Limitations Flashcards
Required crew
Pilot and copilot
Seatbelt and shoulder harness required
Takeoff and landing
EICAS or MFD for takeoff and landing
Summary or flight page
Runway water condition for takeoff and landing
3/4 of an inch
Flaps down maneuvering load factor
2G – 0G
Do you not extend spoilers with flaps extended no intentional stalls flaps or gear extension above
18,000 feet
Auto spoilers armed
Takeoff and landing
YAW damp
Not required
Hydraulic fluid
Red mil spec 5606
ADC and AHRS for takeoff
Normal
Auto pilot for takeoff and landing
Off
Auto pilot minimum used Heights
500 feet AGL – climb enroute or descent
200 feet AGL - approach
Minimum turnaround time
15 minutes
Maximum ramp weight
21,750 pounds
Maximum certified takeoff weight
21,500 pounds
Maximum certified Landing Weight
19,200 pounds
Minimum flight weight
14,000 pounds
Maximum zero fuel weight
16,500 pounds
Maximum aft baggage weight
500 pounds
Approved fuel’s
Referenced the addendum, But we were taught
Jet-A, Jet A1, JP-5, JP-8
Fuel capacity
6062 pounds (904.8 gallons)
Fuselage fuel tank capacity
2708 pounds (404.2 gallons)
Wing fuel tank capacity
Left 1678 pounds
Right 1676
Fuel balance for All phases of flight
200 pounds
Single point pressure refueling limit
55 psi G
Thrust Reverser limitations
• idle only in Manual mode
• max reverse thrust down to 40 kts
• do not back up the aircraft
• Not used for touch-and-go landings
• Ground operations on paved surfaces
Turn Anti-ice on prior to flight and visual moisture in
In flight… One minute prior… +10°C to -40°C and visible moisture
On the ground… Two minutes prior… +10°C and below and visible moisture, 1 mile visibility
Aircraft and components must be warmer than what temperature prior to start?
-23°C
Cabin temperature prior to takeoff?
-15°C
Mmo Mach trim operative?
Mach trim in-operative an auto pilot engaged?
Mach 0.81
Mach trim inoperative and auto pilot disengaged?
23,400-FL420
Above FL420?

M .76-.78
Above FL420 - M.78
Vmo
330 kias