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CRJ-200 Limitations
Comair Flight Standards Chapter 2 Limitations
76
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Professional
03/30/2008
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Term
Maximum Taxi and Ramp Weight
(51k models)
 Definition
51,250
Term
Maximum Taxi and Ramp Weight
(53k models)
 Definition
53,250
Term
Maximum Takeoff Weight
(53k models)
 Definition
53,000
Term
Maximum Landing Weight
(all models)
 Definition
47,000
Term
Maximum Zero Fuel Weight
(all models)
 Definition
44,000
Term
On the ground, Cowl Anti-ice must be ON when OAT is below______and______,or______.
 Definition

10*C(50*F)

 

visible moisture in any form is present(fog with visibility of 1SM or less, rain, snow, sleet and ice crystals).

 

when operating on runways, ramps, or taxiways where surface snow, ice, standing water, or slush is present.
Term
Icing conditions exist in flight at a TAT of________or below, and visible moisture in any form is encountered, except when_______________.
 Definition
10*C(50*F)

SAT is -40*C(-40*F) or below
Term
In flight, Cowl Anti-ice must be ON when_________or___________.
 Definition
in icing conditions when ice is annunciated by the Ice Detection System.
Term
Wing anti-ice must be ON for takeoff when the OAT is________or below and_________or________.
 Definition
5*C(41*F)

visible moisture in any form is present

when the runway is contaminated with surface snow, slush, or standing water.
Term
When Type II, Type III, or type IV anti-icing fluids have been applied, select anti-ice ON_____________.
 Definition
just prior to thrust increase for takeoff.
Term
Wing anti-ice must be ON in flight when__________or__________.
 Definition
ICE is annunciated by the Ice Detection System,

when in icing conditions and airspeed is less than 230 KIAS
Term
Engine starting limits
(all engine models)

N2____, N1____, ITT____
 Definition
N2 - 20%

N1 - not specified

ITT - 900*C
Term
Engine Idle limits
(all engine models)

N2____, N1____, ITT____
 Definition
N2 - 56.5%-68.0%

N1 - not specified

ITT - not specified
Term
Engine Acceleration limits
(all engine models)

N2____, N1____, ITT____
 Definition
N2 - not specified

N1 - not specified

ITT - 900*C
Term
Max Continuous Engine Limits
(3A1)

N2____, N1____, ITT____
 Definition
N2 - 99.2%

N1 - 98.6%

ITT - 860*C
Term

Max Continuous Engine Limits

(3B1)

 

N2____, N1____, ITT____

 Definition

N2 - 99.2%

 

N1 - 98.6%

 

ITT - 874*C
Term

Normal Takeoff Engine limits

(all engine models)

N2____, N1____, ITT____

 Definition

N2 - 98.3%

N1 - 96.2%

ITT - 884*C for 5 minutes(900 for 2 out of 5 transient minutes)
Term

Go-Around or APR Takeoff Engine limits

(all engine models)

N2____, N1____, ITT____

 Definition

N2 - 99.4%

N1 - 98.6%

ITT - 900*C for 5 minutes(928 for 2 out of 5 transient minutes)
Term
Engine to engine N2 split at ground idle should not exceed________.
 Definition
2%
Term
If N2 is_____% or less with an OAT of_____ or colder, do not accelerate above idle.
 Definition
57%

-20*C
Term
Minimum oil temp for starting is______.
 Definition
-40*C
Term
Maximum continuous oil temp is______.
 Definition
155*C
Term
Maximum permissible oil temp is______.
 Definition
163*C(15 minutes maximum)
Term
Minimum oil pressure for takeoff is_____.
 Definition
45 PSI
Term
Engine must remain at idle until oil pressure_________.
 Definition
returns to normal limits
Term
Maximum transient oil pressure after cold start is______.
 Definition
156 PSI (130 PSI at idle, 10 minutes maximum)
Term
Continuous ignition must be used under what circumstances?
 Definition
Takeoff/landing on contaminated runway

