CRJ 200 Limitations. Flashcards
Maximum ramp weight
53,250 lbs
Kinds of operations
Transport category
Day and Night
VFR and IFR
Flight into icing conditions
Maximum take off weight
53,000 lbs
Maximum landing weight
47,000 lbs
Maximum zero fuel weight
44,000 lbs
Maximum take off and landing pressure altitude
10,000’
Maximum operating altitude
41,000’
Max take off and landing air temp
iSA +35
Minimum take off and landing air temp
-40c / -40f
cowl anti ice -Ground
On: OAT <= +10 & Visible moisture. Visibility <=1sm
On: Contaminated surfaces
Cowl anti-ice in flight
On: TAT <= 10c and visible moisture except SAT <=-40c
On: when ICE annunciation illuminates by the ice detection system
Wing anti-ice ground
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
Wing anti-ice. Flight
On: ice annunciation illuminates by the ice detection system
When in icing conditions and airspeed is <=230 KIAS
Super cooled large droplets (SLD) icing
Continued flight operations prohibited, identified by side window icing.
It asks off permitted with frost
Upper surface of fuselage (see surface features)
Underside of cold soaked wing (1/8 in max)
Runway slope
+- 2%
Max tailwind component
10 Kts
Minimum flight crew
1 pilot, 1 co-pilot
Cargo limits
Flight within 60 minutes if cargo is in cargo compartment
Ozone limits.
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
Engines
General Electric CF34-3B1
N1 % RPM
98.6, O-98.5
N2 % RPM.
99.3, 0-99.2
Oil Temp. C
163 max
150-162 caution
-40 - 149 Normal
Oil Pressure
0-25 Red
115-156 Caution
26-115 normal
Airplane Cold Soak
> 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
Use of continuous ignition
Take off and landing on contaminated runway
Rain > moderate
Turbulence > moderate
In the vicinity of thunderstorms
Take off with high crosswinds
Starter limitations
Starts 1&2, 60 seconds on, followed by 10 seconds off
Starts 3 +, 60 seconds on, followed by 5 minutes off
ITT Starting limits
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
N2 RPM limits for starts
N2 must be less than 55%
Starter limits for motoring engine
Start 1: 90 seconds on, 5 minutes off
Starts 2+: 30 seconds on, 5 minutes off
Fuel capacity
Total = 14,518 Wings = 9520 Center = 4998
Minimum go-around fuel
450 lbs per wing, 10 nose up pitch max
Max fuel imbalance in-flight
800 lbs
APU type
Garrett GTPC-36-150RJ
APU max RPM
107%
APU maximum Temp
743c-974c