NCAA PPL Principles of Flight study plan
NCAA PPL Principles of Flight · Give each week a clear focus.
8 weeks · About 7 hours per week
Principles of Flight
Define the four forces of flight and state how each changes across the takeoff, climb, cruise, descent, and landing phases
Explain how lift is generated using both the pressure-distribution and Newtonian (downwash) descriptions, and note where each description is incomplete
Draw and label the four force vectors for steady straight-and-level flight, a constant-airspeed climb, and a constant-airspeed descent
Compute the lift equation for two sample aircraft states, changing one variable at a time, and describe the resulting effect on stall speed
Your checkpoint
A one-page force diagram set (level, climb, descent) plus a worked lift-equation table showing how stall speed shifts with a 10% and 20% weight increase
Principles of Flight
Describe the four relative-wind and chord relationships that define angle of attack, and distinguish angle of attack from pitch attitude
Explain the lift curve: linear region, critical angle of attack, and post-stall behavior, and state why the stall is an angle-of-attack event rather than an airspeed event
Identify the factors that shift the lift curve (flaps, ice, Reynolds number) and predict the direction of each shift
Relate load factor to stall speed using the square-root relationship and calculate stall speed at 2g and 3g
Your checkpoint
A hand-plotted lift coefficient versus angle-of-attack curve with annotated critical angle, plus a load-factor stall-speed table for 1.0, 1.5, 2.0, and 3.0 g
Principles of Flight
Explain induced drag, its origin in wingtip vortices, and why it varies inversely with airspeed squared while parasite drag varies directly
Construct and interpret the total drag curve, marking the minimum-drag speed and the region of backside (reverse command) flight
Describe the four factors affecting parasite drag and the effect of weight, altitude, and bank angle on the drag curve
Explain why the best glide speed changes with weight but not with altitude, and identify the practical consequence for engine-out glide range
Your checkpoint
A labeled total-drag curve with parasite, induced, and total components plotted, annotated with best-glide speed, minimum-drag speed, and a written explanation of backside flight
Principles of Flight
Explain thrust and power required versus available across the airspeed range and locate the speeds for maximum endurance and maximum range
Describe how propeller efficiency, pitch, and slip vary with airspeed and power setting
Explain the four left-turning tendencies and state the phase of flight in which each is most significant
Describe stability: static versus dynamic, and longitudinal, lateral, and directional stability with the design features that provide each
Your checkpoint
A power-required versus power-available graph with endurance and range speeds marked, plus a table matching each left-turning tendency to its cause and most affected flight phase
Principles of Flight
Explain how flaps, slats, and spoilers alter lift, drag, and stall speed, and describe the flap-speed and load-factor limits on flap extension
Describe the aerodynamics of turns: load factor in level turns, the relationship between bank angle and stall speed, and overbanking tendency
Explain adverse yaw, aileron drag, and the correct use of rudder in turns and in cross-controlled situations
Describe the aerodynamics of spins: incipient, fully developed, and recovery, and the role of the stall in spin entry
Your checkpoint
A bank-angle table giving load factor and the resulting stall-speed multiplier from 0 to 75 degrees, plus a written spin-entry and recovery sequence with the aerodynamic reason for each control input
Principles of Flight
Explain ground effect, its effect on induced drag and on the ability to become airborne versus to climb, and the hazard of premature liftoff
Describe wake turbulence generation, its behavior relative to the generating aircraft, and avoidance procedures on takeoff and landing
Explain the aerodynamic effects of aircraft icing on lift, drag, stall speed, and control feel, and identify the critical surfaces
Describe Mach effects, critical Mach number, and shock-induced separation at a conceptual level appropriate to the private pilot certificate
Your checkpoint
A two-page summary card covering ground effect, wake turbulence avoidance, icing effects, and high-speed aerodynamics, written as a preflight briefing you could give from memory
Principles of Flight
Describe the causes of and recovery from the four types of stalls: power-off, power-on, cross-controlled, and accelerated
Explain the aerodynamics of the region-of-reversal and elevator-trim stall scenarios and the correct recovery priorities
Explain how weight, CG position, and density altitude affect takeoff, climb, cruise, and landing performance
Describe the aerodynamic basis for V-speeds (Vx, Vy, Va, Vfe, Vno, Vne) and state how each is affected by weight and altitude
Your checkpoint
A V-speed reference table giving the definition, the aerodynamic reason for the limit, and the effect of weight, altitude, and CG for each of the six listed speeds, plus a written stall-recovery checklist for each of the four stall types
Principles of Flight
Re-derive from memory the lift equation, the load-factor stall relationship, and the drag-curve relationships without reference material
Resolve a set of mixed scenario questions that combine two or more principles (for example, heavy aircraft in a banked turn at high density altitude) and justify each answer
Identify and re-study the three weakest sub-topics from the week 4 and week 7 milestone checks
State, in your own words, how each principle connects to a specific preflight or in-flight decision
Your checkpoint
A closed-book, 40-question self-test scored against a written answer key, with a one-page error log listing each missed concept, its root cause, and the corrective study action
Milestones
Week 2: Explain without notes why a wing stalls at a specific angle of attack regardless of airspeed, weight, or bank angle, and correctly compute stall speed at 2g
Week 4: Sketch the total drag curve from memory, label minimum-drag and best-glide speeds, and explain why flight below minimum-drag speed requires more power to fly slower
Week 6: Pass a 15-question mixed quiz on ground effect, wake turbulence, icing, and flap and turn aerodynamics with at least 80% correct
Week 7: Describe the entry, recognition, and recovery for all four stall types and for a spin, with the aerodynamic reason for each step, without reference material
Week 8: Score at least 85% on the closed-book 40-question self-test, with no missed item in the lift equation, load factor, or drag curve categories