Multiengine test 4
accelerate-stop distance
the runway length required to accelerate to a specific speed (either VR or VLOF, specified by manufacturer), experience an engine failure, and bring the airplane to a complete stop
payload
the weight of occupants, cargo, and baggage.
zero fuel weight
the weight of the aircraft without fuel
common carriage
A common carrier is a person or organization that "hold out" its willingness to transport persons or property from place to place, for compensation
private carriage
A common carrier is a person or organization that "hold out" its willingness to transport persons or property from place to place, for compensation
Max load in cockpit baggage compartment and baggage extension together
100 lbs
Max load in the Cockpit baggage compartment (behind rear seats)
100 lbs
unusable fuel weight
108 lbs
max zero fuel weight
3638 lbs
max landing weight
3748 lbs
max takeoff weight
3935 lbs
max ramp weight
3957 lbs
Max load in baggage extension (behind cockpit baggage)
40 lbs
usable fuel weight
458.4
Max load in the Nose baggage compartment (in fuselage nose)
66 lbs
Datum
an imaginary vertical plane or line from which all measurements of arm are taken.
moment
the product of the weight of an item multiplied by its arm. expressed in (in-lb).
single engine service ceiling
is reached when the multiengine airplane can no longer maintain a 50 fpm rate of climb with OEI, and its single-engine absolute ceiling when climb is no longer possible.
arm
the horizontal distance in inches from the reference datum line to the CG of an item.
accelerate-go distance
the horizontal distance required to continue the takeoff and climb to 50 feet, assuming an engine failure at VR or VLOF, as specified by the manufacturer
