Limitations Flashcards
Max Ramp Weight
85,870
Max Takeoff Weight
85,517
Max Landing Weight
74,957
Max Zero Fuel Weight
69,886
FWD Baggage Compartment Capacity
3,306
AFT Baggage Compartment Capacity
2,534
Max Flap Extension Altitude
20,000FT
VLO/VLE
250kts
Max Speed to Open Direct Vision Window
160kts
MMo
.82M
VMo between 10,000-FL290
320kts
VMo between 0-8,000ft
300kts
VMo between 8,000-10,000ft
300-320kts increasing linear
VFE
Flaps 1-230kts Flaps 2-215kts Flaps 3-200kts Flaps 4-180kts Flaps 5-180kts Full-165kts
Max Tire Groundspeed
195kts
Max Tailwind Component
10kts
Max Recommended X-Wind
Dry Runway-38kts
Wet Runway-31kts
Compacted snow-20kts
Standing Water/Slush/Wet Snow/Dry Snow-18kts
Ice including Wet Ice-12kts
Static Takeoff Due To Compressor Stall-25kts
Kinds of Operation
Day/Night
IFR/VFR
Icing
CAT 1 and 2
Minimum Crew
Pilot and Copilot
Maneuvering Flight Load Factors
Flaps up-2.5 to -1Gs
Flaps down-2 to 0Gs
Max Runway Slope
+- 2% paved
Max N1 with Brakes Applied
60%
Max Usable Fuel Quantity Per Tank
10,392.5lbs
Unusable Quantity Per Tank
75lbs
Max Fuel Capacity
20,935lbs
Max Fuel Imbalance
794lbs
Minimum Fuel Tank Temperature
-37C
X-Feed Selector must be off……
Takeoff/Landing
APU Brand
Sundstrand APS 2300
Minimum Temperature for APU start
-54C
Max APU Start Altitude
30,000ft
Max APU Operating Altitude
33,000ft
Max Altitude for APU GEN
33,000ft
Max APU Altitude for Bleed Air
15,000ft
Max APU Altitude for Engine Start
21,000ft
Max APU Rotor Speed
108%
Max APU EGT for Start
1,032C
Max APU Continuous EGT
717C
APU Starter Limits
Attempt 1-2 60 seconds off
Attempt 3- 5 minutes off
What Type of Engines
GE CF34-8E5
T/O Thrust Limited to…..
10 minutes
Max N1
99.5%
Min and Max N2
58.5/99.4%
Max ITT Engine Start
815C
Max ITT for TOGA
990C
Max Continuous ITT
960C
Min and Max Oil Pressure
25/95PSI
Max Continuous Oil Temperature
155C
Max transient Oil Temperature
163C
Dry Motoring Start Cycle Limits
Attempt 1- 90 seconds on 5 minutes off
Attempt 2-5- 30 seconds on 5 minutes off
*May repeat sequence after 15 minute cool down
Starting Cycle Limits
Attempt 1-2- 90 seconds on ground 120 seconds in flight 10 second cool down
Attempt 3-5- 90 seconds on ground 120 seconds in flight 5 minutes cool down
Max Flex Thrust Reduction
25%
Max Differential Pressure up to FL370
7.8PSI
Max Pressure Differential above FL370
8.34PSI
Max Differential Over Pressure
8.77PSI
Max Differential Negative Pressure
-.5PSI
Max Differential Pressure for T/O and Landing
.2PSI
Max Altitude Single Pack
FL310
T/O Dataset on MCDU must be set to Engine…….
OAT between 5-10C
Visible Moisture up to 1,700AFE
Operating on Contaminated Surface
T/O Dataset on MCDU must be set to All…..
OAT is below 5C
Visible moisture up to 1,700AFE
Operating on contaminated surface
Max Wiper Speed
253kts
Minimum Autopilot Engagement Height
1,000ft AGL
TAS,TAT,SAT are not valid below…..
60kts
Max Latitude for IRS Stationary Alignment
78.25 N/S
CAT II Landing Flap Setting
5
RVSM Required Equipment
1 Autopilot
1 Transponder
2 ADCs
1 Altitude Alerting System
Max T/O and Landing Altitude
8000’
Minimum T/O and Landing Altitude
-1000’
Max Temperature for T/O
54C
EJET Height
32’3”
Wing Span
93’11”
Fuselage Length
103’11”
Minimum Turning Radius
54’4”
Nose Wheel Steering Travel
76 degrees
Rudder Pedal Travel
7 degrees
