Bell 412EP - RFM Limitations Test-Questions with
Correct Solutions
Minimum flight crew consists of?
One pilot who shall operate helicopter from right crew
seat.
The left crew seat may be used for an additional pilot when approved dual controls are installed.
AFCS requirements for IFR operations?
Both autopilots, AP 1 and AP 2, shall be engaged in ATT mode during flight.
Maximum gross weight for takeoff and
landing is?
11,900 pounds (5398 kilograms).
Minimum gross weight for flight is?
6400 pounds (2903 kilograms).
Minimum combined crew weight at fuselage
station 47.0 is?
170 pounds (77.1 kilograms).
Longitudinal center of gravity limits can vary from?
Station 130 to 144 (depending on gross
weight)
Lateral center of gravity limits are?
, 4.5 Inches (114.3 millimeters) left and right of fuselage
centerline for all gross weights.
Minimum IFR airspeed is?
60 KIAS.
Basic VNE is?
140 KIAS from sea level to 3000 feet density altitude at all gross weights.
Max Airspeed when operating above 81% mast torque.
Airspeed shall not exceed 105 KIAS (or placarded VNE, if less)
VNE with only one autopilot engaged is?
115 KIAS (or placarded VNE, if less). If both
autopilots are disengaged, basic VNE applies.
VNE for steady state autorotation is?
105 KIAS at or below 10,000 feet (3048 meters) pressure altitude;
80 KIAS above 10,000 feet (3048 meters) pressure altitude.
VNE with cargo doors opened asymmetrically
is?
80 KIAS.
VNE with cargo doors in transit or in an
unlocked position is?
Correct Solutions
Minimum flight crew consists of?
One pilot who shall operate helicopter from right crew
seat.
The left crew seat may be used for an additional pilot when approved dual controls are installed.
AFCS requirements for IFR operations?
Both autopilots, AP 1 and AP 2, shall be engaged in ATT mode during flight.
Maximum gross weight for takeoff and
landing is?
11,900 pounds (5398 kilograms).
Minimum gross weight for flight is?
6400 pounds (2903 kilograms).
Minimum combined crew weight at fuselage
station 47.0 is?
170 pounds (77.1 kilograms).
Longitudinal center of gravity limits can vary from?
Station 130 to 144 (depending on gross
weight)
Lateral center of gravity limits are?
, 4.5 Inches (114.3 millimeters) left and right of fuselage
centerline for all gross weights.
Minimum IFR airspeed is?
60 KIAS.
Basic VNE is?
140 KIAS from sea level to 3000 feet density altitude at all gross weights.
Max Airspeed when operating above 81% mast torque.
Airspeed shall not exceed 105 KIAS (or placarded VNE, if less)
VNE with only one autopilot engaged is?
115 KIAS (or placarded VNE, if less). If both
autopilots are disengaged, basic VNE applies.
VNE for steady state autorotation is?
105 KIAS at or below 10,000 feet (3048 meters) pressure altitude;
80 KIAS above 10,000 feet (3048 meters) pressure altitude.
VNE with cargo doors opened asymmetrically
is?
80 KIAS.
VNE with cargo doors in transit or in an
unlocked position is?
