Limitations Flashcards
CRJ-701
Maximum takeoff weight
75,000
CRJ-701
Maximum taxi and ramp weight
75,250
CRJ-701
Maximum landing weight
67,000
CRJ-701
Maximum Zero Fuel Weight
62,300
CRJ-701
Maximum Operating Altitude
41,000 feet
CRJ-900
Maximum taxi and ramp weight
85,000
CRJ-900
Maximum takeoff weight
84,500
CRJ-900
Maximum landing weight
75,100
CRJ-900
Maximum zero fuel weight
70,750
CRJ-900
Maximum operating altitude
41,000 feet
Definition of Cowl-Anti Icing conditions
Refer to chapter 3 POH
When must Cowl Anti-Ice be ON
Refer to chapter 3 POH
Definition of Wing Anti-Ice icing conditions
Refer to chapter 3 POH
When must Wing Anti-Ice be ON
Refer to chapter 3 POH
Maximum tailwind for takeoff and landing
10 knots
Maximum 90 degree crosswind for takeoff and landing
27 knots
Maximum 90 crosswind for landing from a CAT II approach
15 knots
Maximum headwind for landing from a CAT II approach
17 knots
CRJ-701
Maximum weight in the forward cargo compartment
1,000 pounds
CRJ-701
Maximum weight in the aft cargo compartment
3,300 pounds
CRJ-900
Maximum weight in the aft cargo compartment
3,740 pounds
CRJ-900
Maximum weight in the forward cargo compartment
1,700 pounds
EICAS Limit Markings
RED - maximum operating range
AMBER - caution range
GREEN - Normal operating range
Maximum ITT for advancement of thrust levers from SHUTOFF to IDLE
120 C (??)
During all starts do not exceed___% N1 for __ minutes after start, or until all indications are in the normal range. Whichever is longer
75%
2 min
Operate engines at or near idle for __ minutes prior to shutdown
2
Maximum oil pressure for takeoff
45 psi
Continuous ignition must be used when….
Refer to POH chapter 3
Starter cranking limits (ground only)
START. MAX TIME ON. FOLLOWED BY
1. 90 sec 10 sec
2. 90 sec. 10 sec
3+. 90 sec. 5 min
What is the limitation associated with the following statement
Within ___ degrees on either direction of the airplane nose -no wind speed limit OR greater than ____ degrees in either direction of the airplane nose with less than 5 knots
30
30
No Limitations - TOGA thrust may be applied before brakes released
What is the limitation associated with the following statement
Wind direction __ degrees in either direction of the airplane nose and wind speed between __ and __ knots:
Apply maximum of 75% N1 before brake release, then TOGA thrust
What is the limitation associated with the following statement
Wind direction greater than __ in either direction of the airplane nose and wind speed greater than __ knots:
Apply maximum of idle/taxi thrust before brake release, then TOGA thrust
Maximum fuel imbalance from the right to left wing for takeoff
300 pounds
Maximum fuel imbalance for all phases of flight except takeoff
800 pounds
Maximum total fuel for pressure refueling
19,594
Takeoff with an excess of ___ pounds in the center tank is not permitted unless each wing tank is above ____
4,400 pounds
APU starter motor duty cycle is limited to not more than __ starts/start attempts in _____ with a __ minute delay between cranking attempts
3
1 hour
2
Maximum altitude for APU bleed air extraction
25,000 pounds
With the APU door not closed or the door position unknown:
The airplane must be limited to:
220 KIAS or the APU must remain in operation
VFE/VFO FLAPS 1
230
VFE/VFO FLAPS 8
230
VFE/VFO FLAPS 20
220
VFE/VFO FLAPS 30
185
VFE/VFO FLAPS 45
170
Gear speeds:
Extension
Down and locked retraction
220
220
200
Maximum airspeed for windshield wiper operation
220
Maximum turbulence penetration speed
280 KIAS / .75 Maxh whichever is lower
CRJ-701
Maximum altitude for single pack operation
31,000 feet
CRJ-900
Maximum altitude for single pack operation
25,000 feet