Takeoff with high crosswind component

Flight through moderate or greater turbulence

Flight through moderate or heaver rain

Flight in vicinity of T-storms (where lightning strikes may be encountered)
Term
Engine operation at or near shaker and pusher settings is predicated on_________.
 Definition
an operable auto-ignition system
Term
APR OFF performance must be used if___________caution message is displayed.
 Definition
APR INOP
Term
APR OFF performance must be used if ambient temp is__________or below, and PA is less than_________feet.
(3A1 engines only)
 Definition
-18*C(0*F)

1000 ft
Term
Engine starter limits:

1st: max time ON____followed by____OFF
2nd: max time ON____followed by____OFF
3rd+: max time ON____followed by____OFF
 Definition
1st: 1 minute ON, 10 seconds OFF
2nd: 1 minute ON, 10 seconds OFF
3rd+: 1 minute ON, 5 minutes OFF
Term
Engine dry-motoring limits:

1st: max time ON____followed by____OFF
2nd+: max time ON____followed by____OFF
 Definition
1st: 90 seconds ON, 5 minutes OFF
2nd+: 30 seconds ON, 5 minutes OFF
Term
At initiation of start(thrust lever movement from SHUTOFF to IDLE):

Max ITT for all ground starts is_____
Max ITT for all air starts is_____
 Definition
120*C

90*C
Term
Maximum permissible fuel imbalance between main left tank and main right tank is____.
 Definition
800 lbs
Term
Fuel remaining when fuel quantity indicator reads zero is_____.
 Definition
not usable
Term
Takeoff with a fuel load in excess of_____in the center tank is not permitted unless each main wing tank is above_____.
 Definition
500 lbs

4400 lbs
Term
Minimum fuel quantity for go-around is_____ lbs per wing, assuming a maximum climb attitude of_____.
 Definition
450 lbs

10* nose up
Term
Takeoff with engine fuel temperature below_____is prohibited.
 Definition
5*C(41*F)
Term
With the APU door open(APU message on EICAS indicates DOOR---), limit airplane speed to_____KIAS OR_____.
 Definition
300 KIAS

APU must remain in operation
Term
Maximum flap extended speeds:

Flaps 08:_____
Flaps 20:_____
Flaps 30:_____
Flaps 45:_____
 Definition
Flaps 08: 215 KIAS
Flaps 20: 215 KIAS
Flaps 30: 185 KIAS
Flaps 45: 170 KIAS
Term
Maximum speed to extend landing gear
 Definition
250 KIAS
Term
Maximum speed to retract landing gear
 Definition
200 KIAS
Term
Maximum speed for aircraft with landing gear extended and locked
 Definition
250 KIAS
Term
Due to ADC tolerance it is possible to get momentary overspeed clacker when the flaps are selected to_____or_____even though the flap extension speed has not been exceeded.
 Definition
30*

45*
Term
Intentional speed reduction below_____, as defined by_____, is prohibited unless a lower speed is specifically authorized for flight testing or training operations.
 Definition

onset of stall warning

 

stick shaker operation
Term
USING PPAS:

Below 10,000 ft, the MOLS is derived from_____. At 10,000 ft and above the MOLS are derived from_____, appropriate for operational mode.
 Definition
V-speed data card

PPAS booklet
Term
USING PPAS:

Upon completion of the takeoff segment(after flap retraction) and at less than 10,000 ft(departure or arrival) the airplane will not be operated at a speed less than the_____.
 Definition
mimimum maneuvering speed depicted on the V-speed Data Card
Term
USING PPAS:

Above 10,000 ft, during climb, the aircraft will not be climbed at a speed less than_____. This is the absolute mimimum speed during climb.
 Definition
Safe speed + 10 knots
(use safe speed for planned cruise weight and altitude)
Term
USING PPAS:

If a climb rate of_____cannot be maintained during a climb, the aircraft must be leveled off and a new altitude coordinated with ATC.
 Definition
300 FPM
Term
USING PPAS:

Above 10,000 ft, cruise/holding/descent - In no case will the aircraft be operated at a speed less than_____, appropriate for weight, altitude, and operation mode.
 Definition
Safe, or Holding - Safe speed depicted in the PPAS booklet
Term
PPAS UNAVAILABLE:

