To understand the forces which affect the aircraft during straight and level flight, and to maintain constant height at varying airspeeds.
To recall from memory the power setting used for straight and level flight in a normal cruise configuration.
From memory, identify the four forces acting on an aeroplane in a straight and level flight.
Correctly recall from memory, the 2 work cycles to configure and maintain an aircraft for straight and level flight.
Changing Cruise (PAST)
Power
Attitude
Speed
Trim
Maintaining Cruise (ALAP)
Attitude
Lookout
Attitude
Performance
Four forces for straight and level flight
BEW Basic Empty Weight
MTOW Maximum Take-Off Weight
TOW Take-Off Weight
Increase AoA against decrease IAS and vice-versa
The lift equation, lift coefficient (Cl)
L = Cl * (A * .5 * r * V^2)
Cl = L / (A * .5 * r * V^2)
Drag
Induced Drag
* By-product of lift
* Decreases as IAS increases
* Types
* Form
* Skin Friction
* Interference
* Increases as IAS increases, not as much as induced drag
Stability
Types
Positive
Neutral
Negative
Axes
Longitudinal axis
Axis on which aircraft rolls
Stability of pitch
Positive stability
Lateral axis
Axis on which aircraft pitches
Stability of roll
Neutral stability
Directional axis
Axis on which aircraft yaws
Positive stability
Application
Normal cruise
Power = 2300 rpm
“5 fingers” attitude
Gives performance = 100KIAS
Fast cruise
Power = 2500rpm
“6 fingers” attitude
Gives performance = 110KIAS
Slow cruise
Power = 2100rpm
“4 fingers” attitude
Gives performance = 80KIAS
Slow cruise (with flaps)
Power = 2100rpm
“5 fingers” attitude
Gives performance = 70KIAS