteries)(Ground/Air)

Back 28

1st - 30 sec.
2nd - 30 sec. - 20 min. off
3rd - 30 sec.
4th - 30 sec. - 40 min. off

2 minute delay between attempts for cooling/drainage.

Front 29

APU Bleed Air for PACKs

Back 29

15,000 ft

Front 30

APU Bleed Air for Engine Start on Ground

Back 30

None. But operating engine N2 cannot exceed 70%.

Front 31

APU Bleed Air for Engine Start in Air

Back 31

Not permitted for Single-engine ops.

Permitted for Double-engine failure below 13,000 ft.

Front 32

APU usage (Altitudes)

Back 32

37,000 - Operating
30,000 - APU Start
15,000 - PACKs
13,000 - Engine Start

Front 33

Engine Stabilization (Takeoff/Landing)

Back 33

Prior to Takeoff: 2 minutes

Prior to Shutdown: 2 minutes at IDLE. Taxi time below 80% N2 is counted.

Front 34

Flap Speeds

Back 34

Flaps 8° - 215 KIAS
Flaps 20° - 215 KIAS
Flaps 30° - 185 KIAS
Flaps 45° - 170 KIAS

Front 35

Landing Gear Operating Speeds (safe to extend, safe to retract)

Back 35

Extend - 250 KIAS
Retract - 200 KIAS

Front 36

Turbulence Penetration Speed

Back 36

280 KIAS or 0.75 Mach (lesser of two)

Front 37

Minimum Operating Limit Speed

Back 37

Not below onset of stall warning (shaker) unless specifically authorized for flight test or training ops.

Front 38

Max. Takeoff Wind Speed - Total

Back 38

60 kts

Front 39

Max. Takeoff Headwind Component

Back 39

55 kts

Front 40

Crosswind Limitations (Max. Demo, Wet Rwy, Contaminated Rwy, Low-Time Capt.)

Back 40

Max Demo - 27 kts
Wet Runways - 17 kts
Contaminated - 15 kts
Low-time Capt - 27 kts

Contaminated means braking less than Good (MU value < 40)

Low-time Capt is < 100 hrs PIC in type (CR2)

Front 41

Minimum Autopilot Altitude

Back 41

600 ft AGL unless:

Visual/Non-Prec. Appr. - 400 ft AGL but no lower than 50 ft below DDA (higher of the two).

Prec. Appr. - 80 ft AGL but not lower than 50 ft below DA (higher of two).

Use of DES mode (FD or AP coupled) during approach not permitted.

Front 42

10th Stage Bleed Air for Takeoff/Landing

Back 42

Closed if cowl and/or wing anti-ice is on.

Front 43

Max. Operation Time on DC Power (Ground)

Back 43

5 min. for CRT display protection (lack of cooling)

Front 44

Circuit Breaker Reset in Flight

Back 44

Permitted only in compliance with OM/QRH or if judgement of PIC deems necessary for safe ops.

Front 45

Flap Usage

Back 45

Not permitted en-route.
Not permitted above 15,000 ft.

Front 46

Flight Spoiler Usage

Back 46

Not permitted:

Below recommended appr. speed plus 17 KIAS.
Below 800 ft AGL.
Flaps > 30°

Front 47

When must both stall protection switches be on?

Back 47

All phases of flight.

Front 48

Engine Ops near/at shaker are predicated on what?

Back 48

Operating auto-ignition system.

Front 49

When must taxi lights be off?

Back 49

Airplane stationary > 10 minutes

Front 50

Takeoff not permitted when what messages are displayed? (Thrust Rev.)

Back 50

THRUST REVERSER UNLK light
REV icon on N1 gauge
L or R REV UNLOCKED caution message

Front 51

Max. Full Thrust-Reverse Speed

Back 51

60 KIAS

IDLE below 60 KIAS is permitted

Front 52

Can thrust reverse be used for pre-flight when airplane is stationary?

Back 52

Yes, IDLE only

Front 53

Can thrust reverse be used for taxi?

Back 53

No, used for taxi only in emergency.

Front 54

Min. BTMS Cooling Period Between Landing/RTO and Next Takeoff

Back 54

15 minutes

Front 55

TCAS RA Compliance and Exceptions

Back 55

Pilot must comply with RAs.

Exceptions:
Performance limited, such as engine failure.
Conditions such that it can be seen that there is an obvious error or malfunction in the TCAS.

Front 56

Integrated Standby Instrument (ISI) with ILS tuned while on BackCourse

Back 56

ISI will show loc and glideslope deviation. Use of this information is prohibited.