Final Review Flashcards
What are the Aircraft’s dimensions?
Length (nose to tail) 119’ 7”
Height 36’ 3”
Width (wing tip to wing tip) 94’ 9”
What are the weight limitations of the aircraft?
Ramp/taxi weight 144 000 T/O weight 143 500 Landing weight 121 000 Zero Fuel weight 113 000 Empty weigth 77 100 Maximum Payload 35900
Main engine manufacturer?
CFM International CFM56-3
How many seats does the Aircraft have?
8 first class + 138 economy
What is the maximum operating latitude of the aircraft?
73 degrees North and 30 degrees South
How many members of the flight crew are required?
2 pilots
What is the maximum and minimum runway slope?
+/-2 degrees
Maximum tailwind component of the aircraft?
15 knots
What is the max differential pressure?
8.65 PSI
What is the max differential pressure for TO/LND?
.125 PSI
How much TO thrust do the engines have?
22000 lbs.
How many fuel tanks does the aircraft have?
- 2 main wing tanks and 1 center tank.
If the center tank is carrying more than 1000 lbs of fuel how much fuel must be in the 2 wing tanks?
The 2 wing tanks must be full of fuel. Each must be carrying 10000 lbs.
How many fuel boost pumps does the aircraft have?
- One powered by each engine.
Can one side of the fuel system feed the other sides engine?
Yes, through the crossfeed valve.