CRJ 200 Limitations Flashcards
Max Ramp Wt ________lbs.
53,250
Max T/O Wt ________lbs.
53,000
Max Lnd Wt______lbs.
47,000
Max Zero Fuel Wt _______lbs.
44,000
Min Flight Wt _______lbs.
30,000
Wing Span
69ft 8in
Aircraft Length
87ft 10in
Tail Height
20ft 8in
Max Ops Alt_______ft.
37,000(SW)
Max T/O & Lnd Altitude_______ft.
10,000
Max Temp T/O & Lnd_______°C
ISA+35
Min Temp T/O_______°C
-40
Max Tailwind T/O & Lnd____kts.
10
Crosswind Limitation: Takeoff or Landing
27kt (SW)
Crosswind Limitation: Takeoff or Landing with RCC 1 or 2 or Poor BA, >1/8” Standing Water, > 1/8” Slush, Ice
10kt (SW)
Crosswind Limitation: Takeoff or Landing with Wet ice, Slush over Ice, Water over Compact Snow, Dry Snow over Ice, Wet Snow over Ice
Prohibited
VMO_____KIAS
335
MMO_______M
0.85
VLO EXT______KIAS(SW)
220
VLO RET______KIAS
200
VLE_____KIAS
220
VTire______kts.(GS)
182
VTire______kts.(GS)
182
V ADG DEPLOY MAX (Wet)______KIAS
250
V ADG DEPLOY MAX (Dry)
VMO/MMO
VB______KIAS
280
MB______M
0.75
V WIPER OPS Max______KIAS
220
VFO 8____KIAS
200
VFO 20____KIAS
200
VFE 8 ____KIAS
215
VFE 20 ____KIAS
215
VFE 30____KIAS
185
VFE 45____KIAS
170
Max Flaps Alt______ft.
15,000
Use of flaps is_______ for enroute ops.
prohibited
Min spoiler speed
Appr. speed + 20
(Appr. speed is current flaps maneuvering or straight-in speed)
Min Alt. Spoilers
1,000 ft. HAT(SW)
Spoilers use with flaps at____ prohibited
45°
Minimum Runway Width____ft.
100
Minimum Taxiway Width____ft.
35 (SW)
STANDING WATER Takeoff/Landing
0.50 in./0.75 in.
SLUSH Takeoff/Landing
0.50 in./ 0.88 in.
WET SNOW Takeoff/Landing
1.00 in./1.50 in
DRY SNOW Takeoff/Landing
3.00 in./3.75 in.
When operating on runways contaminated with ice, dispatch with one thrust reverser is_____.
prohibited
The taxi lights must be switched OFF whenever______.
the airplane is stationary in excess of 10 minutes
FMS - The temperature compensation function should not be used at any time. It should be selected______.
OFF
FMS - The temperature compensation function should not be used at any time. It should be selected______.
OFF
Operations are prohibited on routes where ozone concentrations exceed limits in __________________________________.
Quick Reference Handbook (QRH) Volume 1
APU Min Temp Start______°C
-40
APU Max Ops Alt_______ft.
37,000
APU Max Start Alt_______ft.
30,000
APU Max Alt Bleed use_______ft.
15,000
APU Max Alt Eng Start_______ft.
13,000
Max Door Open with APU not operating_____KIAS
300
APU Starter Duty Cycle
Autopilot must be engaged above_______ unless otherwise permitted by the MEL.
FL200
IAS MODE is ______ during approach
prohibited
DES MODE (F/D or A/P coupled) is ______ during approach
prohibited
APPR MODE is _____ for ___ approaches
prohibited
VOR
ADC SOURCE coupled to active autopilot must be _______ to ATC transponder during flight in RVSM airspace.
the same as that coupled
AUTOMATIC FC SYSTEM(AFCS)
Ground Ops DC ONLY
5 min
Max continuous DC TRU
100 A
APU generator (maximum load)
to FL370-30kVA
CARGO FIREX-Flight time to suitable airport
45 min
Total - Pressure Refueling______lbs.
14,518
Total - Gravity Refueling_______lbs.
13,906
Max Imbalance for T/O____lbs.
800
Min for GA per wing______lbs.
500
(Assumes a maximum airplane climb attitude of 10° nose up)
Min Bulk Fuel Temp for T/O______°C
-30
Min Bulk Fuel Temp in flight______°C
-40
Takeoff with fuel in excess of ____ lbs. in the center tank is not permitted unless: Each main wing tank is above ______lb., or :Each main wing tank is above ______lb., and the allowable zero fuel weight is reduced by the weight of the fuel in the center tank in excess of 500 lb., and the allowable center of gravity (CG) in this configuration is verified to be within allowable CG envelope.
500
4,400
2,000
Powered crossflow and gravity crossflow must be ___ for takeoff.
off
Powered crossflow and gravity crossflow must be ___ for takeoff.
off
When fuel other than Jet-A is to be used, consult _______________ for limitations.
QRH Volume 1
Min Reduced Thrust 3A1:____%
85
Min Reduced Thrust 3B1:____%
83.5
Automatic Performance Reserve (APR) must be used when takeoff performance is predicated upon use of ______.
APR
The APR system must be selected ___ when an APR INOP caution message is displayed on EICAS.
off
APR OFF Performance must be used when an ________ caution message is displayed.
APR INOP
The APR system must be selected OFF for takeoff and APR OFF performance must be used when the ambient temperature is _____ and below, and pressure altitude is less than ______ft. (3A1 engines only)
-18°C
1000
Engine Start(Ground)
Dry Motoring(Ground)
Max wind milling/starter-assisted cross-bleed relight altitude:______
FL210
Until oil pressure reaches green band:______
Do not exceed idle
Do not exceed 75% N1 until:______or_________,whichever is longer.
2 minutes, all operating indications in green band
Ground idle N2 split:_______
≤2%
During 2nd engine APU bleed start:_____
Operating engine ≤70%N2
With OAT ≥-20°C, thrust levers at idle,N2:_______
> 57%. If N2 is ≤57% with OAT of -20°C or greater, do not advance thrust levers above idle. Contact Maintenance.
Engines must not be shutdown until:______
2 minutes at idle/near idle thrust. Note- Taxi time counts towards this limitation.
SkyWest prohibits the use of thrust reversers__________
during taxi operations
Max OIL PRESSURE after cold start:_______
Engine must remain at idle until oil psi returns to normal range. Must be in normal range within 10 min.
Single Pack Ops to FL______
250
Max Ramp Wt ________lbs.
53,250
Max T/O Wt ________lbs.
53,000
Max Tailwind T/O & Lnd____kts.
10
