Limitations Flashcards
Maximum Ramp Weight
36,400 lbs
Maximum Takeoff Weight
36,100 lbs
Maximum Landing Weight
31,800 lbs
Maximum Zero Fuel Weight
24,400 lbs
Maximum Altitude for Takeoff and Landing
14,000 feet
Maximum Tailwind Component
10 knots
Minimum Altitude for In-Flight use of the Speedbrakes
500 feet AGL
Maximum Asymmetric Fuel
400 lbs
Maximum Emergency Asymmetric Fuel
800 lbs
Minimum Wing Fuel Per Tank for Takeoff
500 lbs
Takeoff in High Idle is…..
Prohibited (except for touch and go)
Maximum Operating Altitude
51,000 ft.
Unusable Fuel Quantity - Wings/Center Tank
- 81 gallons in each wing tank
2. 2 gallons in the center tank
Maximum Single Point Refueling PSI
55 psi
Maximum Single Point Defueling PSI
-10 psi
Center tank to wing transfer must be initiated prior to _______ lbs per side wing fuel?
3100 lbs
Simultaneous use of crossfeed and center-to-wing tank transfer is prohibited when the wing fuel quantity is ________ lbs or less per side?
2900 lbs
How many FADEC’s must be operational for takeoff?
All 4 must be operational
Both Air Data Computers Must be Operational for Takeoff: True or False
True
What is the minimum start duct pressure (EICAS) prior to ground start?
25 psi
FADEC automatic overspeed shutdowns are set at ______ % N1 and _______ % N2.
105% N1
105.6% N2
Minimum fan speed for takeoff is _______ ?
73.6% N1
ENGINE AIR TURBINE STARTER LIMITS
____ consecutive normal starts followed by ____ minutes cooling are permitted. One ____ second motoring cycle is equivalent to one normal start.
3
25
30
Do not engage the air turbine starter above ____ % N2 RPM. Air turbine starter drive shaft damage can occur.
25%