Below 10,000 ft - Upon completion of the takeoff segment and at altitudes less than 10,000 ft, the aircraft will not be operated at an airspeed less than_____.
 Definition
minimum maneuvering speed depicted on the V-Speed Data Card
Term
PPAS UNAVAILABLE: Above 10,000 ft during climb, the aircraft will not be climbed at a speed less than_____unless a slower speed is required to comply with airspace or departure requirements.
 Definition
250 KIAS / 0.70 MACH
Term
PPAS UNAVAILABLE:

Above 10,000 ft, cruise, holding, descent - in no case will the aircraft be operated at a speed less than_____,appropriate for weight, altitude, and operational mode.
 Definition
Holding - Safe speed depicted in CRJ Flight Standards Manual
Term
Tire limit speed:
 Definition
182 knots groundspeed
Term
ADG maximum speed:
(wet ADG - tails 7002-7304)
 Definition
250 KIAS
Term
ADG maximum speed:
(dry ADG - tails 7305 and subsequent)
 Definition
Vmo / Mmo
Term
Maximum airspeed for turbulence penetration is the lesser of_______.
 Definition
280 KIAS or 0.75 MACH
Term
Windshield wipers must not be operated above_____.
 Definition
220 KIAS
Term
Use of_____submode(flight director or autopilot coupled)during approach is not permitted.
 Definition
DES (descent)
Term
Autopilot minimum altitudes:

non-approach:_____
visual or non precision approach:_____
precision approach:_____
 Definition
600 AGL

400 AGL

80 AGL
Term
The ADC source coupled to the active autopilot must be the same as that____during flight in RVSM.
 Definition
coupled to the ATC transponder
Term
The Bleed Air 10th Stage Valves must be CLOSED for takeoff and landing if_____.
 Definition
the engine cowl and/or wing anti-ice systems have been selected ON
Term
FLAPS:

_____ use of flaps is prohibited.

Flight with flaps extended at altitudes above_____is prohibited.
 Definition
Enroute

15,000
Term
Flight spoilers must not be extended in flight below_____.
 Definition
300 AGL
Term
At altitudes at and below FL 250, flight spoilers mus not be extended in flight at airspeeds below_____or_____or_____as appropriate.
 Definition
Safe, Holding - Safe speed

minimum maneuvering speed plus 20 KIAS

Vref speed plus 20 KIAS
Term
Above FL 250, do not extend flight spoilers in level flight. During descents above FL 250 flight spoilers must not be extended at airpeeds below_____.
 Definition
applicable Safe or Holding - Safe speed plus 25KIAS.
Term
Do not operate flight spoilers with flaps set to_____.
 Definition
45 degrees
Term
During landing, application of reverse thrust is not permitted at airspeeds below_____. Below this speed, reverse thrust must be limited to_____.
 Definition
60 KIAS

IDLE(not above 30% N1)
Term
During preflight check of the thrust reversers with the airplane stationary, reverse thrust must be limited to_____.
 Definition
30% N1
Term
Taxi lights must be switched OFF whenever the airplane is stationary in excess of____.
 Definition
10 minutes
Term
FMS calculated thrust setting must not be used if the PA is greater than_____.
 Definition
36,000 ft
Term
FMS range and fuel information is_____.
 Definition
advisory only
Term
RNAV, GPS, and GPS overlay approaches must not be continued past the FAF if a_____message is diplayed.
 Definition
NO APPR
Term
With an operable GPS, the FMS is approved for RNAV, GPS and GPS overlay approaches. The FMS shall not be used as a primary guidance for_____regardless of equipment on board the aircraft.
 Definition
any other type of approach
Term
The FMS is approved for use during_____and_____phases of flight.
 Definition
en route

terminal
Term
Reduced Engine "Flex" Thrust takeoff must not be used under the following conditions:
 Definition

if normal takeoff fan speed is less than 85% N1

 

if reduced "flex" thrust value is less than 85% N1

 

with an engine(s) which cannot achieve full rated thrust. (checked every 100 flight hours)

 

if Wing and/or Cowl Anti-icing Bleeds are in use

 

on runways contaminated w/ standing water, slush, snow, or ice

 

when warnings of windshear or downdrafts have been forecast

 

when using performance data derived from the Maximum Gross Load data (Temporary Runway Analysis on Dispatch Release)
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