General Description Flashcards
1
Q
Maximum internal GW for takeoff and landing is
a) 4150 lbs.
b) 4250 lbs.
c) 4450 lbs.
A
C) 4450 lbs.
2
Q
Total fuel capacity for the BH206L4 is
a) 99.4 gallons.
b) 112.0 gallons.
c) 187.0 gallons.
A
B) 112.0 gallons.
3
Q
The BH206L airframe has three main sections,
a) The fore, mid, and aft sections.
b) The forward section, the intermediate section, and the tailboom section.
c) The cockpit section, the passenger station section, and the tail section.
A
B) The forward section, the intermediate section, and the tailboom section.
4
Q
Main rotor diameter for the BH206L4 is
a) 35 feet.
b) 40 feet.
c) 37 feet.
A
C) 37 feet.
